US3891519A - Surface treatment of aluminium and aluminium alloys - Google Patents

Surface treatment of aluminium and aluminium alloys Download PDF

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US3891519A
US3891519A US503936A US50393674A US3891519A US 3891519 A US3891519 A US 3891519A US 503936 A US503936 A US 503936A US 50393674 A US50393674 A US 50393674A US 3891519 A US3891519 A US 3891519A
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bath
process according
alkali metal
indium
copper
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Bernard Grellet
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Centre Stephanois de Recherches Mecaniques Hydromecanique et Frottement SA
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Stephanois De Rech Mechaniques
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    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D5/00Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
    • C25D5/48After-treatment of electroplated surfaces
    • C25D5/50After-treatment of electroplated surfaces by heat-treatment
    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D3/00Electroplating: Baths therefor
    • C25D3/02Electroplating: Baths therefor from solutions
    • C25D3/56Electroplating: Baths therefor from solutions of alloys
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/9335Product by special process
    • Y10S428/934Electrical process
    • Y10S428/935Electroplating
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/9335Product by special process
    • Y10S428/941Solid state alloying, e.g. diffusion, to disappearance of an original layer
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12681Ga-, In-, Tl- or Group VA metal-base component
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12736Al-base component
    • Y10T428/1275Next to Group VIII or IB metal-base component

Definitions

  • the surface of aluminium or an aluminium alloy is s t 4 I973 F 73 3303! treated by electrolytic deposition of a copper-indium ep rance alloy surface layer followed by the diffusion heat treat- 1 U S Cl 204/37 29/197 29/199 ment of the coated surface.
  • Electrolysis is carried out 204/44 in a bath containing, in an aqueous alkaline solution, [5H Int Cl C23) slszrcnb 5/46 B23 3/00 monovalent copper ions, trivalent indium ions, an al- 58]
  • References Cited the heat treatment is carried out at between 120 and 155C. UNITED STATES PATENTS 2,458,839 1 1949 Dyer, Jr. et a1.
  • the present invention relates to a process for the treatment of surfaces of aluminium or aluminium alloys to improve their frictional properties and resistance to wear and seizure by forming on their surface, by diffusion, intermetallic or semi-metallic compounds.
  • the second technique permits the use of a lower diffusion temperature and a shorter temperature holding time.
  • this coating morphology results in rapid wear of the porous zone and a substantial, progressive increase of the coefficient of friction; at a certain degree of wear there may even be epidermic sticking and seizure.
  • the composition of the alloy deposited varies from one point to another on the treated part, and this variation is considerable.
  • the copper content of the mixed coating is above 50 percent by weight, the alloy, when subjected to friction, becomes covered with copper, which in practice is incompatible with the usual mechanical parts, particularly steels, which have to rub against parts of the treated aluminium alloys.
  • the indium content exceeds 65 percent by weight the hardness of the alloys formed decreases very rapidly and the mechanical characteristics of the layer of alloy become insufficient to prevent the phenomenon of surface creep when friction occurs.
  • An object of the present invention is to provide a process by which it is possible, under industrial large-scale production conditions, to obtain on surfaces of aluminium and aluminium alloys a coating having good frictional properties without seizing and without reduced wear, which is capable of following without fracturing any deformation, even substantial deformation, of its substrate, which is not subject to surface creep, and which has a hardness several times greater than that of the uncoated aluminium alloy, while the mechanical properties of the latter are not affected.
