WO2016014653A1 - Chromium free hardfacing materials - Google Patents

Chromium free hardfacing materials Download PDF

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Publication number
WO2016014653A1
WO2016014653A1 PCT/US2015/041514 US2015041514W WO2016014653A1 WO 2016014653 A1 WO2016014653 A1 WO 2016014653A1 US 2015041514 W US2015041514 W US 2015041514W WO 2016014653 A1 WO2016014653 A1 WO 2016014653A1
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coating
work piece
manufacture
article
alloy
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PCT/US2015/041514
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French (fr)
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Justin Lee Cheney
Tianho JIANG
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Scoperta, Inc.
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Publication of WO2016014653A1 publication Critical patent/WO2016014653A1/en

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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C45/00Amorphous alloys
    • C22C45/02Amorphous alloys with iron as the major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/002Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/004Very low carbon steels, i.e. having a carbon content of less than 0,01%
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/08Ferrous alloys, e.g. steel alloys containing nickel
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/12Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/14Ferrous alloys, e.g. steel alloys containing titanium or zirconium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/44Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/46Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/48Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/50Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/58Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06Metallic material
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06Metallic material
    • C23C4/067Metallic material containing free particles of non-metal elements, e.g. carbon, silicon, boron, phosphorus or arsenic
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/12Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
    • C23C4/131Wire arc spraying

Definitions

  • the disclosure generally relates to hardfacing materials which can be deposited as hardfacing coatings without the production of Cr, such as hexavalent Cr dust.
  • Thermal spray processing is a technique which can be utilized to deposit a hard wear resistant and/or corrosion resistant layer onto the surface of a component.
  • Thermal spray inherently creates a significant amount of dust due to the fact that about 10-40% or more of the feedstock material does not stick to the component of interest and rebounds of the surface in the form a fine metallic dust.
  • One particular class of thermal spray materials which is used to form wear resistant layers is amorphous and/or nanocrystalline materials.
  • Fe-based amorphous and nanocrystalline materials used in thermal spray contain chromium as an alloying element. Chromium is effective in stabilizing the fine-grained structure, can increase wear resistance through the formation of chromium carbides and/or borides, and is useful in providing a degree of corrosion resistance.
  • Chromium is effective in stabilizing the fine-grained structure, can increase wear resistance through the formation of chromium carbides and/or borides, and is useful in providing a degree of corrosion resistance.
  • chromium is considered undesirable for use in thermal spray
  • Fe-based chromium free thermal spray materials There are several Fe-based chromium free thermal spray materials which have been developed and are used by industry today. Currently available Fe-based Cr-free materials have hardness levels below 500 Vickers, as shown in Table 1, which can make them inapplicable for many different industrial uses. Table 1 : Conventional Fe-based Cr-free materials and reported hardness values
  • Thermal spray coatings may be produced having a hardness above 500 Vickers without the use of chromium as an alloying element.
  • Some embodiments are directed to a work piece having a coating on at least a surface, the work piece comprising a metal surface onto which a coating is applied, the coating comprising an Fe-based alloy without any chromium, wherein the alloy comprises a Vickers hardness of at least 500 and an adhesion strength of at least 5,000 psi.
  • the coating can be applied via the twin wire arc spray process.
  • the coating can comprise, in weight percent, B: about 0-4, C: about 0-0.25, Si: about 0-15, Mn: about 0 to 25, Mo: about 0-29, Nb: about 0-2, Ta: about 0-4, Ti: about 0-4, V: about 0-10, W: about 0-6, Zr: about 0-10, wherein B + C + Si is about 4-15, and wherein (Mo + Mn + Nb + Ta + Ti + V + W + Zr) is about 5 to 38.
  • the coating can comprise Fe and, in weight percent, C: about 0 to 0.25, Mn: about 5 to 19, Mo: about 7 to 23, Ni: about 0 to 4, and Si: about 5 to 10. [0010]
  • the coating can be non-magnetic and therefore the coating thickness can be accurately measured with an ElcometerTM thickness gauge or similar device.
  • the coating can be non-magnetic and therefore the coating thickness can be accurately measured with an ElcometerTM thickness gauge or similar device after it has been exposed to temperatures exceeding about 1100 K for 2 hours or more and then slow cooled at a rate of lOK/s or less.
  • the coating can be amorphous. In some embodiments, the coating can be nanocrystalline, as defined by having a grain size of 100 nm or less.
  • an article of manufacture comprising a coating which is Fe-based, without chromium, and possesses a melting temperature of 1500K or below and a large atom concentration of at least 5 atom %, large atoms being of the group Mn, Mo, Nb, Ta, Ti, V, W, and Zr.
  • the coating can comprise a Vickers hardness of at least 400 and an adhesion strength of at least 5,000 psi. In some embodiments, the coating can be applied via the twin wire arc spray process.
  • the coating can comprise, in weight percent, B: about 0-4, C: about 0-0.25, Si: about 0-15, Mn: about 0 to 25, Mo: about 0-29, Nb: about 0-2, Ta: about 0-4, Ti: about 0-4, V: about 0-10, W: about 0-6, Zr: about 0-10, wherein B + C + Si is about 4-15, and wherein (Mo + Mn + Nb + Ta + Ti + V + W + Zr) is about 5 to 38.
  • the coating can comprise Fe and, in weight percent, C: about 0 to 0.25, Mn: about 5 to 19, Mo: about 7 to 23, Ni: about 0 to 4, and Si: about 5 to 10.
  • the coating can be non-magnetic and therefore the coating thickness can be accurately measured with an ElcometerTM thickness gauge or similar device. In some embodiments, the coating can be non-magnetic and therefore the coating thickness can be accurately measured with an ElcometerTM thickness gauge or similar device after it has been exposed to temperatures exceeding about 1100 K for 2 hours or more and then slow cooled at a rate of lOK/s or less. [0017] In some embodiments, the coating can be amorphous. In some embodiments, the coating can be nanocrystalline, as defined by having a grain size of 100 nm or less.
  • a work piece having at least one surface comprising a coating applied to the at least one surface, the coating comprising an Fe-based alloy having substantially no chromium, having substantially no carbides, and having substantially no borides, wherein the alloy comprises a Vickers hardness of at least 500 and an adhesion strength of at least 5,000 psi.
  • the coating can comprise Fe and, in weight percent, B: about 0-4, C: about 0-0.25, Si: about 0-15, Mn: about 0 to 25, Mo: about 0-29, Nb: about 0-2, Ta: about 0-4, Ti: about 0-4, V: about 0-10, W: about 0-6, Zr: about 0-10, wherein B + C + Si is about 4-15, and wherein (Mo + Mn + Nb + Ta + Ti + V + W + Zr) is about 5 to 38.
  • the coating can comprise Fe and in weight percent, C: about 0 to 0.25, Mn: about 5 to 19, Mo: about 7 to 23, Ni: about 0 to 4, and Si: about 5 to 10.
  • the coating can comprise one or more of the following compositions in weight percent: Fe, Mn: about 5, Mo: about 13, Si: about 10, Al: about 2; or Fe, Mn: about 5, Mo: about 7, Si: about 10, Al: about 2.
  • the coating can be non-magnetic and the coating thickness can be accurately measured with an ElcometerTM thickness gauge or similar device after it has been exposed to temperatures exceeding about 1100 K for 2 hours or more and then slow cooled at a rate of lOK/s or less.
  • the coating can be amorphous. In some embodiments, the coating can be nanocrystalline, as defined by having a grain size of 100 nm or less.
  • the coating can be applied via a thermal spray process. In some embodiments, the coating can be applied via a twin wire arc spray process. In some embodiments, the work piece can be a yankee dryer. In some embodiments, the work piece can be a roller used in a paper making machine.
  • an article of manufacture comprising an Fe-based coating having substantially no chromium;, wherein the coating possesses a melting temperature of 1500K or below, wherein the coating possesses a large atom concentration of at least 5 atom %, large atoms being of the group consisting of Mn, Mo, Nb, Ta, Ti, V, W, and Zr, and wherein the coating is a primarily single phase finegrained structure of either martensite, ferrite, or austenite.
  • the coating can comprise, in weight percent B: about 0-4, C: about 0-0.25, Si: about 0-15, Mn: about 0 to 25, Mo: about 0-29, Nb: about 0-2, Ta: about 0-4, Ti: about 0-4, V: about 0-10, W: about 0-6, Zr: about 0-10, wherein B + C + Si is about 4-15, and wherein (Mo + Mn + Nb + Ta + Ti + V + W + Zr) is about 5 to 38.
  • the coating can comprise Fe and in weight percent C: about 0 to 0.25, Mn: about 5 to 19, Mo: about 7 to 23, Ni: about 0 to 4, and Si: about 5 to 10.
  • the coating can comprise one or more of the following compositions in weight percent: Fe, Mn: about 5, Mo: about 13, Si: about 10, Al: about 2; or Fe, Mn: about 5, Mo: about 7, Si: about 10, Al: about 2.
  • the coating can be non-magnetic and the coating thickness can be accurately measured with an ElcometerTM thickness gauge or similar device after it has been exposed to temperatures exceeding about 1100 K for 2 hours or more and then slow cooled at a rate of lOK/s or less.
  • the coating can comprise a Vickers hardness of at least 500 and an adhesion strength of at least 5,000 psi.
  • the coating can be applied via the twin wire arc spray process. In some embodiments, the coating can be applied via a thermal spray process.
  • the coating can be amorphous. In some embodiments, the coating can be nanocrystalline, as defined by having a grain size of 100 nm or less.
  • the coating can be applied onto a roller used in a paper making machine. In some embodiments, the coating can be applied onto a Yankee Dryer. In some embodiments, the coating can be applied onto a boiler tube.
  • a work piece having at least one surface comprising a coating applied to the at least one surface, the coating comprising an Fe-based alloy having less than 1 wt. % chromium, less than 5 vol. % carbides, and less than 5 vol. % borides, wherein the alloy comprises a Vickers hardness of at least 500 and an adhesion strength of at least 5,000 psi.
  • the alloy can have less than 1 vol. % carbides and less than 1 vol. % borides.
  • the alloys can have high hardness and can be used as, for example, coatings.
  • computational metallurgy can be used to explore alloy compositional ranges where an alloy is likely to form an amorphous or nanocrystalline coating without the use of chromium as an alloying element.
  • Fe-based thermal spray coatings with a hardness above 500 Vickers have used chromium as an alloying element.
  • This disclosure demonstrates embodiments of alloy compositions which can produce thermal spray coatings with hardness values above 500 Vickers, in addition to describing the design techniques successfully used to identify them.
  • alloys which can achieve high hardness levels through mechanisms other than the use of chromium or the formation of carbides and/or borides. Rather, in some embodiments, a very fine-grain structure can be achieved due to melting temperature and large atom criteria disclosed herein.
  • the alloy can be described by a composition in weight percent comprising the following elemental ranges at least partially based on the ranges disclosed in Table 2 and Table 3 :
  • B 0-4 (or about 0 to about 4), C: 0-0.25 (or about 0 to about 0.25), and Si: 0-15 (or about 0 to about 15), where B+C+Si is 4-15 (or about 4 to about 15)
  • Mn 0-25 (or about 0 to about 25), Mo: 0-29 (or about 0 to about 29), Nb: 0-2 (or about 0 to about 2), Ta: 0-4 (or about 0 to about 4), Ti: 0-4 (or about 0 to about 4), V: 0-10 (or about 0 to about 10), W: 0-6 (or about 0 to about 6), Zr: 0-10 (about 0 to about 10), where (Mo+Mn+Nb+Ta+Ti+V+W+Zr) is 5-38 (or about 5 to about 38) 0 Cr (or about 0 Cr)
  • an alloy can be designed using any of the large elements as long as the other elemental ratios are controlled properly.
  • Fe has an atomic size of 156pm.
  • a large atom can be an atom that is larger than Fe.
  • These large atoms can be advantageous as they can increase the viscosity of an alloy in liquid form and thus slow down the crystallization rate of the alloy. As the crystallization rate decreases, the probability of forming an amorphous, nanocrystalline, or fine-grained structure can increase.
  • the coating can be amorphous. In some embodiments, the coating can be nanocrystalline, as defined by having a grain size of 100 nm or less. In some embodiments, the coating can be nanocrystalline, as defined by having a grain size of 50 nm or less. In some embodiments, the coating can be nanocrystalline, as defined by having a grain size of 20 nm or less.
  • the alloy can be described by a composition in weight percent comprising the following elemental ranges at least partially based on a range composed form the alloys selected for manufacture into experimental ingots:
  • the alloy can be described by the specific compositions, which have been produced and experimentally demonstrated amorphous formation potential, in weight percent, comprising the following elements.
  • Fe BAL, Mn: 5 (or about 5), Mo: 23 (or about 23), Si: 10 (or about 10)
  • Fe BAL, Mn: 5 (or about 5), Mo: 19 (or about 19), Si: 10 (or about 10)
  • Fe BAL, Mn: 5 (or about 5), Mo: 7 (or about 7), Si: 10 (or about 10) 6.
  • Fe BAL, Mn: 19 (or about 19), Mo: 7 (or about 7), Si: 7 (or about 7)
  • Fe BAL, Mn: 19 (or about 19), Mo: 7 (or about 7), Ni: 2 (or about 2), Si: 5 (or about 5)
  • Fe BAL, Mn: 19 (or about 19), Mo: 15 (or about 15), Si: 6 (or about 6)
  • Fe BAL, Mn: 19 (or about 19), Mo: 7 (or about 7), Ni: 2 (or about 2), Si: 5 (or about 5)
  • aluminum can be further added to the above alloy ranges and chemistries to improve coating adhesion in the range of up to 5 (or about 5) wt.%.
  • Fe BAL, Mn: 5 (or about 5), Mo: 13 (or about 13), Si: 10 (or about 10), Al: 2 (or about 2)
  • Fe BAL, Mn: 5 (or about 5), Mo: 7 (or about 7), Si: 10 (or about 10), Al: 2 (or about 2)
  • the alloy may contain boron, such as between 0-4 wt. % (including 1, 2, and 3 wt. %) as indicated above. In some embodiments, the alloy may not contain any boron. In some embodiments, boron may act as an impurity and does not exceed 1 wt. %.
  • the Fe content identified in the composition above may be the balance of the composition as indicated above, or alternatively, the balance of the composition may comprise Fe and other elements. In some embodiments, the balance may consist essentially of Fe and may include incidental impurities. In some embodiments, the above alloys may not contain any chromium. In some embodiments, chromium may act as an impurity and does not exceed 1 wt. %. Thermodynamic and Kinetic Criteria
  • the alloy can be described by thermodynamic and kinetic criteria.
  • the thermodynamic criteria can relate to the stability of the liquid phase, e.g., the melting temperature of the alloy.
  • the melting temperature can be calculated via thermodynamic models and is defined as the highest temperature at which liquid is less than 100% of the mole fraction in the material.
  • the kinetic criterion can be related to the viscosity of the liquid and the concentration in atom percent of large atoms. Large atoms are defined as atoms which are larger than iron atoms. Either or both criteria can be used to predict the tendency towards amorphous formation in thermal spray materials.
  • the alloys can have a microstructure of ferritic iron.
  • a primarily single phase fine-grained structure of either martensite, ferrite, or austenite can be formed.
  • ⁇ 5% (or ⁇ about 5%) borides and carbides are formed.
  • ⁇ % (or ⁇ about 1%) borides and carbides are formed.
  • ⁇ A% (or ⁇ about .1%) borides and carbides are formed.
  • no borides or carbides are formed.
  • the melting temperature can be below 1500 K (or below about 1500K). In some embodiments, the melting temperature can be below 1450K (or below about 1450K). In some embodiments, the melting temperature can be below 1400K (or below about 1400K). In general, amorphous formation is encouraged with lower melting temperatures because, typically, as grain size decreases, hardness increases (known as the Hall-Petch relationship). Amorphous alloys effectively have zero grain size, and thus can be the hardest form of the alloy. As amorphous formation potential increases, the alloy, even if it doesn't always become amorphous in every process, will tend towards a smaller grain size.
  • amorphous forming alloys of the disclosure even if they form fine-grained or nanocrystalline structures and not actually an amorphous structure, will tend to be harder.
  • the alloy may end up being crystalline, specifically nanocrystalline, upon application, such as through thermal spray, while still achieving the high hardness levels disclosed herein.
  • the large atom atomic fraction can be above 5 atom % (or above about 5 atom %). In some embodiments, the large atom atomic fraction can be above 7.5 atom % (or above about 7.5 atom %). In some embodiments, the large atom atomic fraction can be above 10 atom % (or above about 10 atom %). In some embodiments, the higher large atom atomic fraction can encourage amorphous formation and increase amorphous formation potential.
  • Table 2 lists the alloy compositions, all Fe-based, in weight percent which can meet the thermodynamic criteria detailed in this disclosure.
  • the Fe-based alloys can have a composition that is predominantly iron, e.g., at least 50 wt. % iron.
  • Table 2 List of alloy compositions with thermodynamic and kinetic parameters which meet disclosed criteria. Large atom % is the total atom % of elements larger than iron and melt T is the melting temperature of the alloy.
  • the alloy can possess a low FCC-BCC transition temperature. This criteria can be related to the likelihood of the alloy to retain an austenitic structure when deposited and thus be 'readable' by certain measuring devices, as discussed further below. Readable coatings can be non-magnetic and thus the thickness can be measured with standard paint thickness gauges. This can be advantageous for many thermal spray applications.
  • the alloy can be described by performance criteria.
  • the performance criteria that can be advantageous to the field of thermal spray hardfacing is the hardness, wear resistance, coating adhesion, and corrosion resistance.
  • the Vickers hardness of the coating can be 400 or above (or about 400 or above). In some embodiments, the Vickers hardness of the coating can be 500 or above (or about 500 or above). In some embodiments, the Vickers hardness can be 550 or above (or about 550 or above).In some embodiments, the Vickers hardness can be 600 or above (or about 600 or above).
  • the specific microstructure disclosed herein can allow for embodiments of the alloys to have high hardness.
  • the adhesion strength of the coating can be 5,000 psi or above (or about 5,000 psi or above). In some embodiments, the adhesion strength of the coating can be 7,500 psi or above (or about 7,500 psi or above). In some embodiments, the adhesion strength of the coating can be 10,000 psi or above (or about 10,000 psi or above).
  • the abrasion resistance of the coating as measured via ASTM G65B testing can be 0.8 grams loss or below (or about 0.8 grams loss or below). In some embodiments, the abrasion resistance of the coating as measured via ASTM G65B testing can be 0.6 grams loss or below (or about 0.6 grams loss or below). In some embodiments, the abrasion resistance of the coating as measured via ASTM G65B testing can be 0.4 grams loss or below (or about 0.4 grams loss or below).
  • the adhesive wear resistance of the coating as measured via ASTM G77 testing can be 2 mm 3 volume loss or below (or about 2 mm 3 volume loss or below). In some embodiments, the adhesive wear resistance of the coating as measured via ASTM Gil testing can be 0.5 mm 3 volume loss or below (or about 0.5 mm 3 volume loss or below). In some embodiments, the adhesive wear resistance of the coating as measured via ASTM Gil testing can be 0.1 mm 3 volume loss or below (or about 0.1 mm 3 volume loss or below).
