CA2471455A1 - Conductive lithium storage electrode - Google Patents

Abstract

A compound comprising a composition A.(M'1-aM"a)y(XD4)z, .ALPHA.,(M'1-aM"a)y(DXD4)z, or Ax,(M'1-aM''a)y(X2D7)z, and have values such that x, plus y(l -a) times a formal valence or valences of M', plus ya times a formal valence or valence of M", is equal to z times a formal valence of the XD4, X2D7, or DXD4 group; or a compound comprising a composition (A1-aM"a)xM'y(XD4)z, (A1-aM"a)xM'y(DXD4)z (A1-aM"a)xM'y(X2D7)z and have values such that (1-a)x plus the quantity ax times the formal valence or valences of M" plus y times the formal valence or valences of M' is equal to z times the formal valence of the XD4, X2D7 or DXD4 group. In the compound, A is at least one of an alkali metal and hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, molybdenum, and tungsten, M" any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB metal, D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <= 0.1, and x, y, and z are greater than zero. The compound can have a conductivity at 27~ C of at least about 10-8 S/cm. The compound can be a doped lithium phosphate that can intercalate lithium or hydrogen. The compound can be used in an electrochemical device including electrodes and storage batteries and can have a gravimetric capacity of at least about 80 mAh/g while being charged/discharged at greater than about C rate of the compound.

Description

CONDUCTIVE LITHIUM STORAGE ELECTRODE
RELATED APPLICATIONS
This application claims priority under 35 U.S.C. ~ 119(e) to U.S. Provisional s Application Serial No. 60/343,060, filed on December 21, 2001, U.S.
Provisional Application Serial No. 60/388,721, filed on June 14, 2002, and U.S.
Provisional Application Serial No. 60/412,656, filed on September 20, 2002, the disclosures of which are herein incorporated by reference.
to BACKGROUND OF THE INVENTION
1. Field of the Invention The present invention is directed to transition metal polyanion oxides that can be used as alkali ion combined materials and more particularly to lithium-ion intercalating t5 structures that can be used as electrochemical compounds.

2. Description of the Related Art The published literature contains many references by those skilled in the art to the insulating nature of these compounds, and the limitations on their utility as battery 2o storage materials thereby created. For example, Gaubicher et al. (J.
Gaubicher, T. Le Mercier, Y. Chabre, J. Angenault, and M. Quarton, "Li/(3-VOP04: A New 4 V
System for Lithium Batteries," J. Electrochem. Soc., 146[12] 4375-4379 (1999)) comment with respect to the NASICON compounds that "unfortunately, the anionic units tend to isolate the transition elements, which consequently leads to low electronic conductivity."
25 In "Approaching Theoretical Capacity of LiFePOa at Room Temperature at High Rates," H. Huang, S.-C. Yin and L.F. Nazar, Electrochem. Sol. St. Lett., 4[10]

A172 (2001), explain that "however, owing to their very poor conductivity, initial reports indicated that Li+ can only be partially extracted/inserted at room temperature at modest rates." And, in "Issues and challenges facing rechargeable lithium batteries,"
J.-M.
3o Tarascon and M. Armand, Nature, 414, 359-367 (2001), note that with respect to these compounds that "one of the main drawbacks with using these materials is their poor electronic conductivity, and this limitation had to be overcome through various materials processing approaches, including the use of carbon coatings, mechanical grinding or mixing, and low-temperature synthesis routes to obtain tailored particles."
Proposed solutions to the poor electronic conductivity have typically focused entirely on coating with carbon or adding a significant excess of carbon during synthesis.
Coating with carbon has been described by N. Ravet et al. in "Improved iron-based cathode materials," Abstr. No. 12, ECS Fall meeting, Hawaii, 1999 and by Morcrette et al. in M. Morcrette, C. Wurm, J. Gaubicher, and C. Masquelier, "Polyanionic structures as alternative materials for lithium batteries," Abstr. No. 93, Li Battery Discussion Meeting, Bordeaux, Archachon, 27 May - 1 June 2001. Co-synthesizing with carbon 1o has been discussed by H. Huang et al. at the Univ. of Waterloo and by Yamada et al. at the Electrochemical Society Fall Meeting, San Francisco, CA, September 2001.
However, the addition of carbon as a conductive additive can lower the gravimetric and volumetric capacity of the storage material. In some instances, about 20 wt%
carbon is added to the electrode formulation (approximately 30% by volume). This significant t s volume of carbon does not typically store lithium storage at the potentials at which the polyanion compounds store lithium.
It is therefore clear and widely acknowledged by those skilled in the art that poor electronic conductivity is, firstly, an inherent feature of the lithium-metal-polyanion compounds discussed herein, and secondly, that this inherent feature limits the 2o applicability of the materials in lithium storage applications, including lithium battery electrodes, especially at temperatures near room temperature. While published literature and patents describe the addition of various metal additives to such compounds, they are silent as to whether the critical and enabling property of improved electronic conductivity can be obtained.
SUMMARY OF THE INVENTION
The invention provides compounds, methods of forming compounds, electrodes that comprise compounds and storage battery cells that include an electrode that comprises a compound.
3o In one set of embodiments, a compound is provided. The compound comprises a composition AX(M'l.aM"a)y(XD4)Z, Ax(M',-aM"a)y(DXDa)z, or AX(M',_aM"a)Y(X2D~)Z, wherein A is at least one of an alkali metal or hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, boron, aluminum, silicon,

-3-vanadium, molybdenum and tungsten , M" is any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIVA, IB, IIB, IIIB, IVB, VB, and VIB metal, D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <_ 0.1, and x is equal to or greater than 0, y and z are greater than 0 and have values such that x, plus y(1-a) times a formal valence or valences of M', plus ya times a formal valence or valence of M", is equal to z times a formal valence of the XD4, XZD~, or DXD4 group. In some of these embodiments, the compound has a conductivity at 27° C of at least about 10-g S/cm. In some of these embodiments, the compound has a specific surface area of at least 15 m2/g. In some of these embodiments, the compound crystallizes in an ordered or partially disordered structure of the olivine (AXMX04), NASICON (Ax(M',M")2(X04)3), VOP04, LiFe(PZO~) or Fe4(P20~)3 structure-types, and has a molar concentration of the metals (M' + M") relative to the concentration of the elements X that exceeds the ideal stoichiometric ratio y/z of the prototype compounds by at least 0.0001.
In another set of embodiments, a compound is provided. The compound 15 comprises a composition (Ai_aM"a)XM'y(XD4)Z, (A,_aM"a)XM'y(DXDQ)Z, or (A,_aM"a)xM'y(X2D~)Z, wherein A is at least one of an alkali metal or hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, boron, aluminum, silicon, vanadium, molybdenum and tungsten, M" any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIVA, IB, IIB, IIIB, IVB, VB, and VIB metal, D is at least one of 20 oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <_ 0.1, and x, y, and z are greater than zero and have values such that (1-a)x plus the quantity ax times the formal valence or valences of M" plus y times the formal valence or valences of M' is equal to z times the formal valence of the XD4, XzD~ or DXD4 group. In some of these embodiments, the compound has a conductivity at 27° C of at least about 10-g S/cm. In some of these 25 embodiments, the compound has a specific surface area of at least 15 m2/g.
In some of these embodiments, the compound crystallizes in an ordered or partially disordered structure of the olivine (AXMX04), NASICON (AX(M',M")2(X04)3), VOP04, LiFe(P20~) or Fe4(P20~)3 structure-types, and has a molar concentration of the metals (M' + M") relative to the concentration of the elements X that exceeds the ideal stoichiometric ratio 3o y/z of the prototype compounds by at least 0.0001.
In another embodiment, a compound is provided. The compound comprises a composition (A~aM»a)XM~Y(~a)Z~ (A~-aM»a)XM~y(D~a)Z~ or (A~aM~,a)XM'r(XzD~)z~
wherein A is at least one of an alkali metal or hydrogen, M' is a first-row transition

-4-metal, X is at least one of phosphorus, sulfur, arsenic, boron, aluminum, silicon, vanadium, molybdenum and tungsten, M" any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIVA, IB, IIB, IIIB, IVB, VB, and VIB metal, D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <_ 0.1, a <_ b <_ 1, and x, y, and z are greater than zero and have values such that (b-a)x plus the quantity ax times the formal valence or valences of M" plus y times the formal valence or valences of M' is equal to z times the formal valence of the XD4, XZD7 or DXD4 group. In some of these embodiments, the compound has a conductivity at 27° C of at least about 10'$ S/cm. In some of these embodiments, the compound has a specific surface area of at least 15 mz/g. In some of to these embodiments, the compound crystallizes in an ordered or partially disordered structure of the olivine (AXMX04), NASICON (AX(M',M")z(X04)3), VOP04, LiFe(P20~) or Fe4(P20~)3 structure-types, and has a molar concentration of the metals (M' + M") relative to the concentration of the elements X that exceeds the ideal stoichiometric ratio y/z of the prototype compounds by at least 0.0001.
15 In another set of embodiments, methods of forming a compound are provided.
The methods include mixing an alkali metal or hydrogen salt, a first-row transition metal salt, a salt of at least one of phosphorus, sulfur, arsenic, silicon, aluminum, boron, vanadium, molybdenum and tungsten, and a salt of any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIVA, IB, IIB, IIIB, IVB, VB, and VIB metal; milling the mixture;
and heat 2o treating the mixture at a temperature between 300-900°C.
In another set of embodiments, methods of doping a material to form a lithium or hydrogen storage compound are provided. The methods include selecting a starting material to be doped, in conjunction with selection of milling equipment comprising a dopant for doping the starting material at a predetermined level of dopant.
The methods 25 further include milling the starting material in the milling equipment; and recovering from the milling step a material suitable for forming a lithium or hydrogen storage compound comprising the starting material doped with the dopant at the predetermined level.
In another set of embodiments, an electrode comprising a lithium storage 3o compound is provided. The electrode can comprise any of the compounds described above and has a material energy density (i.e., voltage vs. Li x charge capacity) that while: charging or discharging at a rate >_ 30 mA per g of storage compound, is greater -S_ than 350 Wh/kg; or, charging or discharging at a rate >_ 150 mA per g of storage compound, is greater than 280 Wh/kg; or, charging or discharging at a rate >_ 300 mA per g of storage compound, is greater than 270 Wh/kg; or, charging or discharging at a rate 750 mA per g of storage compound, is greater than 250 Wh/kg; or, charging or discharging at a rate >_ 1.5 A per g of storage compound, is greater than 180 Wh/kg; or, charging or discharging at a rate >_ 3 A per g of storage compound, is greater than 40 Wh/kg; or, charging or discharging at a rate >_ 4.5 A per g of storage compound, is greater than 10 Wh/kg.
In another set of embodiments, an electrode comprising a lithium storage t o compound is provided. The lithium storage compound is a compound other than one of ordered or partially ordered rocksalt crystal structure type, or spinel crystal structure type, or vanadium oxide or manganese oxide. The compound has a material energy density (i.e., voltage vs. Li x charge capacity) that while: charging or discharging at a rate >_ 800 mA per g of storage compound, is greater than 250 Wh/kg; or, charging or t 5 discharging at a rate >_ 1.5 A per g of storage compound, is greater than 180 Wh/kg; or, charging or discharging at a rate ? 3 A per g of storage compound, is greater than 40 Wh/kg; or, charging or discharging at a rate >_ 4.5 A per g of storage compound, is greater than 10 Wh/kg.
In another set of embodiments, an electrode is provided. The electrodes includes 2o a current collector comprising any of the compounds described above.
In another set of embodiments, a storage battery cell is provided. The storage battery comprises a positive electrode, a negative electrode and a separator positioned between the positive electrode and the negative electrode. At least one of the positive electrode or negative electrode comprises any of the compounds described above.
25 Other embodiments and novel features of the invention should become apparent from the following detailed description when considered in conjunction with the accompanying drawings. In cases of conflict between an incorporated reference and the present specification, the present specification shall control.
3o BRIEF DESCRIPTION OF DRAWINGS
Preferred, non-limiting embodiments of the present invention will be described by way of example with reference to the accompanying drawings, in which:

FIG. 1 is a copy of an TEM image of a compound with 0.1% Ti doping, prepared according to the method substantially described in Example 1 and heat treated at 600° C
in argon for twenty-four hours, showing that the primary crystallite size is about 100 -200 nm and that the primary crystallites are aggregated into larger particles;
and showing that there is no surface coating or other continuous phase which could provide improved electronic conductivity; thus, the improved electronic conductivity is likely due to an improvement in the compound itself;
FIG. 2 are copies of scanning transmission electron microscope images and energy-dispersive x-ray composition maps of a 1% Ti-doped sample prepared according to to the method substantially described in Example 1 and heat treated at 600° C in nitrogen for twenty-four hours or 800° C in argon for sixteen hours. In the sample heat treated at 600° C, there is detectable Ti in solid solution in the compound as well as an excess of Ti appearing as an additional phase whereas the sample heat treated at 800° C shows no Ti detectable in the phase itself, thus showing that the solid solubility of Ti under these conditions is likely less than about 0.1%;
FIG. 3 are copies of scanning transmission electron microscope images and energy-dispersive x-ray composition maps of an 0.2% Nb-doped sample prepared according to the method substantially described in Example 1 and heat treated at 600° C
for twenty-four hours, 700° C for twenty hours, and 800° C for fifteen hours, all in argon, 2o showing that in the sample heat treated at 600° C, substantial amounts of Nb can be detected within the LiFeP04 grains and a Nb-rich additional phase is substantially absent; in the samples heat treated at 700° C and 800° C, substantially less Nb is detectable in the grains and Nb-rich additional phase has appeared, and thus showing that the solubility of Nb is at least about 0.2% when the material is prepared according to 2s Example 1 and heat treated at 600° C, whereas heat treating at a temperature of 700° C, or greater, causes exsolution ofNb;
FIG. 4 is a graph showing x-ray diffraction patterns of materials prepared according to Example 1, undoped samples and samples containing 1% Ti, 1% Zr, 2% Ti, and 2% Zr, heat treated at 600° C in nitrogen for twenty-four hours, showing that 3o additional phases can be detectable in all of the doped samples and thus that, the solubility limit of the dopants is less than 1% under these preparation conditions; the composition heat treated in argon and nitrogen being substantially similar to that shown in FIG. 15; thus showing that multiple non-oxidizing gas atmospheres can be used to prepare the electronically conductive materials of the invention;
FIG. 5 is a copy of TEM images of a powder of nominal composition LiFeo.99Zro.o~POa and prepared according to the Example 1, showing crystalline particles in which lattice fringes are visible and which do not possess a distinguishable surface phase of another material such as carbon;
FIG. 6A and 6B show X-ray diffraction patterns of various powders showing the effect of canon stoichiometry on dopant solid-solubility. FIG. 35A shows powders containing 1 atom% dopant in the stoichiometry Li~_XMXFePOa are single-phase by XRD
t0 and TEM/STEM analysis. FIG. 35B shows powders containing 1 atom% dopant in the stoichiometry LiFe~_XMXP04 show Li3P04 precipitation by XRD, and secondary phases enriched in the dopant by TEM/STEM (not shown);
FIGS. 7A-7D show elemental maps obtained by STEM of a powder of composition Lio.99Nbo.o~FeP04 (fired 600°C, 20 h, in argon) which illustrate the uniform 15 dopant solid solution observed in compositions of stoichiometry Li~_XMXFeP04;
FIGS. 8 and 9 are graphs showing the conductivity of doped and undoped samples as a function of temperature;
FIG. 10 shows backscattered electron images of the polished cross-section of two Nb-doped and one undoped pellet sintered to high density;
2o FIG. 11 is the configuration of a four-point microcontact measurement performed to determine the electronic conductivity of samples;
FIG. 12 is the electrical conductivity measured at several locations within each of the three samples of FIG. 10;
FIG. 13 shows bright-field TEM images of powders of 1% Nb and 1% Zr doping 25 level and prepared according to the invention;
FIG. 14 shows a TEM image of a conductive 1 % Nb doped composition fired at 600C, showing a particle of incompletely reacted precursor and crystallized olivine phase, and energy-dispersive X-ray spectra taken with a focused electron probe at the locations indicated, showing that carbon is enriched within the particle of unreacted 3o precursor and not detected within several locations of the olivine phase;
FIGS. 15 and 16 show high resolution TEM images of a conductive 1 % Nb doped composition fired at 600C, in which lattice fringes are visible in crystallites of _g-olivine phase, and showing the absence of a significant surface coating of another material;
FIG. 17A shows a first electrochemical cycle for an electrode prepared using a Nb-doped composition, and tested against a lithium metal negative electrode in a laboratory cell using a nonaqueous liquid electrolyte. FIG. 17B shows capacity vs. cycle number for this electrode at a 1C rate (150 mA/g). FIG. 17C shows the coulombic efficiency vs. cycle number at 1C rate (150 mA/g);
FIGS. 18A and 18B show electrochemical test data for electronically conductive olivine of composition Lio.99Zro.oiFeP04 s in a conventional lithium battery electrode to design (78 wt% cathode-active material, 10 wt% Super PT'" carbon, 12 wt%
PVdF
binder; 2.5 mg/cm2 loading) with a lithium metal negative electrode and nonaqueous liquid electrolyte. FIG. 18A shows results of cycle testing which indicates high and stable reversible capacity for more than 150 cycles at a variety of current rates.
Significant capacity with high coulombic efficiency (>99.5%) is retained at rates as high 15 as 3225 mA/g (21.SC). FIG. 18B shows charge-discharge curves indicating little polarization even at the highest current rates, attributed to the high electronic conductivity and high specific surface area of the olivine powder;
FIG. 19 shows discharge curves for continuous cycling between 2-4.2V for an electrode made using Lio.99Zro.o~FeP04 powder and tested to discharge rates of 66.2C
20 (9.93 A/g) at a temperature of 42°C in a conventional cell design using a lithium metal negative electrode and nonaqueous liquid electrolyte;
FIG. 20 shows discharge curves for constant-current constant-voltage cycling between 2-3.8V for an electrode made using Lio.99Zro.oiFeP04 powder and tested to discharge rates of 200C (30 A/g) at a temperature of 22°C in a conventional cell design 25 using a lithium metal negative electrode and nonaqueous liquid electrolyte;
FIG. 21 shows discharge capacity vs. discharge rate curves for several electrodes formulated using Lio.99Zro.o,FeP04 powder heat treated at 600°C or 700°C, and tested to high discharge rates greater than 60C (9 A/g) at 22-23°C in a conventional cell design using a lithium metal negative electrode and nonaqueous liquid electrolyte;
3o FIG. 22 shows discharge capacity vs. discharge rate curves for two electrodes formulated using undoped LiFeP04 powder heat treated at 700°C, and tested at 23°C in a conventional cell design using a lithium metal negative electrode and nonaqueous liquid electrolyte;
FIG. 23 shows discharge capacity vs. discharge rate curves for several LiFeP04 electrodes described in published literature, compared to an electrode of the invention containing Lio,99Zro,o,FeP04 powder, showing the markedly higher discharge capacity available at high discharge rates of the electrodes of the invention;
FIG. 24 shows the discharge energy density in mAh/g vs. the current density in mA/g for an electrode formulated using Lio.99Zro.oiFeP04 powder and measured at a temperature of 22°C;
1o FIG. 25 shows the discharge energy density in mAh/g vs. the current density in mA/g for an electrode formulated using Lio,99Zro.o~FeP04 powder and measured at temperatures of 23, 31, and 42°C;
FIG. 26 shows the discharge energy density in mAh/g vs. the current density in mA/g for an electrode formulated using Li(Feo,98Tio.o2)P04 powder and measured at 15 23°C;
FIG. 27 shows the discharge energy density in mAh/g vs. the current density in mA/g for an electrode formulated using undoped LiFeP04 and measured at temperatures of 23, 31, and 42°C.
FIG. 28 shows a Ragone plot of log power density vs. log energy density for 2o storage battery cells based on the lithium storage materials and electrodes of the invention, compared with other storage battery technology, showing the improved power density that is available while still having high energy density.
FIG. 29 shows a schematic storage battery cell according to one embodiment of the present invention.
DETAILED DESCRIPTION OF THE INVENTION
LiFeP04 and Li(Mn,Fe)P04 are ordered olivine structure compounds also known as the mineral triphylite. They belong to the general group known as polyanion compounds with tetrahedral "anion" structural units (X04)"-, along with oxygen octahedra occupied by a transition metal M, and can include compounds of LiXMX04 (olivine), LiXM2(XO4)3 (NASICON), VOPO4, LiFe(P20~) or Fe4(P20~)3 structure, and structures related to these by having additional metal ions occupying interstitial sites, symmetry-changing displacements, or minor changes in the connectivity of polyhedra.
Here, X is comprised of a metal that can occupy tetrahedral sites within the polyanion groups and has a significant covalent bonding character. X can be P, S, As, Mo, W, Al, Si, or B. According to the present invention, these compounds can be used as lithium storage electrode materials because of their high lithium-insertion potential (relative to lithium metal), high theoretical capacity, low cost, ease of synthesis, and stability when used with common organic electrolyte systems. Despite these characteristics, it has been widely recognized that one of the limitations of this series of compounds is their low electronic conductivity, which greatly limits the practicality of these materials in battery 1o systems. Related compounds such as (Mg,Fe)Si04 are also electronic insulators at an near room temperature, and only have appreciable electronic conductivity at greatly elevated temperatures.
It is therefore a surprising and unexpected discovery that certain compositions of LiFeP04, prepared from starting materials of lithium salts, iron compounds, and 15 phosphorous salts, including but not limited to, lithium carbonate, ammonium phosphate, and iron oxalate, and to which a low additional concentration of a metal supervalent to Li, such as, but not limited to, Mg, AI, Ti, Fe, Mn, Zr, Nb, Ta, and W, such as in the form of a metal oxide or metal alkoxide, have been added, and which is heat treated (HT) at a certain temperature range and atmosphere, exhibit increased electronic conductivity 2o at and near room temperature to render the compounds useful as lithium storage materials.
As used herein, the electrical conductivity of materials will be given in units of S/cm, electrical resistivity in units of ohm-cm (S2-cm), resistance in ohms (S2), charge and discharge capacity in units of ampere hours per kilogram of the storage material 25 (Ah/kg) or milliampere hour per gram of storage material (mAh/g), charge and discharge rate in units of both milliamperes per gram of the storage compound (mA/g), and C rate.
When given in units of C rate, the C rate is defined as the inverse of the time, in hours, necessary to utilize the full capacity of the battery measured at a slow rate.
A rate of 1C
refers to a time of one hour; a rate of 2C refers to a time of half an hour, a rate of C/2 3o refers to a time of two hours, and so forth. Typically, the C rate is computed from the rate, in mA/g, relative to the capacity of the compound or battery measured at a lower rate of C/5 or less. For example, in some examples herein the nominal capacity of a doped LiFeP04 compound at low rate is about 150 mAh/g, and therefore a rate of corresponds to a current rate of 150 mA/g, a rate of C/5 corresponds to 30 mA/g, a rate of SC corresponds to 750 mA/g, and so forth.
In one aspect, the present invention is directed to increasing the electronic conductivity of transition metal polyanion compounds so that they can be used as alkali ion storage materials, for example, rechargeable lithium ion batteries. The compounds of the invention have electronic conductivities near room temperature, for example at a temperature of 22°C-27°C, of at least about 10-8 S/cm. However, in some cases, the conductivity is at least about at least about 10-' S/cm, in other cases, at least about 10-6 S/cm, in yet other cases, at least about 10-5 S/cm, in still other cases, at least about 10-4 to S/cm, in preferred cases, at least about 10'3 S/cm, and in more preferred cases, at least about 10-ZS/cm. Where elements and groups in the Periodic Table are referred to, the Periodic Table catalog number S-18806, published by the Sargent-Welch company in 1994, is used as a reference.
In one aspect, the present invention is directed to increasing the electronic ~ 5 conductivity of transition metal polyanion compounds so that they can be used as alkali ion storage materials, for example, rechargeable lithium ion batteries, without adding excessive amounts of an additional conductive compound such as carbon.
Accordingly, the present invention can include conductivity-enhancing additives, such as but not limited to conductive carbon black, at, for example, less than about 15 weight percent, or 20 in some cases, less than about 10 weight percent, in other cases, less than about 7 weight percent, in other cases, less than 3 weight percent, in other cases, less than 1 weight percent and, in some cases, no conductivity-enhancing additive.
In another aspect, the present invention is directed to decreasing the particle or crystallite size, or increasing the specific surface area (typically given in square meters 25 per gram of the material, m2/g, and measured by such methods as the Brunauer-Emmett-Teller (BET) gas adsorption method) of transition metal polyanion compounds in order to provide improved electrochemical energy storage, including improved charge storage capacity, improved energy density and power density when used in an electrochemical cell, and improved cycle life when the electrochemical cell is reversibly charged and 3o discharged. Compositions are provided for compounds of high specific surface area, including those that are substantially fully crystallized, or those that have substantial electronic conductivity. The materials of the invention have specific surface areas of at least I 5 m2/g. However, in other cases they have specific surface areas of at least 20 mz/g, in other cases at least 30 m2/g, and in other cases at least 40 mz/g.
In another aspect, the present invention provides methods for preparing the transition metal polyanion compounds of the invention, including compounds with substantial electronic conductivity and/or high specific surface area and small particle or crystallite size.
In another aspect, the invention comprises storage electrodes, including those using the transition metal polyanion compounds of the invention. Such storage electrodes have useful properties for electrochemical energy storage including having high storage energy density, high power density, and long cycle life when used reversibly in an electrochemical device. Formulations of and methods for preparing said electrodes are provided.
In another aspect, the invention comprises storage battery cells, including those using the transition metal polyanion compounds of the invention. Such cells have useful t5 energy storage characteristics including high energy density and high power density, and long cycle life.
Electronic Conductivity In one embodiment, the present invention provides an electrochemical device comprising an electrode comprising a compound with a formula LiXFe~_pM"aP04, and a conductivity at 27°C, of at least about 10-$ S/cm. However, in some cases, the conductivity is at least about at least about 10-' S/cm, in other cases, at least about 106 S/cm, in yet other cases, at least about 10-5 S/cm, in still other cases, at least about 10-4 S/cm, in preferred cases, at least about 10-3 S/cm, and in more preferred cases, at least about 10-zS/cm.
In another embodiment, the present invention provides an electrochemical device comprising an electrode comprising a compound with a formula LiXFe,_pM"aP04, the compound having a gravimetric capacity of at least about 80 mAh/g while the device is charging/discharging at greater than about C rate. However, in some embodiments, the capacity is at least about 100 mAh/g, or in other embodiments, at least about 120 mAh/g, in preferred embodiments, at least about 150 mAh/g, and in still other embodiments, at least about 160 mAh/g. The present invention can, in some embodiments, also provide a capacity up to the theoretical gravimetric capacity of the compound.