  • the present invention proposes a process for the treatment of surfaces of aluminium or aluminium alloys by depositing a layer of a copper-indium alloy followed by diffusion heat treatment, characterised in that this deposition is effected galvanically in a bath containing, in an aqueous alkaline solution, monovalent copper ions, trivalent indium ions, an alkali metal hydroxide, an alkali metal cyanide, an alkali metal gluconate, gluconic acid, and oxalic acid, these products being used in accurately defined proportions which, according to the original feature of the invention, must be concurrently respected, and in that the diffusion heat treatment is effected at a temperature between and C.
  • anodic current density between 1.5 and 4 A/dm concentrations of gluconic acid and oxalic acid between 1 and mg/litre.
  • the part After deposition of the desired thickness, the part is rinsed and dried and subjected to the diffusion heat treatment at a temperature between 120 and 155C for a time between 2 and 6 hours.
  • the friction coating produced according to the invention is a good conductor of heat and electricity, while in addition possessing the unexpected property of providing a friction surface having a low coefficient of friction without unalloyed indium appearing on the surface, which occurs in the above mentioned prior art processes.
  • Micrographic examination of a section made in a part of this kind shows the presence of the surface of a layer which is perfectly homogeneous and regular whatever part of the surface is examined, which has perfect adhesion and a hardness between 300 and 450 Vickers under 0.15 N.
  • This coating contains copper and indium in the proportion of from 35 to 50 percent by weight of copper in indium, and is composed of hard but nonfragile Cu/ln compounds.
  • a bearing treated by the process described in the present invention can operate for several hours with a coefficient of friction of 0.03.
  • the aluminium alloy bearing has undergone the treatment of the invention in the following manner:
  • the part was thereupon rinsed and then immersed in a galvanic bath to receive a mixed deposition of copper and indium of a thickness of 20 microns; the bath had the composition previously indicated in the description of the invention and the following conditions were adopted:
  • alkali metal gluconate in this case potassium gluconate, equal to 2.5 g of this gluconate per gram of indium metal in the bath;
  • gluconic acid content equal to 2 mg per litre of bath
  • oxalic acid content equal to 1.5 mg per litre of bath
  • Second Example This relates to a test of friction between two plane surfaces, carried out under the following experimental conditions: plane cursor ofa length of 20 mm with two longitudinal bearing surfaces ofa width of 4 mm; reciprocating movement on a plane track with a stroke of 60 mm; load: 30 daN; speed of movement 1 cm/s; time delay: 1 second stoppage at the end of each stroke; atmosphere: interposition of grease at beginning and then operation in ambient air without additional supply of lubricant.
  • a process for the treatment of the surface of aluminium or an aluminium alloy comprising the steps of a. depositing a copper-indium alloy layer on the said surface by electrolysis in a bath containing, an alkaline solution, monovalent copper ions, trivalent indium ions, an alkali metal hydroxide, an alkali metal cyanide, an alkali metal gluconate, gluconic acid, and oxalic acid, and
  • a process according to claim 1. characterised in that the alkali metal gluconate content in the bath is higher than or equal to 0.5 g of this gluconatc per gram of indium metal in the bath.
  • a process according to claim 1 characterised in that the heat treatment is effected in air for between 2 and 6 hours.