  • the alloy can exhibit similar performance to conventional Cr-bearing thermal spray materials used for hardfacing.
  • the most exemplary and well used thermal spray hardfacing material possesses a chemical composition of Fe: BAL, Cr: 29, Si: 1, Mn: 2, B: 4, which is generally referred to in the industry as Armacor M.
  • Armacor M possesses the following properties which are relevant to thermal spray hardfacing: adhesion of about 8,000 psi, ASTM G65B mass loss of about 0.37 grams, ASTM G77 volume loss of about 0.07 mm , and position in the galvanic series in saltwater of about -500 mV.
  • Armacor M is primarily made of Fe, Cr, and B, has a high melting temperature, and has no large atoms.
  • the alloys can exhibit similar coating adhesion and abrasive wear resistance as Armacor, where 'similar' equates to within 25% (or within about 25%) of the measured performance properties of Armacor M or better. In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion, abrasive wear resistance, and adhesive wear resistance as Armacor, where 'similar' equates to within 25% (or within about 25%) of the measured performance properties of Armacor M or better.
  • the alloys can exhibit similar coating adhesion, abrasive wear resistance, adhesive wear resistance, and corrosion resistance as Armacor, where 'similar' equates to within 25% (or within about 25%) of the measured performance properties of Armacor M or better.
  • the alloys can exhibit similar coating adhesion and abrasive wear resistance as Armacor, where 'similar' equates to within 10% (or within about 10%) of the measured performance properties of Armacor M or better. In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion, abrasive wear resistance, and adhesive wear resistance as Armacor, where 'similar' equates to within 10% (or within about 10%) of the measured performance properties of Armacor M or better.
  • the alloys can exhibit similar coating adhesion, abrasive wear resistance, adhesive wear resistance, and corrosion resistance as Armacor, where 'similar' equates to within 10% (or within about 10%) of the measured performance properties of Armacor M or better.
  • the alloys can exhibit similar coating adhesion and abrasive wear resistance as Armacor, where 'similar' equates to within 1% (or within about 1%) of the measured performance properties of Armacor M or better. In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion, abrasive wear resistance, and adhesive wear resistance as Armacor, where 'similar' equates to within 1% (or within about 1%) of the measured performance properties of Armacor M or better.
  • the alloys can exhibit similar coating adhesion, abrasive wear resistance, adhesive wear resistance, and corrosion resistance as Armacor, where 'similar' equates to within 1% (or within about 1%) of the measured performance properties of Armacor M or better.
  • the alloys can exhibit similar coating adhesion and abrasive wear resistance as Armacor, where 'similar' equates to within 0% (or within about 0%) of the measured performance properties of Armacor M or better. In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion, abrasive wear resistance, and adhesive wear resistance as Armacor, where 'similar' equates to within 0% (or within about 0%) of the measured performance properties of Armacor M or better.
  • the alloys can exhibit similar coating adhesion, abrasive wear resistance, adhesive wear resistance, and corrosion resistance as Armacor, where 'similar' equates to within 0% (or within about 0%) of the measured performance properties of Armacor M or better.
  • the thermal spray coating can be 'readable'.
  • a readable coating produces consistent thickness measurements with an ElcometerTM thickness gauge, or similar device, when properly calibrated.
  • Armacor M is not a readable alloy, unlike embodiments of the disclosure, as it is magnetic.
  • the coating thickness measurement can be accurate to within 5 mils (or within about 5 mils) of the actual physical thickness. In some embodiments, the coating thickness measurement can be accurate to within 3.5 mils (or within about 3.5 mils) of the actual physical thickness. In some embodiments, the coating thickness measurement can be accurate to within 2 mils (or within about 2 mils) of the actual physical thickness.
  • consistent measurements according to the above criteria can be made after the coating has been exposed to heat for an extended period of time.
  • This can be advantageous because when the alloy is heated, there is a potential for a magnetic phase to precipitate out, which would make the alloy non-readable.
  • This can be especially true for amorphous alloys which may be readable in amorphous form, but may crystallize in a different environment due to heat.
  • the alloy can remain non-magnetic even after being exposed to heat for a substantial time period.
  • the coating can be 'readable' after exposure to HOOK (or about HOOK) for 2 hours (or about 2 hours) and cooled at a rate of less than 10K/S (or less than about 10K/S).
  • the coating can be 'readable' after exposure to 1300K (or about 1300K) for 2 hours (or about 2 hours) and cooled at a rate of less than 10K/S (or less than 10K/S).
  • the coating can be 'readable' after exposure to 1500K (r about 1500K) for 2 hours (or about 2 hours) and cooled at a rate of less than 10K/S (or less than about 10K/S). It is expected that increased exposure times above 2 hours will not continue to affect the final 'readability' of these materials.
  • Table 3 List of alloy compositions and thermodynamic and kinetic parameters which meet the criteria described in this disclosure, including the criteria pertained to coating non- magnetism and readability.
  • Large atom % is the total atom % of elements larger than iron, Trans T is the FCC-BCC transition temperature and melt T is the melting temperature of the alloy.

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Abstract

Disclosed are embodiments of Fe-based alloys for use as a hardfacing material having high hardness while avoiding the use of chromium. The alloys can be twin arc or thermally sprayed as coatings on different types of equipment. In some embodiments, the alloys can be readable even after heating of the alloys.

Description

CHROMIUM FREE HARDFACING MATERIALS
INCORPORATION BY REFERENCE TO ANY PRIORITY APPLICATIONS
[0001] This Application claims from the benefit of U.S. Provisional Application
No. 62/028,706, filed July 24, 2014, titled "CHROMIUM FREE HARDFACING ALLOYS," the entirety of which is incorporated herein by reference.
BACKGROUND
Field
[0002] The disclosure generally relates to hardfacing materials which can be deposited as hardfacing coatings without the production of Cr, such as hexavalent Cr dust.
Description of the Related Art
[0003] Thermal spray processing is a technique which can be utilized to deposit a hard wear resistant and/or corrosion resistant layer onto the surface of a component. Thermal spray inherently creates a significant amount of dust due to the fact that about 10-40% or more of the feedstock material does not stick to the component of interest and rebounds of the surface in the form a fine metallic dust. One particular class of thermal spray materials which is used to form wear resistant layers is amorphous and/or nanocrystalline materials. Fe-based amorphous and nanocrystalline materials used in thermal spray contain chromium as an alloying element. Chromium is effective in stabilizing the fine-grained structure, can increase wear resistance through the formation of chromium carbides and/or borides, and is useful in providing a degree of corrosion resistance. However, chromium is considered undesirable for use in thermal spray applications due to the potential to form hexavalent chromium dust. Hexavalent chromium dust is known to cause cancer.
[0004] There are several Fe-based chromium free thermal spray materials which have been developed and are used by industry today. Currently available Fe-based Cr-free materials have hardness levels below 500 Vickers, as shown in Table 1, which can make them inapplicable for many different industrial uses. Table 1 : Conventional Fe-based Cr-free materials and reported hardness values
Figure imgf000003_0001
[0005] There have also been efforts to specifically design Cr-free hardfacing materials for welding processes, such as that shown in 2012/0097658. However, the alloys disclosed in the reference require the formation of borides and carbides. Further, the reference requires the use of boron.
SUMMARY
[0006] Disclosed herein are embodiments of alloy compositions used to produce thermal spray coatings, methods of identifying these compositions, the coatings themselves, and methods of making and using the coatings. Thermal spray coatings according to certain embodiments may be produced having a hardness above 500 Vickers without the use of chromium as an alloying element. Some embodiments are directed to a work piece having a coating on at least a surface, the work piece comprising a metal surface onto which a coating is applied, the coating comprising an Fe-based alloy without any chromium, wherein the alloy comprises a Vickers hardness of at least 500 and an adhesion strength of at least 5,000 psi.
[0007] In some embodiments, the coating can be applied via the twin wire arc spray process.
[0008] In some embodiments, the coating can comprise, in weight percent, B: about 0-4, C: about 0-0.25, Si: about 0-15, Mn: about 0 to 25, Mo: about 0-29, Nb: about 0-2, Ta: about 0-4, Ti: about 0-4, V: about 0-10, W: about 0-6, Zr: about 0-10, wherein B + C + Si is about 4-15, and wherein (Mo + Mn + Nb + Ta + Ti + V + W + Zr) is about 5 to 38.
[0009] In some embodiments, the coating can comprise Fe and, in weight percent, C: about 0 to 0.25, Mn: about 5 to 19, Mo: about 7 to 23, Ni: about 0 to 4, and Si: about 5 to 10. [0010] In some embodiments, the coating can be non-magnetic and therefore the coating thickness can be accurately measured with an Elcometer™ thickness gauge or similar device. In some embodiments, the coating can be non-magnetic and therefore the coating thickness can be accurately measured with an Elcometer™ thickness gauge or similar device after it has been exposed to temperatures exceeding about 1100 K for 2 hours or more and then slow cooled at a rate of lOK/s or less.
[0011] In some embodiments, the coating can be amorphous. In some embodiments, the coating can be nanocrystalline, as defined by having a grain size of 100 nm or less.
[0012] Also disclosed herein are embodiments of an article of manufacture comprising a coating which is Fe-based, without chromium, and possesses a melting temperature of 1500K or below and a large atom concentration of at least 5 atom %, large atoms being of the group Mn, Mo, Nb, Ta, Ti, V, W, and Zr.
[0013] In some embodiments, the coating can comprise a Vickers hardness of at least 400 and an adhesion strength of at least 5,000 psi. In some embodiments, the coating can be applied via the twin wire arc spray process.
[0014] In some embodiments, the coating can comprise, in weight percent, B: about 0-4, C: about 0-0.25, Si: about 0-15, Mn: about 0 to 25, Mo: about 0-29, Nb: about 0-2, Ta: about 0-4, Ti: about 0-4, V: about 0-10, W: about 0-6, Zr: about 0-10, wherein B + C + Si is about 4-15, and wherein (Mo + Mn + Nb + Ta + Ti + V + W + Zr) is about 5 to 38.
[0015] In some embodiments, the coating can comprise Fe and, in weight percent, C: about 0 to 0.25, Mn: about 5 to 19, Mo: about 7 to 23, Ni: about 0 to 4, and Si: about 5 to 10.
[0016] In some embodiments, the coating can be non-magnetic and therefore the coating thickness can be accurately measured with an Elcometer™ thickness gauge or similar device. In some embodiments, the coating can be non-magnetic and therefore the coating thickness can be accurately measured with an Elcometer™ thickness gauge or similar device after it has been exposed to temperatures exceeding about 1100 K for 2 hours or more and then slow cooled at a rate of lOK/s or less. [0017] In some embodiments, the coating can be amorphous. In some embodiments, the coating can be nanocrystalline, as defined by having a grain size of 100 nm or less.
[0018] Disclosed herein are embodiments of a work piece having at least one surface, the work piece comprising a coating applied to the at least one surface, the coating comprising an Fe-based alloy having substantially no chromium, having substantially no carbides, and having substantially no borides, wherein the alloy comprises a Vickers hardness of at least 500 and an adhesion strength of at least 5,000 psi.
[0019] In some embodiments, the coating can comprise Fe and, in weight percent, B: about 0-4, C: about 0-0.25, Si: about 0-15, Mn: about 0 to 25, Mo: about 0-29, Nb: about 0-2, Ta: about 0-4, Ti: about 0-4, V: about 0-10, W: about 0-6, Zr: about 0-10, wherein B + C + Si is about 4-15, and wherein (Mo + Mn + Nb + Ta + Ti + V + W + Zr) is about 5 to 38. In some embodiments, the coating can comprise Fe and in weight percent, C: about 0 to 0.25, Mn: about 5 to 19, Mo: about 7 to 23, Ni: about 0 to 4, and Si: about 5 to 10. In some embodiments, the coating can comprise one or more of the following compositions in weight percent: Fe, Mn: about 5, Mo: about 13, Si: about 10, Al: about 2; or Fe, Mn: about 5, Mo: about 7, Si: about 10, Al: about 2.
[0020] In some embodiments, the coating can be non-magnetic and the coating thickness can be accurately measured with an Elcometer™ thickness gauge or similar device after it has been exposed to temperatures exceeding about 1100 K for 2 hours or more and then slow cooled at a rate of lOK/s or less.
[0021] In some embodiments, the coating can be amorphous. In some embodiments, the coating can be nanocrystalline, as defined by having a grain size of 100 nm or less.
[0022] In some embodiments, the coating can be applied via a thermal spray process. In some embodiments, the coating can be applied via a twin wire arc spray process. In some embodiments, the work piece can be a yankee dryer. In some embodiments, the work piece can be a roller used in a paper making machine.
[0023] Also disclosed herein are embodiments of an article of manufacture comprising an Fe-based coating having substantially no chromium;, wherein the coating possesses a melting temperature of 1500K or below, wherein the coating possesses a large atom concentration of at least 5 atom %, large atoms being of the group consisting of Mn, Mo, Nb, Ta, Ti, V, W, and Zr, and wherein the coating is a primarily single phase finegrained structure of either martensite, ferrite, or austenite.
[0024] In some embodiments, the coating can comprise, in weight percent B: about 0-4, C: about 0-0.25, Si: about 0-15, Mn: about 0 to 25, Mo: about 0-29, Nb: about 0-2, Ta: about 0-4, Ti: about 0-4, V: about 0-10, W: about 0-6, Zr: about 0-10, wherein B + C + Si is about 4-15, and wherein (Mo + Mn + Nb + Ta + Ti + V + W + Zr) is about 5 to 38.
[0025] In some embodiments, the coating can comprise Fe and in weight percent C: about 0 to 0.25, Mn: about 5 to 19, Mo: about 7 to 23, Ni: about 0 to 4, and Si: about 5 to 10.
[0026] In some embodiments, the coating can comprise one or more of the following compositions in weight percent: Fe, Mn: about 5, Mo: about 13, Si: about 10, Al: about 2; or Fe, Mn: about 5, Mo: about 7, Si: about 10, Al: about 2.
[0027] In some embodiments, the coating can be non-magnetic and the coating thickness can be accurately measured with an Elcometer™ thickness gauge or similar device after it has been exposed to temperatures exceeding about 1100 K for 2 hours or more and then slow cooled at a rate of lOK/s or less. In some embodiments, the coating can comprise a Vickers hardness of at least 500 and an adhesion strength of at least 5,000 psi.
[0028] In some embodiments, the coating can be applied via the twin wire arc spray process. In some embodiments, the coating can be applied via a thermal spray process.
[0029] In some embodiments, the coating can be amorphous. In some embodiments, the coating can be nanocrystalline, as defined by having a grain size of 100 nm or less.
[0030] In some embodiments, the coating can be applied onto a roller used in a paper making machine. In some embodiments, the coating can be applied onto a Yankee Dryer. In some embodiments, the coating can be applied onto a boiler tube.
[0031] Also disclosed herein are embodiments of a work piece having at least one surface, the work piece comprising a coating applied to the at least one surface, the coating comprising an Fe-based alloy having less than 1 wt. % chromium, less than 5 vol. % carbides, and less than 5 vol. % borides, wherein the alloy comprises a Vickers hardness of at least 500 and an adhesion strength of at least 5,000 psi. In some embodiments, the alloy can have less than 1 vol. % carbides and less than 1 vol. % borides.
DETAILED DESCRIPTION
[0032] Disclosed herein are embodiments of chromium free, iron based alloys, and methods of manufacturing the alloys. In some embodiments, the alloys can have high hardness and can be used as, for example, coatings. In some embodiments, computational metallurgy can be used to explore alloy compositional ranges where an alloy is likely to form an amorphous or nanocrystalline coating without the use of chromium as an alloying element. Prior to this disclosure, Fe-based thermal spray coatings with a hardness above 500 Vickers have used chromium as an alloying element. This disclosure demonstrates embodiments of alloy compositions which can produce thermal spray coatings with hardness values above 500 Vickers, in addition to describing the design techniques successfully used to identify them.
[0033] Specifically, disclosed herein are embodiments of alloys which can achieve high hardness levels through mechanisms other than the use of chromium or the formation of carbides and/or borides. Rather, in some embodiments, a very fine-grain structure can be achieved due to melting temperature and large atom criteria disclosed herein.
Metal Alloy Composition
[0034] In some embodiments, the alloy can be described by a composition in weight percent comprising the following elemental ranges at least partially based on the ranges disclosed in Table 2 and Table 3 :
• Fe: BAL
• B: 0-4 (or about 0 to about 4), C: 0-0.25 (or about 0 to about 0.25), and Si: 0-15 (or about 0 to about 15), where B+C+Si is 4-15 (or about 4 to about 15)
• Mn: 0-25 (or about 0 to about 25), Mo: 0-29 (or about 0 to about 29), Nb: 0-2 (or about 0 to about 2), Ta: 0-4 (or about 0 to about 4), Ti: 0-4 (or about 0 to about 4), V: 0-10 (or about 0 to about 10), W: 0-6 (or about 0 to about 6), Zr: 0-10 (about 0 to about 10), where (Mo+Mn+Nb+Ta+Ti+V+W+Zr) is 5-38 (or about 5 to about 38) 0 Cr (or about 0 Cr)
[0035] Generally, embodiments of an alloy can be designed using any of the large elements as long as the other elemental ratios are controlled properly. The following atomic sizes, in picometers, were used for the large elements, large atoms defined as atoms which are larger than iron atoms: Mn: 161, Mo: 190, Nb, 198, Ta: 200, Ti: 176, V: 171, W: 193, Zr: 206. Fe has an atomic size of 156pm. A large atom can be an atom that is larger than Fe. These large atoms can be advantageous as they can increase the viscosity of an alloy in liquid form and thus slow down the crystallization rate of the alloy. As the crystallization rate decreases, the probability of forming an amorphous, nanocrystalline, or fine-grained structure can increase.
[0036] In some embodiments, the coating can be amorphous. In some embodiments, the coating can be nanocrystalline, as defined by having a grain size of 100 nm or less. In some embodiments, the coating can be nanocrystalline, as defined by having a grain size of 50 nm or less. In some embodiments, the coating can be nanocrystalline, as defined by having a grain size of 20 nm or less.
[0037] In some embodiments, the alloy can be described by a composition in weight percent comprising the following elemental ranges at least partially based on a range composed form the alloys selected for manufacture into experimental ingots:
• Fe: BAL, C: 0-0.25 (or about 0 to about 0.25), Mn: 5-19 (or about 5 to about 19), Mo:
7-23 (or about 7 to about 23), Ni: 0-4 (or about 0 to about 4), Si: 5-10 (or about 5 to about 10)
[0038] In some embodiments, the alloy can be described by the specific compositions, which have been produced and experimentally demonstrated amorphous formation potential, in weight percent, comprising the following elements.