In another embodiment, the present invention provides an electrochemical device comprising an electrode comprising a compound with a formula LiX_pM"pFeP04.
In another embodiment, the present invention provides an electrochemical device comprising an electrode comprising a compound with a formula LiX_aM"oFeP04, and a conductivity at 27° C of at least about 10-g S/cm. However, in some cases, the conductivity is at least about at least about 10-~ S/cm, in other cases, at least about 10-6 S/cm, in yet other cases, at least about 10-5 S/cm, in still other cases, at least about 10~
S/cm, and in preferred cases, at least about 10-3 S/cm, and in more preferred cases, at least about 10-2 S/cm.
t0 In another embodiment, the present invention provides an electrochemical device comprising an electrode comprising a compound with a formula LiX_aM"pFeP04, the compound having a gravimetric capacity of at least about 80 mAh/g while the device is charging/discharging at greater than about C rate. However, in some embodiments, the capacity is at least about 100 mAh/g, or in other embodiments, at least about 120 mAh/g, t5 in preferred embodiments, at least about 150 mAh/g and in still other preferred embodiments, at least about 170 mAh/g. The present invention can, in some embodiments, also provide a capacity up to the theoretical gravimetric capacity of the compound.
According to one embodiment, a composition comprising a compound with a 20 formula Ax(M'1_pM"Q)y(XD4)Z, AX(M'i-aM"o)y(DXD4)Z, or Ax(M'~_aM"p)y(XzD~)Z, has a conductivity at about 27° C of at least about 10-g S/cm, wherein A is at least one of an alkali metal and hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, molybdenum and tungsten, M" is any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIVA, IB, IIB, IIIB, IVB, VB, and VIB metal, D is at least one of 25 oxygen, nitrogen, carbon, or a halogen, 0.0001 < a S 0.1, and x, y, and z have values such that x plus the quantity y(1-a) times a formal valence or valences of M', plus the quantity ya times a formal valence or valence of M", is equal to z times a formal valence of the XD4 , XZD~, or DXD4 group. x, y, and z are typically greater than 0. The conductivity of the compound can be at least about 10-5 S/cm, at least about 10'4 S/cm, and, in some 3o cases, at least about 10'2 S/cm. In some embodiments, A is lithium and x/(x+y+z) can range from about zero to about one third, or about zero to about two thirds.
In one embodiment, X is phosphorus, while in other embodiments, M' is iron. M" can be any of aluminum, titanium, zirconium, niobium, tantalum, tungsten, or magnesium.
M" can be substantially in solid solution in the crystal structure of the compound.
Typically, the compound has at least one of an olivine, NASICON, VOP04, LiFe(P20~) or Fe4(P20~)3 structure, or mixtures thereof.
In some embodiments, the compound is LiFeP04.
In some embodiments, M" is at least partially in solid solution in the crystal structure of the compound at a concentration of at least 0.01 mole % relative to the concentration of M', the balance appearing as an additional phase, at least 0.02 mole relative to the concentration of M', the balance appearing as an additional phase, and in yet other embodiments, at least 0.05 mole % relative to the concentration of M', the 1o balance appearing as an additional phase and, in still other embodiments, at a concentration of at least 0.1 mole % relative to the concentration of M', the balance appearing as an additional phase.
In some embodiments, the compound can be formed as particles or crystallites wherein at least 50% of which have a smallest dimension that is less than about 500 nm.
t s However, in some cases, the smallest dimension is less than 200 nm, in yet other cases, the smallest dimension is less than 100 nm, in still other cases, the smallest dimension is less than 50 nm, in still other cases, the smallest dimension is less than 20 nm, and in still other cases, the smallest dimension is less than 10 nm. In some embodiments, the compound forms an interconnected porous network comprising crystallites with a 2o specific surface area of at least about 10 m2/g. However, in some cases, the specific surface area is at least about 20 mz/g, in other cases, the specific surface area is at least about 30 m2/g, in other cases, the specific surface area is at least about 40 mz/g, in other cases, the specific surface area is at least about 50 mz/g. Smallest dimension, in this context, means a cross-section.
2s In some cases, the present invention provides a compound with a formula (A,_aM"p)xM'v(XDa)z, (Ai_pM"p)xM'y(DXD4)Z, or (A~_aM"p)xM'y(X2D~)Z that has a conductivity at 27° C of at least about 10-g S/cm, wherein A is at least one of an alkali metal and hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, molybdenum, and tungsten, M" any of a Group IIA, IIIA, IVA, VA, VIA, 3o VIIA, VIVA, IB, IIB, IIIB, IVB, VB, and VlB metal, D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0002 < a < 0.1, and x, y, and z have values such that (1-a)x plus the quantity ax times the formal valence or valences of M" plus y times the formal valence or valences of M' is equal to z times the formal valence of the XD4, XZD~

-IS-or DXD4 group. x, y, and z are typically greater than zero. The conductivity of the compound can be at least about 10'S S/cm, at least about 10-4 S/cm, and, in some cases, at least about 10'2 S/cm. In some embodiments, A is lithium and x/(x+y+z) can range from about zero to about one third. In one embodiment, X is phosphorus, while in other embodiments, M' is iron. M" can be any of aluminum, titanium, zirconium, niobium, tantalum, tungsten, or magnesium. M" can be substantially in solid solution in the crystal structure of the compound. Typically, the compound has at least one of an olivine, NASICON, VOP04, LiFe(P20~) or Fe4(P20~)3 structure, or mixtures thereof. In some embodiments, the compound is LiFeP04. In some embodiments, M" is at least to partially in solid solution in the crystal structure of the compound at a concentration of at least 0.01 mole % relative to the concentration of M', the balance appearing as an additional phase, at least 0.02 mole % relative to the concentration of M', the balance appearing as an additional phase, and in yet other embodiments, at least 0.05 mole relative to the concentration of M', the balance appearing as an additional phase and, in still other embodiments, at a concentration of at least 0.1 mole % relative to the concentration of M', the balance appearing as an additional phase.
In some embodiments, the electronically conductive lithium transition metal phosphate olivine compound has a suitable electronic conductivity greater than about 10'g S/cm. The electronically conductive lithium transition metal phosphate compound 2o can be a composition Lix(M'~_aM"p)P04 or Lix_aM"aM'P04, and can crystallize in the ordered-olivine or triphylite structure, or a structure related to the ordered olivine or triphylite structure with small displacements of atoms without substantial changes in the coordination number of anions around cations, or cations around anions. In such compounds Li+ substantially occupies the octahedral site typically designated as M1, and a substantially divalent cation M' substantially occupies the octahedrally-coordinated site typically designated as M2, as described in the olivine structure given in "Crystal Chemistry of Silicate Minerals of Geophysical Interest," by J. J. Papike and M.
Cameron, Reviews of Geophysics and Space Physics, Vol. 14, No. 1, pages 37-80, 1976.
In some embodiments, the exchange of Li and the metal M' between their respective sites in a perfectly ordered olivine structure is allowed so that M' may occupy either site.
M' is typically one or more of the first-row transition metals, V, Cr, Mn, Fe, Co, or Ni.
M" is typically a metal with formal valence greater than 1+ as an ion in the crystal structure.

In some embodiments, M', M", x, and a are selected such that the compound is a crystalline compound that has in solid solution charge compensating vacancy defects to preserve overall charge neutrality in the compound. In the compositions of type LiX(M' 1~M"Q)P04 or L1x_pM"pM'P04, this condition can be achieved when a times the formal valence of M" plus (1-a) times the formal valence of M' plus x is greater than 3+, necessitating an additional cation deficiency to maintain charge neutrality, such that the crystal composition is Lix(M'i_a_yM"pvacy)P04 or Lix_pM"aM'~_yvacyP04, where vac is a vacancy. In the language of defect chemistry, the dopant can be supervalent and can be added under conditions of temperature and oxygen activity that promote ionic to compensation of the donor, resulting in nonstoichiometry. The vacancies can occupy either M1 or M2 sites. When x<1, the compound also has additional cation vacancies on the Ml site in a crystalline solid solution, said vacancies being compensated by increasing the oxidation state of M" or M'. In order to increase the electronic conductivity usefully, a suitable concentration of said cation vacancies should be greater than or equal to 10~g per cubic centimeter.
In some cases, the compound has an olivine structure and contains in crystalline solid solution, amongst the metals M' and M", simultaneously the metal ions Fe2+ and Fe3+, Mnz+ and Mn3+, Coz+ and Co3+, Ni2+ and Ni3+, V2+ and V3+, or Cr2+ and Cr3+, with the ion of lesser concentration being at least 10 parts per million of the sum of the two ion concentrations.
In some embodiments, the compound has an ordered olivine structure and A, M', M", x, and a are selected such that there can be Li substituted onto M2 sites as an acceptor defect. In the compositions of type Lix(M' i_aM"p)P04 or Lix_aM"aM'P04, typical corresponding crystal compositions are Llx(M',_pyM"aLly)POq Or Lix_pM"pM'~_yLiyP04. In this instance, the subvalent Li substituted onto M2 sites for M' or M" can act as an acceptor defect. In order to increase the electronic conductivity usefully, a suitable concentration of said Li on M2 sites should be greater than or equal to 10'8 per cubic centimeter.
In some embodiments, the present invention provides a p-type semiconducting 3o composition, Lix(M',_aM"Q)P04, LiXM"pM'P04, Lix(M'i_Q_yM"avacy)PO4, Lix_pM"pM'~_yvacyP04, Lix(M',_a_yM"aLiy)P04 or Lix_pM"aM'~_yLiyPO4. M" is a Group IIA, II1A, IVA, VA, VIA, VIIA, VIVA, IB, IIB, IIIB, IVB, VB, and VIB element of the Periodic Table (catalog number S-18806, published by the Sargent-Welch company in 1994.) Magnesium is an example of a dopant from Group IIA, Y is an example of a dopant from Group IIIA, Ti and Zr are examples of dopants from Group IVA, Nb and Ta are examples of dopants from Group VA, W is an example of a dopant from Group VIA, Fe is an example of a metal from Group VIVA, and Al is an example of a dopant from Group IIIB.
x can have a value between zero and 1.1 in the initially prepared material, and during its use as an lithium ion storage compound, x can vary between about zero and about 1.1. a can have a value between about 0.0001 and 0.1. In some embodiments, out of the total amount a of M", at least 0.0001 is in solid solution in the crystalline structure of the compound.
In some embodiments, M' is Fe and the solubility of M" in the lattice can be improved if M" has an ionic radius, in octahedral coordination, that is less than that of Fe2+. Achieving solid solubility sufficient to increase the electronic conductivity above 10~g S/cm can require that processing conditions (for example, temperature, atmosphere, 1s starting materials) allow M" to be stabilized in a particular valence state that would provide an ionic radius less than that of Fez+. In some cases, for example, when solid solubility is achieved, the M" ion may occupy the M1 site, or it may preferentially occupy the M2 site and cause Fe2+ or Fe3+, which would normally occupy the M2 site, to occupy the M1 site.
Generalizing the M" solubility requirement to other olivines of composition Lix_ aM"pM'P04, M" typically has an ionic radius that is less than the average ionic radius of ions M' at the Li concentration x at which the compound is first synthesized.
Electrochemical insertion and removal can later change the valence distribution amongst the M' and M" ions.
2s In some cases, M" can be in the desired valence state and concentration by adding, to the starting material, a salt of M" having the desired final valence. However, the desired valence distribution amongst metals M' and M" can be obtained by synthesizing or heat treating under appropriate conditions of temperature and gas atmosphere. For example, if M' is Fe, heat treatment should be conducted under temperature and atmosphere conditions that preserve a predominantly 2+ valence state, although some Fe3+ is allowable and can even be beneficial for increasing conductivity.
In other cases, for example, for Lix(M',_aM"Q)P04 compositions, firing or heat treating at 600° C, can render the compositions conductive, even if M", or M', is a divalent cation, such as Mg2+ or Mn2+. In some cases, a Li3P04 secondary phase can be present. Thus, the olivine composition according to some embodiments of the present invention may have a lithium deficiency that can result in a Lix_aM"pM'P04 crystal composition.
s The possible dopants M" are not limited to those Groups of the Periodic Table that were previously identified, rather, M" can be any metal that satisfies the above requirements of size and valence. Specifically, for compositions Lix_pM'pM"P04, where M' is Fe, M" may be Mg2+, Mn2+, Fe3+, A13+, Ce3+, Ti4+, Zr4+, Hf +, Nbs+, Tas+, W4+, W6+, or combinations thereof.
to In another embodiment, the compounds of this invention can be used as mixed protonic-electronic conductors for such applications as fuel cell electrodes and gas-separation membranes. Phospho-olivines, such as LiFePOa, can be doped to be highly electronically conducting, while at the same time they can be sufficiently lithium-ion conducting to provide good performance as a lithium battery electrode.
Electrochemical 1s results show good cycling and also demonstrate that the compound can be delithiated while retaining good electronic conductivity. In some cases, the olivine structure can be retained in the fully delithiated state. That is, FeP04 has an olivine structure-type polymorph. Therefore, a doped FeP04 may be protonatable to be a good mixed protonic-electronic conductor, since phosphates are good protonic conductors.
2o The conductive LiMP04 compounds of this invention may also be protonatable to form HxFeP04 conductors, where 0 < x < I .l . Such compounds can be used as the electrode in a proton-conducting fuel cell. Typically such an electrode can be used with a proton-conducting and electronically insulating electrolyte. Such compounds can also be used as a solid membrane for separating hydrogen gas from gas mixtures. For 25 example, hydrogen can be dissociated to protons and electrons at one surface of the membrane that is under a higher hydrogen partial pressure, the protons would typically diffuse through the membrane to a second surface at lower hydrogen partial pressure, and are recombined with electrons to form hydrogen gas that would be released to the atmosphere from the second surface.
3o In some embodiments, compounds of the invention have a structure comprising a continuous network of transition-metal filled anion polyhedral units. The polyhedral units may be octahedrals or distorted octahedrals. The polyhedral units in the structure can, for example, share at least one of vertices, corners, edges, or faces with other polyhedral units. In some cases, the polyhedral units share corners and edges with other polyhedral units.
In some embodiments, the compound is an n-type conductor. In others, the compound is a mixture of an n-type conductor and a p-type conductor. In still others, the compound is a p-type conductor.
In some embodiments, the compound is substantially fully delithiated. The compound may be a p-type conductor when substantially fully lithiated and an n-type conductor when substantially fully delithiated. In some cases, the compound, upon delithiation, undergoes phase-separation into a substantially lithiated compound and a 1 o substantially delithiated compound, each of which have an electronic conductivity of at least 10-6 S/cm.
The compounds of the present invention can be prepared through a variety of techniques, including, for example, solid-state reactions, co-precipitation from liquid solutions, so-called sol-gel methods, or deposition from the vapor phase by methods such 15 as sputtering, laser ablation, electron-beam evaporation, thermal evaporation, and chemical vapor deposition. For large volume production, for example, such compositions can be prepared by solid state reaction methods. For such reactions, numerous possible starting materials are possible, the use of which allows a general classification of the methods.
2o Salts of each of the metals are typically selected so that they can react and decompose upon heating. Examples include salts such as NH4HzP04, LiZC03, and FeC204~2Hz0 for the main constituents (when, for example, M" is Fe), and an alkoxide or metal(organic compound such as Zr(OCZH4)4, Ti(OCH3)4(CH30H)2, Nb(OC6H5)s, Ta(OCH3)5, W(OCZHS)6, Al(OCZHS)3, or Mg(OCZHS)Z as the source of the metal M".
25 When using one or more of these materials as the starting materials, gaseous species such as carbon oxides, hydrogen, water, and ammonia can be generated and removed, if necessary, during preparation.
The oxide Li20, a divalent oxide of the metal M" (such as FeO, MnO, or Co0), and P205 can be used as the source of the main constituents. The metal M" is typically 3o added as its oxide in the preferred valence state, for example, as MgO, Ti02, Zr02, Fe203, Nb205, Ta205, A1203, W03, or W06. When using such exemplary starting materials, the compound can be crystallized with substantially little or no evolution, or introduction, of gaseous species. That is, the reaction of the starting can be conducted in a closed-reaction system, typically without substantial mass transport in, or out.
The present invention allows any mixture of starting materials, some of which will yield a decomposition product, and some of which will not. For example, a portion of the starting materials can react to evolve or absorb gaseous species during formation thereof. If Li2C03 or LiOHwHzO is used as the lithium source, carbon oxide, or water, or both can be generated during formation. Other constituents of the compound are typically provided as oxide thereof, typically in the preferred formal valence, (for example, as FeO, P205, and Nb205), which typically do not evolve or absorb gaseous 1o species during the reaction. In other instances, starting materials may be used that substantially comprise a closed system in which there is little or no mass transport in or out of the reactants during formation of the materials of the invention. One preferred such reaction uses LiP03 and Fe0 to form LiFeP04 as the product. Adjustments to the relative amounts of the reactants, and the addition of other constituents such as the 15 dopants in the form of oxides in which the cations have their preferred formal valence state, are readily used in order to obtain compositions comprising the materials of the invention.
The dopants M" can also be added by milling the starting materials in milling media comprising the desired doping materials. For example, zirconia or alumina 2o milling balls or cylinders can be used to introduce Zr or Al as the dopant.
Milling equipment, such as a milling container, made of such materials can also be used as the source of dopant. The amount of dopant can be controlled by monitoring the extent, intensity or duration or both, of milling and controlling such until a predetermined dopant level is achieved.
25 Further, milling media or containers can be used to add carbon, for example, to the materials of the invention in small quantities that can have a beneficial effect on the conductivity of the material without substantially decreasing the energy density of the material. The amount of carbon added in this instance is preferably less than about 10 weight percent of the total mass of the material, more preferably less than about 5 weight 30 percent, and still more preferably less than about 3 weight percent.
Milling containers or milling media that have such effect include those made from polypropylene, polyethylene, polystyrene, and fluoropolymers such as Teflon~ (E.I du Pont de Nemours and Company, Wilmington, Delaware).