Abstract

The surface of aluminium or an aluminium alloy is treated by electrolytic deposition of a copper-indium alloy surface layer followed by the diffusion heat treatment of the coated surface. Electrolysis is carried out in a bath containing, in an aqueous alkaline solution, monovalent copper ions, trivalent indium ions, an alkali metal hydroxide, an alkali metal cyanide, an alkali metal gluconate, gluconic acid, and oxalic acid, and the heat treatment is carried out at between 120* and 155*C.

Description

, United States Patent I :91 m1 3,891,519 Grellet June 24, 1975 [54] SURFACE TREATMENT OF ALUIVIINIUM 2,765,520 1 10/1956 Donley 204/37 R X AND ALUMINIUM ALLOYS 3,108,006 10/1963 Kenedi et 211.... lO6/I 3,8l2,020 5/1974 Vander Me 204/24 {75] Inventor: Bernard Grellet, Saint-Etienne, y
France FOREIGN PATENTS OR APPLICATIONS 173] Assignee: Centre Stephanois de Recherches 2 gzgzg 204/37 R Mechaniques Hydromccanique et y g jgrgg AndrezleuxBoutheon Primary Examiner.lohn H. Mack Assistant ExaminerAar0n Weisstuch [22] Filed: Sept. 9, 1974 Attorney, Agent, or Firm-Young & Thompson [2]] Appl. No: 503,936
[57] ABSTRACT {30] Foreign Application prioriy Data The surface of aluminium or an aluminium alloy is s t 4 I973 F 73 3303! treated by electrolytic deposition of a copper-indium ep rance alloy surface layer followed by the diffusion heat treat- 1 U S Cl 204/37 29/197 29/199 ment of the coated surface. Electrolysis is carried out 204/44 in a bath containing, in an aqueous alkaline solution, [5H Int Cl C23) slszrcnb 5/46 B23 3/00 monovalent copper ions, trivalent indium ions, an al- 58] Field 'g b 44 kali metal hydroxide, an alkali metal cyanide, an alkali metal gluconate, gluconic acid, and oxalic acid, and I 56] References Cited the heat treatment is carried out at between 120 and 155C. UNITED STATES PATENTS 2,458,839 1 1949 Dyer, Jr. et a1. 204/43 R x 10 Clams Drawmgs SURFACE TREATMENT OF ALUMINIUM AND ALUMINIUM ALLOYS BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a process for the treatment of surfaces of aluminium or aluminium alloys to improve their frictional properties and resistance to wear and seizure by forming on their surface, by diffusion, intermetallic or semi-metallic compounds.
2. Description of the Prior Art Various processes are known for forming coatings of this kind on the surface of a metal. This is in particular true of French Patent No. l530 of the 6th May l967 and its five certificates of addition, which describe processes for forming composite anti-friction layers by depositing a metal coating on a metal surface and then subjecting it to a suitable heat treatment. Two techniques have been proposed: lst technique First, the deposition of successive layers of metals on the metal parts to be treated;
then diffusion in a preferably neutral or reducing atmosphere, in accordance with a thermal cycle comprising two separate phases: first heating to a temperature at least 20C below the melting point of the most readily fusible of the metals present, then heating to a temperature between the said melting point and 800C. 2nd technique First, deposition on the part of a layer of an alloy of two or more metals,
then the baking of the part coated in this manner, optionally in a single stage.
In comparison with the first technique, the second technique permits the use ofa lower diffusion temperature and a shorter temperature holding time.
After diffusion using either technique, the treated part presents from inside to outside:
the base metal;
a layer of residual metal;
a layer formed of metallic compounds of a thickness greater than 10 microns and of a hardness above 500 Vickers',
a residual surface layer of a thickness less than 4 microns of one of the metals present.
The preceding technique is applicable to aluminium alloys and an example is described in the previously mentioned French Patent, in which the diffusion coating is produced from copper and indium, the temperature of the last stage of the heat treatment being indicated as equal to 200C. In this case the part presents after treatment, from inside to outside:
the aluminium base alloy,
a residual layer of copper,
a layer of compounds of copper and indium,
a residual surface layer of indium.
These techniques for producing diffused coatings based on copper and indium, when applied to aluminium and its alloys, nevertheless have the following disadvantages: (a) the heat treatment temperature, which must be higher than 155C (melting point of indium), is too high and results in a deterioration of the mechanical properties of the aluminium alloys, particularly those subjected to substantial structural hardening, such as for example the aluminium-zinc alloys, whose mechanical properties start to fall at a temperature close to l30-135C; in addition, since the heat treatment temperature is higher than the melting point of indium 155C), the coatings formed have great porosity.
When subjected to friction, this coating morphology results in rapid wear of the porous zone and a substantial, progressive increase of the coefficient of friction; at a certain degree of wear there may even be epidermic sticking and seizure.