1. Fe: BAL, Mn: 5 (or about 5), Mo: 23 (or about 23), Si: 10 (or about 10)
2. Fe: BAL, Mn: 5 (or about 5), Mo: 19 (or about 19), Si: 10 (or about 10)
3. Fe: BAL, Mn: 5 (or about 5), Mo: 11 (or about 11), Si: 10 (or about 10)
4. Fe: BAL, Mn: 5 (or about 5), Mo: 13 (or about 13), Si: 10 (or about 10)
5. Fe: BAL, Mn: 5 (or about 5), Mo: 7 (or about 7), Si: 10 (or about 10) 6. Fe: BAL, Al: 2 (or about 2), Mn: 5 (or about 5), Mo: 5 (or about 5), Si: 13 (or about 13)
7. Fe: BAL, Al: 2 (or about 2), Mn: 5 (or about 5), Mo: 7 (or about 7), Si: 15 (or about 15)
8. Fe: BAL, C: 0.25 (or about 0.25), Mn: 19 (or about 19), Mo: 7 (or about 7), Si: (5 or about 5)
9. Fe: BAL, C: 0.25 (or about 0.25), Mn: 5 (or about 5), Mo: 7 (or about 7), Ni: (4 or about 4), Si: 5 (or about 5)
10. Fe: BAL, Mn: 19 (or about 19), Mo: 7 (or about 7), Si: 7 (or about 7)
11. Fe: BAL, Mn: 19 (or about 19), Mo: 7 (or about 7), Ni: 2 (or about 2), Si: 5 (or about 5)
12. Fe: BAL, Mn: 19 (or about 19), Mo: 15 (or about 15), Si: 6 (or about 6)
13. Fe: BAL, Mn: 19 (or about 19), Mo: 7 (or about 7), Ni: 2 (or about 2), Si: 5 (or about 5)
[0039] In some embodiments, aluminum can be further added to the above alloy ranges and chemistries to improve coating adhesion in the range of up to 5 (or about 5) wt.%. Some exemplary examples of aluminum additions, based upon the #4 and #5 base chemistries, are:
14. Fe: BAL, Mn: 5 (or about 5), Mo: 13 (or about 13), Si: 10 (or about 10), Al: 2 (or about 2)
15. Fe: BAL, Mn: 5 (or about 5), Mo: 7 (or about 7), Si: 10 (or about 10), Al: 2 (or about 2)
[0040] In some embodiments, the alloy may contain boron, such as between 0-4 wt. % (including 1, 2, and 3 wt. %) as indicated above. In some embodiments, the alloy may not contain any boron. In some embodiments, boron may act as an impurity and does not exceed 1 wt. %.
[0041] The Fe content identified in the composition above may be the balance of the composition as indicated above, or alternatively, the balance of the composition may comprise Fe and other elements. In some embodiments, the balance may consist essentially of Fe and may include incidental impurities. In some embodiments, the above alloys may not contain any chromium. In some embodiments, chromium may act as an impurity and does not exceed 1 wt. %. Thermodynamic and Kinetic Criteria
[0042] In some embodiments, the alloy can be described by thermodynamic and kinetic criteria. In some embodiments, the thermodynamic criteria can relate to the stability of the liquid phase, e.g., the melting temperature of the alloy. The melting temperature can be calculated via thermodynamic models and is defined as the highest temperature at which liquid is less than 100% of the mole fraction in the material. The kinetic criterion can be related to the viscosity of the liquid and the concentration in atom percent of large atoms. Large atoms are defined as atoms which are larger than iron atoms. Either or both criteria can be used to predict the tendency towards amorphous formation in thermal spray materials. In some embodiments, the alloys can have a microstructure of ferritic iron. In some embodiments, a primarily single phase fine-grained structure of either martensite, ferrite, or austenite can be formed. In some embodiments, <5% (or < about 5%) borides and carbides are formed. In some embodiments, <\% (or < about 1%) borides and carbides are formed. In some embodiments, <A% (or < about .1%) borides and carbides are formed. In some embodiments, no borides or carbides are formed.
[0043] In some embodiments, the melting temperature can be below 1500 K (or below about 1500K). In some embodiments, the melting temperature can be below 1450K (or below about 1450K). In some embodiments, the melting temperature can be below 1400K (or below about 1400K). In general, amorphous formation is encouraged with lower melting temperatures because, typically, as grain size decreases, hardness increases (known as the Hall-Petch relationship). Amorphous alloys effectively have zero grain size, and thus can be the hardest form of the alloy. As amorphous formation potential increases, the alloy, even if it doesn't always become amorphous in every process, will tend towards a smaller grain size. Thus, amorphous forming alloys of the disclosure, even if they form fine-grained or nanocrystalline structures and not actually an amorphous structure, will tend to be harder. For example, in some embodiments, while there is the potential for an amorphous structure, the alloy may end up being crystalline, specifically nanocrystalline, upon application, such as through thermal spray, while still achieving the high hardness levels disclosed herein.
[0044] In some embodiments, the large atom atomic fraction can be above 5 atom % (or above about 5 atom %). In some embodiments, the large atom atomic fraction can be above 7.5 atom % (or above about 7.5 atom %). In some embodiments, the large atom atomic fraction can be above 10 atom % (or above about 10 atom %). In some embodiments, the higher large atom atomic fraction can encourage amorphous formation and increase amorphous formation potential.
[0045] Table 2 lists the alloy compositions, all Fe-based, in weight percent which can meet the thermodynamic criteria detailed in this disclosure. In some embodiments, the Fe-based alloys can have a composition that is predominantly iron, e.g., at least 50 wt. % iron.
[0046] Combining the alloys in Table 2 and Table 3 yields 1,141 compositions which meet the criteria. These alloys were compiled through computational searching tools which evaluated 16,362 alloys according to the disclosed criteria. Thus, the alloys disclosed cover only 6.9% of the total explored space explicitly investigated to design an alloy with the disclosed performance parameters.
Table 2: List of alloy compositions with thermodynamic and kinetic parameters which meet disclosed criteria. Large atom % is the total atom % of elements larger than iron and melt T is the melting temperature of the alloy.
No B Mn Mo Nb Si Ta Ti V w Zr Large Atom % Melt T
Ml 0 0 10 1 10 0 0 0 0 0 6.1% 1500
M2 0 0 15 1 9 0 0 0 0 0 9.1% 1500
M3 0 0 15 1 10 0 0 0 0 0 9.0% 1500
M4 0 0 20 0 7 0 0 0 0 0 11.8% 1500
M5 0 0 20 0 8 0 0 0 0 0 11.7% 1500
M6 0 0 20 0 9 0 0 0 0 0 11.6% 1450
M7 0 0 20 0 10 0 0 0 0 0 11.5% 1450
M8 0 0 20 1 7 0 0 0 0 0 12.5% 1500
M9 0 0 20 1 8 0 0 0 0 0 12.3% 1500
M10 0 0 20 1 9 0 0 0 0 0 12.2% 1500
Mil 0 0 20 1 10 0 0 0 0 0 12.1% 1500
M12 0 1 10 0 10 0 0 0 0 0 6.5% 1500
M13 0 1 10 1 10 0 0 0 0 0 7.1% 1500
M14 0 1 15 1 8 0 0 0 0 0 10.2% 1500
M15 0 1 15 1 9 0 0 0 0 0 10.1% 1500
M16 0 1 15 1 10 0 0 0 0 0 10.0% 1450
M17 0 1 20 0 7 0 0 0 0 0 12.8% 1500 M18 0 1 20 0 8 0 0 0 0 0 12.7% 1500
M19 0 1 20 0 9 0 0 0 0 0 12.6% 1450
M20 0 1 20 0 10 0 0 0 0 0 12.5% 1450
M21 0 1 20 1 7 0 0 0 0 0 13.5% 1500
M22 0 1 20 1 8 0 0 0 0 0 13.4% 1450
M23 0 1 20 1 9 0 0 0 0 0 13.2% 1500
M24 0 1 20 1 10 0 0 0 0 0 13.1% 1500
M25 0 2 10 0 10 0 0 0 0 0 7.4% 1500
M26 0 2 10 1 9 0 0 0 0 0 8.1% 1500
M27 0 2 10 1 10 0 0 0 0 0 8.0% 1500
M28 0 2 15 1 8 0 0 0 0 0 11.2% 1500
M29 0 2 15 1 9 0 0 0 0 0 11.1% 1500
M30 0 2 15 1 10 0 0 0 0 0 11.0% 1450
M31 0 2 20 0 7 0 0 0 0 0 13.9% 1500
M32 0 2 20 0 8 0 0 0 0 0 13.7% 1450
M33 0 2 20 0 9 0 0 0 0 0 13.6% 1450
M34 0 2 20 0 10 0 0 0 0 0 13.5% 1400
M35 0 2 20 1 6 0 0 0 0 0 14.7% 1500
M36 0 2 20 1 7 0 0 0 0 0 14.5% 1500
M37 0 2 20 1 8 0 0 0 0 0 14.4% 1450
M38 0 2 20 1 9 0 0 0 0 0 14.2% 1500
M39 0 2 20 1 10 0 0 0 0 0 14.1% 1500
M40 0 3 10 0 9 0 0 0 0 0 8.5% 1500
M41 0 3 10 0 10 0 0 0 0 0 8.4% 1500
M42 0 3 10 1 9 0 0 0 0 0 9.1% 1500
M43 0 3 10 1 10 0 0 0 0 0 9.0% 1500
M44 0 3 15 1 7 0 0 0 0 0 12.3% 1500
M45 0 3 15 1 8 0 0 0 0 0 12.2% 1500
M46 0 3 15 1 9 0 0 0 0 0 12.1% 1450
M47 0 3 15 1 10 0 0 0 0 0 12.0% 1500
M48 0 3 20 0 6 0 0 0 0 0 15.0% 1500
M49 0 3 20 0 8 0 0 0 0 0 14.7% 1450
M50 0 3 20 1 6 0 0 0 0 0 15.7% 1500
M51 0 3 20 1 8 0 0 0 0 0 15.4% 1450
M52 0 3 20 1 10 0 0 0 0 0 15.1% 1500
M53 0 4 5 1 10 0 0 0 0 0 7.1% 1500
M54 0 4 10 0 9 0 0 0 0 0 9.4% 1500
M55 0 4 10 0 10 0 0 0 0 0 9.3% 1500
M56 0 4 10 1 8 0 0 0 0 0 10.1% 1500
M57 0 4 10 1 9 0 0 0 0 0 10.0% 1500
M58 0 4 10 1 10 0 0 0 0 0 10.0% 1500
M59 0 4 15 1 7 0 0 0 0 0 13.4% 1500
M60 0 4 15 1 8 0 0 0 0 0 13.2% 1500 M61 0 4 15 1 9 0 0 0 0 0 13.1% 1450
M62 0 4 15 1 10 0 0 0 0 0 13.0% 1500
M63 0 4 15 2 6 0 0 0 0 0 14.1% 1500
M64 0 4 20 0 6 0 0 0 0 0 16.1% 1500
M65 0 4 20 0 7 0 0 0 0 0 15.9% 1450
M66 0 4 20 0 8 0 0 0 0 0 15.8% 1450
M67 0 4 20 0 9 0 0 0 0 0 15.6% 1400
M68 0 4 20 0 10 0 0 0 0 0 15.5% 1400
M69 0 4 20 1 5 0 0 0 0 0 16.9% 1500
M70 0 4 20 1 6 0 0 0 0 0 16.8% 1500
M71 0 4 20 1 7 0 0 0 0 0 16.6% 1450
M72 0 4 20 1 8 0 0 0 0 0 16.4% 1450
M73 0 4 20 1 9 0 0 0 0 0 16.3% 1500
M74 0 4 20 1 10 0 0 0 0 0 16.1% 1500
M75 0 4 20 2 5 0 0 0 0 0 17.6% 1500
M76 0 5 5 1 10 0 0 0 0 0 8.0% 1500
M77 0 5 10 0 8 0 0 0 0 0 10.5% 1500
M78 0 5 10 0 9 0 0 0 0 0 10.4% 1500
M79 0 5 10 0 10 0 0 0 0 0 10.3% 1500
M80 0 5 10 1 8 0 0 0 0 0 11.1% 1500
M81 0 5 10 1 9 0 0 0 0 0 11.0% 1500
M82 0 5 10 1 10 0 0 0 0 0 10.9% 1450
M83 0 5 15 1 6 0 0 0 0 0 14.5% 1500
M84 0 5 15 1 7 0 0 0 0 0 14.4% 1500
M85 0 5 15 1 8 0 0 0 0 0 14.2% 1450
M86 0 5 15 1 9 0 0 0 0 0 14.1% 1450
M87 0 5 15 1 10 0 0 0 0 0 14.0% 1500
M88 0 5 15 2 6 0 0 0 0 0 15.2% 1500
M89 0 5 20 0 5 0 0 0 0 0 17.3% 1500
M90 0 5 20 0 6 0 0 0 0 0 17.1% 1500
M91 0 5 20 0 7 0 0 0 0 0 17.0% 1450
M92 0 5 20 0 8 0 0 0 0 0 16.8% 1450
M93 0 5 20 0 9 0 0 0 0 0 16.6% 1400
M94 0 5 20 0 10 0 0 0 0 0 16.5% 1400
M95 0 5 20 1 5 0 0 0 0 0 18.0% 1500
M96 0 5 20 1 6 0 0 0 0 0 17.8% 1500
M97 0 5 20 1 7 0 0 0 0 0 17.6% 1450
M98 0 5 20 1 8 0 0 0 0 0 17.5% 1500
M99 0 5 20 1 9 0 0 0 0 0 17.3% 1500
M100 0 5 20 1 10 0 0 0 0 0 17.1% 1500
M101 0 5 20 2 5 0 0 0 0 0 18.7% 1500
M102 4 0 0 0 0 0 0 2 0 6 5.1% 1350
M103 4 0 0 0 0 0 0 2 2 6 5.7% 1400 M104 4 0 0 0 0 0 0 2 4 4 5.2% 1500
M105 4 0 0 0 0 0 0 2 4 6 6.3% 1450
M106 4 0 0 0 0 0 0 4 0 4 5.9% 1350
M107 4 0 0 0 0 0 0 4 0 6 7.0% 1350
M108 4 0 0 0 0 0 0 4 2 2 5.4% 1400
M109 4 0 0 0 0 0 0 4 2 4 6.5% 1400
MHO 4 0 0 0 0 0 0 4 2 6 7.6% 1350
Mill 4 0 0 0 0 0 0 4 4 2 6.0% 1450
M112 4 0 0 0 0 0 0 4 4 4 7.1% 1450
M113 4 0 0 0 0 0 0 4 4 6 8.3% 1450
M114 4 0 0 0 0 0 0 6 0 0 5.6% 1350
M115 4 0 0 0 0 0 0 6 0 2 6.7% 1350
M116 4 0 0 0 0 0 0 6 0 4 7.8% 1350
M117 4 0 0 0 0 0 0 6 0 6 8.9% 1400
M118 4 0 0 0 0 0 0 6 2 0 6.2% 1400
M119 4 0 0 0 0 0 0 6 2 2 7.3% 1400