For Lix(M',_aM"Q)P04 compositions, a is preferably less than about 0.05 and the compound is preferably heat treated under various conditions.
A substantially reducing or inert gas atmosphere can be used, for example, nitrogen, argon, nitrogen-hydrogen mixtures, carbon dioxide-carbon monoxide mixtures, or mixtures of nitrogen with oxygen or argon with oxygen. The oxygen partial pressure in the gas mixture under the firing conditions applied to the composition is typically less than about 10-3 atm, preferably less than about 10~ atm, more preferably less than about 10-5 atm, and still preferably less than about 10-6 atm. When using salts that can decompose to yield gaseous products upon heating, the compounds can be exposed to a 1o first heat treatment to decompose, in some cases, the salts leaving substantially only the oxides of each metal, at a lower temperature than the final crystallization heat treatment.
For example, heat treatment at 350° C for ten hours in flowing nitrogen or argon is typically sufficient to transform the starting materials if the batch size is a few grams. A
final heat treatment at a higher temperature typically follows. In some cases, the material is not heated to temperatures greater than about 800° C for longer than about four hours. Preferably, the material is heated at less than about 750°
C but greater than about 500° C, and is held at that temperature between four and twenty-four hours.
For Lix_pM"pM'P04 compositions, a is preferably less than 0.1 and the material can be heated to higher temperatures and for longer times than described above, without losing electronic conductivity. That is, these compositions can be subjected to much wider ranges of heat treatment temperature and time while still yielding high electronic conductivity. Various heat treatments can also be used. For example, a substantially reducing or inert gas atmosphere is used, for example, nitrogen, argon, nitrogen-hydrogen mixtures, carbon dioxide-carbon monoxide mixtures, or mixtures of nitrogen with oxygen or argon with oxygen. The oxygen partial pressure in the gas mixture under the firing conditions applied to the composition is typically less than about 10~
atmosphere, preferably less than about 10'5 atm, and still preferably less than about 106 atm. When using salts that decompose to yield gaseous products upon heating, the compounds may be exposed to a first heat treatment to decompose, in some cases, the 3o salts leaving substantially only the oxides of each metal, at a lower temperature than the final crystallization heat treatment. For example, a heat treatment at 350° C for ten hours in flowing nitrogen or argon can be sufficient to transform the starting materials if the batch size is a few grams. A final heat treatment at a higher temperature typically follows. In some cases, the material is heated to a temperature preferably greater than 500° C and less than about 900° C, still preferably greater than about 550° C and less than about 800° C, and is held at that temperature between four and twenty-four hours.
While a detailed understanding of the conduction mechanism in the materials of the present invention is not necessary to define or to practice the invention, it is useful to elaborate a possible mechanism that is consistent with the experimental observations.
Measurements show that the highly conductive compositions are typically p-type, not necessarily n-type, while the undoped compositions can be n-type. This shows that acceptor defects can be introduced by doping and heat treating as described herein.
to Having a supervalent cation on the M1 site can introduce a donor on that site. However, since the resulting materials are p-type, it is believed that electronic compensation of a donor cation is not necessarily the mechanism by which conductivity increases.
Having vacancies on the M2 iron sites, for ionic compensation of supervalent cations on the Ml sites, or in order to charge-compensate an excess of Fe3+ introduced on the M2 sites, can 15 introduce acceptor states on the M2 sites. This is analogous to having a subvalent dopant on the Fe site, and can create an acceptor defect on the M2 sites. Having lithium substituted for a cation of higher valence on the M2 sites can also create acceptor defects on those sites. Having lithium deficiency on the Ml site can also create acceptor defects on those sites.
2o Therefore, highly conductive p-type behavior can be obtained when there are acceptor defects or ions on the M1 or M2 sites that are not simultaneously charge-compensated by other solutes or defects. However, for increased p-type conductivity to be obtained in the compound, it is preferred that such acceptor defects form a crystalline solid solution of the compound. For instance, in the undoped and insulating compound 25 LiFeP04, if upon delithiation to an overall composition LiXFeP04 where x<1, the compound forms two compositions or phases, LiFeP04 in which Fe is substantially all in the ferrous (2+) state, and FeP04 in which Fe is substantially all in the ferric (3+) state, then each individual compound comprising the material is substantially insulating, resulting in a whole material that is also insulating.
3o Thus, in one embodiment, the present invention provides a compound comprising a composition with a formula AX(M'~_aM"a)y(XD4)Z, AX(M'~-aM"a)y(DXD4)~, or AX(M' ~_aM"a)y(XZD~)Z, having a conductivity at 27° C of at least about 10-8 S/cm. In some embodiments, A is at least one of an alkali metal and hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, molybdenum and tungsten, M" is any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIVA, IB, IIB, IIIB, IVB, VB, and VIB metal of the Periodic Table (catalog number S-18806, published by Sargent-Welch, 1994), D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <_ 0.1, and x, y, and z are greater than 0 and have values such that x, plus y(1-a) times a formal valence or valences of M', plus ya times a formal valence or valence of M", is equal to z times a formal valence of the XD4, XzD~, or DXD4 group. In another embodiment, the present invention provides a compound comprising a composition with a formula (A,_pM"p)xM'y(XD4)Z, (Al_aM"a)xM'y(DXD4)Z, or (A~_aM"Q)xM'y(XzD~)Z, having 1o a conductivity at 27° C of at least about 10~g S/cm. In some embodiments, A is at least one of an alkali metal and hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, molybdenum and tungsten, M" is any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIVA, IB, IIB, IIIB, IVB, VB, and VIB metal, 0.0001 < a <_ 0.1, and x, y, and z are greater than 0 and have values such that x, plus y(1-a) times a formal valence or valences of M', plus ya times a formal valence or valence of M", is equal to z times a formal valence of the XD4, X2D~, or DXD4 group.
In yet another embodiment, the present invention provides a fuel cell comprising a mixed proton conducting and electronically conducting material having a formula AX(M' ~-aM"a)y(XD4)z~ Ax(M' 1-aM"a)y(DXD4)Z, Ax(M' ~-aM"a)Y(X2D~)Z~
(A1_pM"p)xM'y(XDa)Z, (A,_aM"Q)xM'y(DXD4)Z, or (Al_pM"p)xM'v(X2D~)z. In the compound, A is at least one of an alkali metal and hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, molybdenum, and tungsten, M"
any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIVA, IB, IIB, IIIB, IVB, VB, and VIB
metal, D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <_ 0.1, and x, y, and z are greater than 0 and have values such that x, plus y(1-a) times the formal valence or valences of M', plus ya times the formal valence or valences of M", is equal to z times the formal valence of the XD4, XZD~ or DXD4 group.
In some embodiments of the invention, it may be preferable for the compound to be substantially free of silicon. That is, silicon is not present in amounts greater than trace amounts.
In a further embodiment, the present invention provides a composition having a conductivity at about 27° C of at least about 10-8 S/cm comprising primary crystallites with a formula LiFeP04. The primary crystallites having an olivine structure that can form at least a part of an interconnected porous network.
In still another embodiment, the present invention provides a method of providing electrical energy. The method comprises the step of providing a battery having an electrode comprising a compound having a conductivity at 27°
C of at least about 10-8 S/cm and a capacity of at least about 80 mAh/g. The method further comprises the step of charging the battery at a rate that is greater than about C rate of the compound.
In still another embodiment, the present invention provides a method of forming to a compound. The methods include mixing an alkali metal or hydrogen salt, a first-row transition metal salt, a salt of at least one of phosphorus, sulfur, arsenic, silicon, aluminum, boron, vanadium, molybdenum and tungsten, and a salt of any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIVA, IB, IIB, IIIB, IVB, VB, and VIB metal.
The method further includes milling the mixture and heat treating the mixture at a is temperature between 300-900°C. This method may be used to form any suitable compound described herein.
In yet another embodiment, the present invention is directed to a method of doping a material to form a conductive material. The method comprises the steps of mixing powders of a lithium salt and an iron oxide and adding an oxide of a dopant, the 2o dopant having the same valence state in the oxide as in the conductive material. The method also comprises the step of heat treating the mixed powders to form the doped conductive material.
And, in one embodiment, the present invention is directed to a method of doping a material to form a conductive compound. The method comprises the steps of selecting 25 a starting material to be doped, in conjunction with selection of milling equipment comprising a dopant for doping the starting material at a predetermined level of dopant and milling the starting material in the milling equipment. The method further comprises the step of recovering from the milling step a material suitable for forming a conductive material comprising the starting material doped with the dopant at the predetermined 30 level.
Amongst other applications, the compounds, electrodes, and battery cells of the invention are useful for high power, safe, rechargeable lithium batteries for applications such as hybrid and electric vehicles, back-up power, implantable medical devices, and applications that currently use supercapacitor technology. The combination of high electronic and ion transport at reduced temperatures in these compounds also makes proton conducting analogs useful as electrode materials for other electrochemical applications such as low-temperature protonic fuel cell electrodes or hydrogen gas separation membranes.
In some embodiments, electrodes are formed from any of the compounds described herein. In some embodiments, though not all, it may be preferable for the electrode materials to be lithium storage compounds other than one of ordered or partially ordered rocksalt crystal structure type, or spinet crystal structure type, or 1o vanadium oxide or manganese oxide. Examples of ordered or partially ordered rocksalt crystal structure types include LiCo02, LiNi02, LiMn02, and their solid solutions.
Examples of spinet crystal structure type include LiMn204 and its solid solutions.
The electrode materials of the invention may have a variety of material energy densities at different charging or discharging rates. In one set of embodiments, the electrode has a material energy density that, while charging or discharging at a rate >_ 800 mA per g of storage compound, is greater than 250 Wh/kg, or charging or discharging at a rate >_ 1.5 A per g of storage compound, is greater than 180 Wh/kg, or charging or discharging at a rate >_ 3 A per g of storage compound, is greater than 40 Wh/kg, or charging or discharging at a rate >_ 4.5 A per g of storage compound, is greater than 10 2o Wh/kg.
In another set of embodiments, the electrode has a material energy density that, while charging or discharging at a rate >_ 800 mA per g of storage compound, is greater than 350 Wh/kg, or charging or discharging at a rate >_ 1.5 A per g of storage compound, is greater than 270 Wh/kg, or charging or discharging at a rate >_ 3 A per g of storage 2s compound, is greater than 150 Wh/kg, or charging or discharging at a rate >_ 4.5 A per g of storage compound, is greater than 80 Wh/kg, or charging or discharging at a rate >_ 6 A per g of storage compound, is greater than 35 Wh/kg, or charging or discharging at a rate >_ 7.5 A per g of storage compound, is greater than 50 Wh/kg, or charging or discharging at a rate >_ 15 A per g of storage compound, is greater than 10 Wh/kg.
3o In another set of embodiments, the electrode has a material energy density that, while charging or discharging at a rate >_ 800 mA per g of storage compound, is greater than 390 Wh/kg, or charging or discharging at a rate >_ 1.5 A per g of storage compound, is greater than 350 Wh/kg, or charging or discharging at a rate ? 3 A per g of storage compound, is greater than 300 Wh/kg, or charging or discharging at a rate >_ 4.5 A per g of storage compound, is greater than 250 Wh/kg, or charging or discharging at a rate >_ 7.5 A per g of storage compound, is greater than 150 Wh/kg, or charging or discharging at a rate >_ 11 A per g of storage compound, is greater than 50 Wh/kg, or charging or discharging at a rate >_ 15 A per g of storage compound, is greater than 30 Wh/kg.
Electrodes of the invention may have a variety of different configurations depending on the application in which the electrode is used. In some cases, the electrode may comprise a sheet or a mesh coated or impregnated with the storage compound. In to other cases, the electrode comprises a metal foil coated one or both sides with the storage compound.
The electrode may include different loading amounts of the storage compound.
For example, the electrode may include a loading of at least 4 mg, 8 mg, 10 mg, 14 mg, or 20 mg per square centimeter of projected area of the sheet or mesh.
The electrode may be a sheet or a mesh having a total thickness of at least 20 micrometers, 40 micrometers, 60 micrometers, 80 micrometers, 100 micrometers, micrometers, or 200 micrometers.
It should be understood that the electrodes of the invention may have other configurations and structures than those described herein.
2o Fig. 28 schematicaly illustrates a storage battery cell 10 according to one embodiment of the present invention. Storage battery cell 10 includes a positive current collector 12 in contact with a positive electrode 14. The storage battery cell further includes a negative current collector 18 in contact with a negative electrode 16. A
separator 20 is positioned between the positive electrode and the negative electrode.
Either the positive or the negative electrode (or both) may be comprised of any of the compositions described herein.
Storage battery cells of the present invention may exhibit different properties.
For example, the cell may exhibit, upon discharge, an energy of at least 0.25 Wh; in other cases, at least 1 Wh; in other cases, at least 5 Wh; in other cases, at least 10 Wh; in other cases, at least 20 Wh; in other cases, at least 30 Wh; in other cases, at least 40 Wh;
in other cases, at least 60 Wh; and, in other cases, at least 100 Wh.

The storage battery cells may also exhibit a variety of combinations of gravimetric energy and/or volumetric energy density upon discharge. For example, the storage battery cell may exhibit a discharge a gravimetric energy density of at least 30 Wh/kg or a volumetric energy density of at least 100 Wh/liter; a gravimetric energy s density of at least 50 Wh/kg or a volumetric energy density of at least 200 Wh/liter; a gravimetric energy density of at least 90 Wh/kg or a volumetric energy density of at least 300 Wh/liter; a gravimetric power density of at least 500 W/kg or a volumetric power density of at least 500 W/liter; a gravimetric power density of at least 1000 W/kg or a volumetric power density of at least 1000 W/liter; a gravimetric power density of at least 2000 W/kg or a volumetric power density of at least 2000 Wh/liter.
Storage battery cells of the invention may also exhibit a variety of gravimetric energy density at different power densities. For example, the storage cells may exhibit, upon discharge, a gravimetric energy density of at least 30 Wh/kg at a power density of at least 500 W/kg, or 20 Wh/kg at a power density of at least 1000 W/kg, or 10 Wh/kg at is a power density of at least 1500 W/kg, or 5 Wh/kg at a power density of at least 2000 W/kg, or 2 Wh/kg at a power density of at least 2500 W/kg, or 1 Wh/kg at a power density of at least 3000 W/kg.
In another embodiment, the storage cells may exhibit, upon discharge, a gravimetric energy density of SO Wh/kg at a power density of at least 500 W/kg, or 40 Wh/kg at a power density of at least 1000 W/kg, or 20 Wh/kg at a power density of at least 2000 W/kg, or 10 Wh/kg at a power density of at least 3000 W/kg, or 4 Wh/kg at a power density of at least 4000 W/kg, or I Wh/kg at a power density of at least W/kg.
In another embodiment, the storage cells may exhibit, upon discharge, a gravimetric energy density of at least 80 Wh/kg at a power density of at least 1000 W/kg, or 70 Wh/kg at a power density of at least 2000 W/kg, or 60 Wh/kg at a power density of at least 3000 W/kg, or 55 Wh/kg at a power density of at least 4000 W/kg, or 50 Wh/kg at a power density of at least 5000 W/kg, or 30 Wh/kg at a power density of at least 6000 W/kg, or 10 Wh/kg at a power density of at least 8000 W/kg.
3o It should be understood that certain storage cells of the invention may have a variety of different structures than those described herein and exhibit different properties than those described herein.

The present invention will be further illustrated through the following examples, which are illustrative in nature and are not intended to limit the scope of the invention.
Example 1. Metal-Doped Compositions s This example demonstrates the preparation of compositions having the formulation Li(Fe~_aM"a)P04, where M" is Al, Ti, Zr, Mn, Nb, Ta, W, Mg, or Li.
Specific compositions, heat treatments, and results are listed in Tables 2 and 3, respectively. It was found that the electronic conductivity increased only for certain low concentrations of the metal additive or dopant. The specific range of concentration 1o providing a high electronic conductivity (greater than about 10'5 S/cm) varied for each dopant but was generally less than about 5 mole % of the Fe concentration. In addition to having a low concentration of the dopant, it was necessary to heat treat the material under conditions such that high electronic conductivity was obtained. These conditions included heat treatment in a non-oxidizing gas atmosphere, including but not limited to t s argon, nitrogen, and nitrogen-hydrogen mixtures. Moreover, the temperature of heat treatment was less than about 800° C. At 600° C, the firing time in the above described gas atmosphere was less than about 100 hours.
Sample Preparation 2o Compositions as listed in Table 2 or otherwise described herein were prepared as follows or as adjusted to suit the particular composition by procedures illustrated for the following compositions. The starting materials of this Example are listed in Table 1.
Table 1. Starting materials for a synthesis method for doped LiFeP04 Theoretical*Analyzed Compound Manufacturer/Purity Elementcontent content (~%) wt%) (Wt%

LiZC03 Alfa-Aesar, 99.999 Li 18.8 18.9 FeC204~2H20Aldrich, 99.99 Fe 31.0 30.7 NH4HzP04 Alfa-Aesar, 99.998 ~ 26.9 ~ 27.2 * The metals content was analyzed using Direct Current Plasma (DCP) emission spectroscopy following ASTM E1097.