b. the presence ofa layer of copper having poor mechanical characteristics under a layer of fragile compounds having good mechanical characteristics results in pronounced overall fragility of the composite layer, which prevents it from following any substantial deformations of the substrate without fracturing.
In the above mentioned known process the alloy of copper and indium originally deposited on the metal part was obtained from known baths, for example baths based on sulphamates.
Nevertheless, these baths have the following main disadvantages:
a. the composition of the alloy deposited varies from one point to another on the treated part, and this variation is considerable. When the copper content of the mixed coating is above 50 percent by weight, the alloy, when subjected to friction, becomes covered with copper, which in practice is incompatible with the usual mechanical parts, particularly steels, which have to rub against parts of the treated aluminium alloys. When the indium content exceeds 65 percent by weight the hardness of the alloys formed decreases very rapidly and the mechanical characteristics of the layer of alloy become insufficient to prevent the phenomenon of surface creep when friction occurs.
b. These baths are chemically unstable, that is to say they rapidly change in the course of time and it is not possible for an alloy ofa constant given composition to be deposited on successive parts.
An object of the present invention is to provide a process by which it is possible, under industrial large-scale production conditions, to obtain on surfaces of aluminium and aluminium alloys a coating having good frictional properties without seizing and without reduced wear, which is capable of following without fracturing any deformation, even substantial deformation, of its substrate, which is not subject to surface creep, and which has a hardness several times greater than that of the uncoated aluminium alloy, while the mechanical properties of the latter are not affected.
SUMMARY The present invention proposes a process for the treatment of surfaces of aluminium or aluminium alloys by depositing a layer of a copper-indium alloy followed by diffusion heat treatment, characterised in that this deposition is effected galvanically in a bath containing, in an aqueous alkaline solution, monovalent copper ions, trivalent indium ions, an alkali metal hydroxide, an alkali metal cyanide, an alkali metal gluconate, gluconic acid, and oxalic acid, these products being used in accurately defined proportions which, according to the original feature of the invention, must be concurrently respected, and in that the diffusion heat treatment is effected at a temperature between and C.
In order to obtain a friction coating having the properties indicated above, after being subjected to degreasing and pickling treatments known per se the part is electrolytically coated with a copper-indium alloy in a bath according to the invention, the operating conditions of which are controlled within the undermentioned limits:
mass ratio of indium metal to copper metal between 2 and 8;
content of alkali metal gluconate above or equal to 0.5g per gram of indium metal in the bath;
pH between 12 and 14 and kept between those values by adjusting the content of alkali metal hydroxide;
content of free alkali metal cyanide between 1.1 and 1.8g per gram of copper metal in the bath;
temperature of the bath between 30 and 60C;
cathodic current density between 3 and 8 A/dm";
anodic current density between 1.5 and 4 A/dm concentrations of gluconic acid and oxalic acid between 1 and mg/litre.
After deposition of the desired thickness, the part is rinsed and dried and subjected to the diffusion heat treatment at a temperature between 120 and 155C for a time between 2 and 6 hours.
By this process it is possible to form a friction coating which does not have the disadvantages of those obtained by the previously mentioned known processes, that is to say which is non-porous, of constant composition throughout its thickness and at any point on the treated surface, and is capable of deformation without fracturing, while the diffusion treatment temperature does not affect the mechanical characteristics of the base aluminium alloy and does not bring about local fusion.
Furthermore, the friction coating produced according to the invention is a good conductor of heat and electricity, while in addition possessing the unexpected property of providing a friction surface having a low coefficient of friction without unalloyed indium appearing on the surface, which occurs in the above mentioned prior art processes.
Micrographic examination ofa section made in a part of this kind shows the presence of the surface of a layer which is perfectly homogeneous and regular whatever part of the surface is examined, which has perfect adhesion and a hardness between 300 and 450 Vickers under 0.15 N. This coating contains copper and indium in the proportion of from 35 to 50 percent by weight of copper in indium, and is composed of hard but nonfragile Cu/ln compounds.