M120 4 0 0 0 0 0 0 6 2 4 8.4% 1350
M121 4 0 0 0 0 0 0 6 2 6 9.6% 1400
M122 4 0 0 0 0 0 0 6 4 0 6.8% 1450
M123 4 0 0 0 0 0 0 6 4 2 7.9% 1450
M124 4 0 0 0 0 0 0 6 4 4 9.1% 1450
M125 4 0 0 0 0 0 0 6 4 6 10.2% 1450
M126 4 0 0 0 0 0 0 6 6 0 7.4% 1500
M127 4 0 0 0 0 0 0 6 6 2 8.6% 1500
M128 4 0 0 0 0 0 0 6 6 4 9.7% 1500
M129 4 0 0 0 0 0 0 6 6 6 10.9% 1500
M130 4 0 0 0 0 0 0 6 6 8 12.1% 1500
M131 4 0 0 0 0 0 0 6 6 10 13.3% 1500
M132 4 0 0 0 0 0 0 8 6 6 12.9% 1500
M133 4 0 0 0 0 0 0 8 6 8 14.1% 1500
M134 4 0 0 0 0 0 0 8 6 10 15.3% 1500
M135 4 0 0 0 0 0 0 10 6 6 14.8% 1500
M136 4 0 0 0 0 0 0 10 6 8 16.0% 1500
M137 4 0 0 0 0 0 0 10 6 10 17.3% 1500
M138 0 3 20 0 10 0 0 0 0 0 14.5% 1400
M139 0 3 20 0 10 0 0 0 0 2 15.8% 1350
M140 0 3 20 0 10 0 0 0 0 4 17.1% 1350
M141 0 3 20 0 10 0 0 0 2 0 15.3% 1400
M142 0 3 20 0 10 0 0 0 2 2 16.6% 1400
M143 0 3 20 0 10 0 0 0 2 4 18.0% 1400
M144 0 3 20 0 10 0 0 0 4 0 16.1% 1450
M145 0 3 20 0 10 0 0 0 4 2 17.5% 1450
M146 0 3 20 0 10 0 0 0 4 4 18.9% 1450 M147 0 3 20 0 10 0 0 2 0 0 16.6% 1400
M148 0 3 20 0 10 0 0 2 0 2 17.9% 1350
M149 0 3 20 0 10 0 0 2 0 4 19.3% 1350
M150 0 3 20 0 10 0 0 2 2 0 17.4% 1400
M151 0 3 20 0 10 0 0 2 2 2 18.8% 1400
M152 0 3 20 0 10 0 0 2 2 4 20.2% 1400
M153 0 3 20 0 10 0 0 2 4 0 18.3% 1450
M154 0 3 20 0 10 0 0 2 4 2 19.7% 1450
M155 0 3 20 0 10 0 0 2 4 4 21.1% 1450
M156 0 3 20 0 10 0 0 4 0 0 18.7% 1400
M157 0 3 20 0 10 0 0 4 0 2 20.1% 1350
M158 0 3 20 0 10 0 0 4 0 4 21.4% 1350
M159 0 3 20 0 10 0 0 4 2 0 19.6% 1400
M160 0 3 20 0 10 0 0 4 2 2 20.9% 1400
M161 0 3 20 0 10 0 0 4 2 4 22.4% 1400
M162 0 3 20 0 10 0 0 4 4 0 20.5% 1450
M163 0 3 20 0 10 0 0 4 4 2 21.9% 1450
M164 0 3 20 0 10 0 0 4 4 4 23.3% 1450
M165 0 3 20 0 10 0 2 0 0 0 16.7% 1400
M166 0 3 20 0 10 0 2 0 0 2 18.0% 1350
M167 0 3 20 0 10 0 2 0 0 4 19.4% 1350
M168 0 3 20 0 10 0 2 0 2 0 17.5% 1450
M169 0 3 20 0 10 0 2 0 2 2 18.9% 1450
M170 0 3 20 0 10 0 2 0 2 4 20.3% 1450
M171 0 3 20 0 10 0 2 0 4 0 18.4% 1500
M172 0 3 20 0 10 0 2 0 4 2 19.8% 1500
M173 0 3 20 0 10 0 2 0 4 4 21.2% 1500
M174 0 3 20 0 10 0 2 2 0 0 18.8% 1400
M175 0 3 20 0 10 0 2 2 0 2 20.2% 1350
M176 0 3 20 0 10 0 2 2 0 4 21.5% 1350
M177 0 3 20 0 10 0 2 2 2 0 19.7% 1450
M178 0 3 20 0 10 0 2 2 2 2 21.1% 1450
M179 0 3 20 0 10 0 2 2 2 4 22.5% 1450
M180 0 3 20 0 10 0 2 2 4 0 20.6% 1500
M181 0 3 20 0 10 0 2 2 4 2 22.0% 1500
M182 0 3 20 0 10 0 2 2 4 4 23.4% 1500
M183 0 3 20 0 10 0 2 4 0 0 20.9% 1400
M184 0 3 20 0 10 0 2 4 0 2 22.3% 1350
M185 0 3 20 0 10 0 2 4 0 4 23.7% 1350
M186 0 3 20 0 10 0 2 4 2 0 21.8% 1450
M187 0 3 20 0 10 0 2 4 2 2 23.2% 1450
M188 0 3 20 0 10 0 2 4 2 4 24.6% 1400
M189 0 3 20 0 10 0 2 4 4 0 22.7% 1450 M190 0 3 20 0 10 0 2 4 4 2 24.2% 1450
M191 0 3 20 0 10 0 2 4 4 4 25.6% 1450
M192 0 3 20 0 10 0 4 0 0 0 18.9% 1400
M193 0 3 20 0 10 0 4 0 0 2 20.3% 1400
M194 0 3 20 0 10 0 4 0 0 4 21.7% 1400
M195 0 3 20 0 10 0 4 0 2 0 19.8% 1450
M196 0 3 20 0 10 0 4 0 2 2 21.2% 1450
M197 0 3 20 0 10 0 4 0 2 4 22.6% 1450
M198 0 3 20 0 10 0 4 0 4 0 20.7% 1500
M199 0 3 20 0 10 0 4 0 4 2 22.1% 1500
M200 0 3 20 0 10 0 4 0 4 4 23.5% 1500
M201 0 3 20 0 10 0 4 2 0 0 21.0% 1400
M202 0 3 20 0 10 0 4 2 0 2 22.4% 1400
M203 0 3 20 0 10 0 4 2 0 4 23.8% 1400
M204 0 3 20 0 10 0 4 2 2 0 21.9% 1450
M205 0 3 20 0 10 0 4 2 2 2 23.3% 1450
M206 0 3 20 0 10 0 4 2 2 4 24.7% 1450
M207 0 3 20 0 10 0 4 2 4 0 22.8% 1500
M208 0 3 20 0 10 0 4 2 4 2 24.3% 1500
M209 0 3 20 0 10 0 4 2 4 4 25.7% 1500
M210 0 3 20 0 10 0 4 4 0 0 23.1% 1400
M211 0 3 20 0 10 0 4 4 0 2 24.5% 1400
M212 0 3 20 0 10 0 4 4 0 4 25.9% 1400
M213 0 3 20 0 10 0 4 4 2 0 24.1% 1450
M214 0 3 20 0 10 0 4 4 2 2 25.5% 1450
M215 0 3 20 0 10 0 4 4 2 4 26.9% 1450
M216 0 3 20 0 10 0 4 4 4 0 25.0% 1500
M217 0 3 20 0 10 0 4 4 4 2 26.4% 1500
M218 0 3 20 0 10 0 4 4 4 4 27.9% 1500
M219 0 3 20 0 10 2 0 0 0 0 15.3% 1400
M220 0 3 20 0 10 2 0 0 0 2 16.6% 1350
M221 0 3 20 0 10 2 0 0 0 4 18.0% 1350
M222 0 3 20 0 10 2 0 0 2 0 16.1% 1400
M223 0 3 20 0 10 2 0 0 2 2 17.5% 1400
M224 0 3 20 0 10 2 0 0 2 4 18.9% 1400
M225 0 3 20 0 10 2 0 0 4 0 17.0% 1450
M226 0 3 20 0 10 2 0 0 4 2 18.4% 1500
M227 0 3 20 0 10 2 0 0 4 4 19.8% 1500
M228 0 3 20 0 10 2 0 2 0 0 17.4% 1400
M229 0 3 20 0 10 2 0 2 0 2 18.8% 1350
M230 0 3 20 0 10 2 0 2 0 4 20.2% 1350
M231 0 3 20 0 10 2 0 2 2 0 18.3% 1400
M232 0 3 20 0 10 2 0 2 2 2 19.7% 1400 M233 0 3 20 0 10 2 0 2 2 4 21.1% 1400
M234 0 3 20 0 10 2 0 2 4 0 19.2% 1450
M235 0 3 20 0 10 2 0 2 4 2 20.6% 1450
M236 0 3 20 0 10 2 0 2 4 4 22.0% 1450
M237 0 3 20 0 10 2 0 4 0 0 19.6% 1400
M238 0 3 20 0 10 2 0 4 0 2 21.0% 1350
M239 0 3 20 0 10 2 0 4 0 4 22.4% 1350
M240 0 3 20 0 10 2 0 4 2 0 20.5% 1400
M241 0 3 20 0 10 2 0 4 2 2 21.9% 1400
M242 0 3 20 0 10 2 0 4 2 4 23.3% 1400
M243 0 3 20 0 10 2 0 4 4 0 21.4% 1450
M244 0 3 20 0 10 2 0 4 4 2 22.8% 1450
M245 0 3 20 0 10 2 0 4 4 4 24.3% 1450
M246 0 3 20 0 10 2 2 0 0 0 17.5% 1350
M247 0 3 20 0 10 2 2 0 0 2 18.9% 1350
M248 0 3 20 0 10 2 2 0 0 4 20.3% 1350
M249 0 3 20 0 10 2 2 0 2 0 18.4% 1450
M250 0 3 20 0 10 2 2 0 2 2 19.8% 1450
M251 0 3 20 0 10 2 2 0 2 4 21.2% 1450
M252 0 3 20 0 10 2 2 0 4 0 19.3% 1500
M253 0 3 20 0 10 2 2 0 4 2 20.7% 1500
M254 0 3 20 0 10 2 2 0 4 4 22.1% 1500
M255 0 3 20 0 10 2 2 2 0 0 19.7% 1350
M256 0 3 20 0 10 2 2 2 0 2 21.1% 1350
M257 0 3 20 0 10 2 2 2 0 4 22.5% 1350
M258 0 3 20 0 10 2 2 2 2 0 20.6% 1450
M259 0 3 20 0 10 2 2 2 2 2 22.0% 1450
M260 0 3 20 0 10 2 2 2 2 4 23.4% 1450
M261 0 3 20 0 10 2 2 2 4 0 21.5% 1500
M262 0 3 20 0 10 2 2 2 4 2 22.9% 1500
M263 0 3 20 0 10 2 2 2 4 4 24.4% 1500
M264 0 3 20 0 10 2 2 4 0 0 21.8% 1350
M265 0 3 20 0 10 2 2 4 0 2 23.2% 1350
M266 0 3 20 0 10 2 2 4 0 4 24.6% 1350
M267 0 3 20 0 10 2 2 4 2 0 22.7% 1450
M268 0 3 20 0 10 2 2 4 2 2 24.2% 1450
M269 0 3 20 0 10 2 2 4 2 4 25.6% 1450
M270 0 3 20 0 10 2 2 4 4 0 23.7% 1500
M271 0 3 20 0 10 2 2 4 4 2 25.1% 1500
M272 0 3 20 0 10 2 2 4 4 4 26.6% 1450
M273 0 3 20 0 10 2 4 0 0 0 19.8% 1400
M274 0 3 20 0 10 2 4 0 0 2 21.2% 1400
M275 0 3 20 0 10 2 4 0 0 4 22.6% 1400 M276 0 3 20 0 10 2 4 0 2 0 20.7% 1450
M277 0 3 20 0 10 2 4 0 2 2 22.1% 1450
M278 0 3 20 0 10 2 4 0 2 4 23.5% 1450
M279 0 3 20 0 10 2 4 0 4 0 21.6% 1500
M280 0 3 20 0 10 2 4 0 4 2 23.0% 1500
M281 0 3 20 0 10 2 4 0 4 4 24.5% 1500
M282 0 3 20 0 10 2 4 2 0 0 21.9% 1400
M283 0 3 20 0 10 2 4 2 0 2 23.3% 1400
M284 0 3 20 0 10 2 4 2 0 4 24.7% 1400
M285 0 3 20 0 10 2 4 2 2 0 22.9% 1450
M286 0 3 20 0 10 2 4 2 2 2 24.3% 1450
M287 0 3 20 0 10 2 4 2 2 4 25.7% 1450
M288 0 3 20 0 10 2 4 2 4 0 23.8% 1500
M289 0 3 20 0 10 2 4 2 4 2 25.2% 1500
M290 0 3 20 0 10 2 4 2 4 4 26.7% 1500
M291 0 3 20 0 10 2 4 4 0 0 24.1% 1400
M292 0 3 20 0 10 2 4 4 0 2 25.5% 1400
M293 0 3 20 0 10 2 4 4 0 4 26.9% 1400
M294 0 3 20 0 10 2 4 4 2 0 25.0% 1450
M295 0 3 20 0 10 2 4 4 2 2 26.4% 1450
M296 0 3 20 0 10 2 4 4 2 4 27.9% 1450
M297 0 3 20 0 10 2 4 4 4 0 26.0% 1500
M298 0 3 20 0 10 2 4 4 4 2 27.4% 1500
M299 0 3 20 0 10 2 4 4 4 4 28.9% 1500
M300 0 3 20 0 10 4 0 0 0 0 16.1% 1350
M301 0 3 20 0 10 4 0 0 0 2 17.5% 1350
M302 0 3 20 0 10 4 0 0 0 4 18.9% 1350
M303 0 3 20 0 10 4 0 0 2 0 17.0% 1400
M304 0 3 20 0 10 4 0 0 2 2 18.4% 1400
M305 0 3 20 0 10 4 0 0 2 4 19.8% 1450
M306 0 3 20 0 10 4 0 0 4 0 17.8% 1500
M307 0 3 20 0 10 4 0 0 4 2 19.3% 1500
M308 0 3 20 0 10 4 0 0 4 4 20.7% 1500
M309 0 3 20 0 10 4 0 2 0 0 18.3% 1350
M310 0 3 20 0 10 4 0 2 0 2 19.7% 1350
M311 0 3 20 0 10 4 0 2 0 4 21.1% 1350
M312 0 3 20 0 10 4 0 2 2 0 19.2% 1400
M313 0 3 20 0 10 4 0 2 2 2 20.6% 1400
M314 0 3 20 0 10 4 0 2 2 4 22.0% 1400
M315 0 3 20 0 10 4 0 2 4 0 20.1% 1450
M316 0 3 20 0 10 4 0 2 4 2 21.5% 1450
M317 0 3 20 0 10 4 0 2 4 4 23.0% 1450
M318 0 3 20 0 10 4 0 4 0 0 20.5% 1350 M319 0 3 20 0 10 4 0 4 0 2 21.9% 1350
M320 0 3 20 0 10 4 0 4 0 4 23.3% 1350
M321 0 3 20 0 10 4 0 4 2 0 21.4% 1400
M322 0 3 20 0 10 4 0 4 2 2 22.8% 1400
M323 0 3 20 0 10 4 0 4 2 4 24.3% 1400
M324 0 3 20 0 10 4 0 4 4 0 22.3% 1450
M325 0 3 20 0 10 4 0 4 4 2 23.8% 1450
M326 0 3 20 0 10 4 0 4 4 4 25.3% 1450
M327 0 3 20 0 10 4 2 0 0 0 18.4% 1350
M328 0 3 20 0 10 4 2 0 0 2 19.8% 1400
M329 0 3 20 0 10 4 2 0 0 4 21.2% 1400
M330 0 3 20 0 10 4 2 0 2 0 19.3% 1450
M331 0 3 20 0 10 4 2 0 2 2 20.7% 1450
M332 0 3 20 0 10 4 2 0 2 4 22.2% 1450
M333 0 3 20 0 10 4 2 0 4 0 20.2% 1500
M334 0 3 20 0 10 4 2 0 4 2 21.7% 1500
M335 0 3 20 0 10 4 2 0 4 4 23.1% 1500
M336 0 3 20 0 10 4 2 2 0 0 20.6% 1350
M337 0 3 20 0 10 4 2 2 0 2 22.0% 1350
M338 0 3 20 0 10 4 2 2 0 4 23.4% 1350
M339 0 3 20 0 10 4 2 2 2 0 21.5% 1450
M340 0 3 20 0 10 4 2 2 2 2 22.9% 1450
M341 0 3 20 0 10 4 2 2 2 4 24.4% 1450
M342 0 3 20 0 10 4 2 2 4 0 22.4% 1500
M343 0 3 20 0 10 4 2 2 4 2 23.9% 1500
M344 0 3 20 0 10 4 2 2 4 4 25.4% 1500
M345 0 3 20 0 10 4 2 4 0 0 22.7% 1350
M346 0 3 20 0 10 4 2 4 0 2 24.2% 1350
M347 0 3 20 0 10 4 2 4 0 4 25.6% 1350
M348 0 3 20 0 10 4 2 4 2 0 23.7% 1450
M349 0 3 20 0 10 4 2 4 2 2 25.1% 1450
M350 0 3 20 0 10 4 2 4 2 4 26.6% 1450
M351 0 3 20 0 10 4 2 4 4 0 24.7% 1500
M352 0 3 20 0 10 4 2 4 4 2 26.1% 1500
M353 0 3 20 0 10 4 2 4 4 4 27.6% 1450
M354 0 3 20 0 10 4 4 0 0 0 20.7% 1400
M355 0 3 20 0 10 4 4 0 0 2 22.1% 1400
M356 0 3 20 0 10 4 4 0 0 4 23.5% 1400
M357 0 3 20 0 10 4 4 0 2 0 21.6% 1500
M358 0 3 20 0 10 4 4 0 2 2 23.0% 1500
M359 0 3 20 0 10 4 4 0 2 4 24.5% 1450
M360 0 3 20 0 10 4 4 0 4 2 24.0% 1500
M361 0 3 20 0 10 4 4 0 4 4 25.5% 1500 M362 0 3 20 0 10 4 4 2 0 0 22.9% 1400
M363 0 3 20 0 10 4 4 2 0 2 24.3% 1400
M364 0 3 20 0 10 4 4 2 0 4 25.7% 1400
M365 0 3 20 0 10 4 4 2 2 0 23.8% 1450
M366 0 3 20 0 10 4 4 2 2 2 25.2% 1450
M367 0 3 20 0 10 4 4 2 2 4 26.7% 1450
M368 0 3 20 0 10 4 4 2 4 0 24.8% 1500
M369 0 3 20 0 10 4 4 2 4 2 26.2% 1500
M370 0 3 20 0 10 4 4 2 4 4 27.7% 1500
M371 0 3 20 0 10 4 4 4 0 0 25.0% 1400
M372 0 3 20 0 10 4 4 4 0 2 26.4% 1400
M373 0 3 20 0 10 4 4 4 0 4 27.9% 1400
M374 0 3 20 0 10 4 4 4 2 0 26.0% 1450
M375 0 3 20 0 10 4 4 4 2 2 27.4% 1450
M376 0 3 20 0 10 4 4 4 2 4 28.9% 1450
M377 0 3 20 0 10 4 4 4 4 0 27.0% 1500
M378 0 3 20 0 10 4 4 4 4 2 28.5% 1500
M379 0 3 20 0 7 0 0 0 0 0 14.9% 1500
M380 0 3 20 0 9 0 0 0 0 0 14.6% 1450
M381 0 3 20 0 11 0 0 0 0 0 14.3% 1400
M382 0 3 20 0 13 0 0 0 0 0 14.1% 1400
M383 0 3 20 0 15 0 0 0 0 0 13.8% 1450
M384 0 3 20 1 7 0 0 0 0 0 15.6% 1450
M385 0 3 20 1 9 0 0 0 0 0 15.3% 1500
M386 0 3 20 1 11 0 0 0 0 0 15.0% 1500
M387 0 3 20 2 5 0 0 0 0 0 16.6% 1500
M388 0 0 11 0 10 0 0 0 0 0 6.1% 1500
M389 0 0 13 0 10 0 0 0 0 0 7.2% 1500
M390 0 0 15 0 9 0 0 0 0 0 8.5% 1500
M391 0 0 15 0 10 0 0 0 0 0 8.4% 1500
M392 0 0 17 0 8 0 0 0 0 0 9.8% 1500
M393 0 0 17 0 9 0 0 0 0 0 9.7% 1500