The starting materials were weighed to high precision using a laboratory balance.
For example, Zr-doped LiFeP04 samples of the following doping levels and batch sizes were prepared using the following starting materials, wherein zirconium ethoxide served as the source of the dopant:
mole % Zr. 1 mole% Zr 2 mole % Zr

5 g batch 2.5 g batch2.5 g batch NH4H2P04 3.6465g 1.7254g 1.7254g LizC03 1.1171g 0.554g 0.554g o FeC204~2H20 5.4177g 2.6715g 2.6715g Zr(OCZHS)4 0.4303g 0.0407g 0.0814g Similarly, 1 mole % and 2 mole % Ti-doped LiFeP04 were prepared using the starting materials as above, except that titanium methoxide, Ti(OCH3)4(CH30H)2 was t 5 used as the source of Ti (in place of the Zr(OCZHS)4):
1 mole % Ti 2 mole % Ti 2.5 g batch 2.5 g batch NH4HzP04 1.7254g 1.7254g 2o LizC03 0.554g 0.554g FeC2042Hz0 2.6715g 2.6715g Ti(OCH3)4(CH30H)Z 0.0354g 0.0708g Undoped LiFeP04 samples were prepared from the same materials except 25 without the dopant salt. For the other samples, with the dopants as listed in Table 2, an appropriate metal salt was used. In particular, to prepare the Nb-doped samples, niobium phenoxide, Nb(OC6H5)5, was used as the dopant salt; to prepare the Ta-doped samples, tantalum methoxide, Ta(OCH3)5, was used as the dopant salt; to prepare the W-doped samples, tungsten ethoxide, W(OCZHS)6, was used as the dopant salt; to prepare the Al-3o doped sample, aluminum ethoxide, Al(OC2H5)3, was used as the dopant salt;
and to prepare the Mg-doped samples, magnesium ethoxide, Mg(OCZHS)2, was used as the dopant salt.
To prepare each sample, each of the components was weighed in an argon-filled glove box. They were then removed from the glove box and ball milled, using zirconia 35 milling balls, in a polypropylene jar for about twenty hours in acetone.
The milled mixture was dried at a temperature not exceeding 100° C, and then ground with a mortar and pestle in the argon-filled glove box. Each of the mixtures was then heat treated,

6 PCT/US02/41471 given as "HT1" through "HT7" under the conditions listed in Table 3. In each case, a first heat treatment at 350° C for ten hours was conducted in a flowing atmosphere of the specified gas. Each of the powder samples was then ground, using a mortar and pestle, and subjected to a second heat treatment at a higher temperature, in a flowing atmosphere of the specified gas.
Conductivity Measurements It is well-known that the electrical conductivity of solid compounds is difficult to accurately measure from a finely divided powder form of the compound. On the other to hand, powders that have been compacted and fired so as to achieve sintered contacts between the powder particles, or have been partially or completely densified, allow more accurate measurement of the conductivity of the compound. For sintered pellets of reasonably high density, and in which the particle contacts do not have a higher specific resistance, the conductivity of the pellet is reduced from that of the compound itself in 15 approximately linear proportion to the amount of porosity that is present.
For example, a pellet that has I O% porosity may be judged to have about 90% of the conductivity of the compound. In order to measure the conductivity when samples were prepared in a powder form, pellets were pressed out of the heat treated powder sample prior to the second heat treatment, and placed in alumina crucibles during the second heat treatment 2o so that the powders and sintered pellets were heat treated together. The density of the fired pellets were from about 60% to about 95% of the crystal density, depending on composition and heat treatment.
In order to measure electrical conductivity, 2-point and 4-point (van der Pauw, vdP) conductivity measurements were performed according to known conventional 25 procedures. Because metal contacts that are blocking to lithium ions and conductive to electrons were used, the resulting conductivities are understood to reflect the electronic conductivity of the compound. The room temperature conductivities of several of the doped samples are listed in Table 2.
30 X-ray Diffraction, Electron Microscopy, Specific Surface Area Measurement, and Chemical Analysis Several methods were used to determine the crystalline phase, extent of crystallization, powder particle size and morphology, specific surface area of the powder, and the location of dopants. Samples were evaluated by x-ray diffraction after heat treatment to determine the crystalline structure as well as to determine if there was a detectable secondary phase. In some cases, some of the powder samples were examined at higher resolution by transmission electron microscopy (TEM) and/or scanning transmission electron microscopy (STEM) to determine whether secondary phases were present, whether a surface coating of another phase were present, and to measure the concentration of the dopant metal within the crystalline grains of the LiFeP04 phase.
This allowed a determination of whether the metal dopant, at the added concentration and heat treatment, was soluble or had exceeded its solubility limit in the LiFeP04 phase.
t o It was also possible to determine whether the particles of crystallized compound had a surface coating of another material. In some cases, the composition of the powders or pellets were determined using direct current plasma (DCP) emission spectroscopy according to ASTM ASTM E1097, or combustion IR detection according to ASTM
E1019.
15 In the samples listed in Table 2, the first numeral indicates the dopant, the second the concentration, and the third, the heat treatment. For example, sample 3c1 refers to a Ti-doped sample of 0.1 mole % concentration subjected to the heat treatment HT1.
Where the concentration of dopant is given herein in mole percent, it refers to the relative molar fraction, Ti/(Ti+Fe) multiplied by 100.
Table 2. Results for Undoped and Doped Lithium Iron Phosphates Room Temperature Composition Heat Conductivity ~/TEM/ Minor (Sample) TreatS/cm STEM phases ment van observations(by XRD) der 2-point pauw 1. Undoped (lal) HT1 < 10-6 __ Single None detected phase LiFeP04 olivine (lb2) HT2 < 10-6 __ Single None detected phase LiFeP04 olivine (lc3) HT3 < 10-6 __ Single None detected phase LiFeP04 olivine (ld6) HT6 2 __ Single None detected 2 x 10-9t phase LiFeP04 . olivine (le6) HT6 74x10-$ __ Single None detected 3 phase LiFePOa . olivine Room Temperature Composition Heat Conductivity XRD/TEM/ Minor (Sample) TreatS/cm STEM phases ment van observations(by XRD) der 2-point pauw HT7 2.22x10'9t__ __ __ LiFeP04 ( 1 g8) HT8 1.8 x __ Multi-phaseLi3P04, 10' Fe3P
"' LiFeP04 2. Aluminum HT1 8.2 x -- Dopant None detected 10-5 soluble Li Al. o Fe 998 P04 (2b6) HT6 10'3 -- Dopant None detected soluble Li.99Al.o, FeP04 3. Titanium ( HTS < 10'5 -- Dopant None detected soluble Fe 999 P04 Li Ti.

(3d1) HT1 1 __ Exceeds Not identified

7 x 10'4 LI(TI,002Fe.998)P~4 . solubillt (3e1) HT1 2.0 x __ Exceeds Li3p04 10'4 Li(Ti.o,Fe,99)POa solubilit (3e2) HT2 1.9 x __ Exceeds Li3p04 10'4 Li(Ti,o,Fe,99)P04 solubili (3e3) HT3 < 10'6 __ Exceeds Not identified Li(Ti.o,Fe,99)P04 solubilit HT2 1 -- ds Not identified 4 x 10'6 Li(Ti, ZFe,98)PO4 . solub li (3g6) HT6 1.3 x -- Dopant None detected 10'3$ soluble Li,99Ti.o, FeP04 (3g7) HT7 2.3 x -_ Exceeds Li3p04, 10'2 Fe2P

(Li.99Ti.o,)FeP04 solubilit 4. Zirconium 4 HT1 5.0 x -- Dopant None detected 10'5 soluble Fe998 P04 Li Zr, o (4b1) HT1 3.7 x __ Exceeds Li3p04 10'4 Li(Zr.oIFe,99)P04 solubility (4b2) 1..1~4.5 x __ Exceeds Li3pp4 10'5 Li(Zr_o,Fe,99)P04 solubili (4b3) HT3 < 10'6 __ Exceeds Not identified Li(Zr,o, solubi Fe,99)P04 1 ity (4c2) H~ 1.8 x __ Exceeds Li2Zr03 Li(Zr,ozFe.98)POa solubilit (4d2) HT2 ~ 10'5 __ Exceeds Li2Zr03 Li(Zr,o5Fe,95)P04 solubility l HT1 ~ 104 -- Dopant None detected soluble Li,~,Zro, FeP04 Room Temperature Composition Heat Conductivity x~~'EM/ Minor (Sample) TreatS/cm STEM phases ment van observations(by XRD) der 2-point pauw (4e2) HT8 1.6 x __ Exceeds Li3p04, 10-2 Fe2P

(Li.99Zr.o,)FeP04 solubili 5. Niobium ) HT1 1.3 x -- Dopant None detected S 10-4 soluble Fe Li Nb, o ( HT1 5.8 x -- Dopant None detected 10-4 soluble zFe 998 P04 Li b.

HT4 < 10-6 __ __ __ Li b, ozFe 99s P04 ) HT6 1.1 x -- Dopant None detected 10-3 soluble Li.998Nb oo FeP04 ) HT7 1.1 x -- Dopant None detected 10-2$ soluble FeP04 Li_998Nb o Z

HT6 4.1 x -- Dopant None detected 10-2 soluble Li.99sNb oos FeP04 (5g6) HT6 2.2 x 2.73x10-2Dopant None detected 10-2 soluble Li.99Nb,o, FeP04 g HT7 4.3 x -- ' Fe2P
10-2$ d LisP04 )FeP04 ty , (Li.99Nb solub 1 ~

(Sh6) HT6 2.8 x __ Exceeds FezP

(Li.98Nb.oz)FeP04 solubility (Si6) _6 Exceeds HT6 ~ 10 -- Fe2P

(Li.96Nb.~)FeP04 solubili 6. Tantalum 6 HT1 3.0 x -- Dopant None detected 10-5 soluble Fe998 POQ
Li(Ta. o 7. Tungsten HT1 1.5 x -- Dopant None detected 10-4 soluble Li W: zFe99g

8. Magnesium 8 HT1 ~ 10-4 -- Dopant None detected ) soluble Li M .o Fe 99s POa 8 HT6 6.8 x -- Dopant None detected 6 10'4$ soluble FeP04 L1.99M

(8b7) HT7 2.4 x __ Exceeds Li3pOa, 10-2$ Fe2P

(Li.99Mg,o,)FeP04 solubilit (8bg) HT8 3.8 x __ Exceeds Li3p04, 10-3$ Fe2P

(Li.99Mg.o,)FeP04 solubilit

9. Manganese (2+) (9a1) HT1 ~ 10-4 -- Dopant None detected soluble Li(Mn.~zFe.99a POa Room Temperature Composition Heat Conductivity ~/TEM/ Minor (Sample) TreatS/cm STEM phases ment van observations(by XRD) der 2-point pauw

10. Iron (2+) ( 10a6) HT6 < 10'6 __ Exceeds Li3P04, Fe, (Li,99Fe.o~)FeP04 solubilit Fe3P

11. Iron (3+) ( 11 a6) HT6 3.3 x 4.1 Exceeds Li3P04, 10-z x Fe, 10-z (Li.99Fe.oOFeP04 solubilityFe3P

12. Lithium (12a6) HT6 < 10'6 __ Exceeds Li3P04, Fe, Li(Fe.99Li solubilit Fe3P
,o,)POa ~ measurement by AC Impedance Spectroscopy ~ measurement by two point method, using sputtered Au electrodes.
Table 3. Heat Treatment Conditions Heat Conditions Treatment(all gases at 1 atm total ressure) HT1 350 C, 10 hours,600 C, 24 hours,-Ar Ar HT2 350 C, 10 hours,600 C, 24 hours,-NZ NZ