DESCRIPTION OF THE PREFERRED EMBODIMENTS First Example This relates to the rubbing of a bearing of aluminium alloy against a shaft of hardened cemented steel, the mechanism being kept in an oil bath and the temperature being that of the ambient air. The characteristics of the parts are as follows: shaft diameter: 40 mm; clearance between shaft and bearing: 0.08 mm; sliding speed: 2 metres per second; specific load: 140 bars.
Under these conditions a bearing of aluminium alloy of the AU4G type containing 94.5 percent of aluminium, 3.8 percent of copper, and 1.5 percent of magnesium cannot undergo friction for more than 5 seconds, at the end of which time there is an abrupt seizure with the transfer of aluminium to the shaft of cemented hardened steel.
On the other hand, a bearing treated by the process described in the present invention can operate for several hours with a coefficient of friction of 0.03.
In this example, given without limitation, the aluminium alloy bearing has undergone the treatment of the invention in the following manner:
a. the part was first degreased and pickled;
b. the part was thereupon rinsed and then immersed in a galvanic bath to receive a mixed deposition of copper and indium of a thickness of 20 microns; the bath had the composition previously indicated in the description of the invention and the following conditions were adopted:
ratio of indium metal to copper metal in the bath equal to 2.7;
content of alkali metal gluconate, in this case potassium gluconate, equal to 2.5 g of this gluconate per gram of indium metal in the bath;
gluconic acid content equal to 2 mg per litre of bath;
oxalic acid content equal to 1.5 mg per litre of bath;
bath temperature 50C;
pH of bath equal to 13.3;
cathodic current density 4 A/dm anodic current density 2 A/dm c. finally, the part coated in this manner was washed and dried and then kept for 4 hours at a temperature of C in an atmosphere of air.
By way of comparison, a bearing of aluminium alloy AU4G treated by thick anodic oxidation can operate for no more than 2 minutes, after which time there is an abrupt transfer of aluminium to the steel shaft. Second Example This relates to a test of friction between two plane surfaces, carried out under the following experimental conditions: plane cursor ofa length of 20 mm with two longitudinal bearing surfaces ofa width of 4 mm; reciprocating movement on a plane track with a stroke of 60 mm; load: 30 daN; speed of movement 1 cm/s; time delay: 1 second stoppage at the end of each stroke; atmosphere: interposition of grease at beginning and then operation in ambient air without additional supply of lubricant.
Under these conditions, when the cursor and the track are of untreated aluminium alloy of the A8 0 type, that is to say containing 91.2 percent of aluminium, 7.2 percent of silicon, 1.1 percent of magnesium, the movement is halted by sticking and seizure at the end of cycles.
On the other hand, when the cursor and the track are treated as in the preceding example by the process described in the present invention, the test is voluntarily stopped at the end of 5,000 cycles, the mean coeffi cient of friction then being 0.10.
By way of comparison, when thick anodic oxidation is effected on the track of A8 6, the movment is stopped with the emission of numerous particles at the end of 320 cycles.
1 claim:
1. A process for the treatment of the surface of aluminium or an aluminium alloy, comprising the steps of a. depositing a copper-indium alloy layer on the said surface by electrolysis in a bath containing, an alkaline solution, monovalent copper ions, trivalent indium ions, an alkali metal hydroxide, an alkali metal cyanide, an alkali metal gluconate, gluconic acid, and oxalic acid, and
h. subjecting the coated surface to a diffusion heat treatment at a temperature between 120 and 155C.
2. A process according to claim 1, characterised in that the mass ratio of indium metal to copper metal in the bath is between 2 and 8.
3. A process according to claim 1., characterised in that the alkali metal gluconate content in the bath is higher than or equal to 0.5 g of this gluconatc per gram of indium metal in the bath.
4. A process according to claim 1, characterised in that the pH of the bath is between I25 and 14, this pH being maintained between these values by adjusting the alkali metal hydroxide content of the bath.
5. A process according to claim 1, characterised in that the free cyanide content of the bath is between L] and L8 g of the said alkali metal cyanide per gram of copper metal in the bath.
6. A process according to claim 1, characterised in that the temperature of the bath is between 30 and 60C.
7. A process according to claim 1, characterised in that the cathodic current density is between 3 and 8 A/dm*.
8. A process according to claim 1, characterised in that the anodic current density is between L5 and 4 A/dm.
9. A process according to claim 1, characterised in that the gluconic acid and oxalic acid contents are between l and l0 milligrams per litre.
10. A process according to claim 1, characterised in that the heat treatment is effected in air for between 2 and 6 hours.