M394 0 0 17 0 10 0 0 0 0 0 9.6% 1450
M395 0 0 19 0 8 0 0 0 0 0 11.1% 1500
M396 0 0 19 0 9 0 0 0 0 0 11.0% 1500
M397 0 0 19 0 10 0 0 0 0 0 10.8% 1450
M398 0 0 21 0 7 0 0 0 0 0 12.5% 1500
M399 0 0 21 0 8 0 0 0 0 0 12.3% 1500
M400 0 0 21 0 9 0 0 0 0 0 12.2% 1450
M401 0 0 21 0 10 0 0 0 0 0 12.1% 1450
M402 0 0 23 0 7 0 0 0 0 0 13.8% 1500
M403 0 0 23 0 8 0 0 0 0 0 13.6% 1450
M404 0 0 23 0 9 0 0 0 0 0 13.5% 1450 M405 0 0 23 0 10 0 0 0 0 0 13.3% 1400
M406 0 0 25 0 6 0 0 0 0 0 15.2% 1500
M407 0 0 25 0 7 0 0 0 0 0 15.1% 1500
M408 0 0 25 0 8 0 0 0 0 0 14.9% 1450
M409 0 0 25 0 9 0 0 0 0 0 14.8% 1400
M410 0 0 25 0 10 0 0 0 0 0 14.6% 1400
M411 0 0 27 0 6 0 0 0 0 0 16.6% 1500
M412 0 0 27 0 7 0 0 0 0 0 16.4% 1450
M413 0 0 27 0 8 0 0 0 0 0 16.3% 1450
M414 0 0 27 0 9 0 0 0 0 0 16.1% 1400
M415 0 0 27 0 10 0 0 0 0 0 15.9% 1400
M416 0 0 29 0 5 0 0 0 0 0 18.2% 1500
M417 0 0 29 0 6 0 0 0 0 0 18.0% 1500
M418 0 0 29 0 7 0 0 0 0 0 17.8% 1450
M419 0 0 29 0 8 0 0 0 0 0 17.6% 1400
M420 0 0 29 0 9 0 0 0 0 0 17.4% 1400
M421 0 0 29 0 10 0 0 0 0 0 17.3% 1400
M422 0 1 11 0 10 0 0 0 0 0 7.0% 1500
M423 0 1 13 0 9 0 0 0 0 0 8.3% 1500
M424 0 1 13 0 10 0 0 0 0 0 8.2% 1500
M425 0 1 15 0 9 0 0 0 0 0 9.5% 1500
M426 0 1 15 0 10 0 0 0 0 0 9.4% 1500
M427 0 1 17 0 8 0 0 0 0 0 10.8% 1500
M428 0 1 17 0 9 0 0 0 0 0 10.7% 1500
M429 0 1 17 0 10 0 0 0 0 0 10.6% 1450
M430 0 1 19 0 7 0 0 0 0 0 12.2% 1500
M431 0 1 19 0 8 0 0 0 0 0 12.1% 1500
M432 0 1 19 0 9 0 0 0 0 0 12.0% 1450
M433 0 1 19 0 10 0 0 0 0 0 11.8% 1450
M434 0 1 21 0 7 0 0 0 0 0 13.5% 1500
M435 0 1 21 0 8 0 0 0 0 0 13.4% 1450
M436 0 1 21 0 9 0 0 0 0 0 13.2% 1450
M437 0 1 21 0 10 0 0 0 0 0 13.1% 1400
M438 0 1 23 0 6 0 0 0 0 0 14.9% 1500
M439 0 1 23 0 7 0 0 0 0 0 14.8% 1500
M440 0 1 23 0 8 0 0 0 0 0 14.6% 1450
M441 0 1 23 0 9 0 0 0 0 0 14.5% 1450
M442 0 1 23 0 10 0 0 0 0 0 14.4% 1400
M443 0 1 25 0 6 0 0 0 0 0 16.3% 1500
M444 0 1 25 0 7 0 0 0 0 0 16.1% 1450
M445 0 1 25 0 8 0 0 0 0 0 16.0% 1450
M446 0 1 25 0 9 0 0 0 0 0 15.8% 1400
M447 0 1 25 0 10 0 0 0 0 0 15.7% 1400 M448 0 1 27 0 5 0 0 0 0 0 17.9% 1500
M449 0 1 27 0 6 0 0 0 0 0 17.7% 1500
M450 0 1 27 0 7 0 0 0 0 0 17.5% 1450
M451 0 1 27 0 8 0 0 0 0 0 17.3% 1400
M452 0 1 27 0 9 0 0 0 0 0 17.1% 1400
M453 0 1 27 0 10 0 0 0 0 0 17.0% 1400
M454 0 1 29 0 5 0 0 0 0 0 19.3% 1500
M455 0 1 29 0 6 0 0 0 0 0 19.1% 1450
M456 0 1 29 0 7 0 0 0 0 0 18.9% 1450
M457 0 1 29 0 8 0 0 0 0 0 18.7% 1400
M458 0 1 29 0 9 0 0 0 0 0 18.5% 1400
M459 0 1 29 0 10 0 0 0 0 0 18.3% 1400
M460 0 2 9 0 10 0 0 0 0 0 6.8% 1500
M461 0 2 11 0 9 0 0 0 0 0 8.1% 1500
M462 0 2 11 0 10 0 0 0 0 0 8.0% 1500
M463 0 2 13 0 9 0 0 0 0 0 9.3% 1500
M464 0 2 13 0 10 0 0 0 0 0 9.2% 1500
M465 0 2 15 0 8 0 0 0 0 0 10.6% 1500
M466 0 2 15 0 9 0 0 0 0 0 10.5% 1500
M467 0 2 15 0 10 0 0 0 0 0 10.4% 1450
M468 0 2 17 0 7 0 0 0 0 0 11.9% 1500
M469 0 2 17 0 8 0 0 0 0 0 11.8% 1500
M470 0 2 17 0 9 0 0 0 0 0 11.7% 1450
M471 0 2 17 0 10 0 0 0 0 0 11.6% 1450
M472 0 2 19 0 7 0 0 0 0 0 13.2% 1500
M473 0 2 19 0 8 0 0 0 0 0 13.1% 1500
M474 0 2 19 0 9 0 0 0 0 0 13.0% 1450
M475 0 2 19 0 10 0 0 0 0 0 12.8% 1450
M476 0 2 21 0 6 0 0 0 0 0 14.7% 1500
M477 0 2 21 0 7 0 0 0 0 0 14.5% 1500
M478 0 2 21 0 8 0 0 0 0 0 14.4% 1450
M479 0 2 21 0 9 0 0 0 0 0 14.2% 1450
M480 0 2 21 0 10 0 0 0 0 0 14.1% 1400
M481 0 2 23 0 6 0 0 0 0 0 16.0% 1500
M482 0 2 23 0 7 0 0 0 0 0 15.8% 1450
M483 0 2 23 0 8 0 0 0 0 0 15.7% 1450
M484 0 2 23 0 9 0 0 0 0 0 15.5% 1400
M485 0 2 23 0 10 0 0 0 0 0 15.4% 1400
M486 0 2 25 0 5 0 0 0 0 0 17.5% 1500
M487 0 2 25 0 6 0 0 0 0 0 17.4% 1500
M488 0 2 25 0 7 0 0 0 0 0 17.2% 1450
M489 0 2 25 0 8 0 0 0 0 0 17.0% 1400
M490 0 2 25 0 9 0 0 0 0 0 16.8% 1400 M491 0 2 25 0 10 0 0 0 0 0 16.7% 1350
M492 0 2 27 0 5 0 0 0 0 0 18.9% 1500
M493 0 2 27 0 6 0 0 0 0 0 18.7% 1450
M494 0 2 27 0 7 0 0 0 0 0 18.6% 1450
M495 0 2 27 0 8 0 0 0 0 0 18.4% 1400
M496 0 2 27 0 9 0 0 0 0 0 18.2% 1400
M497 0 2 27 0 10 0 0 0 0 0 18.0% 1400
M498 0 2 29 0 5 0 0 0 0 0 20.4% 1500
M499 0 2 29 0 6 0 0 0 0 0 20.2% 1450
M500 0 2 29 0 7 0 0 0 0 0 19.9% 1400
M501 0 2 29 0 8 0 0 0 0 0 19.7% 1400
M502 0 2 29 0 9 0 0 0 0 0 19.5% 1400
M503 0 2 29 0 10 0 0 0 0 0 19.3% 1400
M504 0 3 7 0 10 0 0 0 0 0 6.7% 1500
M505 0 3 9 0 10 0 0 0 0 0 7.8% 1500
M506 0 3 11 0 9 0 0 0 0 0 9.1% 1500
M507 0 3 11 0 10 0 0 0 0 0 9.0% 1500
M508 0 3 13 0 8 0 0 0 0 0 10.4% 1500
M509 0 3 13 0 9 0 0 0 0 0 10.3% 1500
M510 0 3 13 0 10 0 0 0 0 0 10.2% 1450
M511 0 3 15 0 8 0 0 0 0 0 11.6% 1500
M512 0 3 15 0 9 0 0 0 0 0 11.5% 1500
M513 0 3 15 0 10 0 0 0 0 0 11.4% 1450
M514 0 3 17 0 7 0 0 0 0 0 13.0% 1500
M515 0 3 17 0 8 0 0 0 0 0 12.8% 1500
M516 0 3 17 0 9 0 0 0 0 0 12.7% 1450
M517 0 3 17 0 10 0 0 0 0 0 12.6% 1450
M518 0 3 19 0 6 0 0 0 0 0 14.4% 1500
M519 0 3 19 0 7 0 0 0 0 0 14.2% 1500
M520 0 3 19 0 8 0 0 0 0 0 14.1% 1450
M521 0 3 19 0 9 0 0 0 0 0 14.0% 1450
M522 0 3 19 0 10 0 0 0 0 0 13.8% 1400
M523 0 3 21 0 6 0 0 0 0 0 15.7% 1500
M524 0 3 21 0 7 0 0 0 0 0 15.6% 1500
M525 0 3 21 0 8 0 0 0 0 0 15.4% 1450
M526 0 3 21 0 9 0 0 0 0 0 15.2% 1400
M527 0 3 21 0 10 0 0 0 0 0 15.1% 1400
M528 0 3 23 0 5 0 0 0 0 0 17.2% 1500
M529 0 3 23 0 6 0 0 0 0 0 17.1% 1500
M530 0 3 23 0 7 0 0 0 0 0 16.9% 1450
M531 0 3 23 0 8 0 0 0 0 0 16.7% 1450
M532 0 3 23 0 9 0 0 0 0 0 16.5% 1400
M533 0 3 23 0 10 0 0 0 0 0 16.4% 1400 M534 0 3 25 0 5 0 0 0 0 0 18.6% 1500
M535 0 3 25 0 6 0 0 0 0 0 18.4% 1450
M536 0 3 25 0 7 0 0 0 0 0 18.2% 1450
M537 0 3 25 0 8 0 0 0 0 0 18.0% 1400
M538 0 3 25 0 9 0 0 0 0 0 17.9% 1400
M539 0 3 25 0 10 0 0 0 0 0 17.7% 1350
M540 0 3 27 0 5 0 0 0 0 0 20.0% 1500
M541 0 3 27 0 6 0 0 0 0 0 19.8% 1450
M542 0 3 27 0 7 0 0 0 0 0 19.6% 1400
M543 0 3 27 0 8 0 0 0 0 0 19.4% 1400
M544 0 3 27 0 9 0 0 0 0 0 19.2% 1350
M545 0 3 27 0 10 0 0 0 0 0 19.0% 1400
M546 0 3 29 0 4 0 0 0 0 0 21.7% 1500
M547 0 3 29 0 5 0 0 0 0 0 21.5% 1500
M548 0 3 29 0 6 0 0 0 0 0 21.2% 1450
M549 0 3 29 0 7 0 0 0 0 0 21.0% 1400
M550 0 3 29 0 8 0 0 0 0 0 20.8% 1400
M551 0 3 29 0 9 0 0 0 0 0 20.6% 1400
M552 0 3 29 0 10 0 0 0 0 0 20.4% 1400
M553 0 4 7 0 10 0 0 0 0 0 7.6% 1500
M554 0 4 9 0 9 0 0 0 0 0 8.8% 1500
M555 0 4 9 0 10 0 0 0 0 0 8.8% 1500
M556 0 4 11 0 9 0 0 0 0 0 10.0% 1500
M557 0 4 11 0 10 0 0 0 0 0 9.9% 1500
M558 0 4 13 0 8 0 0 0 0 0 11.3% 1500
M559 0 4 13 0 9 0 0 0 0 0 11.2% 1500
M560 0 4 13 0 10 0 0 0 0 0 11.1% 1450
M561 0 4 15 0 7 0 0 0 0 0 12.7% 1500
M562 0 4 15 0 8 0 0 0 0 0 12.6% 1500
M563 0 4 15 0 9 0 0 0 0 0 12.5% 1450
M564 0 4 15 0 10 0 0 0 0 0 12.3% 1450
M565 0 4 17 0 7 0 0 0 0 0 14.0% 1500
M566 0 4 17 0 8 0 0 0 0 0 13.8% 1450
M567 0 4 17 0 9 0 0 0 0 0 13.7% 1450
M568 0 4 17 0 10 0 0 0 0 0 13.6% 1400
M569 0 4 19 0 6 0 0 0 0 0 15.4% 1500
M570 0 4 19 0 7 0 0 0 0 0 15.3% 1500
M571 0 4 19 0 8 0 0 0 0 0 15.1% 1450
M572 0 4 19 0 9 0 0 0 0 0 15.0% 1450
M573 0 4 19 0 10 0 0 0 0 0 14.8% 1400
M574 0 4 21 0 6 0 0 0 0 0 16.8% 1500
M575 0 4 21 0 7 0 0 0 0 0 16.6% 1450
M576 0 4 21 0 8 0 0 0 0 0 16.4% 1450 M577 0 4 21 0 9 0 0 0 0 0 16.3% 1400
M578 0 4 21 0 10 0 0 0 0 0 16.1% 1400
M579 0 4 23 0 5 0 0 0 0 0 18.3% 1500
M580 0 4 23 0 6 0 0 0 0 0 18.1% 1500
M581 0 4 23 0 7 0 0 0 0 0 17.9% 1450
M582 0 4 23 0 8 0 0 0 0 0 17.7% 1400
M583 0 4 23 0 9 0 0 0 0 0 17.6% 1400
M584 0 4 23 0 10 0 0 0 0 0 17.4% 1350
M585 0 4 25 0 5 0 0 0 0 0 19.7% 1500
M586 0 4 25 0 6 0 0 0 0 0 19.5% 1450
M587 0 4 25 0 7 0 0 0 0 0 19.3% 1450
M588 0 4 25 0 8 0 0 0 0 0 19.1% 1400
M589 0 4 25 0 9 0 0 0 0 0 18.9% 1350
M590 0 4 25 0 10 0 0 0 0 0 18.7% 1350
M591 0 4 27 0 4 0 0 0 0 0 21.3% 1500
M592 0 4 27 0 5 0 0 0 0 0 21.1% 1500
M593 0 4 27 0 6 0 0 0 0 0 20.9% 1450
M594 0 4 27 0 7 0 0 0 0 0 20.7% 1400
M595 0 4 27 0 8 0 0 0 0 0 20.5% 1400
M596 0 4 27 0 9 0 0 0 0 0 20.2% 1350
M597 0 4 27 0 10 0 0 0 0 0 20.0% 1400
M598 0 4 29 0 4 0 0 0 0 0 22.8% 1500
M599 0 4 29 0 5 0 0 0 0 0 22.5% 1450
M600 0 4 29 0 6 0 0 0 0 0 22.3% 1450
M601 0 4 29 0 7 0 0 0 0 0 22.1% 1400
M602 0 4 29 0 8 0 0 0 0 0 21.8% 1400
M603 0 4 29 0 9 0 0 0 0 0 21.6% 1400
M604 0 4 29 0 10 0 0 0 0 0 21.4% 1400
M605 0 5 5 0 10 0 0 0 0 0 7.4% 1500
M606 0 5 7 0 10 0 0 0 0 0 8.6% 1500
M607 0 5 9 0 9 0 0 0 0 0 9.8% 1500
M608 0 5 9 0 10 0 0 0 0 0 9.7% 1500
M609 0 5 11 0 8 0 0 0 0 0 11.1% 1500
M610 0 5 11 0 9 0 0 0 0 0 11.0% 1500
M611 0 5 11 0 10 0 0 0 0 0 10.9% 1450
M612 0 5 13 0 7 0 0 0 0 0 12.5% 1500
M613 0 5 13 0 8 0 0 0 0 0 12.3% 1500
M614 0 5 13 0 9 0 0 0 0 0 12.2% 1450
M615 0 5 13 0 10 0 0 0 0 0 12.1% 1450
M616 0 5 15 0 7 0 0 0 0 0 13.7% 1500
M617 0 5 15 0 8 0 0 0 0 0 13.6% 1500
M618 0 5 15 0 9 0 0 0 0 0 13.4% 1450
M619 0 5 15 0 10 0 0 0 0 0 13.3% 1450 M620 0 5 17 0 6 0 0 0 0 0 15.1% 1500
M621 0 5 17 0 7 0 0 0 0 0 15.0% 1500
M622 0 5 17 0 8 0 0 0 0 0 14.8% 1450
M623 0 5 17 0 9 0 0 0 0 0 14.7% 1450
M624 0 5 17 0 10 0 0 0 0 0 14.6% 1400
M625 0 5 19 0 6 0 0 0 0 0 16.5% 1500
M626 0 5 19 0 7 0 0 0 0 0 16.3% 1450
M627 0 5 19 0 8 0 0 0 0 0 16.1% 1450
M628 0 5 19 0 9 0 0 0 0 0 16.0% 1400
M629 0 5 19 0 10 0 0 0 0 0 15.8% 1400
M630 0 5 21 0 5 0 0 0 0 0 18.0% 1500
M631 0 5 21 0 6 0 0 0 0 0 17.8% 1500
M632 0 5 21 0 7 0 0 0 0 0 17.6% 1450
M633 0 5 21 0 8 0 0 0 0 0 17.4% 1450
M634 0 5 21 0 9 0 0 0 0 0 17.3% 1400
M635 0 5 21 0 10 0 0 0 0 0 17.1% 1400
M636 0 5 23 0 5 0 0 0 0 0 19.4% 1500
M637 0 5 23 0 6 0 0 0 0 0 19.2% 1450
M638 0 5 23 0 7 0 0 0 0 0 19.0% 1450
M639 0 5 23 0 8 0 0 0 0 0 18.8% 1400
M640 0 5 23 0 9 0 0 0 0 0 18.6% 1400
M641 0 5 23 0 10 0 0 0 0 0 18.4% 1350
M642 0 5 25 0 4 0 0 0 0 0 21.0% 1500
M643 0 5 25 0 5 0 0 0 0 0 20.8% 1500
M644 0 5 25 0 6 0 0 0 0 0 20.5% 1450
M645 0 5 25 0 7 0 0 0 0 0 20.3% 1400
M646 0 5 25 0 8 0 0 0 0 0 20.1% 1400
M647 0 5 25 0 9 0 0 0 0 0 19.9% 1350
M648 0 5 25 0 10 0 0 0 0 0 19.7% 1350
M649 0 5 27 0 4 0 0 0 0 0 22.4% 1500
M650 0 5 27 0 5 0 0 0 0 0 22.2% 1450
M651 0 5 27 0 6 0 0 0 0 0 22.0% 1450
M652 0 5 27 0 7 0 0 0 0 0 21.7% 1400
M653 0 5 27 0 8 0 0 0 0 0 21.5% 1350
M654 0 5 27 0 9 0 0 0 0 0 21.3% 1350
M655 0 5 27 0 10 0 0 0 0 0 21.1% 1400
M656 0 5 29 0 4 0 0 0 0 0 23.9% 1500
M657 0 5 29 0 5 0 0 0 0 0 23.6% 1450
M658 0 5 29 0 6 0 0 0 0 0 23.4% 1400
M659 0 5 29 0 7 0 0 0 0 0 23.1% 1400
M660 0 5 29 0 8 0 0 0 0 0 22.9% 1400
M661 0 5 29 0 9 0 0 0 0 0 22.7% 1400
M662 0 5 29 0 10 0 0 0 0 0 22.4% 1400 M663 0 5 5 0 10 1 1 1 1 1 10.8% 1450
M664 0 5 5 0 10 0 0 0 1 0 7.7% 1500
M665 0 5 5 0 10 0 0 0 2 0 8.1% 1500
M666 0 5 5 0 10 0 0 0 3 0 8.4% 1500
M667 0 5 5 0 10 0 0 0 4 0 8.8% 1500
M668 0 5 5 0 10 0 0 1 0 0 8.4% 1500
M669 0 5 5 0 10 0 0 1 1 0 8.8% 1500
M670 0 5 5 0 10 0 0 1 2 0 9.1% 1500
M671 0 5 5 0 10 0 0 1 3 0 9.4% 1500
M672 0 5 5 0 10 0 0 1 4 0 9.8% 1500