HT3 350 C, 10 hours,800 C, 24 hours,-HT4 350 C, 10 hours,800 C, 24 hours,-HTS 350 C, 10 hours,600 C, 24 hours,600 C, 76 hours, Ar Ar Ar HT6 350 C, 10 hours,700 C, 20 hours,-Ar Ar HT7 350 C, 10 hours,850 C, 20 hours,-Ar Ar HT8 350 C, 10 hours,800 C, 15 hours, Ar Ar Results 1o X-ray diffraction showed that after the 350°C heat treatment, the powders of this example were poorly crystallized and not of a single major crystalline phase.
After the second, higher temperature heat treatment, all samples subjected to XRD showed peaks associated with the olivine structure. The relative intensity of X-ray peaks showed that the olivine phase was the major crystalline phase. Visual observation of the heat treated 15 powders and pellets proved to be a reliable indication of whether or not increased electronic conductivity had been obtained. While the undoped LiFeP04 was light to medium gray, the conductive doped powders and sintered pellets, regardless of specific dopant, concentration, or heat treatment, were colored black. Conductive sintered pellets were also easily distinguished from insulating pellets with a simple ohmmeter measurement using two steel probes placed 0.5-1 cm apart. Insulating compositions had resistances too great to measure (being greater than the instrument limit of 200 MS2), while conductive samples had resistances of typically 30 kS2 to 300 kS2.
The results in Table 2 show that heat treating undoped LiFeP04 was not effective in producing an acceptable conductive material; each of the conductivities of sintered pellets was less than about 10-6 S/cm. The undoped compound was also found to have a 1o very narrow range of cation nonstoichiometry, with as little as 1%
deficiency of the ferrous iron oxalate resulting in a detectable amount of Li3P04 phase.
In contrast, for the dopants listed, at low concentrations, it was possible to produce a sample having a room temperature conductivity greater than about 10-5 S/cm.
These conductivity values exceed known values for the positive electrode compound 1s LiMn204. Further, Al, Ti, Zr, Nb, W, Mg, Mn, and Fe(3+)-doped samples could be produced with a conductivity greater than 10~ S/cm.
Electron microscopy showed that the highly electronically conductive samples did not have a surface coating or other form of an additional conductive phase. A typical image is shown in FIG. l, which is a copy of a TEM image of a 0.01% Ti-doped sample.
2o The figures show that the doped compositions of LiFeP04, synthesized in non-oxidizing or inert atmosphere at temperatures below about 800° C, had increased electronic conductivity compared to the undoped LiFeP04 compositions, thus making them useful as lithium storage electrodes especially at practical charge/discharge rates.
At the low doping levels used, the doping does not limit the ability of the material to 25 store lithium at a high voltage (about 3.SV relative to lithium metal) or achieve a high lithium storage capacity.
The results also showed that too high a heat treatment temperature, and/or too long a heat treatment period, can result in insulating materials. As a specific comparison, the Ti-doped sample, sample 3e3, which was heat treated at 800° C for twenty-four 3o hours, was insulating (less than 10-6 S/cm) whereas a similar 1% Ti-doped composition, samples 3e1 and 3e2, which were heat treated at 600° C for twenty-four hours, were highly conductive (2 x 10~ and 1.9 x 10-4 S/cm). The insulating sample 3e3 was examined using an STEM, which showed that, unlike the conductive samples, the amount of Ti in solid solution in the parent phase was not detectable (by energy-dispersive x-ray analysis). Titanium appeared to aggregate as a second phase, as shown in FIG. 2 (right side images). Thus, a high temperature heat treatment can cause the dopant to become insoluble. Similarly, the Zr-doped sample, 4b3; was also heat treated at 800° C for twenty-four hours, and was insulating (less than 10-6 S/cm). A similar 1%
Zr-doped composition, which was heat treated at 600° C for twenty-four hours in argon or nitrogen, 4bl and 4b2, was conductive. The Nb-doped sample, Sc4, was heat treated at 800° C for twenty-four hours and was found to be insulating, whereas a similar 0.2%
Nb-doped composition that was heat treated at 600° C for twenty-four hours in argon or l0 nitrogen, Sal and 5b1, was highly conductive. Copies of STEM images of the Nb-doped samples are shown in FIG. 3. Notably, Nb appears to have a higher solubility limit than either Ti or Zr.
Moreover, even at a lower heat treatment temperature (600° C), too long a heat treatment time can convert a conductive composition to insulating composition.
For t 5 example, sample 3c5 was initially heat treated at HT1. A pellet was then pressed and heat treated an additional 76 hours, in argon, and was found to be less conductive relative to sample 3c1, which had a similar composition but was not heat treated an additional 76 hours.
Further, the results also showed that there is a dopant limit and that too much 2o dopant can result in an insulating composition. For example, a 2 mole % Ti-doped composition, 3f2,, is less conductive than a 1 mole % Ti-doped composition, 3e2.
Notably, a 2 mole % Zr-doped composition, 4c2, is still relatively conductive, if not more conductive, compared to a 1 mole % Zr-doped composition, 4b2. However, increasing the Zr concentration to 5 mole %, as in sample 4d2, reduced the conductivity.
25 X-ray diffraction analysis showed that the 5 mole % Zr-doped sample had a small amount of secondary phase, which appeared to be LizZr03. In contrast, the 2 mole % Zr-doped sample had peaks, corresponding to the latter phase, which were negligible, as shown in FIG. 4.
Further, the results showed that the powders prepared were free of coatings of 3o carbon or other conductive additive phases. TEM and STEM showed that the powders of Examples 1 and 2 typically contained a small fraction of unreacted precursors in addition to the majority phase of the olivine structure. However, TEM images at resolution levels high enough to image the lattice planes of the olivine phase, an example of which is shown in FIG. 5, showed that the surfaces of the particles were not coated with another distinguishable phase of material. Thus the increased conductivity of the conductive powders of this Example was obtained in the absence of a continuous phase of a conductive additive.
Other polyanion compounds, aside from those having the olivine structure, such as those of the NASICON VOP04, LiFe(P20~) or Fe4(P20~)3 structures, can be similarly doped and synthesized to achieve high electronic conductivity. Further, based on the results obtained using Mg as a dopant, it is believed that other Group IIA
alkaline earth metals, such as Be, Ca, Sr, and Ba, should have similar effects. Based on the results to obtained using Ti and Zr, which are Group IVA elements, it is believed that other Group IVA elements, such as Hf, should have similar effects. Based on the results obtained using Nb and Ta, which are Group VA elements, it is believed that other Group VA
elements, such as V, should have similar effects. Based on the results obtained using W, which is a Group VIA element, it is understood that other Group VIA elements, such as ~ 5 Cr and Mo, should have similar effects. Based on the results obtained using Al, it is believed that other Group IIIB elements, such as B, Ga, and In, should have similar effects.
Example 2. Lithium Deficient and Substituted Compositions 2o Several compositions were prepared with an overall composition of the formula Lil_aM"aFeP04, included in Table 2. The starting materials and synthesis procedure of Example 1 were used, with the exception that both plastic and porcelain milling containers were used with the zirconia milling media. Because the abrasion of polymeric milling containers and milling media can be a source of carbon, the porcelain containers 25 were used to compare results with and without this potential carbon source.
As shown in Table 2 and also in Table 4, the doped samples of this doping formulation generally had higher conductivity than those of Example 1, with room-temperature conductivities of as much as about 4 x 10'2 S/cm being measured by a two-point method (samples Sf6 and Sg7). Highly conductive samples were obtained using 30 either plastic or porcelain milling containers, showing that excess carbon added from the milling container is not necessary to achieve such conductivities. The results show that introducing Li/metal canon nonstoichiometry can promote Li deficiency, relative to the ideal LiMP04 stoichiometry, which, combined with doping with selected metals, can increase electronic conductivity. Also, higher temperature heat treatments, such as HT6 and HT7, can be used with these lithium-deficient cation stoichiometry compositions without losing electronic conductivity or exsolving the dopant, in comparison to the LiFe~_aM"aP04 compositions (Example 1). STEM observations showed that compositions exhibiting a detectable concentration of the added dopant in the crystalline LiFeP04 grains were conductive.
Compositions Li~_XMXFeP04, that, while not being bound by any particular crystal chemical interpretation, have a formulation that allows substitution onto the M1 sites by a cation supervalent to Li+, exhibited higher solubility for several dopants (Mg2+, Al3+, to Ti4+, Nbs+, and W6+) than did compositions LiFe,_XMXP04. FIG. 6 compares the X-ray diffraction patterns for several 1 mol% doped powders of each canon stoichiometry; in each case the lithium-deficient stoichiometry (FIG. 6a) exhibits no detectable impurity phases. By contrast, samples with the same dopants and concentrations in the iron-deficient stoichometry showed detectable precipitation of Li3P04 by XRD (FIG.
6b) and 15 impurity phases enriched in the dopant, using electron microscopy. FIG. 7 shows an example ofthe first stoichiometry, Lio.99Nbo.o~FeP04, in which elemental mapping shows a uniform distribution of the Nb dopant. The amount of the dopant in solid solution may be less than the total amount of dopant added to the sample. For example, in the Li,_pNbpFeP04 compositions, heat treated at 850° C, a concentration x about 0.0023 was 2o detected in solid solution for an overall composition a about 0.01. This shows that the solid solubility was limited to about a = 0.0023 at 850° C.
Nonetheless, compositions with a values, both greater than or less than 0.0023, were made conductive. In the Lix(Fel_aM"p)P04 compositions, samples processed at 600° C were conductive while those processed at 700° C and higher were not. Correspondingly, the samples processed 25 at 600° C had detectable dopants in solid solution when examined by STEM, while those processed at 700° C did not.
The observed results that the increase in conductivity is not directly proportional to dopant concentration is consistent with a limited dopant solubility in some cases. That is, for those dopants that increased electronic conductivity, there was a large increase in 3o conductivity at lower doping levels and weaker conductivity-concentration dependence at slightly higher dopant levels. For example, in the case of LiFel_pM"aPOa, the greater than 100 times increase in conductivity, compared to the undoped material, at dopant concentrations as low as 0.02% (for M" = Ti, Nb, and Mg), is followed by much smaller changes in conductivity with further increases in dopant concentration. For compositions Li~_aM"pFeP04, the electronic conductivity is firstly higher overall by at least about an order of magnitude than for any of the LiFe~_pM"pP04 compositions.
Compared to the undoped material, the increase in conductivity is significant, greater by a factor of more than 10' times, with a doping level as low as 0.2% (Nb-doped).
However, further doping increases the conductivity only modestly.
Materials were also synthesized that contained an excess of Fe, typically in the form of an Fez+ or Fe3+ salt, as shown in Table 2. While an excess of either Fe2+ or Fe3+
can be substituted into the composition Li,_aM"pFeP04, as with the other dopants M", a t o certain concentration must be in solid solution (i.e., form part of the crystal lattice) for the conductivity to be increased substantially, since this determines the electronic carrier concentration. The results with Fe2+ and Fe3+ doping are consistent with the experiments using other dopants M" that show that when conductivity increased, the dopant in question was found to be in solid solution (either through STEM measurements of dopant distribution in the crystallites or by the appearance/absence of impurity phases by STEM or XRD).
Further, it is believed that the solubility of dopants M" is a function of ion size.
With the exception of Mn2+, all of the dopants that can be effective as M' dopants have an ionic radius, in octahedral coordination, that was less than that of Fe2+.
This is 2o supported by the following ionic radii values, taken from the tabulation by Shannon ( 1976):
R(Fe2+) = 0.78 A R(Li+) = 0.76 A
R(Fe3+) = 0.65 A R(Mgz+) = 0.72 A R(MnZ+) = 0.83 A R(Ti4+) = 0.61 A
R(Zr4+) = 0.72 A R(Nbs+) = 0.64 A R(Ta5+) = 0.64 A R(W6+) = 0.60 A
R(Al3+) = 0.54 A
The temperature dependence of conductivity in the materials of the invention was measured using 2-point and 4-point electrical conductivity measurements of fired pellets pressed from powder samples prepared according to Examples 1 and 2. Both undoped 3o and doped compositions were measured. In addition, ac (impedance spectroscopy) measurements were made on pellets prepared from undoped powder. The temperature dependence of electrical conductivity is shown in FIGS. 8 and 9 as a plot of logio conductivity against 1000/T(K). It is seen that the doped compositions can have more than 10' greater conductivity than an undoped sample. While both types exhibited increasing conductivity with increasing temperature, indicating semiconducting behavior, the doped materials had much shallower temperature dependence. An activation energy in the range of 25 - 75 meV was determined for the highly conductive doped samples, which is reasonable for ionization of shallow acceptors or donors, while an activation energy of about 500 meV was observed for the undoped sample. The high conductivity of the doped samples is maintained, with little temperature dependence, over the -20C to +150C temperature range of interest for many battery applications.
Near room temperature, for example between 21 C to 27C, the variation of electronic conductivity with temperature is minor, such that where a temperature within this range 1o is referred to herein, it is understood that a range of temperatures around any particular value is included.
The highly conductive samples were also subjected to a Seebeck coefficient measurement. Platinum leads were attached to two ends of a sintered sample, whereupon one end was heated to a higher temperature than the other end, and the induced voltage was measured. The heated end was found to be at a negative potential relative to the cold end, exhibiting easily measured and significant potential values of -0.1 mV to -0.3 mV. This shows that the conductive LiFeP04 compositions were p-type conductors. An undoped LiFeP04 composition subjected to the same measurement was found to be n-type.
2o In some cases, the electrical conductivity of the samples was measured using a four-point microcontact method in order to determine the conductivity of individual crystalline grains. For these measurements, densely sintered pellets with an average grain size of about 10 micrometers were cut and polished. A co-linear array of microcontacts were used. Current probes were placed about 100 micrometers apart on 2s the polished surface, while voltage probes were placed about 10 micrometers apart. FIG.
10 shows three samples whose conductivities at the microscopic scale were measured, two being 1 % Nb-doped conductive compositions sintered at 850C and 900C
respectively, and one being an undoped composition sintered at 900C.
Combustion IR
detection showed that all three samples had low carbon content, less than 0.5 wt%. The 3o gray phase in FIG. 10 is the olivine phase, the black contrast features are porosity, and the bright contrast particles are iron phosphide phase. FIG. 11 shows the microcontact measurement geometry, in which it is seen that the inner voltage contacts are about 10 micrometers apart, or about the same separation as individual grains in the samples of FIG. 10. Thus the voltage contacts typically span one grain or one grain boundary. The microcontact array was placed in 12 to 15 separate locations on each sample, and the current-voltage relationship was measured at teach point over a range of currents in a room-temperature laboratory. FIG. 12 shows histograms of the conductivity obtained from the measurements, in which each bar represents one location of the microcontact array. It is seen that firstly, within each sample the conductivity has a similar value from place to place showing relatively uniform conductivity across a sample.
Secondly, the conductivity of the doped samples is of about the same magnitude as measured by two-point and four-point measurements across entire sintered pellets, and is several orders of t0 magnitude greater than the conductivity of the undoped sample.
TEM observations were made of the powders of Example 2. FIG. 13 shows copies of TEM images of powders doped with 1% Nb or 1% Zr. It is seen that the average size of individual crystallites is less than about 100 nm in the Nb-doped sample, less than about 50 nm in the Zr-doped sample, and that the powder has an aggregated ~ 5 morphology. Energy-dispersive X-ray analysis was conducted to determine the location of residual carbon, typically present at a level determined by combustion IR
analysis to be between 0.2 and 2.5 wt% depending on the firing conditions. FIG. 14 shows TEM
images and corresponding chemical analyses of regions in a 1 % Nb doped sample fired at 600C and that was analysed to have about 2.4% residual carbon. This sample of 2o relatively high residual carbon content compared to others of Example 2 was selected for TEM in order to determine if a carbon coating on the particles as practiced in prior art was present. FIG. 14 shows a particle of unreacted precursor, present in small amounts in the sample, in which carbon is found at an enriched level. In the other regions, containing the olivine phase, no carbon is detected. FIG. 15 and 16 show high resolution 25 TEM images of olivine phase particles, in which lattice fringes are imaged.
No continuous surface phase of carbon or other separate conductive compound was found.
Thus it is seen that the fine particle size and increased conductivity of these samples is observed in samples without a significant amount of free carbon.
Surface area measurements are another well-known measure of effective particle 30 size. The specific surface area was measured, using the BET method, of doped and undoped samples heat treated under several conditions. Table 4 shows results for several powder samples. It is observed that the undoped powders have a specific surface area that is typically less than about 10 m2/g for heat treatment temperatures of 600°C or greater. These are heat treatment conditions sufficient to provide a nearly completely crystallized powder. However, the doped compositions have much higher surface area, typically greater than 40 m2/g for 1% Zr-doped powder fired at 600C, and greater than 30 m2/g for 1% Nb-doped powder fired at 600C. In the doped samples the powder is also nearly completely crystallized after firing at these temperatures although a small quantity of incompletely crystallized precursor to the olivine phase remains.
Other powders doped with 0.2-1 mole % of dopants such as Al, Mg, and Ti also had specific surface areas of 35 to 42 m2/g after firing at 600C. At higher firing temperatures of 700 to 800°C the specific surface area of the doped samples remains higher than of the to undoped samples. Having a crystal density of 3.6 g/cm3, the diameter of monosized spheres of the compound having an equivalent specific surface area (i.e., the equivalent spherical particle size) of 40 m2/g is 21 nm, of 30 m2/g is 28 nm, of 29 m2/g is 42 nm, of 15 m2/g is 56 nm, of 10 m2/g is 83 nm, of 5 m2/g is 167 nm, and of 1 m2/g is 833 nm.
Thus it is seen that the doping methods of the present example provide for complete or ~ 5 nearly complete crystallization of the olivine structure compound while also providing for a high specific surface area, higher than that of the undoped compound under identical processing and firing conditions.
Table 4. Compositions, Firing Conditions, and Specific Surface Areas of Insulating and 20 Conductive Samples Composition Temp. Container BELT ~ ConductivityColor (C) rea LiFeP04 600 plastic 9.5 insulatingGray bottle 700 Porcelain 3.9 insulatingGray jar 800 Porcelain ~1 insulatingLight jar Gra LiFeo,99Zro.o~POa600 Porcelain 43.2 conductiveBlack jar 600 Porcelain 41.8 conductiveBlack jar 700 Porcelain 26.4 conductiveBlack jar 750 Porcelain 11.6 conductiveDark jar gray LiFeo.99Nbo.o~POa600 Porcelain 34.7 conductive Black jar 800 P Porcelain 15.3 conductive Black jar Without being bound by any particular interpretation, these results show that conductivities, higher than those obtained using the method and compositions of Example 1, can be obtained in a composition that is deficient in the alkali ion and excess in the other metals that would normally occupy octahedral sites in a LiFePOa structure.
As mentioned, the results show that the solubility of the metal, M", was higher when the composition was formulated in this manner. Without being bound by any interpretation, it is reasonable to expect that having a deficiency of Li and excess of Mg allows one or the other octahedral site cations, Mg or Fe, to occupy octahedral sites in the structure that to would normally be occupied by Li.
Based on the results obtained in this instance, where there is an excess of the non-alkaline metal and a deficiency of the alkali, it is believed that almost any metal added to the structure of the parent compound such that substitution of the metal onto the M1 crystallographic sites normally occupied by the main alkaline metal occurs, would have 15 the desired effect of improving the electronic conductivity of the resulting compound.
Without being bound by any particular interpretation, we note that LiFePOa is found by first-principles calculations of the spin-polarized type to have an unusual band structure of the type known as a half metal. The band gap is spin-sensitive and may in one spin have a gap of about 1 eV while in the other being a metal. It is also found that 2o the electron effective mass is much larger than the hole effective mass, which is consistent with observation of higher electronic conductivity in a p-type conductor.
Without being bound by any particular interpretation, it is noted that a mechanism of defect formation can be understood from the observations that the increased electronic conductivity of the present materials is thermally activated and p-25 type, that there is not a strict proportionality between dopant concentration and conductivity, that similar increases in conductivity are possible for dopants of 2+ through 6+ valence, that a two-phase reaction exists upon delithiation, as shown in later Examples and as is seen in undoped LiFeOa, and that a high capacity and high rate capability are maintained over a wide range of lithiation of the doped compounds. The 30 olivine structure has continuous networks of metal-filled anion polyhedra, including having the cations that occupy the M2 sites (Fe site in LiFeP04) forming a corner-sharing network of octahedra in the (O10) plane, while the cations on Ml (Li) sites form edge-sharing chains of octahedra in the [100] direction. It is noted that the substitution of a cation Mthat is supervalent to Li+ in the composition Lil_XMXFeP04 is normally s expected to result in donor doping. In oxides, aliovalent solutes can be compensated by electronic or ionic defects. The following point defect reactions (in Kroger-Vink notation), illustrate these mechanisms for an M3+ cation that is respectively compensated by electrons or by canon vacancies on the M2 site:
'/z MZO3 + Fe0 +'/z Pz05 ~ ML;w + FeFe" + PP" + 400" + 2e~ +'/z OZ(g) to (I) '/z M203 +'/2 P205 ~ ML;" + VFe~ + PP" + 400" (2) In the first instance, electroneutrality is given by [M~;w] = n, namely the dopant acts directly as a donor species. If the second mechanism is dominant, electroneutrality is given by [ML;"] = 2[VFe~], in which case the donor and vacancy charge-compensate 15 one another and no direct effect on the electronic carrier concentration is expected.
However, it can be shown that in this instance as well, secondary defect equilibria should lead to an increase in the n-type conductivity. Neither of these simple mechanisms can explain a material of high p-type conductivity. An excess of acceptor point defects above and beyond the dopant concentration, or a large difference between hole and 2o electron mobilities as discussed earlier, are necessary. Possible acceptors in the LiFeP04 structure are cation vacancies (VL;~, VFe~), or oxygen interstitials (O;~).
The latter defect is unlikely given the nearly hexagonal close-packed oxygen sublattice in olivine, which should result in a high anion vacancy formation energy.
A mechanism whereby cation doping on the M1 sites allows the stabilization of 25 solid solutions with a net canon deficiency, that is, where the doped olivine endmember has a solid solution of composition Li,_a_XMXFeP04 or Li,_XMxFe,_bP04, in which a and b are Ml or M2 vacancy concentrations respectively, is consistent with the results. If the net charge due to a and b exceed that due to x, then the material will have a net excess of acceptor defects (Fe3+ ions). Taking for example an M3+ dopant, the respective valences 3o for a lithium deficient solid solution are Ll'+,-a-x~+X(Fe2+i-a+~Fe3+~~)(P04)3-. It is noted that lithium deficiency is particularly likely under high temperature firing conditions due to lithium volatility. The above defect mechanism is analogous to allowing an extension of the solid solution field for the pure Li-rich endmember phase to cation deficient solid solutions, Lil_aFeP04. We recall that pure LiFeP04 has been observed to decompose immediately to two co-existing phases upon delithiation, LiFeP04 and FeP04, thereby pinning the Li chemical potential and resulting in the flat intercalation voltage vs. lithium concentration. Thus the insulating behavior of undoped LiFeP04 throughout electrochemical cycling suggests negligible mixed (Fe2+/Fe3+) iron valency in either phase. The retention of either lithium or iron deficiency in the highly lithiated solid solution can therefore result in charge compensation by Fe3+ and p-type conductivity.
Regarding the delithiated FeP04 endmember phase, our electrochemical data in to later Examples indicate that it also retains high electronic conductivity throughout cycling. The influence of M1 site cation doping is expected to be quite different for this phase. Starting with pure FeP04, in which all iron is trivalent, cation doping will result in the formation of divalent iron: M3+x(Fe2+3xFe3+~_3x)PO4. This composition is obtained upon delithiation of the solid solution given earlier. The dopant in this instance may be 15 viewed as an "interstitial" cation donor, occupying normally unoccupied M1 sites, and n-type conductivity should result. During operation as a lithium storage material, the present materials may be a two-phase material, one phase p-type and the other n-type, that change in their relative proportions as the overall lithium concentration changes. A
transition from p- to n-type conductivity may be measurable for the two-phase material 2o as a whole as delithiation proceeds. This behavior may be observed whether the cation dopant Moccupies the M1 site, or preferentially occupies the M2 site and displaces Fe to the Ml site.
The room temperature conductivity of some of the compounds of the invention exceeds that of the well-established intercalation cathodes LiCo02 and LiMn204 in their 25 lithiated (discharged) states. At these high levels of electronic conductivity, lithium ion transport is likely to limit the overall rate of intercalation and deintercalation. That is, the effective lithium chemical diffusion coefficient is likely to be limited by lithium transport (i.e., the ionic transference number tL; is ~0). Because it is known that delithiation of LiFeP04 results in coexistence of two phases, lithium ingress and egress 3o from particles of the storage material requires growth in the amount of one phase and a decrease in the amount of the other. Without being bound by any particular interpretation of the rate-limiting microscopic mechanism of phase transformation, it is understood that a decrease in the crystallite size is beneficial to ion transport. At the same time, it is necessary to simultaneously accommodate electron flow to and from the particles. The structure of the materials of the invention are almost ideal for providing optimal mixed electronic-ionic transport in a battery system, having a porous aggregate s structure in which the nanoscale primary crystallites can be surrounded by the electrolyte, allowing lithium ion transport through a very small cross-sectional dimension, while remaining electronically "wired" together through the sinter necks. For materials in which electronic transport is limiting, it can still be beneficial to decrease the crystallite size, as the potential drop across particle is less for a material of higher 1o conductivity. (If ion transport is limiting, further increases in the electronic conductivity are not expected to improve the rate capability of a single particle significantly, but can improve the electronic conductivity of a network of particles such as that present in a typical composite electrode.) Having a fine primary crystallite size due to doping as provided by the present t s invention provides high rate capability. Therefore, another feature of the materials of the present invention is a structure characterized by primary crystallites having at least a smallest dimension that is less than 200 nm, preferably less than 100nm, still preferably less than 50 nm, and still more preferably less than 30nm. According to the invention the individual crystallites ofthe stated sizes are typically joined by sintering, forming an 2o interconnected but porous network. In some cases, an average of at least 50% of the surface area of the primary crystallites is exposed so that it can contact the electrolyte.
To determine the percentage of exposed surface area, the following procedure can be used: the average primary particle size and shape was measured, for instance by electron microscopy, and the surface area per unit mass can be thus computed. This would be the 2s surface area that would result for completely isolated particles. The specific surface area of the powder can then be measured and compared to the first number. The latter should be at least 50% of the former. In accordance with having a very small primary crystallite size and aggregates that are not highly densified, the specific surface areas of the materials of the invention are preferably greater than about 10 m2/g, more preferably 3o greater than about 20 mz/g, more preferably greater than about 30 m2/g, and still more preferably greater than about 40 m2/g.