M673 0 5 5 0 10 0 0 2 0 0 9.4% 1500
M674 0 5 5 0 10 0 0 2 1 0 9.8% 1500
M675 0 5 5 0 10 0 0 2 2 0 10.1% 1500
M676 0 5 5 0 10 0 0 2 3 0 10.5% 1500
M677 0 5 5 0 10 0 0 2 4 0 10.8% 1500
M678 0 5 5 0 10 0 0 3 0 0 10.4% 1500
M679 0 5 5 0 10 0 0 3 1 0 10.8% 1500
M680 0 5 5 0 10 0 0 3 2 0 11.1% 1500
M681 0 5 5 0 10 0 0 3 3 0 11.5% 1500
M682 0 5 5 0 10 0 0 3 4 0 11.9% 1500
M683 0 5 5 0 10 0 0 4 0 0 11.4% 1500
M684 0 5 5 0 10 0 0 4 1 0 11.8% 1500
M685 0 5 5 0 10 0 0 4 2 0 12.2% 1500
M686 0 5 5 0 10 0 0 4 3 0 12.5% 1500
M687 0 5 5 0 10 0 0 4 4 0 12.9% 1500
M688 0 5 5 0 10 0 1 0 0 0 8.5% 1500
M689 0 5 5 0 10 0 1 0 1 0 8.8% 1500
M690 0 5 5 0 10 0 1 0 2 0 9.2% 1500
M691 0 5 5 0 10 0 1 0 3 0 9.5% 1500
M692 0 5 5 0 10 0 1 0 4 0 9.9% 1500
M693 0 5 5 0 10 0 1 1 0 0 9.5% 1500
M694 0 5 5 0 10 0 1 1 1 0 9.8% 1500
M695 0 5 5 0 10 0 1 1 2 0 10.2% 1500
M696 0 5 5 0 10 0 1 1 3 0 10.5% 1500
M697 0 5 5 0 10 0 1 1 4 0 10.9% 1500
M698 0 5 5 0 10 0 1 2 0 0 10.5% 1500
M699 0 5 5 0 10 0 1 2 1 0 10.8% 1500
M700 0 5 5 0 10 0 1 2 2 0 11.2% 1500
M701 0 5 5 0 10 0 1 2 3 0 11.6% 1500
M702 0 5 5 0 10 0 1 2 4 0 11.9% 1500
M703 0 5 5 0 10 0 1 3 0 0 11.5% 1500
M704 0 5 5 0 10 0 1 3 1 0 11.8% 1500
M705 0 5 5 0 10 0 1 3 2 0 12.2% 1500 M706 0 5 5 0 10 0 1 3 3 0 12.6% 1500
M707 0 5 5 0 10 0 1 3 4 0 12.9% 1450
M708 0 5 5 0 10 0 1 4 0 0 12.5% 1500
M709 0 5 5 0 10 0 1 4 1 0 12.9% 1500
M710 0 5 5 0 10 0 1 4 2 0 13.2% 1500
M711 0 5 5 0 10 0 1 4 3 0 13.6% 1500
M712 0 5 5 0 10 0 1 4 4 0 14.0% 1450
M713 0 5 5 0 10 0 2 0 0 0 9.5% 1500
M714 0 5 5 0 10 0 2 0 1 0 9.9% 1500
M715 0 5 5 0 10 0 2 0 2 0 10.2% 1500
M716 0 5 5 0 10 0 2 0 3 0 10.6% 1450
M717 0 5 5 0 10 0 2 0 4 0 10.9% 1450
M718 0 5 5 0 10 0 2 1 0 0 10.5% 1500
M719 0 5 5 0 10 0 2 1 1 0 10.9% 1500
M720 0 5 5 0 10 0 2 1 2 0 11.3% 1500
M721 0 5 5 0 10 0 2 1 3 0 11.6% 1450
M722 0 5 5 0 10 0 2 1 4 0 12.0% 1450
M723 0 5 5 0 10 0 2 2 0 0 11.5% 1500
M724 0 5 5 0 10 0 2 2 1 0 11.9% 1500
M725 0 5 5 0 10 0 2 2 2 0 12.3% 1500
M726 0 5 5 0 10 0 2 2 3 0 12.6% 1450
M727 0 5 5 0 10 0 2 2 4 0 13.0% 1450
M728 0 5 5 0 10 0 2 3 0 0 12.5% 1500
M729 0 5 5 0 10 0 2 3 1 0 12.9% 1500
M730 0 5 5 0 10 0 2 3 2 0 13.3% 1450
M731 0 5 5 0 10 0 2 3 3 0 13.7% 1450
M732 0 5 5 0 10 0 2 3 4 0 14.0% 1450
M733 0 5 5 0 10 0 2 4 0 0 13.5% 1500
M734 0 5 5 0 10 0 2 4 1 0 13.9% 1500
M735 0 5 5 0 10 0 2 4 2 0 14.3% 1450
M736 0 5 5 0 10 0 2 4 3 0 14.7% 1450
M737 0 5 5 0 10 0 2 4 4 0 15.1% 1450
M738 0 5 5 0 10 0 3 0 0 0 10.6% 1500
M739 0 5 5 0 10 0 3 0 1 0 11.0% 1450
M740 0 5 5 0 10 0 3 0 2 0 11.3% 1450
M741 0 5 5 0 10 0 3 0 3 0 11.7% 1450
M742 0 5 5 0 10 0 3 0 4 0 12.0% 1450
M743 0 5 5 0 10 0 3 1 0 0 11.6% 1500
M744 0 5 5 0 10 0 3 1 1 0 12.0% 1450
M745 0 5 5 0 10 0 3 1 2 0 12.3% 1450
M746 0 5 5 0 10 0 3 1 3 0 12.7% 1450
M747 0 5 5 0 10 0 3 1 4 0 13.1% 1450
M748 0 5 5 0 10 0 3 2 0 0 12.6% 1450 M749 0 5 5 0 10 0 3 2 1 0 13.0% 1450
M750 0 5 5 0 10 0 3 2 2 0 13.3% 1450
M751 0 5 5 0 10 0 3 2 3 0 13.7% 1450
M752 0 5 5 0 10 0 3 2 4 0 14.1% 1450
M753 0 5 5 0 10 0 3 3 0 0 13.6% 1450
M754 0 5 5 0 10 0 3 3 1 0 14.0% 1450
M755 0 5 5 0 10 0 3 3 2 0 14.3% 1450
M756 0 5 5 0 10 0 3 3 3 0 14.7% 1450
M757 0 5 5 0 10 0 3 3 4 0 15.1% 1450
M758 0 5 5 0 10 0 3 4 0 0 14.6% 1450
M759 0 5 5 0 10 0 3 4 1 0 15.0% 1450
M760 0 5 5 0 10 0 3 4 2 0 15.4% 1450
M761 0 5 5 0 10 0 3 4 3 0 15.7% 1450
M762 0 5 5 0 10 0 3 4 4 0 16.1% 1450
M763 0 5 5 0 10 0 4 0 0 0 11.7% 1450
M764 0 5 5 0 10 0 4 0 1 0 12.0% 1450
M765 0 5 5 0 10 0 4 0 2 0 12.4% 1450
M766 0 5 5 0 10 0 4 0 3 0 12.7% 1450
M767 0 5 5 0 10 0 4 0 4 0 13.1% 1450
M768 0 5 5 0 10 0 4 1 0 0 12.7% 1450
M769 0 5 5 0 10 0 4 1 1 0 13.0% 1450
M770 0 5 5 0 10 0 4 1 2 0 13.4% 1450
M771 0 5 5 0 10 0 4 1 3 0 13.8% 1450
M772 0 5 5 0 10 0 4 1 4 0 14.1% 1450
M773 0 5 5 0 10 0 4 2 0 0 13.7% 1450
M774 0 5 5 0 10 0 4 2 1 0 14.0% 1450
M775 0 5 5 0 10 0 4 2 2 0 14.4% 1450
M776 0 5 5 0 10 0 4 2 3 0 14.8% 1450
M777 0 5 5 0 10 0 4 2 4 0 15.2% 1450
M778 0 5 5 0 10 0 4 3 0 0 14.7% 1450
M779 0 5 5 0 10 0 4 3 1 0 15.0% 1450
M780 0 5 5 0 10 0 4 3 2 0 15.4% 1450
M781 0 5 5 0 10 0 4 3 3 0 15.8% 1450
M782 0 5 5 0 10 0 4 3 4 0 16.2% 1450
M783 0 5 5 0 10 0 4 4 0 0 15.6% 1450
M784 0 5 5 0 10 0 4 4 1 0 16.0% 1450
M785 0 5 5 0 10 0 4 4 2 0 16.4% 1450
M786 0 5 5 0 10 0 4 4 3 0 16.8% 1450
M787 0 5 5 0 10 0 4 4 4 0 17.2% 1450
M788 0 5 7 0 10 0 0 0 1 0 8.9% 1500
M789 0 5 7 0 10 0 0 0 2 0 9.2% 1500
M790 0 5 7 0 10 0 0 0 3 0 9.6% 1500
M791 0 5 7 0 10 0 0 0 4 0 9.9% 1500 M792 0 5 7 0 10 0 0 1 0 0 9.6% 1500
M793 0 5 7 0 10 0 0 1 1 0 9.9% 1500
M794 0 5 7 0 10 0 0 1 2 0 10.3% 1500
M795 0 5 7 0 10 0 0 1 3 0 10.6% 1500
M796 0 5 7 0 10 0 0 1 4 0 11.0% 1500
M797 0 5 7 0 10 0 0 2 0 0 10.6% 1500
M798 0 5 7 0 10 0 0 2 1 0 10.9% 1500
M799 0 5 7 0 10 0 0 2 2 0 11.3% 1500
M800 0 5 7 0 10 0 0 2 3 0 11.7% 1500
M801 0 5 7 0 10 0 0 2 4 0 12.0% 1450
M802 0 5 7 0 10 0 0 3 0 0 11.6% 1500
M803 0 5 7 0 10 0 0 3 1 0 12.0% 1500
M804 0 5 7 0 10 0 0 3 2 0 12.3% 1500
M805 0 5 7 0 10 0 0 3 3 0 12.7% 1500
M806 0 5 7 0 10 0 0 3 4 0 13.1% 1450
M807 0 5 7 0 10 0 0 4 0 0 12.6% 1500
M808 0 5 7 0 10 0 0 4 1 0 13.0% 1500
M809 0 5 7 0 10 0 0 4 2 0 13.3% 1500
M810 0 5 7 0 10 0 0 4 3 0 13.7% 1450
M811 0 5 7 0 10 0 0 4 4 0 14.1% 1450
M812 0 5 7 0 10 0 1 0 0 0 9.6% 1500
M813 0 5 7 0 10 0 1 0 1 0 10.0% 1500
M814 0 5 7 0 10 0 1 0 2 0 10.3% 1500
M815 0 5 7 0 10 0 1 0 3 0 10.7% 1450
M816 0 5 7 0 10 0 1 0 4 0 11.0% 1450
M817 0 5 7 0 10 0 1 1 0 0 10.6% 1500
M818 0 5 7 0 10 0 1 1 1 0 11.0% 1500
M819 0 5 7 0 10 0 1 1 2 0 11.4% 1450
M820 0 5 7 0 10 0 1 1 3 0 11.7% 1450
M821 0 5 7 0 10 0 1 1 4 0 12.1% 1450
M822 0 5 7 0 10 0 1 2 0 0 11.7% 1500
M823 0 5 7 0 10 0 1 2 1 0 12.0% 1500
M824 0 5 7 0 10 0 1 2 2 0 12.4% 1450
M825 0 5 7 0 10 0 1 2 3 0 12.7% 1450
M826 0 5 7 0 10 0 1 2 4 0 13.1% 1450
M827 0 5 7 0 10 0 1 3 0 0 12.7% 1500
M828 0 5 7 0 10 0 1 3 1 0 13.0% 1500
M829 0 5 7 0 10 0 1 3 2 0 13.4% 1450
M830 0 5 7 0 10 0 1 3 3 0 13.8% 1450
M831 0 5 7 0 10 0 1 3 4 0 14.2% 1450
M832 0 5 7 0 10 0 1 4 0 0 13.7% 1500
M833 0 5 7 0 10 0 1 4 1 0 14.0% 1450
M834 0 5 7 0 10 0 1 4 2 0 14.4% 1450 M835 0 5 7 0 10 0 1 4 3 0 14.8% 1450
M836 0 5 7 0 10 0 1 4 4 0 15.2% 1450
M837 0 5 7 0 10 0 2 0 0 0 10.7% 1500
M838 0 5 7 0 10 0 2 0 1 0 11.1% 1450
M839 0 5 7 0 10 0 2 0 2 0 11.4% 1450
M840 0 5 7 0 10 0 2 0 3 0 11.8% 1450
M841 0 5 7 0 10 0 2 0 4 0 12.1% 1450
M842 0 5 7 0 10 0 2 1 0 0 11.7% 1450
M843 0 5 7 0 10 0 2 1 1 0 12.1% 1450
M844 0 5 7 0 10 0 2 1 2 0 12.4% 1450
M845 0 5 7 0 10 0 2 1 3 0 12.8% 1450
M846 0 5 7 0 10 0 2 1 4 0 13.2% 1450
M847 0 5 7 0 10 0 2 2 0 0 12.7% 1450
M848 0 5 7 0 10 0 2 2 1 0 13.1% 1450
M849 0 5 7 0 10 0 2 2 2 0 13.5% 1450
M850 0 5 7 0 10 0 2 2 3 0 13.8% 1450
M851 0 5 7 0 10 0 2 2 4 0 14.2% 1450
M852 0 5 7 0 10 0 2 3 0 0 13.7% 1450
M853 0 5 7 0 10 0 2 3 1 0 14.1% 1450
M854 0 5 7 0 10 0 2 3 2 0 14.5% 1450
M855 0 5 7 0 10 0 2 3 3 0 14.9% 1450
M856 0 5 7 0 10 0 2 3 4 0 15.2% 1450
M857 0 5 7 0 10 0 2 4 0 0 14.7% 1450
M858 0 5 7 0 10 0 2 4 1 0 15.1% 1450
M859 0 5 7 0 10 0 2 4 2 0 15.5% 1450
M860 0 5 7 0 10 0 2 4 3 0 15.9% 1450
M861 0 5 7 0 10 0 2 4 4 0 16.3% 1450
M862 0 5 7 0 10 0 3 0 0 0 11.8% 1450
M863 0 5 7 0 10 0 3 0 1 0 12.1% 1450
M864 0 5 7 0 10 0 3 0 2 0 12.5% 1450
M865 0 5 7 0 10 0 3 0 3 0 12.9% 1450
M866 0 5 7 0 10 0 3 0 4 0 13.2% 1450
M867 0 5 7 0 10 0 3 1 0 0 12.8% 1450
M868 0 5 7 0 10 0 3 1 1 0 13.1% 1450
M869 0 5 7 0 10 0 3 1 2 0 13.5% 1450
M870 0 5 7 0 10 0 3 1 3 0 13.9% 1450
M871 0 5 7 0 10 0 3 1 4 0 14.3% 1450
M872 0 5 7 0 10 0 3 2 0 0 13.8% 1450
M873 0 5 7 0 10 0 3 2 1 0 14.2% 1450
M874 0 5 7 0 10 0 3 2 2 0 14.5% 1450
M875 0 5 7 0 10 0 3 2 3 0 14.9% 1450
M876 0 5 7 0 10 0 3 2 4 0 15.3% 1450
M877 0 5 7 0 10 0 3 3 0 0 14.8% 1450 M878 0 5 7 0 10 0 3 3 1 0 15.2% 1450
M879 0 5 7 0 10 0 3 3 2 0 15.6% 1450
M880 0 5 7 0 10 0 3 3 3 0 15.9% 1450
M881 0 5 7 0 10 0 3 3 4 0 16.3% 1450
M882 0 5 7 0 10 0 3 4 0 0 15.8% 1450
M883 0 5 7 0 10 0 3 4 1 0 16.2% 1450
M884 0 5 7 0 10 0 3 4 2 0 16.6% 1450
M885 0 5 7 0 10 0 3 4 3 0 17.0% 1450
M886 0 5 7 0 10 0 3 4 4 0 17.4% 1450
M887 0 5 7 0 10 0 4 0 0 0 12.8% 1450
M888 0 5 7 0 10 0 4 0 1 0 13.2% 1450
M889 0 5 7 0 10 0 4 0 2 0 13.6% 1450
M890 0 5 7 0 10 0 4 0 3 0 14.0% 1450
M891 0 5 7 0 10 0 4 0 4 0 14.3% 1450
M892 0 5 7 0 10 0 4 1 0 0 13.8% 1450
M893 0 5 7 0 10 0 4 1 1 0 14.2% 1450
M894 0 5 7 0 10 0 4 1 2 0 14.6% 1450
M895 0 5 7 0 10 0 4 1 3 0 15.0% 1450
M896 0 5 7 0 10 0 4 1 4 0 15.4% 1450
M897 0 5 7 0 10 0 4 2 0 0 14.8% 1450
M898 0 5 7 0 10 0 4 2 1 0 15.2% 1450
M899 0 5 7 0 10 0 4 2 2 0 15.6% 1450
M900 0 5 7 0 10 0 4 2 3 0 16.0% 1450
M901 0 5 7 0 10 0 4 2 4 0 16.4% 1450
M902 0 5 7 0 10 0 4 3 0 0 15.8% 1450
M903 0 5 7 0 10 0 4 3 1 0 16.2% 1450
M904 0 5 7 0 10 0 4 3 2 0 16.6% 1450
M905 0 5 7 0 10 0 4 3 3 0 17.0% 1400
M906 0 5 7 0 10 0 4 3 4 0 17.4% 1450
M907 0 5 7 0 10 0 4 4 0 0 16.8% 1450
M908 0 5 7 0 10 0 4 4 1 0 17.2% 1450
M909 0 5 7 0 10 0 4 4 2 0 17.6% 1450
M910 0 5 7 0 10 0 4 4 3 0 18.0% 1400
M911 0 5 7 0 10 0 4 4 4 0 18.4% 1450
M912 0 5 9 0 10 0 0 0 1 0 10.1% 1500
M913 0 5 9 0 10 0 0 0 2 0 10.4% 1450
M914 0 5 9 0 10 0 0 0 3 0 10.8% 1450
M915 0 5 9 0 10 0 0 0 4 0 11.2% 1450
M916 0 5 9 0 10 0 0 1 0 0 10.7% 1500
M917 0 5 9 0 10 0 0 1 1 0 11.1% 1500
M918 0 5 9 0 10 0 0 1 2 0 11.5% 1450
M919 0 5 9 0 10 0 0 1 3 0 11.8% 1450
M920 0 5 9 0 10 0 0 1 4 0 12.2% 1450 M921 0 5 9 0 10 0 0 2 0 0 11.8% 1500
M922 0 5 9 0 10 0 0 2 1 0 12.1% 1450
M923 0 5 9 0 10 0 0 2 2 0 12.5% 1450
M924 0 5 9 0 10 0 0 2 3 0 12.9% 1450
M925 0 5 9 0 10 0 0 2 4 0 13.2% 1450
M926 0 5 9 0 10 0 0 3 0 0 12.8% 1500
M927 0 5 9 0 10 0 0 3 1 0 13.2% 1450
M928 0 5 9 0 10 0 0 3 2 0 13.5% 1450
M929 0 5 9 0 10 0 0 3 3 0 13.9% 1450
M930 0 5 9 0 10 0 0 3 4 0 14.3% 1450
M931 0 5 9 0 10 0 0 4 0 0 13.8% 1500
M932 0 5 9 0 10 0 0 4 1 0 14.2% 1450
[0047] In some embodiments, the alloy can possess a low FCC-BCC transition temperature. This criteria can be related to the likelihood of the alloy to retain an austenitic structure when deposited and thus be 'readable' by certain measuring devices, as discussed further below. Readable coatings can be non-magnetic and thus the thickness can be measured with standard paint thickness gauges. This can be advantageous for many thermal spray applications.
Performance Criteria:
[0048] In some embodiments, the alloy can be described by performance criteria. The performance criteria that can be advantageous to the field of thermal spray hardfacing is the hardness, wear resistance, coating adhesion, and corrosion resistance.
[0049] In some embodiments, the Vickers hardness of the coating can be 400 or above (or about 400 or above). In some embodiments, the Vickers hardness of the coating can be 500 or above (or about 500 or above). In some embodiments, the Vickers hardness can be 550 or above (or about 550 or above).In some embodiments, the Vickers hardness can be 600 or above (or about 600 or above). The specific microstructure disclosed herein can allow for embodiments of the alloys to have high hardness.
[0050] In some embodiments, the adhesion strength of the coating can be 5,000 psi or above (or about 5,000 psi or above). In some embodiments, the adhesion strength of the coating can be 7,500 psi or above (or about 7,500 psi or above). In some embodiments, the adhesion strength of the coating can be 10,000 psi or above (or about 10,000 psi or above).
[0051] In some embodiments, the abrasion resistance of the coating as measured via ASTM G65B testing can be 0.8 grams loss or below (or about 0.8 grams loss or below). In some embodiments, the abrasion resistance of the coating as measured via ASTM G65B testing can be 0.6 grams loss or below (or about 0.6 grams loss or below). In some embodiments, the abrasion resistance of the coating as measured via ASTM G65B testing can be 0.4 grams loss or below (or about 0.4 grams loss or below).
[0052] In some embodiments, the adhesive wear resistance of the coating as measured via ASTM G77 testing, hereby incorporated by reference in its entirety, can be 2 mm 3 volume loss or below (or about 2 mm 3 volume loss or below). In some embodiments, the adhesive wear resistance of the coating as measured via ASTM Gil testing can be 0.5 mm 3 volume loss or below (or about 0.5 mm 3 volume loss or below). In some embodiments, the adhesive wear resistance of the coating as measured via ASTM Gil testing can be 0.1 mm 3 volume loss or below (or about 0.1 mm 3 volume loss or below).
[0053] In some embodiments, the alloy can exhibit similar performance to conventional Cr-bearing thermal spray materials used for hardfacing. The most exemplary and well used thermal spray hardfacing material possesses a chemical composition of Fe: BAL, Cr: 29, Si: 1, Mn: 2, B: 4, which is generally referred to in the industry as Armacor M. Armacor M possesses the following properties which are relevant to thermal spray hardfacing: adhesion of about 8,000 psi, ASTM G65B mass loss of about 0.37 grams, ASTM G77 volume loss of about 0.07 mm , and position in the galvanic series in saltwater of about -500 mV. Armacor M is primarily made of Fe, Cr, and B, has a high melting temperature, and has no large atoms.
[0054] In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion and abrasive wear resistance as Armacor, where 'similar' equates to within 25% (or within about 25%) of the measured performance properties of Armacor M or better. In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion, abrasive wear resistance, and adhesive wear resistance as Armacor, where 'similar' equates to within 25% (or within about 25%) of the measured performance properties of Armacor M or better. In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion, abrasive wear resistance, adhesive wear resistance, and corrosion resistance as Armacor, where 'similar' equates to within 25% (or within about 25%) of the measured performance properties of Armacor M or better.
[0055] In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion and abrasive wear resistance as Armacor, where 'similar' equates to within 10% (or within about 10%) of the measured performance properties of Armacor M or better. In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion, abrasive wear resistance, and adhesive wear resistance as Armacor, where 'similar' equates to within 10% (or within about 10%) of the measured performance properties of Armacor M or better. In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion, abrasive wear resistance, adhesive wear resistance, and corrosion resistance as Armacor, where 'similar' equates to within 10% (or within about 10%) of the measured performance properties of Armacor M or better.
[0056] In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion and abrasive wear resistance as Armacor, where 'similar' equates to within 1% (or within about 1%) of the measured performance properties of Armacor M or better. In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion, abrasive wear resistance, and adhesive wear resistance as Armacor, where 'similar' equates to within 1% (or within about 1%) of the measured performance properties of Armacor M or better. In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion, abrasive wear resistance, adhesive wear resistance, and corrosion resistance as Armacor, where 'similar' equates to within 1% (or within about 1%) of the measured performance properties of Armacor M or better.
[0057] In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion and abrasive wear resistance as Armacor, where 'similar' equates to within 0% (or within about 0%) of the measured performance properties of Armacor M or better. In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion, abrasive wear resistance, and adhesive wear resistance as Armacor, where 'similar' equates to within 0% (or within about 0%) of the measured performance properties of Armacor M or better. In some embodiments of this disclosure, the alloys can exhibit similar coating adhesion, abrasive wear resistance, adhesive wear resistance, and corrosion resistance as Armacor, where 'similar' equates to within 0% (or within about 0%) of the measured performance properties of Armacor M or better.
[0058] In some embodiments, the thermal spray coating can be 'readable'. A readable coating produces consistent thickness measurements with an Elcometer™ thickness gauge, or similar device, when properly calibrated. Armacor M is not a readable alloy, unlike embodiments of the disclosure, as it is magnetic.
[0059] As a standard to verify 'readability', a 25 mil standard thermal spray coupon is used for measurements. In some embodiments, the coating thickness measurement can be accurate to within 5 mils (or within about 5 mils) of the actual physical thickness. In some embodiments, the coating thickness measurement can be accurate to within 3.5 mils (or within about 3.5 mils) of the actual physical thickness. In some embodiments, the coating thickness measurement can be accurate to within 2 mils (or within about 2 mils) of the actual physical thickness.
[0060] In some embodiments, consistent measurements according to the above criteria, + 5 mils to actual physical thickness, can be made after the coating has been exposed to heat for an extended period of time. This can be advantageous because when the alloy is heated, there is a potential for a magnetic phase to precipitate out, which would make the alloy non-readable. This can be especially true for amorphous alloys which may be readable in amorphous form, but may crystallize in a different environment due to heat. Thus, in some embodiments, the alloy can remain non-magnetic even after being exposed to heat for a substantial time period.
[0061] In some embodiments, the coating can be 'readable' after exposure to HOOK (or about HOOK) for 2 hours (or about 2 hours) and cooled at a rate of less than 10K/S (or less than about 10K/S). In some embodiments, the coating can be 'readable' after exposure to 1300K (or about 1300K) for 2 hours (or about 2 hours) and cooled at a rate of less than 10K/S (or less than 10K/S). In some embodiments, the coating can be 'readable' after exposure to 1500K (r about 1500K) for 2 hours (or about 2 hours) and cooled at a rate of less than 10K/S (or less than about 10K/S). It is expected that increased exposure times above 2 hours will not continue to affect the final 'readability' of these materials.
Table 3: List of alloy compositions and thermodynamic and kinetic parameters which meet the criteria described in this disclosure, including the criteria pertained to coating non- magnetism and readability. Large atom % is the total atom % of elements larger than iron, Trans T is the FCC-BCC transition temperature and melt T is the melting temperature of the alloy.
No. C Mn Mo Ni Si Large Atom % Trans T Melt T
M934 0 19 20 0 10 30% 1000 1300
M935 0 20 19 0 10 31% 1000 1300
M936 0 20 20 0 10 31% 900 1300
M937 0 13 11 4 5 20% 800 1500
M938 0 13 11 5 5 20% 800 1500
M939 0 13 13 3 5 21% 800 1500
M940 0 13 13 4 5 21% 800 1500
M941 0 13 13 5 5 21% 800 1500
M942 0 13 13 5 6 21% 850 1450
M943 0 13 15 2 5 22% 800 1500
M944 0 13 15 3 5 22% 800 1500
M945 0 13 15 4 5 22% 800 1500
M946 0 13 15 4 6 22% 850 1450
M947 0 13 15 5 5 22% 800 1500
M948 0 13 15 5 6 22% 850 1450
M949 0 16 7 1 6 20% 850 1500
M950 0 16 7 2 6 20% 850 1500
M951 0 16 7 3 6 20% 850 1500
M952 0 16 7 3 7 20% 900 1500
M953 0 16 7 4 6 20% 800 1500
M954 0 16 7 4 7 20% 900 1500
M955 0 16 7 5 6 20% 800 1500
M956 0 16 7 5 7 20% 900 1500
M957 0 16 9 1 6 21% 850 1500
M958 0 16 9 2 6 21% 800 1500
M959 0 16 9 2 7 21% 900 1450
M960 0 16 9 3 6 21% 800 1500
M961 0 16 9 3 7 21% 900 1450
M962 0 16 9 4 6 21% 800 1500
M963 0 16 9 4 7 21% 900 1450 M964 0 16 9 4 8 21% 1000 1450
M965 0 16 9 5 5 21% 750 1500
M966 0 16 9 5 6 21% 800 1500
M967 0 16 9 5 7 21% 850 1450
M968 0 16 9 5 8 21% 1000 1450
M969 0 16 11 0 5 23% 800 1500
M970 0 16 11 1 5 23% 800 1500
M971 0 16 11 1 6 22% 850 1500
M972 0 16 11 1 7 22% 900 1450
M973 0 16 11 2 5 23% 750 1500
M974 0 16 11 2 6 22% 800 1500
M975 0 16 11 2 7 22% 900 1450
M976 0 16 11 3 5 23% 750 1500
M977 0 16 11 3 6 22% 800 1500
M978 0 16 11 3 7 22% 850 1450
M979 0 16 11 3 8 22% 1000 1400
M980 0 16 11 4 5 23% 750 1500
M981 0 16 11 4 6 22% 800 1500
M982 0 16 11 4 7 22% 850 1450
M983 0 16 11 4 8 22% 950 1400
M984 0 16 11 5 5 23% 750 1500
M985 0 16 11 5 6 22% 800 1500
M986 0 16 11 5 7 22% 850 1450
M987 0 16 13 0 5 24% 800 1500
M988 0 16 13 1 5 24% 750 1500
M989 0 16 13 1 6 24% 800 1450
M990 0 16 13 1 7 23% 900 1450
M991 0 16 13 2 5 24% 750 1500
M992 0 16 13 2 6 24% 800 1450
M993 0 16 13 2 7 23% 850 1450
M994 0 16 13 2 8 23% 950 1400
M995 0 16 13 3 5 24% 750 1500
M996 0 16 13 3 6 24% 800 1450
M997 0 16 13 3 7 23% 850 1450
M998 0 16 13 4 5 24% 750 1500
M999 0 16 13 4 6 24% 750 1450
M 1000 0 16 13 5 5 24% 750 1500
M 1001 0 16 15 0 5 25% 750 1450
M 1002 0 16 15 0 6 25% 800 1450
M 1003 0 16 15 0 7 25% 900 1400
M 1004 0 16 15 1 5 25% 750 1450
M 1005 0 16 15 1 6 25% 800 1450
M 1006 0 16 15 1 7 25% 850 1400 M1007 0 16 15 2 5 25% 750 1450
M1008 0 16 15 2 6 25% 750 1450
M1009 0 16 15 3 5 25% 750 1450
M1010 0 16 15 3 6 25% 750 1450
M1011 0 16 15 4 5 25% 750 1450
M1012 0 19 7 0 6 23% 800 1500
M1013 0 19 7 0 7 22% 900 1450
M1014 0 19 7 1 6 23% 800 1500
M1015 0 19 7 1 7 22% 900 1450
M1016 0 19 7 2 6 23% 750 1500
M1017 0 19 7 2 7 22% 850 1450
M1018 0 19 7 2 8 22% 1000 1450
M1019 0 19 7 3 6 23% 750 1500
M1020 0 19 7 3 7 22% 850 1450
M1021 0 19 7 3 8 22% 950 1450
M1022 0 19 7 4 6 23% 750 1500
M1023 0 19 7 4 7 22% 850 1450
M1024 0 19 7 4 8 22% 950 1450
M1025 0 19 7 5 5 23% 750 1500
M1026 0 19 7 5 6 23% 750 1500
M1027 0 19 7 5 7 22% 800 1450
M1028 0 19 7 5 8 22% 950 1450
M1029 0 19 9 0 5 24% 750 1500
M1030 0 19 9 0 6 24% 800 1500
M1031 0 19 9 0 7 24% 900 1450
M1032 0 19 9 1 5 24% 750 1500
M1033 0 19 9 1 6 24% 750 1500
M1034 0 19 9 1 7 24% 850 1450
M1035 0 19 9 1 8 24% 1000 1400
M1036 0 19 9 2 5 24% 750 1500
M1037 0 19 9 2 6 24% 750 1500
M1038 0 19 9 2 7 24% 800 1450
M1039 0 19 9 2 8 24% 950 1400
M1040 0 19 9 3 5 24% 700 1500
M1041 0 19 9 3 6 24% 750 1500
M1042 0 19 9 3 7 24% 800 1450
M1043 0 19 9 3 8 24% 900 1400
M1044 0 19 9 4 5 24% 700 1500
M1045 0 19 9 4 6 24% 750 1500
M1046 0 19 9 4 7 24% 800 1450
M1047 0 19 9 5 5 24% 700 1500
M1048 0 19 9 5 6 24% 750 1500
M1049 0 19 11 0 5 26% 700 1500 M1050 0 19 11 0 6 25% 750 1450
M1051 0 19 11 0 7 25% 850 1450
M1052 0 19 11 0 8 25% 1000 1400
M1053 0 19 11 1 5 26% 700 1500
M1054 0 19 11 1 6 25% 750 1450
M1055 0 19 11 1 7 25% 800 1450
M1056 0 19 11 1 8 25% 950 1400
M1057 0 19 11 2 5 26% 700 1500
M1058 0 19 11 2 6 25% 750 1450
M1059 0 19 11 2 7 25% 800 1450
M1060 0 19 11 3 5 26% 700 1500
M1061 0 19 11 3 6 25% 750 1450
M1062 0 19 11 3 7 25% 800 1450
M1063 0 19 11 4 5 26% 700 1500
M1064 0 19 11 4 6 25% 750 1450
M1065 0 19 11 5 5 26% 700 1500
M1066 0 19 13 0 5 27% 700 1500
M1067 0 19 13 0 6 27% 750 1450
M1068 0 19 13 0 7 26% 800 1400
M1069 0 19 13 1 5 27% 700 1450
M1070 0 19 13 1 6 27% 750 1450
M1071 0 19 13 2 5 27% 700 1450
M1072 0 19 13 3 5 27% 700 1450
M1073 0 19 15 0 5 28% 700 1450
M1074 0 19 15 0 6 28% 750 1400
M1075 0 19 15 1 5 28% 700 1450
M1076 0 22 7 0 5 26% 700 1500
M1077 0 22 7 0 6 26% 750 1500
M1078 0 22 7 0 7 25% 850 1450
M1079 0 22 7 0 8 25% 1000 1400
M1080 0 22 7 1 5 26% 700 1500
M1081 0 22 7 1 6 26% 700 1500
M1082 0 22 7 1 7 25% 800 1450
M1083 0 22 7 1 8 25% 950 1400
M1084 0 22 7 2 5 26% 700 1500
M1085 0 22 7 2 6 26% 700 1500
M1086 0 22 7 2 7 25% 800 1450
M1087 0 22 7 2 8 25% 900 1400
M1088 0 22 7 3 5 26% 700 1500
M1089 0 22 7 3 6 26% 700 1500
M1090 0 22 7 3 7 25% 750 1450
M1091 0 22 7 4 5 26% 700 1500
M1092 0 22 7 4 6 26% 700 1500 M1093 0 22 7 5 5 26% 700 1500
M1094 0 22 9 0 5 27% 700 1500
M1095 0 22 9 0 6 27% 700 1450
M1096 0 22 9 0 7 27% 800 1450
M1097 0 22 9 0 8 26% 950 1400
M1098 0 22 9 1 5 27% 700 1500
M1099 0 22 9 1 6 27% 700 1450
M1100 0 22 9 1 7 27% 750 1450
M1101 0 22 9 2 5 27% 700 1500
M1102 0 22 9 2 6 27% 700 1450
M1103 0 22 9 3 5 27% 700 1500
M1104 0 22 9 3 6 27% 700 1450
M1105 0 22 9 4 5 27% 700 1500
M1106 0 22 11 0 5 29% 700 1500
M1107 0 22 11 0 6 28% 700 1450
M1108 0 22 11 1 5 29% 650 1500
M1109 0 22 13 0 5 30% 650 1450
M1110 0 25 7 0 5 29% 650 1500
Mllll 0 25 7 0 6 29% 700 1450
M1112 0 25 7 0 7 28% 750 1450
M1113 0 25 7 1 5 29% 650 1500
M1114 0 25 7 1 6 29% 650 1450
M1115 0 25 7 2 5 29% 650 1500
M1116 0 25 7 3 5 29% 650 1500
M1117 0 25 9 0 5 30% 650 1500
M1118 0 25 9 0 6 30% 650 1450
M1119 0 25 9 1 5 30% 650 1500
M1120 0.25 16 7 3 5 20% 750 1500
M1121 0.25 16 7 4 5 20% 750 1500
M1122 0.25 16 7 5 5 20% 750 1500
M1123 0.25 16 9 0 5 21% 800 1500
M1124 0.25 19 7 0 5 23% 750 1500
M1125 0.25 19 7 1 5 23% 750 1500
M1126 0.25 19 7 2 5 23% 750 1500
M1127 0.25 19 7 3 5 23% 750 1500
M1128 0.25 19 7 4 5 23% 700 1500
M1129 0.25 19 7 5 5 23% 700 1500
M1130 0.25 19 9 0 5 24% 750 1500
M1131 0.25 22 7 0 5 26% 700 1500
M1132 0.25 22 7 1 5 26% 700 1500
M1133 0.25 22 7 2 5 26% 700 1500
Ml 134 0.25 22 7 3 5 26% 700 1500
M1135 0.25 22 7 4 5 26% 700 1500 M 1136 0.25 22 7 5 5 26% 700 1500
M 1137 0.25 22 9 0 5 27% 700 1500
M 1138 0.25 25 7 0 5 29% 650 1500
M 1139 0.25 25 7 1 5 29% 650 1500
M l 140 0.25 25 7 2 5 29% 650 1500
M 1141 0.25 25 9 0 5 30% 650 1500
Applications and processes for use:
[0062] Embodiments of alloys disclosed herein can be used in a variety of applications and industries. Some non-limiting examples of applications of use include:
[0063] Surface mining applications including but not limited to the following components and coatings for the following components: wear resistant sleeves and/or wear resistant hardfacing for slurry pipelines, mud pump components including pump housing or impeller or hardfacing for mud pump components, ore feed chute components including chute blocks or hardfacing of chute blocks, separation screens including but not limited to rotary breaker screens, banana screens, and shaker screens, liners for autogenous grinding mills and semi-autogenous grinding mills, ground engaging tools and hardfacing for ground engaging tools, wear plate for buckets and dumptruck liners, heel blocks and hardfacing for heel blocks on mining shovels, grader blades and hardfacing for grader blades, stacker reclaimers, siazer crushers, general wear packages for mining components and other communition components.
[0064] Upstream oil and gas applications including but not limited to the following components and coatings for the following components: Downhole casing and downhole casing, drill pipe and coatings for drill pipe including hardbanding, mud management components, mud motors, tracking pump sleeves, tracking impellers, tracking blender pumps, stop collars, drill bits and drill bit components, directional drilling equipment and coatings for directional drilling equipment including stabilizers and centralizers, blow out preventers and coatings for blow out preventers and blow out preventer components including the shear rams, oil country tubular goods and coatings for oil country tubular goods.