It is understood that olivines with other metals partially or completely substituted for Fe, including but not limited to LiMnP04 and LiCoP04, or others in the family of polyanion compounds, including but not limited to those with continuously joined networks of transition metal filled polyhedra within the structure, may enjoy the benefits of improved electronic conductivity, reduced crystallite size, high reversible charge capacity, high rate capability, and other benefits described herein when they are doped or processed according to the invention.
Example 3. Electrode Fabrication and Electrochemical Tests 0 A composition Lio.99sNbo.oo2FeP04 was prepared as described in examples 1 and 2 using lithium carbonate, niobium phenoxide, iron oxalate, and ammonium dihydrogen phosphate, and heat treated according to the procedure labeled as HT1 shown in Table 2.
The resulting powder was black and conductive, and was cast as an electrode coating on an aluminum foil current collector, using a standard formulation of 85 wt% of said 15 composition, 10 wt% SUPER PT"' carbon, and 5 wt% PVDF binder. y-butyroactone was used as the solvent. The positive electrode (cathode) coating was tested against a lithium metal foil counterelectrode (anode) in a standard cell assembly using CELGARD~

separator film and EC:DMC (+1M LiPF6) as the electrolyte. Galvanostatic tests were performed at several current rates. FIG. 17A shows the first electrochemical cycle at 2o C/30 rate, in which it is seen that a capacity of about 150 mA/g is obtained. A flat voltage plateau is observed, indicating a two-phase equilibrium of constant lithium chemical potential. FIG. 17B shows capacity vs. cycle number for this electrode at a 1C
rate (150 mA/g), to about 260 cycles. FIG. 17C shows that the coulombic efficiency vs.
cycle number at 1C rate (150 mA/g) is generally greater than about 0.997.
These results 2s show that this material of the invention had good performance as a storage cathode for rechargeable lithium battery systems, at practical rates of charge and discharge, without requiring special procedures, such as coating with conductive additives.
Example 4. Electrode Fabrication and Electrochemical Tests of the Lithium Storage 3o Compounds and Electrodes of the Invention at High Discharge Rates The electrochemical performance of the undoped and doped powders of Examples 1 and 2 were evaluated by using them in electrodes of a variety of formulations and testing said electrodes under a wide range of conditions as the positive electrode in a liquid electrolyte cell, using lithium metal foil as the negative electrode.
Table 5 lists several of the electrode formulations that were prepared and tested. All samples were tested using CELGARD~ 2400 or 2500 separator film and 1:1 EC:DEC
with 1M LiPF6 liquid electrolyte.
Table 5. Lithium Storage Materials and Electrode Formulations SampleActive MaterialsSpecific Electrode Active Composition Surface Formulation Material and Heat Treatment Area (mz/g)(wt percentagesLoadin m /cm A LiFeP04, 700C/Ar3.9 Cathode/Super-5.3 P/Kynar 461 B LiFeP04, 700C/Ar3.9 Cathode/Super-7.8 P/Kynar 461 C (Lio.99Zro.o~)FeP04,~40 Cathode/Super->3.9 600C/Ar P/Alfa-Aesar PVdF

78.3/10.1 /11.6 D (Lio.99Zro.oi)FeP04,~40 Cathode/Super-2.5 600C/Ar P/Alfa-Aesar PVdF

78.4/10.0/11.6 E (Lio.99Zro.o~)FeP04,41.8 Cathode/Super-4.0 600C/Ar P/Kynar 2801 F (Lio.99Zro.o~)FeP04,41.8 Cathode/Super-4.3 600C/Ar P/Kynar 2801 lasticized G (Lio.99Zro,o,)FePOa,41.8 Cathode/Super-4.4 600C/Ar P/Kynar 2801 lasticized H (Lio,99Zro.o,)FeP04,26.4 Cathode/Super-5.3 700C/Ar P/Kynar 461 I Li(Feo.98Tio.oz)POa~~40 Cathode/Super-5.9 600C/Ar P/Kynar 461 J (Lio.99sNbo.ooz)FeP04,~40 Cathode/Super--600C/Ar P/Alfa-Aesar PVdF

Table S, Sample D.
A composition (Lio.99Zro.o~)FeP04, fired at 600°C in Ar according to the methods of Example 2, and having a specific surface area of about 40 m2/g, was formulated into an electrode by mixing 78.4 wt% of the active material, 10.0 wt% of SUPER PTM
carbon, and 11.6 wt% Alfa-Aesar PVdF as the binder, using y-butyrolactone as solvent.
The mixing was done in a small plastic container containing one Teflon~ ball using a dental amalgamator (Wig-L-Bug) for 5 minutes. Mixed suspensions were cast onto aluminum foil current collectors, dried, and pressed at 4 tons/cm2. Electrochemical test samples were cut from the pressed castings and assembled in stainless steel test cells with lithium to metal foil (Alfa Aesar, Ward Hill, MA, USA) as the counterelectrode and CELGARD~
2400 (Hoechst Celanese, Charlotte, NC, USA) as the separator. The liquid electrolyte used was 1:1 by wt ethylene carbonate and diethyl carbonate with 1M LiPFb added as the conductive salt.
Figure 18A shows the charge and discharge capacities of a cell with about 2.5 mg/cmz loading of the active material, observed in continuous cycling at rates varying from 15 mA/g (C/10) to 3225 mA/g (21.SC) between the voltage limits of 2.8-4.2V, at room temperature. It is noted that a stable capacity is obtained upon cycling over a wide range of rates, to more, than 150 cycles. Figure 18B shows corresponding charge-discharge curves for the doped sample, in which there is only a modest polarization, with 2o a clear voltage plateaus at ~3.1 V even at a discharge rate of 21.SC.
Comparing with published data for LiFeP04, it is clear that the low doping levels used to increase conductivity and increase specific surface area do not decrease the storage capacity at low rates, but greatly increase the power density that is possible. The low polarization is attributed to the high electronic conductivity at the particle scale. Thus this electrode made using a compound of the invention is seen to have high energy density at much higher current rates than previously seen for undoped LiFeP04.
Table 5, Sample C.
An electrode prepared as described for Sample D of Table 5, and having >3.9 3o mg/cm2 loading of active material, was assembled in a Teflon~ and stainless steel Swagelok~ test vessel with lithium metal foil (Alfa Aesar, Ward Hill, MA, USA) as the counterelectrode and CELGARD~ 2400 (Hoechst Celanese, Charlotte, NC, USA) as separator. The liquid electrolyte used was 1:1 by wt ethylene carbonate and diethyl carbonate with 1 M LiPF6 added as the conductive salt.
Figure 19A shows discharge capacities measured at 42°C observed in continuous cycling tests. For the curve labeled 0.2C, the cell was charged and discharged at a current rate of 0.2C (30 mA/g) between the voltage limits of 2-4.2V. For the other curves, the cell was charged at a rate of 1.1C (165 mA/g) and then discharged at the rates shown. It is seen that this cell maintains a significant discharge capacity and relatively little polarization upon discharging at rates as high as 66.2C (9.93 A/g).
Compared to previously reported electrochemical test data for LiFeP04, this cell can be discharged at to a remarkably high power density while still having significant energy density.
Table 5, Sample F, E, G, H.
Sample F was prepared from a composition (Lio.99Zro.o~)FeP04, fired at 600°C in Ar according to the methods of Example 2, and having a specific surface area of 41.8 ~ 5 m2/g. It was formulated into an electrode by mixing 79 wt% of the active material, 10 wt% of SUPER P~ carbon, and 11 wt% Kynar 2801 binder in y-butyrolactone as solvent, using the procedures of Sample D and C. After casting and drying, the coating was immersed in a plasticizing solvent of 15 wt% propylene carbonate in methanol, then pressed and dried. The resulting positive electrode (cathode) was tested against a lithium 2o metal foil counterelectrode (anode) in a Swagelok cell assembly using CELGARD~ 2500 separator film and 1:1 EC:DEC with 1M LiPF6 liquid electrolyte.
FIG. 20 shows discharge curves for this cell measured by the constant-current constant-voltage (CCCV) method whereby the cell was first charged at 0.5C rate (75 mA/g), then held at the upper limiting voltage of 3.8V until the charging current decayed 25 to 0.001 mA, before discharging to 2V at the stated rate. Note that in comparison to FIG.
19, the initial linear behavior upon discharge is not seen, indicating that the linear region is a capacitive response due to incomplete equilibration in the cell. (In later calculations of the energy density of cell tested in continuous cycling, the capacity of this linear region is not included.) The results in FIG. 20 show quite remarkably that even at a SOC
30 (7.5 A/g) discharge rate, about half of the capacity available at C/5 rate is provided by the cell.
FIG. 21 compares the discharge energy density of Sample F with Samples E, G, and H from Table 5. All tests were conducted at 22-23°C. Sample G was prepared in the same manner as Sample F, and was tested by continuous cycling according to the procedure of Sample C. Sample E was prepared and tested in the same manner as Sample G, except that the electrode was not plasticized. Sample H was prepared from a powder fired to a higher temperature than the others in FIG. 21, 700C in Ar, and has a lower specific surface area of 26.4 m2/g, and used Kynar 461 binder, but was otherwise processed and tested in like manner. It is seen that all four of the samples in FIG. 21 exhibit a remarkably high capacity at high discharge C rates.
Table 5, Samples A and B
1o Samples A and B were prepared from undoped LiFeP04, which after firing at 700C has a relatively low specific surface area of 3.9 m2/g. The electrodes were prepared and tested in like manner to Sample H in Table 5, and the results are shown in FIG. 22, measured at 23, 31, and 42°C. Unlike the results in FIG. 21, however, the undoped samples show greatly inferior discharge capacity that falls to about 20 mAh/g by about 5C (750 mA/g) rate. It is also seen in FIG. 22 that heating to a temperature of 42°C does not significantly improve the discharge capacity.
Comparison with Literature Data Electrochemical test results have been reported for several LiFeP04-based electrodes in the published literature. FIG. 23 compares the results from Sample F in Table 5 to results from several published papers. It is seen that the electrodes of the invention have markedly higher discharge capacity at high rates, whereas the literature data typically shows a rapid decrease in capacity with increasing rate at rates below 5C
or I OC rate. This comparison illustrates the novel high performance properties of the lithium storage materials and electrodes of the current invention.
Energy Density vs. Current Density In FIGS. 24 - 27, we show the discharge energy density available from the total mass of storage compound available in several electrodes of Table 5, plotted against the 3o current per gram of storage material. The energy densities are obtained by integrating the voltage vs. charge capacity curves. In FIG. 24, results from Sample F are shown for a measurement temperature of 22°C; in FIG. 25, results for Sample G are shown for measurement temperatures of 23, 31, and 42°C; in FIG. 26, results for Sample I
measured at 23°C; and in FIG. 27, results are shown for Sample A for measurement temperatures of 23, 31, and 42°C. Comparing FIGS. 24-26 with FIG. 27, the vast improvement in the energy density of the lithium storage materials of the invention compared to undoped LiFeP04 is clearly seen Example 5: Storage Battery Cells Example 4 illustrates the high discharge capacity available from the lithium storage compounds of the invention, and electrodes utilizing said compounds, at high 1o discharge rates. Having shown clearly the improved electrochemical properties of the lithium storage compounds and electrodes of the invention, we now illustrate storage battery cells of exceptional power density and high energy density based on these compounds and electrodes.
It is well-known that typical lithium-ion batteries based on laminated electrodes 15 and designed for high energy density contain 25-35% by weight and 13-18% by volume of the positive electrode storage compound, typically LiCo02. While more detailed calculations of the weight and volume fractions of materials are used for specific designs, these approximate values provide an adequate basis for determining the energy density and power density of conventional cell designs utilizing the present lithium 2o storage compounds. Accounting for the 29% lower crystal density of LiFeP04 compared to LiCo02, and assuming a somewhat lower packing density due to the high specific surface area, it is conservatively estimated that an optimized cell could contain 10-20 wt% of the positive electrode active material. Using the results of Example 4 for electrodes tested against lithium metal negative electrodes, and taking into account its 25 slightly lower cell voltage when used in conjunction with a carbon electrode (3.25 vs. 3.7 V), the power density - energy density results shown in FIG. 28 are obtained.
Results are shown for 10 wt%, 15 wt%, and 20 wt% of the positive electrode active material.
Power and energy densities for complete discharge of a cell of 800-1500 W/kg and 30-60 Wh/kg at a 20C (3 A/g) rate, 1500-4200 W/kg and 15-30 Wh/kg at a SOC (7.5 A/g) rate, 3o and 2500-5000 W/kg and 5-10 Wh/kg at a 80C (12 A/g) rate, are obtained.
Such cells could provide power densities not possible in current nickel metal-hydride (400-1200 W/kg, 40-80 Wh/kg) and lithium-ion battery technology (800-2000 W/kg, 80-170 Wh/kg). These capabilities, in a low-cost and ultra-safe storage material, may be especially attractive for high power and large battery applications including but not limited to power tools and hybrid and electric vehicles.
Example 6. Doping From Milling Media and Containers This example shows that doping to yield high electronic conductivity can be accomplished by using suitable milling media and containers. It also shows that the high electronic conductivity of the materials of the invention is obtained without excessive i o carbon or other conductive additives. Table 6 shows the results of carbon and zirconium analysis of several materials prepared according to the methods of Examples 1 and 2. It is seen that milling with 3/8" ZrOz milling media can add a detectable concentration of Zr to the samples. Amongst the nominally undoped samples, a high conductivity of about 10-3 S/cm is observed when the Zr concentration from the milling media is 0.018.
t 5 Taking this added Zr into account, the composition of the sample is of type Li~_aZraFeP04, similar to other high conductivity samples. It is also seen that the polypropylene milling jar has added some excess carbon to this sample.
When'/4" ZrOz milling media are used, negligible Zr doping occurs. An undoped sample fired at 800C
has 0.25 wt % carbon, and a low conductivity of 10-g S/cm.
20 Lightly doped samples such as in Table 1 that have been milled with zirconia milling media can thus also be doped with Zr in addition, improving the conductivity.
The four Zr and Nb doped samples, were formulated to have Li~_aM"aFeP04 composition and have high electronic conductivity. The concentration of carbon is less than 2 weight percent in one instance, and less than 1 weight percent in the other three 2s instances. The sample of highest conductivity, 10'2 S/cm, has the lowest carbon concentration, only 0.32 weight percent, nearly the same as the highly insulating undoped samples. The sample with the highest carbon concentration has the lowest conductivity. These results show that the high electronic conductivity of doped samples is not correlated with carbon concentration but instead with doping as described herein.
Table 6. Carbon analysis of conductive lithium iron phosphate materials.
Composition Preparation Carbon Z Conductivity Method r (wt 2- robe /o) (wt S/cm) /o) Undo ed (large Pol ro ylene 0.25 0.009 10' batch bottle, 700 C 3/8" Zr02 media Undoped (Lio.99FeP04)Polypropylene 2,41 0.018 010-3) bottle, "

Zr02 media Undoped Porcelain jar, 0.25 10-8 800 C '/e" Zr02 media 1% Zr doped Porcelain jar, 1.46 10~

700 C '/4" ZrOz balls 1 % Zr doped Porcelain jar, 0.86 10-3 800 C '/4" Zr02 balls 1% Nb doped Porcelain jar, 0.56 103 800 C Tin ZrOz balls 1 % Nb doped Polypropylene 0,32 10-2 bottle, 800 C 3/8" Zr02 media Example 7. Compositions With Dopant Not in Solid Solution In this example, as in Example l, it is shown that when a doped composition similar to the preceding examples of high electronic conductivity is prepared, but the dopant is not in solid solution, then the composition is not conductive. In Example 2, it was shown that a composition (Llo 99Nbo.o1 F~a_ has markedly improved conductivity and electrochemical storage properties compared to an undoped LiFeP04 when the Nb dopant is in solid solution in the crystal lattice. Here it is shown that the same composition prepared with the dopant not in solid solution, but precipitated as a to secondary phase, is substantially insulating.
1 mole % Nb-doped LiFeP04 was prepared using iron acetate, Fe(CH3C00)2 as the Fe precursor. Niobium phenoxide, Nb(C6H50)5 was used as the source of the dopant.
The theoretical content of Fe in iron acetate is 32.12 wt%. However, the iron content of iron acetate frequently deviates from the ideal value. Thus it was expected that the t s composition of the compound would deviate from a nominal composition Lio.99Nbo.o1 FeP04 that provides good electronic conductivity. A batch of powder was formulated according to the following proportions of starting materials:
1 mole % Nb-doled LiFeP04 20 ~4 g batch NH4HzP04 2.3006 g (99.998%, Alfa-Aesar) LiZC03 0.7316 g (99.999%, Alfa-Aesar) Fe(CH3C00)2 3.7867 g (99.9%, Alfa-Aesar) Nb(C6H50)5 0.1116 g (Alfa-Aesar) Each of the components was weighed in an argon-filled glove box. They were then removed from the glove box and ball milled, using zirconia milling balls (~l/4"
diameter, 400-450g total weight) in a porcelain milling jar (300m1 capacity) for 24 hours in acetone (150-160m1) at 230 rpm. The milled mixture was dried at a temperature not exceeding 80°C, and then ground with a mortar and pestle in the argon-filled glove box.
The mixture was then heat treated in two steps. A first heat treatment at 350°C for 10 hours was conducted in a flowing Ar (99.999% purity) atmosphere (>400cc/min).
The powder sample was then ground in laboratory air atmosphere, using a mortar and pestle, and subjected to a second heat treatment at a higher temperature (600°C
to 700°C) for 20 1o hours, in flowing Ar gas (>400cc/min). The heating and cooling rates for each step were 5°C/min. Before heating, purging of the furnace tube in flowing Ar for about 1 hour was conducted.
In contrast to the cases where iron oxalate (FeC204~2H20) is used as the starting materials, a 2-probe resistance measurement of this sample showed that the conductivity is less than 10-~ S/cm at a temperature of 23-27°C. X-ray diffraction of a sample fired at 600C for 20h in Ar showed that it was predominantly LiFeP04 but had a small amount of an unidentified secondary phase. TEM analysis showed that the dopant Nb was not detectable inside the particles, but was segregated as a secondary phase.
Furthermore, the specific surface area of this material was much lower than it is in samples prepared 2o so that the Nb dopant is in solid solution, being 14.3 m2/g for 600C
firing. Thus it is shown that in this material, when a substantial amount of the added Nb dopant is not in solid solution in the crystalline particles, an increased conductivity is not observed, nor is the advantageous feature of metal additives of diminishing the crystallite size realized. It is understood that the iron acetate precursor, being a suitable reactant for the formation of LiFeP04, is suitable for producing highly conductive compositions when the overall composition is known and more precisely controlled.
Example 8. Solid State Reaction Synthesis of LiFeP04 This example describes the preparation of LiFeP04, using wustite iron oxide, 3o FeO, and lithium metaphosphate, LiP03, as precursors. An advantage of these precursors is that they form a closed or nearly closed reaction system, by which it is meant that upon heat treatment, few if any gaseous species are produced as a reaction by product. Adjustments to the relative amounts of the reactants, and the addition of other constituents such as the dopants in the form of oxides can be used in order to obtain compositions comprising the materials of the invention.
A batch of 6 g LiFeP04 was prepared by using starting materials of the following amounts: 2.733 g Fe0 (99.5%, Alfa-Aesar, Ward Hill, MA, USA) and 3.267 g LiP03 (97%, City Chemical LLC., West Haven, CT, USA). The components were weighed in an Ar-filled glove box, and transferred to a porcelain jar and ball-milled in acetone for 48 h using zirconia milling balls. The acetone was evaporated from the milled powder at a low temperature (<100°C), and the dried powder was ground with a mortar and pestle and pressed into pellets. The pellets were embedded in loose powder of the same to material and placed in alumina crucibles and subjected to a single heat treatment under Ar atmosphere at 550-900°C for 20 h.
The heat-treated samples were light to medium grey in color. Predominantly single-phase LiFeP04 was obtained for all heat-treatment temperatures, as identified by X-ray diffraction. Minor amounts of Fe2P and Fe phases were detected by XRD at heat-15 treatment temperatures at and above 600°C.
Example 9. Solid State Reaction Synthesis of Nb-doped LiFeP04 Conductive compositions of the invention are obtained using the starting materials and basic procedure of Example 8, and by adding dopants in the form of oxides, 2o hydroxides or alkoxides to obtain the dopant metal ion in the preferred valence state. A
conductive sample with the nominal formulation LiFeP04 + 1 mole% Nb was prepared using the precursors of Example 8 and adding a small amount of the dopant niobium phenoxide, Nb(C6H50)5. A batch of about lg powder was prepared by using 0.4530 g FeO, 0.5416 g LiP03 and 0.0352 g Nb(C6H50)5 (99.99%, Alfa-Aesar, Ward Hill, MA, 25 USA). The powders were milled, as described in Example 6, and then pressed into pellets and heat-treated under Ar atmosphere at 600°C for 20 h. Some sintered pellets were also annealed at 850°C to obtain more densified samples or samples with more coarsened crystallites.
In contrast to the undoped powder of Example 8, the resulting powder was dark 3o grey in color, which gave an indication of increased electronic conductivity, compared to the undoped sample. X-ray diffraction analysis showed predominantly a single crystalline phase of the triphylite LiFeP04 structure. Resistance measurements were made using a two-contact method with metal probes located about 5 mm apart on the fired pellets, and showed a resistivity of about 150 kS2, in contrast to the insulating sample of Example 8, which when made by the same procedure and from the same starting materials except for the absence of doping with niobium phenoxide showed a resistance of >200 mega ohms (MS2). Thus it is shown that the doped compositions of the invention prepared according to the methods of this example provide an increased electronic conductivity compared to an undoped composition.
Example 10. Solid State Reaction Synthesis of Conductive LiFeP04 o In this example, doped LiFeP04 with increased electronic conductivity is prepared using the starting materials and methods of Example 8 and 9, except that the conductive compositions of the invention are obtained by adding dopants in the form of oxides wherein the dopant are in the preferred final valence state, including but not limited to Ti02, Nb205, Ta205, Zr02, A1203, MgO, or W06. The dopant oxide is added 15 to the starting mixture of reactants in a quantity sufficient to give a desired concentration in the final product. Using the mixing and firing procedures of Examples 8 and 9, conductive compositions of the invention are obtained.
Example 11. Solid-state Reaction Synthesis zo This example describes the all-solid state reaction synthesis of LiFeP04 or conductive doped LiFeP04, using wustite iron oxide, FeO, lithium oxide, Li20, and phosphorous(V) oxide, P205, as precursors to the major metallic constituents and metal alkoxides and metal oxides as the source of the dopants. This set of precursors also forms a closed or nearly closed reaction system, from which few if any gaseous species 25 are evolved during synthesis.
A batch of 12 g LiFeP04 was prepared by using starting materials of the following amounts: 5.463 g Fe0 (99.5%, Alfa-Aesar, Ward Hill, MA, USA), 1.136 g Li20 (99.5%, Alfa-Aesar, Ward Hill, MA, USA) and 5.398 g Pz05 (99.99%, Alfa-Aesar, Ward Hill, MA, USA). The components were weighed in an Ar-filled glove box, transferred to a 30 polypropylene jar and ball-milled for 48 h using zirconia milling balls.
Special precautions were taken to avoid any exposure of the reactant mixture to air, due to the very hygroscopic nature ofP205. For instance, a liquid milling medium (e.g.
acetone) was not added prior to milling. The dry, milled powder was extracted from the milling jar in the glove box, ground with mortar and pestle and pressed into pellets.
The pellets were placed in alumina crucibles and subjected to a single heat treatment at 550°C or 850°C for 20 h., after which the samples were found by X-ray diffraction to contain LiFeP04 as the major crystalline phase. Doped samples are prepared in the same manner, except with the addition of a dopant salt such as a metal alkoxide or metal oxide prior to the mixing and milling steps.
Example 12. Solid-state Reaction Synthesis This example describes the preparation of undoped or doped LiFeP04, using iron oxalate, FeC204~2H20, and lithium metaphosphate, LiP03, as precursors. Gaseous species formed during synthesis are limited to one formula unit carbon dioxide CO2, one formula unit carbon monoxide CO and two formula units water H20 per formula unit reacted FeC204~2H20.
A batch of 1 g LiFeP04 was prepared by using starting materials of the following amounts: 1.134 g FeC204~2H20 (99.99%, Aldrich, Milwaukee, WI, USA) and 0.5410 g LiP03 (97%, City Chemical LLC., West Haven, CT, USA). The components were weighed in an Ar-filled glove box, and ball milled in acetone in a porcelain jar for about 24 h, using zirconia milling balls. The acetone was evaporated from the milled powder at a low temperature (<100°C), and the dried powder was ground using a mortar and pestle.
2o The milled powder was heat treated at 350°C for 10 h under flowing Ar gas. The heat-treated powder samples were then ground again with a mortar and pestle and pressed into pellets before a second heat-treatment step. The pellets were placed in alumina crucibles and heated to 600°C or 700°C for 20 h under Ar gas. X-ray diffraction showed that a predominantly single-phase LiFeP04 was obtained for both heat-treatment temperatures.
A minor amount of another detectable phase (28 ~ 27, 28, 30 and 31°) was also observed. Doped samples are prepared in the same manner, except with the addition of a dopant salt prior to mixing and milling.
Example 13. Solid-state Reaction Synthesis 3o This example describes the preparation of undoped or doped LiFeP04, using iron oxalate, FeC204~2H20, lithium oxide, Li20, and phosphorous(V) oxide, PZOS, as precursors. The formation of gaseous species during synthesis is limited to one formula unit carbon dioxide COz, one formula unit carbon monoxide CO and two formula units water H20 per formula unit reacted FeC2042H20.
A batch of 1 g LiFeP04 was prepared by using starting materials of the following amounts: 1.134 g FeC204~2H20 (99.99%, Aldrich, Milwaukee, WI, USA), 0.09421 g s Li20 (99.5%, Alfa-Aesar, Ward Hill, MA, USA) and 0.4475 g P205 (99.99%, Alfa-Aesar, Ward Hill, MA, USA). The components were weighed in an Ar-filled glove box, and dry-milled in a porcelain jar for about 24 h using zirconia milling balls.
The milled powder was extracted from the milling jar in the glove box and ground using a mortar and pestle. The powder was then heat treated at 300°C for 10 h under flowing Ar gas, to ground again and pressed into pellets before a second heat treatment step.
The pellets were placed in alumina crucibles and heated to 600°C or 700°C
for 20 h under Ar gas.
X-ray diffraction showed a predominantly single-phase LiFeP04 for both heat-treatment temperatures. A minor amount of another detectable phase (28 ~ 27and 28°) and possibly a minor amount of Fe304 was also observed. Doped samples are prepared in the same 1s manner, except with the addition of a dopant salt prior to mixing and milling.
Example 14. Chemically Delithiated Doped Conductive LiFeP04 This example describes the chemical delithiation of a doped and conductive LiFeP04, after which it remains highly electronically conductive as predominantly an 2o FeP04 phase. The chemical reduction of LiFeP04 was conducted by the addition of a strong reducing agent, in this case nitronium hexafluorophosphate, NOzPFb, to a suspension of the starting material and acetonitrile, CH3CN. Nitrogen dioxide gas, N02, and solvated lithium hexafluorophosphate, LiPF6, is formed during the reaction together with the reduced FeP04, according to:
2s LiFeP04(s) + NOZPF6(sol.) -~NOZ(g) + LiPF6(sol.) + FePOa(s) (sol.=solvated) Specif cally a powder of (Lio.99Nbo.o~) FePOa was delithiated. To obtain a relatively complete level of delithiation, the molar ratio NOzPF6 :
(Lio.99Nbo.oO FeP04 3o was set to 2:1. For a batch of 0.6 g (Lio.99Nbo.oO FeP04 (prepared according to Example 2), an amount of 1.453 g of NOzPFb (98%, Matrix Scientific, Columbia, SC, USA) was used. Both reactants were weighed in an Ar-filled glove box and transferred to a filtering flask equipped with a rubber stopper. A thin glass tube was fitted through a hole in the rubber stopper and a silicone tube was fitted to the tubulation opening on the flask side.
100 ml of acetonitrile (99.998%, anhydrous, Alfa-Aesar, Ward Hill, MA, USA) was added to the beaker, and the glass tube was adjusted so that the tip was positioned under the liquid surface. The resulting concentration of NOZPF6 in the solution was ca. 0.08 M.
A flow of Ar gas was introduced at the glass tube end, so that the gaseous species formed during the reaction were led away through the silicone tube to an. exhaust hood. The reaction was allowed to proceed for 24 h, while stirring with a magnetic stirrer. The resulting powder was separated from the solution by filtering through a Buchner funnel to equipped with filter paper (#595, Schleicher & Schuell). The powder was thoroughly rinsed in pure acetonitrile and dried under vacuum for two hours. The remaining powder was analysed by X-ray diffraction and showed a single-phase orthorhombic FeP04 structure. The powder was black in color, and when pressed into a pellet, was highly conductive. Thus this example shows that the compounds of the invention remain highly t 5 electronically conductive upon delithiation, and that a partially delithiated compound comprises two phases, one relatively highly delithiated and the other relatively delithiated, both of which are electronically conductive.
Those skilled in the art would readily appreciate that all parameters and 2o configurations described herein are meant to be exemplary and that actual parameters and configurations will depend upon the specific application for which the systems and methods of the present invention are used. Those skilled in the art will recognize, or be able to ascertain using no more than routine experimentation, many equivalents to the specific embodiments of the invention described herein. It is, therefore, to be understood 25 that the foregoing embodiments are presented by way of example only and that, within the scope of the appended claims and equivalents thereto, the invention may be practiced otherwise than as specifically described. Accordingly, those skilled in the art would recognize that the use of an electrochemical device in the examples should not be limited as such. The present invention is directed to each individual feature, system, or method 3o described herein. In addition, any combination of two or more such features, systems or methods, if such features, systems or methods are not mutually inconsistent, is included within the scope of the present invention.
What is claimed is:

Claims (178)

1. A compound comprising a composition A x(M'1-a M''a)y(XD4)z, A x(M'1-a M''a)y(DXD4)z, or A x(M'1-a M''a)y(X2D7)z, having a conductivity at 27° C of at least about 10 -8 S/cm, wherein A is at least one of an alkali metal or hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, boron, aluminum, silicon, vanadium, molybdenum and tungsten , M'' is any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB metal, D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <= 0.1, and x is equal to or greater than 0, y and z are greater than 0 and have values such that x, plus y(1-a) times a formal valence or valences of M', plus ya times a formal valence or valence of M'', is equal to z times a formal valence of the XD4, X2D7, or DXD4 group.

2. A compound comprising a composition (A1-a M''a)x M'y(XD4)z, (A1-a M''a)x M'y(DXD4)z, or (A1-a M''a)x M'y(X2D7)z, having a conductivity at 27° C of at least about 10 -8 S/cm, wherein A is at least one of an alkali metal or hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, boron, aluminum, silicon, vanadium, molybdenum and tungsten, M'' any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB metal, D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <= 0.1, and x, y, and z are greater than zero and have values such that (1-a)x plus the quantity ax times the formal valence or valences of M'' plus y times the formal valence or valences of M' is equal to z times the formal valence of the XD4, X2D7 or DXD4 group.

3. A compound comprising a composition (A b-a M''a)x M'y(XD4)z, (A b-a M''a)x M'y(DXD4)z, or (A b-a M''a)x M'y(X2D7z, having a conductivity at 27° C of at least about 10 -8 S/cm, wherein A is at least one of an alkali metal or hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, boron, aluminum, silicon, vanadium, molybdenum and tungsten, M'' any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB metal, D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <= 0.1, a <= b <= 1, and x, y, and z are greater than zero and have values such that (b-a)x plus the quantity ax times the formal valence or valences of M'' plus y times the formal valence or valences of M' is equal to z times the formal valence of the XD4, X2D7 or DXD4 group.

4. A compound comprising a composition A x(M'1-a M''a)y(XD4)z, A x(M'1-a M''a)y(DXD4)z, or A x(M'1-a M''a)y(X2D7)z, having a specific surface area of at least 15 m2/g, wherein A is at least one of an alkali metal or hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, boron, aluminum, silicon, vanadium, molybdenum and tungsten, M'' is any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB metal, D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <= 0.1, and x is equal to or greater than 0, y and z are greater than 0 and have values such that x, plus y(1-a) times a formal valence or valences of M', plus ya times a formal valence or valence of M'', is equal to z times a formal valence of the XD4, X2D7, or DXD4 group.

5. A compound comprising a composition (A1-a M''a)x M'y(XD4)z, (A1-a M''a)x M'y(DXD4)z, or (A1-a M''a)x M'y(X2D7)z, having a specific surface area of at least 15 m2/g, wherein A is at least one of an alkali metal or hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, boron, aluminum, silicon, vanadium, molybdenum and tungsten, M'' any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB metal, D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <= 0.1, and x, y, and z are greater than zero and have values such that (1-a)x plus the quantity ax times the formal valence or valences of M'' plus y times the formal valence or valences of M' is equal to z times the formal valence of the XD4, X2D7 or DXD4 group.

6. A compound comprising a composition (A b-a M''a)x M'y(XD4)z, (A b-a M''a)x M'y(DXD4)z, or (A b-a M''a)x M'y(X2D7)z, having a specific surface area of at least 15 m2/g, wherein A is at least one of an alkali metal or hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, boron, aluminum, silicon, vanadium, molybdenum and tungsten, M'' any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB metal, D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <= 0.1, a <= b < 1, and x, y, and z are greater than zero and have values such that (b-a)x plus the quantity ax times the formal valence or valences of M'' plus y times the formal valence or valences of M' is equal to z times the formal valence of the XD4, X2D7 or DXD4 group.

7. A compound comprising a composition A x(M'1-a M''a)y(XD4)z, A x(M'1-a M''a)y(DXD4)z, or A x(M'1-a M''a)y(X2D7)z, wherein A is at least one of an alkali metal or hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, boron, aluminum, silicon, vanadium, molybdenum and tungsten, M'' is any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB
metal, D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <= 0.1, and x is equal to or greater than 0, y and z are greater than 0 and have values such that x, plus y(1-a) times a formal valence or valences of M', plus ya times a formal valence or valence of M'', is equal to z times a formal valence of the XD4, X2D7, or DXD4 group, crystallizing in an ordered or partially disordered structure of the olivine (A x MXO4), NASICON (A x(M',M'')2(XO4)3), VOPO4, LiFe(P2O7) or Fe4(P2O7)3 structure-types, and additionally having a molar concentration of the metals (M' + M'') relative to the concentration of the elements X that exceeds the ideal stoichiometric ratio y/z of the prototype compounds by at least 0.0001.

8. A compound comprising a composition (A1-a M''a)x M'y(XD4)z, (A1-a M''a)x M'y(DXD4)z, or (A1-a M''a)x M'y(X2D7)z, wherein A is at least one of an alkali metal or hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, boron, aluminum, silicon, vanadium, molybdenum and tungsten, M'' any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB
metal, D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <= 0.1, and x, y, and z are greater than zero and have values such that (1-a)x plus the quantity ax times the formal valence or valences of M'' plus y times the formal valence or valences of M' is equal to z times the formal valence of the XD4, X2D7 or DXD4 group, crystallizing in an ordered or partially disordered structure of the olivine (A x MXO4), NASICON (A x(M',M'')2(XO4)3), VOPOP4, LiFe(P2O7) or Fe4(P2O7)3 structure-types, and additionally having a molar concentration of the metals (M' + M'') relative to the concentration of the elements X that exceeds the ideal stoichiometric ratio y/z of the prototype compounds by at least 0.0001.

9. A compound comprising a composition (A b-a M" a)X M'y (XD4)Z, (A b-a M"a)x M' y(DXD4)z, or (A b-a M" a)x M'y(X2D7)z, wherein A is at least one of an alkali metal or hydrogen, M' is a first-row transition metal, X is at least one of phosphorus, sulfur, arsenic, boron, aluminum, silicon, vanadium, molybdenum and tungsten, M" any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIVA, IB, IIB, IIIB, IVB, VB, and VIB
metal, D is at least one of oxygen, nitrogen, carbon, or a halogen, 0.0001 < a <= 0.1, a <= b <= 1, and x, y, and z are greater than zero and have values such that (b-a)x plus the quantity ax times the formal valence or valences of M" plus y times the formal valence or valences of M' is equal to z times the formal valence of the XD4, X2D7 or group, crystallizing in an ordered or partially disordered structure of the olivine (A x MXO4), NASICON (A x(M',M")2(XO4)3), VOPO4, LiFe(P2O7) or Fe4(P2O7)3 structure-types, and additionally having a molar concentration of the metals (M' + M") relative to the concentration of the elements X that exceeds the ideal stoichiometric ratio y/z of the prototype compounds by at least 0.0001.

10. A compound as in any of claims 1-9, wherein the compound can intercalate at least one of an alkali or hydrogen.

11. A compound as in any of claims 1-9, wherein M" has a formal valence greater than 1+ as an ion in the compound.

12. A compound as in any of claims 1-9, wherein M" is any of aluminum, titanium, zirconium, niobium, tantalum, tungsten, and magnesium.

13. A compound as in any of claims 1-9, wherein A is lithium.

14. A compound as in any of claims 1-9, wherein X is phosphorus.

15. A compound as in any of claims 1-9, wherein D is oxygen.

16. A compound as in any of claims 1-9, wherein M' is any of iron, vanadium, chromium, manganese, cobalt or nickel.

17. A compound as in any of claims 1-9, wherein M' is Fe2+.

18. A compound as in any of claims 1-9, wherein at least one of M' and M" has an ionic radius less than the ionic radius of Fe2+.

19. A compound as in any of claims 1-9, wherein the compound is substantially free of silicon.

20. A compound as in any of claims 1-9, wherein the compound has a crystalline structure in which at least one of the M' or M" atoms occupy lattice sites coordinated by anion polyhedra, said polyhedra forming a continuous network through the structure by sharing at least one of vertices, corners, edges, or faces.

21. A compound as in claim 20, wherein the polyhedra of the continuous network are filled with transition-metals.

22. A compound as in any of claims 20-21, wherein the polyhedral units are octahedra or distorted octahedra.

23. A compound as in any of claims 20-22, wherein polyhedral units share corners and edges with other polyhedral units containing M' or M".

24. A compound as in any of claims 1-9, wherein the compound is an n-type conductor.

25. A compound as in any of claims 1-9, wherein the compound comprises a mixture of an n-type conductor and a p-type conductor.

26. A compound as in any of claims 1-9, wherein the compound is a p-type conductor.

27. A compound as in any of claims 1-9, wherein A is lithium and during preparation or use the compound is substantially fully delithiated.

28. A compound as in any of claims 1-9, wherein the compound is a p-type conductor when substantially fully lithiated and an n-type conductor when substantially fully delithiated.

29. A compound as in any of claims 1-9, wherein the compound, upon delithiation, undergoes phase-separation into a substantially lithiated compound and a substantially delithiated compound, each of which have an electronic conductivity of at least 10-6 S/cm.

30. A compound as in any of claims 1-9, wherein x has a value between zero and about 1, y is about 1, and z is about 1.

31. A compound as in any of claims 1-9, wherein x has a value between zero and about 1, and y is about 1.

32. A compound as in any of claims 1-9, wherein x has a value between zero and about 5, y is about 2, and z is about 3.

33. A compound as in any of claims 1-9, wherein x has a value between zero and about 2, y is about 1, and z is about 1.

34. A compound as in any of claims 1-9, wherein x has a value between zero and about 4, y is about 4, and z is about 3.

35. A compound as in any of claims 1-9, wherein 0 < x/(x+y+z) <=2/3.

36. A compound as in any of claims 1-9, wherein the compound has at least one of an ordered or partially disordered structure of the olivine (A x M XO4), NASICON
(AX(M',M")2(XO4)3), VOPO4, LiFe(P2O7) or Fe4(P2O7)3 structure-types.

37. A compound as in any of claims 1-9, wherein the compound is LiFePO4 containing additional metals M".

38. A compound as in any of claims 1-9, wherein the compound has an olivine structure and contains in crystalline solid solution, amongst the metals M' and M", simultaneously metal ions of at least one type that is oxidizable and another that is reducible at 23°C.

39. A compound as in any of claims 1-9, wherein the compound has an olivine structure and contains in crystalline solid solution, amongst the metals M' and M", simultaneously the metal ions Fe2+ and Fe3+, Mn2+ and Mn3+, Co2+ and Co3+, Ni2+ and Ni3+, V2+ and V3+, or Cr2+ and Cr3+, with the ion of lesser concentration being at least 10 parts per million of the sum of the two ion concentrations.

40. A compound as in any of claims 1-9, wherein the compound has an olivine structure, M' includes Fe, and at least one of M' and M" has an ionic radius less than the ionic radius of Fe2+.

41. A compound as in any of claims 1-9, wherein the compound has an olivine structure, and M" includes at least one metal with ionic radius less than the average ionic radius of the M' ions.

42. A compound as in any of claims 1-9, wherein the compound has an olivine structure with a crystalline solid solution of formula A X vac y (M'1-aM"a)XO4, A x-a-y M" a vac y M'XO4, A x (M'1-a-y M" a vacy)XO4 or A x-a M" a M' 1-y vac y XO4, wherein vac represents a vacancy in any of an M1 and M2 site of the primary crystallites.

43. A compound as in any of claims 1-9, wherein said compound has the ordered olivine structure type and A is lithium and is substituted onto a M2 site of a crystal of the composition at a concentration of at least about 10 18 per cubic centimeter.

44. A compound as in any of claims 1-9, wherein said compound has the ordered olivine structure type and A is lithium and x and a are selected such that lithium can substitute into an M2 site of a crystal of the composition as an acceptor defect.

45. A compound as in any of claims 1-9, wherein the composition is any of Li x (M'1-a M"a)PO4, Li X M" a M'PO4, Li x (M'1-a-y M" a Li y)PO4, or Li x-a M" a M'1-y Li y PO4.

46. A compound as in any of claims 1-9, wherein the composition is any of Li x (Fe1-a M"a)PO4, Li X M"a FePO4, Li x (Fe1-a-y M" a Li y)PO4, or Li x-a M"a Fe1-y Li y PO4.

47. A compound as in any of claims 1-9; wherein the composition is Li x vac 1-X
(M'1-a M"a)PO4, Li x M"a vac 1-a-y M'PO4, Li x(M'1-a-y M" a vac y)PO4 or Li x-a M" a M'1-y vac y PO4, wherein vac represents a vacancy in a structure of the compound.

48. A compound as in any of claims 1-9, wherein the composition is Li x vac 1-x (Fe 1-a M"a)PO4, Li x M" a vac 1-a-y (FePO4, Li x(Fe1-a-y M" a vac y)PO4 or Li x-a M"a Fe1-y vac y PO4, wherein vac represents a vacancy in a structure of the compound.

49. A compound as in any of claims 1-9, wherein the compound has an olivine structure and at least a portion of A occupies a M1 site.

50. A compound as in any of claims 1-9, wherein M" is substantially in solid solution in a crystal structure of the compound.

51. A compound as in any of claims 1-9, wherein M" is partially in solid solution in a crystal structure of the compound at a concentration of at least 0.01 atom %
relative to the concentration of M', the balance appearing as an additional phase.