[0065] Downstream oil and gas applications including but not limited to the following components and coatings for the following components: Process vessels and coating for process vessels including steam generation equipment, amine vessels, distillation towers, cyclones, catalytic crackers, general refinery piping, corrosion under insulation protection, sulfur recovery units, convection hoods, sour stripper lines, scrubbers, hydrocarbon drums, and other refinery equipment and vessels.
[0066] Pulp and paper applications including but not limited to the following components and coatings for the following components: Rolls used in paper machines including yankee dryers and other dryers, calendar rolls, machine rolls, press rolls, digesters, pulp mixers, pulpers, pumps, boilers, shredders, tissue machines, roll and bale handling machines, doctor blades, evaporators, pulp mills, head boxes, wire parts, press parts, M.G. cylinders, pope reels, winders, vacuum pumps, deflakers, and other pulp and paper equipment.
[0067] Power generation applications including but not limited to the following components and coatings for the following components: boiler tubes, precipitators, fireboxes, turbines, generators, cooling towers, condensers, chutes and troughs, augers, bag houses, ducts, ID fans, coal piping, and other power generation components.
[0068] Agriculture applications including but not limited to the following components and coatings for the following components: chutes, base cutter blades, troughs, primary fan blades, secondary fan blades, augers and other agricultural applications.
[0069] Construction applications including but not limited to the following components and coatings for the following components: cement chutes, cement piping, bag houses, mixing equipment and other construction applications.
[0070] Machine element applications including but not limited to the following components and coatings for the following components: Shaft journals, paper rolls, gear boxes, drive rollers, impellers, general reclamation and dimensional restoration applications and other machine element applications.
[0071] Steel applications including but not limited to the following components and coatings for the following components: cold rolling mills, hot rolling mills, wire rod mills, galvanizing lines, continue pickling lines, continuous casting rolls and other steel mill rolls, and other steel applications. [0072] Embodiments of alloys disclosed herein can be produced and or deposited in a variety of techniques effectively. Some non-limiting examples of processes include:
[0073] Thermal spray process including but not limited to those using a wire feedstock such as twin wire arc, spray, high velocity arc spray, combustion spray and those using a powder feedstock such as high velocity oxygen fuel, high velocity air spray, plasma spray, detonation gun spray, and cold spray. Wire feedstock can be in the form of a metal core wire, solid wire, or flux core wire. Powder feedstock can be either a single homogenous alloy or a combination of multiple alloy powder which result in the desired chemistry when melted together.
[0074] Welding processes including but not limited to those using a wire feedstock including but not limited to metal inert gas (MIG) welding, tungsten inert gas (TIG) welding, arc welding, submerged arc welding, open arc welding, bulk welding, laser cladding, and those using a powder feedstock including but not limited to laser cladding and plasma transferred arc welding. Wire feedstock can be in the form of a metal core wire, solid wire, or flux core wire. Powder feedstock can be either a single homogenous alloy or a combination of multiple alloy powder which result in the desired chemistry when melted together.
[0075] Casting processes including but not limited to processes typical to producing cast iron including but not limited to sand casting, permanent mold casting, chill casting, investment casting, lost foam casting, die casting, centrifugal casting, glass casting, slip casting and process typical to producing wrought steel products including continuous casting processes.
[0076] Post processing techniques including but not limited to but not limited to rolling, forging, surface treatments such as carburizing, nitriding, carbonitriding, heat treatments including but not limited to austenitizing, normalizing, annealing, stress relieving, tempering, aging, quenching, cryogenic treatments, flame hardening, induction hardening, differential hardening, case hardening, decarburization, machining, grinding, cold working, work hardening, and welding.
[0077] One of the more applicable uses of this technology is in applications where coatings are deposited on-site, in the field, or in locations where proper ventilation, dust collection, and other safety measures cannot be easily met. Some well-known non-limiting examples of these applications include power generation applications such as the coating of boiler tubes, upstream refinery applications such as the coating of refinery vessels, and pulp and paper applications such as the coating and grinding of yankee dryers.
Examples:
[0078] The following examples are intended to be illustrative and non-limiting. Example 1)
[0079] The previously disclosed alloy #4, Fe: BAL, Mn: about 5, Mo: about 13, Si: about 10 was produced in the form of a 40 gram trial ingot to verify hardness and thermal spray vitrification potential. The ingot hardness was measured to be 534 Vickers (converting from a Rockwell C measurement). The microstructure of the ingot showed a fully eutectic structure indicating a strong possibility for amorphous or nanocrystalline structure under the rapid cooling rate of the spray process. This material has been selected for manufacture into 1/16" cored thermal spray wire for twin wire arc spray trials after slight modification to the alloy #14, Fe: BAL, Mn: about 5, Mo: about 13, Si: about 10, Al: about 2.
Example 2)
[0080] The previously presented alloy #5, Fe: BAL, Mn: about 5, Mo: about 7, Si: about 10 was produced in the form of a 40 gram trial ingot to verify hardness and thermal spray vitrification potential. The ingot hardness was measured to be 534 Vickers (converting from a Rockwell C measurement). The microstructure of the ingot showed a fully eutectic structure indicating a strong possibility for amorphous or nanocrystalline structure under the rapid cooling rate of the spray process. This material has been selected for manufacture into 1/16" cored thermal spray wire for twin wire arc spray trials after slight modification to alloy #15, Fe: BAL, Mn: about 5, Mo: about 7, Si: about 10, Al: about 2.
Example 3)
[0081] The previously disclosed alloy #8, Fe: BAL, C: about 0.25, Mn: about 19, Mo: about 7, Si: about 5 was produced in the form of a 40 gram ingot to verify hardness, thermal spray vetrification potential and magnetic permeability. In this example, the alloy candidate is being developed as a 'readable' coating which requires the alloy to be nonmagnetic in the sprayed form. The ingot hardness was measured to be 300 Vickers (converting from a Rockwell C measurement). While this is below the desired hardness threshold, it is well known by those skilled in the art that the rapid cooling process achieved in thermal spray will increase the hardness of the alloy in this form. Thus, it is not unreasonable to expect an increase in hardness in the sprayed form up to the desired level of 400 Vickers. The relative magnetic permeability was measured via a Low-Mu Magnetic Permeability Tester and was determined to be less than 1.01, well below the threshold required to ensure 'readability' .
Example 4)
[0082] The previously disclosed alloy #5, Fe: BAL, Mn: about 5, Mo: about 7, Si: about 10 was produced in the form of a cored thermal spray wire. This alloy was sprayed using the twin wire arc spray technique, specifically using the parameters shown in
Table 3. A series of tests were run to evaluate the alloys performance in reference to standard Cr-bearing thermal spray materials used for hardfacing. The specific alloy of reference is known by the commercial names, Armacor M, TAFA 95MXC, PMet 273, etc. and has an alloy composition of about Fe: BAL, Cr: 29, Si: 1, Mn: 2, B: 4. Table 2 highlights the result of the testing. As shown in Table 4, Alloy #5 has comparable adhesion and abrasion resistance as measure via ASTM G65B testing.
Table 2: List of properties of disclosed alloys in relation to Armacor M
Figure imgf000046_0001
Table 3: Spray parameters used in Example 4 and 5 testing
Figure imgf000046_0002
Example 5)
[0083] The previously disclosed alloy #4, Fe: BAL, Mn: about 5, Mo: about 7, Si: about 10 was produced in the form of a cored thermal spray wire. This alloy was sprayed using the twin wire arc spray technique using the parameters shown in
Table 3. Yankee dryers are typically sprayed using this parameter set. A series of tests were run to evaluate the alloys performance in reference to standard Cr-bearing thermal spray materials used for hardfacing similar to that described in Example 4. The preliminary results of this testing are shown in Table 2.
[0084] As shown, Alloy #4 replicates the key performance criteria of Armacor M in all key criteria. As Alloy #4 represents an exemplary embodiment of this disclosure, additional testing was performed in order to compare other performance criteria specifically as it relates to the coating of yankee dryers, a specific article of manufacture used in paper machines. This testing including corrosion testing, grinding studies, spray characteristics, thorough metallographic evaluation, and evaluation of surface properties as related to surface tension. In all cases, alloy #4 was deemed to have similar or better performance than the Armacor M coating.
[0085] Corrosion testing was conducted by exposing the coating to saltwater and measuring the voltage against a reference bare steel plate, which could be then used to place the material on the Galvanic Series. Both the Armacor M and Alloy #4 coatings showed significant rust on the coating surface after the 2 week test exposure. The position of the Armacor M coating on the galvanic series is -450 to -567 and the position of Alloy #4 is -510 to -640. Increasingly negative values reflect more active potentials, which is less desirable as it indicates reduced corrosion resistance. This represents a 'similarity' in that the quantified performance does not vary by more than 25%.
[0086] Grinding studies were performed due to its specific relevance to the yankee dryer application. In this application it is desirable for the coating to exhibit faster grinding times, as it reduces the downtime of the paper machine. Grinding times were quantified by removing a specific material thickness and measuring the tie to do so, as shown in
Table 4. As shown, Alloy #4 showed reduced grinding time, which is advantageous. Table 4: Grinding Study Measurements
Thickness Removed Time to Grind (sec)
Alloy #4 ARM-M % Change
5 mil 140s 150s 7.14%
10 mil 210s 210s 0%
15 mil 310s 345s 11.29%
20 mil 398s 488s 22.61%
[0087] The characteristics of the spray for both materials was also studied. It was evident that Alloy #4 produced significantly less dust during spraying than Armacor M, which is desirable. Metallographic examination also showed that less oxides were present in the Alloy #4 coating, 7% versus 13% in the Armacor M coating.
[0088] Finally the surface tension properties of each coating were evaluated. In the Yankee dryer application it is desirable for the coating to be hydrophilic, which enables the adsorption of water based organic compounds used in paper making into the surface. The contact angle that a water droplet makes on the surface can be used to quantify the surface tension of the material. The Armacor M water droplet formed a 63.9° angle, and Alloy #4 formed a 41.5° angle. A smaller angle indicates increased hydrophillicity, which is advantageous because in Yankee dryer applications, a monoammonium phosphate (MAP) water-based solution is typically sprayed onto the coating for paper release properties. It can be advantageous for this water-based solution to immerse itself into the coating structure and stick well to the coating surface, which can be enhanced by having a hydrophilic coating.
[0089] From the foregoing description, it will be appreciated that an inventive chromium free hardfacing alloy and method of manufacturing are disclosed. While several components, techniques and aspects have been described with a certain degree of particularity, it is manifest that many changes can be made in the specific designs, constructions and methodology herein above described without departing from the spirit and scope of this disclosure.
[0090] Certain features that are described in this disclosure in the context of separate implementations can also be implemented in combination in a single implementation. Conversely, various features that are described in the context of a single implementation can also be implemented in multiple implementations separately or in any suitable subcombination. Moreover, although features may be described above as acting in certain combinations, one or more features from a claimed combination can, in some cases, be excised from the combination, and the combination may be claimed as any subcombination or variation of any subcombination.
[0091] Moreover, while methods may be depicted in the drawings or described in the specification in a particular order, such methods need not be performed in the particular order shown or in sequential order, and that all methods need not be performed, to achieve desirable results. Other methods that are not depicted or described can be incorporated in the example methods and processes. For example, one or more additional methods can be performed before, after, simultaneously, or between any of the described methods. Further, the methods may be rearranged or reordered in other implementations. Also, the separation of various system components in the implementations described above should not be understood as requiring such separation in all implementations, and it should be understood that the described components and systems can generally be integrated together in a single product or packaged into multiple products. Additionally, other implementations are within the scope of this disclosure.
[0092] Conditional language, such as "can," "could," "might," or "may," unless specifically stated otherwise, or otherwise understood within the context as used, is generally intended to convey that certain embodiments include or do not include, certain features, elements, and/or steps. Thus, such conditional language is not generally intended to imply that features, elements, and/or steps are in any way required for one or more embodiments.
[0093] Conjunctive language such as the phrase "at least one of X, Y, and Z," unless specifically stated otherwise, is otherwise understood with the context as used in general to convey that an item, term, etc. may be either X, Y, or Z. Thus, such conjunctive language is not generally intended to imply that certain embodiments require the presence of at least one of X, at least one of Y, and at least one of Z.
[0094] Language of degree used herein, such as the terms "approximately," "about," "generally," and "substantially" as used herein represent a value, amount, or characteristic close to the stated value, amount, or characteristic that still performs a desired function or achieves a desired result. For example, the terms "approximately", "about", "generally," and "substantially" may refer to an amount that is within less than or equal to 10% of, within less than or equal to 5% of, within less than or equal to 1% of, within less than or equal to 0.1% of, and within less than or equal to 0.01% of the stated amount. If the stated amount is 0 (e.g., none, having no), the above recited ranges can be specific ranges, and not within a particular % of the value. For example, within less than or equal to 10 wt./vol. % of, within less than or equal to 5 wt./vol. % of, within less than or equal to 1 wt./vol. % of, within less than or equal to 0.1 wt./vol. % of, and within less than or equal to 0.01 wt./vol. % of the stated amount.
[0095] Some embodiments have been described in connection with the accompanying drawings. The figures are drawn to scale, but such scale should not be limiting, since dimensions and proportions other than what are shown are contemplated and are within the scope of the disclosed inventions. Distances, angles, etc. are merely illustrative and do not necessarily bear an exact relationship to actual dimensions and layout of the devices illustrated. Components can be added, removed, and/or rearranged. Further, the disclosure herein of any particular feature, aspect, method, property, characteristic, quality, attribute, element, or the like in connection with various embodiments can be used in all other embodiments set forth herein. Additionally, it will be recognized that any methods described herein may be practiced using any device suitable for performing the recited steps.
[0096] While a number of embodiments and variations thereof have been described in detail, other modifications and methods of using the same will be apparent to those of skill in the art. Accordingly, it should be understood that various applications, modifications, materials, and substitutions can be made of equivalents without departing from the unique and inventive disclosure herein or the scope of the claims.

Claims

WHAT IS CLAIMED IS:
1. A work piece having at least one surface, the work piece comprising:
a coating applied to the at least one surface, the coating comprising an Fe- based alloy having substantially no chromium, having substantially no carbides, and having substantially no borides;
wherein the alloy comprises a Vickers hardness of at least 500 and an adhesion strength of at least 5,000 psi.
2. The work piece of Claim 1 , wherein the coating comprises Fe and, in weight percent:
B: about 0-4;
C: about 0-0.25;
Si: about 0-15;
Mn: about 0 to 25;
Mo: about 0-29;
Nb: about 0-2;
Ta: about 0-4;
Ti: about 0-4;
V: about 0-10;
W: about 0-6;
Zr: about 0-10;
wherein B + C + Si is about 4-15; and
wherein (Mo + Mn + Nb + Ta + Ti + V + W + Zr) is about 5 to 38.
3. The work piece of Claim 1, wherein the coating comprises Fe and in weight percent:
C: about 0 to 0.25;
Mn: about 5 to 19;
Mo: about 7 to 23;
Ni: about 0 to 4; and
Si: about 5 to 10.
4. The work piece of Claim 1, wherein the coating comprises one or more of the following compositions in weight percent:
Fe, Mn: about 5, Mo: about 13, Si: about 10, Al: about 2; or
Fe, Mn: about 5, Mo: about 7, Si: about 10, Al: about 2.
5. The work piece of Claim 1, wherein the coating is non-magnetic and the coating thickness can be accurately measured with an Elcometer™ thickness gauge or similar device after it has been exposed to temperatures exceeding about 1100 K for 2 hours or more and then slow cooled at a rate of lOK/s or less.
6. The work piece of Claim 1, wherein the coating is amorphous.
7. The work piece of Claim 1, wherein the coating is nanocrystalline, as defined by having a grain size of 100 nm or less.
8. The work piece of Claim 1, wherein the coating is applied via a thermal spray process.
9. The work piece of Claim 1, wherein the coating is applied via a twin wire arc spray process.
10. The work piece of Claim 1, wherein the work piece is a yankee dryer.
11. The work piece of Claim 1 , wherein the work piece is a roller used in a paper making machine.
12. An article of manufacture comprising:
an Fe-based coating having substantially no chromium;
wherein the coating possesses a melting temperature of 1500K or below;
wherein the coating possesses a large atom concentration of at least 5 atom %, large atoms being of the group consisting of Mn, Mo, Nb, Ta, Ti, V, W, and Zr; and wherein the coating is a primarily single phase fine-grained structure of either martensite, ferrite, or austenite.
13. The article of manufacture of Claim 12, wherein the coating comprises, in weight percent:
B: about 0-4;
C: about 0-0.25;
Si: about 0-15; Mn: about 0 to 25;
Mo: about 0-29;
Nb: about 0-2;
Ta: about 0-4;
Ti: about 0-4;
V: about 0-10;
W: about 0-6;
Zr: about 0-10;
wherein B + C + Si is about 4-15; and
wherein (Mo + Mn + Nb + Ta + Ti + V + W + Zr) is about 5 to 38.
14. The article of manufacture of Claim 12, wherein the coating comprises Fe and in weight percent:
C: about 0 to 0.25;
Mn: about 5 to 19;
Mo: about 7 to 23;
Ni: about 0 to 4; and
Si: about 5 to 10.
15. The work piece of Claim 12, wherein the coating comprises one or more of the following compositions in weight percent:
Fe, Mn: about 5, Mo: about 13, Si: about 10, Al: about 2; or
Fe, Mn: about 5, Mo: about 7, Si: about 10, Al: about 2.
16. The article of manufacture of Claim 12, wherein the coating is non-magnetic and the coating thickness can be accurately measured with an Elcometer™ thickness gauge or similar device after it has been exposed to temperatures exceeding about 1100 K for 2 hours or more and then slow cooled at a rate of lOK/s or less.
17. The article of manufacture of Claim 12, wherein the coating comprises a Vickers hardness of at least 500 and an adhesion strength of at least 5,000 psi.
18. The article of manufacture of Claim 12, wherein the coating is applied via the twin wire arc spray process.
19. The article of manufacture of Claim 12, wherein the coating is amorphous.
20. The article of manufacture of Claim 12, wherein the coating is nanocrystalline, as defined by having a grain size of 100 nm or less.
21. The article of manufacture of Claim 12, wherein the coating is applied via a thermal spray process.
22. The article of manufacture of Claim 12, wherein the coating is applied onto a roller used in a paper making machine.
23. The article of manufacture of Claim 12, wherein the coating is applied onto a Yankee Dryer.
24. The article of manufacture of Claim 12, wherein the coating is applied onto a boiler tube.
25. A work piece having at least one surface, the work piece comprising:
a coating applied to the at least one surface, the coating comprising an Fe- based alloy having less than 1 wt. % chromium, less than 5 vol. % carbides, and less than 5 vol. % borides;
wherein the alloy comprises a Vickers hardness of at least 500 and an adhesion strength of at least 5,000 psi.
26. The work piece of Claim 25, wherein the alloy has less than 1 vol. % carbides and less than 1 vol. % borides.
PCT/US2015/041514 2014-07-24 2015-07-22 Chromium free hardfacing materials WO2016014653A1 (en)

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