52. A compound as in claim 51, wherein the concentration is at least 0.02 mole %.

53. A compound as in claim 51, wherein the concentration is at least 0.05 mole %.

54. A compound as in claim 51, wherein the concentration is at least 0.1 mole %.

55. A compound as in any of claims 1-9, wherein the compound comprises doped LiFePO4 in an olivine structure.

56. A compound as in any of claims 1-9, wherein the compound forms primary crystallites, at least 50 % of which have a smallest dimension less than 500 nm.

57. A compound as in any of claims 1-9, wherein the smallest dimension is less than 200 nm.

58. A compound as in any of claims 1-9, wherein the smallest dimension is less than 100 nm.

59. A compound as in any of claims 1-9, wherein the smallest dimension is less than 50 nm.

60. A compound as in any of claims 1-9, wherein the smallest dimension is less than 20 nm.

61. A compound as in any of claims 1-9, wherein the smallest dimension is less than 10 nm.

62. A compound as in any of claims 1-9, wherein the primary crystallites form an interconnected porous network

63. A compound as in any of claims 1-9, wherein at least about 25 % of the surface area of the primary crystallites is available for contact with an electrolyte.

64. A compound as in any of claims 1-9, wherein at least about 50 % of the surface area of the primary crystallites is in contact with an electrolyte.

65. A compound as in any of claims 1-9, wherein the compound has a specific surface area of at least about 10 m2/g.

66. A compound as in any of claims 1-9, wherein the specific surface area is at least about 20 m2/g.

67. A compound as in any of claims 1-9, wherein the specific surface area is at least about 30 m2/g.

68. A compound as in any of claims 1-9, wherein the specific surface area is at least about 40 m2/g.

69. A compound as in any of claims 1-9, wherein the specific surface area is at least about 50 m2/g.

70. A compound as in any of claims 1-9, wherein the conductivity is at least about 10 -7 S/cm.

71. A compound as in any of claims 1-9, wherein the conductivity is at least about 10 -6 S/cm.

72. A compound as in any of claims 1-9, wherein the conductivity is at least about 10 -5 S/cm.

73. A compound as in any of claims 1-9, wherein the conductivity is at least about 10 -4 S/cm.

74. A compound as in any of claims 1-9, wherein the conductivity is at least about 10 -3 S/cm.

75. A compound as in any of claims 1-9, wherein the conductivity is at least about 10 -2 S/cm.

76. A compound as in any of claims 1-9, further comprising less than about 15 weight percent of a conductivity-enhancing additive based on the weight of the composition.

77. A compound as in claim 76, wherein the conductivity-enhancing additive is present in an amount of less than about 10 weight percent.

78. A compound as in claim 76, wherein the conductivity-enhancing additive is present in an amount of less than about 7 weight percent.

79. A compound as in claim 76, wherein the conductivity-enhancing additive is present in an amount of less than about 5 weight percent.

80. A compound as in claim 76, wherein the conductivity-enhancing additive is present in an amount of less than about 3 weight percent.

81. A compound as in claim 76, wherein the conductivity-enhancing additive is present in an amount of less than about 2 weight percent.

82. A compound as in claim 76, wherein the conductivity-enhancing additive is present in an amount of less than about 1 weight percent.

83. A compound as in claim 76, wherein the conductivity-enhancing additive comprises carbon.

84. A compound as in any of claims 1-9, wherein the compound forms at least part of an electrode in an electrochemical device.

85. A compound as in any of claims 1-9, wherein the electrochemical device is a fuel cell.

86. A compound as in any of claims 1-9, wherein the compound is a mixed proton conducting and electronically conducting material.

87. A compound as in any of claims 1-9, wherein the compound is a gas separation membrane comprising a mixed proton conducting and electronically conducting material.

88. A compound as in any of claims 1-9, wherein the compound is a gas separation membrane comprising a mixed proton conducting and electronically conducting material comprising LiFePO4.

89. A compound as in any of claims 1-9 formed by mixing an alkali metal or hydrogen salt, a first-row transition metal compound, a salt of at least one of phosphorus, sulfur, arsenic, molybdenum and tungsten, and an ethoxide or methoxide of any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB
metal;
milling the mixture; and heat treating the mixture at a first temperature sufficient to form at least one of an olivine, NASICON, VOPO4, LiFe(P2O7) or Fe4(P2O7)3 structure.

90. A method of forming a compound, comprising:
mixing an alkali metal or hydrogen salt, a first-row transition metal salt, a salt of at least one of phosphorus, sulfur, arsenic, silicon, aluminum, boron, vanadium, molybdenum and tungsten, and a salt of any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB metal;
milling the mixture; and heat treating the mixture at a temperature between 300-900°C.

91. A method as in claim 90, wherein the alkali metal salt is a metal carbonate.

92. A method as in claim 90, wherein the alkali metal salt is lithium carbonate.

93. A method as in claim 90, wherein the alkali metal salt is LiPO3.

94. A method as in claim 90, wherein the salt of the first-row transition metal is a metal oxalate.

95. A method as in claim 90, wherein the salt of the first-row transition metal is a metal acetate.

96. A method as in claim 90, wherein the salt of the first-row transition metal is a metal oxide.

97. A method as in claim 90, wherein the salt of the first-row transition metal is iron oxalate.

98. A method as in claim 90, wherein the salt of the first-row transition metal is iron acetate.

99. A method as in claim 90, wherein the salt of the first-row transition metal is iron oxide.

100. A method as in claim 90, wherein the salt of at least one of phosphorus, sulfur, arsenic, silicon, aluminum, boron, vanadium, molybdenum and tungsten, is ammonium phosphate.

101. A method as in claim 90, wherein the salt of at least one of phosphorus, sulfur, arsenic, silicon, aluminum, boron, vanadium, molybdenum and tungsten, is LiPO3.

102. A method as in claim 90, wherein the salt of at least one of phosphorus, sulfur, arsenic, silicon, aluminum, boron, vanadium, molybdenum and tungsten, is P2O5.

103. A method as in claim 90, wherein the salt of at least one of phosphorus, sulfur, arsenic, silicon, aluminum, boron, vanadium, molybdenum and tungsten, is phosphoric acid.

104. A method as in claim 90, wherein the salt of any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB metal is a metal alkoxide.

105. A method as in claim 90, wherein the salt of any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB metal is a metal oxide.

106. A method as in claim 90, wherein the salt of any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB metal is a metal acetate.

107. A method as in claim 90, wherein the salt of any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB metal is a metal nitrate.

108. A method as in claim 90, wherein the salts comprise lithium carbonate, iron oxalate, ammonium phosphate, and an alkoxide of any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB metal.

109. A method as in claim 90, wherein the salts comprise lithium carbonate, iron oxalate, ammonium phosphate, and an alkoxide of any of magnesium, aluminum, iron, manganese, titanium, zirconium, niobium, tantalum, or tungsten.

110. A method as in claim 90, wherein the salts comprise lithium carbonate, iron oxalate, ammonium phosphate, and an oxide of any of magnesium, aluminum, iron, titanium, zirconium, niobium, tantalum, or tungsten.

111. A method as in claim 90, wherein the salts comprise LiPO3, FeO, and an alkoxide of any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB metal.

112. A method as in claim 90, wherein the salts comprise LiPO3, FeO, and an oxide of any of a Group IIA, IIIA, IVA, VA, VIA, VIIA, VIIIA, IB, IIB, IIIB, IVB, VB, and VIB
metal.

113. A method as in claim 90, wherein the salts comprise LiPO3, FeO, and an alkoxide of any of magnesium, aluminum, iron, manganese, titanium, zirconium, niobium, tantalum, or tungsten.

114. A method as in claim 90, wherein mixing is performed while the mixture is under a nonreactive atmosphere.

115. A method as in claim 90, wherein heat-treating is performed while the mixture is under a gaseous atmosphere with an oxygen partial pressure of less than about atmospheres.

116. A method as in claim 90, wherein heat-treating is performed while the mixture is under a gaseous atmosphere with an oxygen partial pressure of less than about atmospheres.

117. A method as in claim 90, wherein heat-treating is performed while the mixture is under a gaseous atmosphere with an oxygen partial pressure of less than about atmospheres.

118. A method as in claim 90, wherein heat-treating is performed in a gaseous atmosphere that is substantially nitrogen gas.

119. A method as in claim 90, wherein heat-treating is performed in a gaseous atmosphere that is substantially argon gas.

120. A method as in claim 90, wherein heat-treating is performed in a gaseous atmosphere that is substantially hydrogen gas.

121. A method as in claim 90, wherein heat-treating is performed in a gaseous atmosphere that is substantially a mixture of nitrogen and hydrogen gas.

122. A method as in claim 90, wherein heat-treating is performed in a gaseous atmosphere that is substantially a mixture of carbon monoxide and carbon dioxide gas.

123. A method as in claim 90, wherein heat-treating is performed in a gaseous atmosphere that is substantially nitrogen gas.

124. A method as in claim 90, further comprising heat treatment at two temperatures, the second heat treatment being at a temperature higher the first temperature.

125. A method as in claim 90, further comprising heat treatment at two temperatures, the first temperature being from 300-400°C and the second temperature being from 500-900°C.

126. A method of doping a material to form a lithium or hydrogen storage compound, comprising:

selecting a starting material to be doped, in conjunction with selection of milling equipment comprising a dopant for doping the starting material at a predetermined level of dopant;
milling the starting material in the milling equipment; and recovering from the milling step a material suitable for forming a lithium or hydrogen storage compound comprising the starting material doped with the dopant at the predetermined level.

127. A method as in claim 126, wherein the lithium or hydrogen storage compound is any one of the compounds of claims 1-9.

128. A method as in claim 126, wherein the dopant added from the milling equipment is at least one of zirconium, aluminum, iron, carbon, or fluorine.

129. A method as in claim 126, wherein the dopant comprises at least zirconium and the milling equipment comprises zirconia milling media or containers.

130. A method as in claim 126, wherein the dopant comprises at least aluminum and the milling equipment comprises aluminum oxide milling media or containers.

131. A method as in claim 126, wherein the dopant comprises at least iron and the milling equipment comprises iron or steel milling media or containers.

132. A method as in claim 126, wherein the dopant comprises at least carbon and the milling equipment comprises polymer milling media or containers.

133. A method as in claim 126, wherein said milling equipment includes at least one of polypropylene-bearing, polystyrene-bearing, or polytetrafluoroethylene-bearing milling media or milling containers.

134. A method as in claim 126, wherein the dopant comprises at least fluorine and the milling equipment comprises fluoropolymer milling media or containers.

135. An electrode comprising a compound of any one of claims 1-9 and having a material energy density that while:
charging or discharging at a rate >= 30 mA per g of storage compound, is greater than 350 Wh/kg, or charging or discharging at a rate >= 150 mA per g of storage compound, is greater than 280 Wh/kg, or charging or discharging at a rate >= 300 mA per g of storage compound, is greater than 270 Wh/kg, or charging or discharging at a rate >= 750 mA per g of storage compound, is greater than 250 Wh/kg, or charging or discharging at a rate >= 1.5 A per g of storage compound, is greater than 180 Wh/kg, or charging or discharging at a rate >= 3 A per g of storage compound, is greater than 40 Wh/kg, or charging or discharging at a rate >= 4.5 A per g of storage compound, is greater than 10 Wh/kg.

136. An electrode as in claim 135, having a material energy density that while:
charging or discharging at a rate >= 30 mA per g of storage compound, is greater than 420 Wh/kg, or charging or discharging at a rate >= 150 mA per g of storage compound, is greater than 400 Wh/kg, or charging or discharging at a rate >= 300 mA per g of storage compound, is greater than 370 Wh/kg, or charging or discharging at a rate >= 750 mA per g of storage compound, is greater than 350 Wh/kg, or charging or discharging at a rate >= 1.5 A per g of storage compound, is greater than 270 Wh/kg, or charging or discharging at a rate >= 3 A per g of storage compound, is greater than 150 Wh/kg, or charging or discharging at a rate >= 4.5 A per g of storage compound, is greater than 80 Wh/kg, or charging or discharging at a rate >= 6 A per g of storage compound, is greater than 35 Wh/kg, or charging or discharging at a rate >= 7.5 A per g of storage compound, is greater than 50 Wh/kg, or charging or discharging at a rate >= 15 A per g of storage compound, is greater than 10 Wh/kg.

137. An electrode as in claim 135, having a material energy density that while:
charging or discharging at a rate >= 30 mA per g of storage compound, is greater than 475 Wh/kg, or charging or discharging at a rate >= 150 mA per g of storage compound, is greater than 450 Wh/kg, or charging or discharging at a rate >= 300 mA per g of storage compound, is greater than 430 Wh/kg, or charging or discharging at a rate >= 750 mA per g of storage compound, is greater than 390 Wh/kg, or charging or discharging at a rate >= 1.5 A per g of storage compound, is greater than 350 Wh/kg, or charging or discharging at a rate >= 3 A per g of storage compound, is greater than 300 Wh/kg, or charging or discharging at a rate >= 4.5 A per g of storage compound, is greater than 250 Wh/kg, or charging or discharging at a rate >= 7.5 A per g of storage compound, is greater than 150 Wh/kg, or charging or discharging at a rate >= 11 A per g of storage compound, is greater than 50 Wh/kg, or charging or discharging at a rate >= 15 A per g of storage compound, is greater than 30 Wh/kg.

138. An electrode comprising a lithium storage compound other than one of ordered or partially ordered rocksalt crystal structure type, or spinel crystal structure type, or vanadium oxide or manganese oxide, the electrode having a material energy density that while:
charging or discharging at a rate >= 800 mA per g of storage compound, is greater than 250 Wh/kg; or charging or discharging at a rate >= 1.5 A per g of storage compound, is greater than 180 Wh/kg, or charging or discharging at a rate >= 3 A per g of storage compound, is greater than 40 Wh/kg, or charging or discharging at a rate >= 4.5 A per g of storage compound, is greater than 10 Wh/kg.

139. An electrode as in claim 138, having a material energy density that while:
charging or discharging at a rate >= 800 mA per g of storage compound, is greater than 350 Wh/kg, or charging or discharging at a rate >= 1.5 A per g of storage compound, is greater than 270 Wh/kg, or charging or discharging at a rate >= 3 A per g of storage compound, is greater than 150 Wh/kg, or charging or discharging at a rate >= 4.5 A per g of storage compound, is greater than 80 Wh/kg, or charging or discharging at a rate >= 6 A per g of storage compound, is greater than 35 Wh/kg, or charging or discharging at a rate >= 7.5 A per g of storage compound, is greater than 50 Wh/kg, or charging or discharging at a rate >= 15 A per g of storage compound, is greater than 10 Wh/kg,

140. An electrode as in claim 138, having a material energy density that while:
charging or discharging at a rate >= 800 mA per g of storage compound, is greater than 390 Wh/kg, or charging or discharging at a rate >= 1.5 A per g of storage compound, is greater than 350 Wh/kg, or charging or discharging at a rate >= 3 A per g of storage compound, is greater than 300 Wh/kg, or charging or discharging at a rate >= 4.5 A per g of storage compound, is greater than 250 Wh/kg, or charging or discharging at a rate >= 7.5 A per g of storage compound, is greater than 150 Wh/kg, or charging or discharging at a rate >= 11 A per g of storage compound, is greater than 50 Wh/kg, or charging or discharging at a rate >= 15 A per g of storage compound, is greater than 30 Wh/kg.

141. An electrode comprising a compound as in any one of claims 1-9.

142. An electrode as in claim 141, wherein the electrode comprises a sheet or a mesh coated or impregnated with the storage compound.

143. An electrode as in claim 141, wherein the electrode comprises a metal foil coated one or both sides with the storage compound.

144. An electrode as in claim 141, wherein the electrode is a sheet or mesh of electronically conductive material coated with a loading of at least 4 mg of said storage compound per square centimeter of projected area of the sheet or mesh.

145. An electrode as in claim 141, wherein said electrode is a sheet or mesh of electronically conductive material coated with a loading of at least 8 mg of said storage compound per square centimeter of projected area of the sheet or mesh.

146. An electrode as in claim 141, wherein said electrode is a sheet or mesh of electronically conductive material coated with a loading of at least 10 mg of said storage compound per square centimeter of projected area of the sheet or mesh.

147. An electrode as in claim 141, wherein said electrode is a sheet or mesh of electronically conductive material coated with a loading of at least 14 mg of said storage compound per square centimeter of projected area of the sheet or mesh.

148. An electrode as in claim 141, wherein said electrode is a sheet or mesh of electronically conductive material coated with a loading of at least 20 mg of said storage compound per square centimeter of projected area of the sheet or mesh.

149. An electrode as in claim 141, wherein said electrode is a sheet or mesh of electronically conductive material coated with said storage material and has a total thickness of at least 20 micrometers.

150. An electrode as in claim 141, wherein said electrode is a sheet or mesh of electronically conductive material coated with said storage material and has a total thickness of at least 40 micrometers.

151. An electrode as in claim 141, wherein said electrode is a sheet or mesh of electronically conductive material coated with said storage material and has a total thickness of at least 60 micrometers.

152. An electrode as in claim 141, wherein said electrode is a sheet or mesh of electronically conductive material coated with said storage material and has a total thickness of at least 80 micrometers.

153. An electrode as in claim 141, wherein said electrode is a sheet or mesh of electronically conductive material coated with said storage material and has a total thickness of at least 100 micrometers.

154. An electrode as in claim 141, wherein said electrode is a sheet or mesh of electronically conductive material coated with said storage material and has a total thickness of at least 150 micrometers.

155. An electrode as in claim 141, wherein said electrode is a sheet or mesh of electronically conductive material coated with said storage material and has a total thickness of at least 200 micrometers.

156. A storage battery cell comprising:
a positive electrode;
a negative electrode; and a separator positioned between the positive electrode and the negative electrode.
wherein at least one of the positive electrode or negative electrode comprises the compound of claim 1.

157. A storage battery cell as in claim 156 wherein the cell is a disposable battery cell.

158. A storage battery cell as in claim 156 wherein the cell is a rechargeable battery cell.

159. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge an energy of at least 0.25 Wh.

160. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge an energy of at least 1 Wh.

161. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge an energy of at least 5 Wh.

162. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge an energy of at least 10 Wh.

163. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge an energy of at least 20 Wh.

164. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge an energy of at least 30 Wh.

165. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge an energy of at least 40 Wh.

166. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge an energy of at least 50 Wh.

167. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge an energy of at least 100 Wh.

168. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge a gravimetric energy density of at least 30 Wh/kg or a volumetric energy density of at least 100 Wh/liter.

169. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge a gravimetric energy density of at least 50 Wh/kg or a volumetric energy density of at least 200 Wh/liter.

170. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge a gravimetric energy density of at least 90 Wh/kg or a volumetric energy density of at least 300 Wh/liter.

171. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge a gravimetric power density of at least 100 W/kg or a volumetric power density of at least 350 W/liter.

172. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge a gravimetric power density of at least 500 W/kg or a volumetric power density of at least 500 W/liter.

173. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge a gravimetric power density of at least 1000 W/kg or a volumetric power density of at least 1000 W/liter.

174. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge a gravimetric power density of at least 2000 W/kg or a volumetric power density of at least 2000 Wh/liter.

175. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge a gravimetric energy density of at least:
30 Wh/kg at a power density of at least 500 W/kg, or 20 Wh/kg at a power density of at least 1000 W/kg, or 10 Wh/kg at a power density of at least 1500 W/kg, or 5 Wh/kg at a power density of at least 2000 W/kg, or 2 Wh/kg at a power density of at least 2500 W/kg, or 1 Wh/kg at a power density of at least 3000 W/kg.

176. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge a gravimetric energy density of at least:
50 Wh/kg at a power density of at least 500 W/kg, or 40 Wh/kg at a power density of at least 1000 W/kg, or 20 Wh/kg at a power density of at least 2000 W/kg, or 10 Wh/kg at a power density of at least 3000 W/kg, or 4 Wh/kg at a power density of at least 4000 W/kg, or 1 Wh/kg at a power density of at least 5000 W/kg.

177. A storage battery cell as in claim 156 wherein the cell exhibits upon discharge a gravimetric energy density of at least:
80 Wh/kg at a power density of at least 1000 W/kg, or 70 Wh/kg at a power density of at least 2000 W/kg, or 60 Wh/kg at a power density of at least 3000 W/kg, or 55 Wh/kg at a power density of at least 4000 W/kg, or 50 Wh/kg at a power density of at least 5000 W/kg, or 30 Wh/kg at a power density of at least 6000 W/kg, or 10 Wh/kg at a power density of at least 8000 W/kg.

178. A storage battery cell as in claim 156, wherein the lithium storage compound is any other than a compound with an ordered or partially disordered rocksalt or spinet structure type, or vanadium oxide, or manganese oxide.