Claims (10)

1. A PROCESS FOR THE TREATMENT OF THE SURFACE OF ALUMINUM OR AN ALUMINIUM ALLOY, COMPRISING THE STEPS OF A. DEPOSITING A COPPER-INDIUM ALLOY LAYER ON THE SAID SURFACE BY ELECTROLYSIS IN A BATH CONTAINING, AN ALKALINE SOLUTION, MONOVALENT COPPER IONS, TRIVALENT INDIUM IONS, AN ALKALI METAL HYDROXIDE, AN ALKALI METAL CYANIDE, AN ALKALI METAL GLUCONATE, GLUCONIC ACID, AND OXALIC ACID, AND B. SUBJECTING THE COATED SURFACE TO A DIFFUSION HEAT TREATMENT AT A TEMPERATURE BETWEEN 120* AND 155*C.
2. A process according to claim 1, characterised in that the mass ratio of indium metal to copper metal in the bath is between 2 and 8.
3. A process according to claim 1, characterised in that the alkali metal gluconate content in the bath is higher than or equal to 0.5 g of this gluconate per gram of indium metal in the bath.
4. A process according to claim 1, characterised in that the pH of the bath is between 12.5 and 14, this pH being maintained between these values by adjusting the alkali metal hydroxide content of the bath.
5. A process according to claim 1, characterised in that the free cyanide content of the bath is between 1.1 and 1.8 g of the said alkali metal cyanide per gram of copper metal in the bath.
6. A process according to claim 1, characterised in that the temperature of the bath is between 30* and 60*C.
7. A process according to claim 1, characterised in that the cathodic current density is between 3 and 8 A/dm2.
8. A process according to claim 1, characterised in that the anodic current density is between 1.5 and 4 A/dm2.
9. A process according to claim 1, characterised in that the gluconic acid and oxalic acid contents are between 1 and 10 milligrams per litre.
10. A process according to claim 1, characterised in that the heat treatment is effected in air for between 2 and 6 hours.
US503936A 1973-09-14 1974-09-09 Surface treatment of aluminium and aluminium alloys Expired - Lifetime US3891519A (en)

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US8329501B1 (en) 2004-02-19 2012-12-11 Nanosolar, Inc. High-throughput printing of semiconductor precursor layer from inter-metallic microflake particles

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US3108006A (en) * 1959-07-13 1963-10-22 M & T Chemicals Inc Plating on aluminum
US3812020A (en) * 1969-08-11 1974-05-21 Allied Chem Electrolyte and method for electroplating an indium-copper alloy and printed circuits so plated

Cited By (16)

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JPS5461163U (en) * 1977-10-07 1979-04-27
US6279221B1 (en) 1999-09-08 2001-08-28 Visteon Global Tech., Inc. Vehicle driveshaft
US8372734B2 (en) 2004-02-19 2013-02-12 Nanosolar, Inc High-throughput printing of semiconductor precursor layer from chalcogenide nanoflake particles
US8329501B1 (en) 2004-02-19 2012-12-11 Nanosolar, Inc. High-throughput printing of semiconductor precursor layer from inter-metallic microflake particles
US8642455B2 (en) 2004-02-19 2014-02-04 Matthew R. Robinson High-throughput printing of semiconductor precursor layer from nanoflake particles
US20080121277A1 (en) * 2004-02-19 2008-05-29 Robinson Matthew R High-throughput printing of semiconductor precursor layer from chalcogenide microflake particles
US8623448B2 (en) 2004-02-19 2014-01-07 Nanosolar, Inc. High-throughput printing of semiconductor precursor layer from chalcogenide microflake particles
US20090107550A1 (en) * 2004-02-19 2009-04-30 Van Duren Jeroen K J High-throughput printing of semiconductor precursor layer from chalcogenide nanoflake particles
US20100267222A1 (en) * 2004-02-19 2010-10-21 Robinson Matthew R High-Throughput Printing of Semiconductor Precursor Layer from Nanoflake Particles
US20070163644A1 (en) * 2004-02-19 2007-07-19 Nanosolar, Inc. High-throughput printing of semiconductor precursor layer by use of chalcogen-containing vapor and inter-metallic material
US8309163B2 (en) 2004-02-19 2012-11-13 Nanosolar, Inc. High-throughput printing of semiconductor precursor layer by use of chalcogen-containing vapor and inter-metallic material
US8193442B2 (en) 2004-09-18 2012-06-05 Nanosolar, Inc. Coated nanoparticles and quantum dots for solution-based fabrication of photovoltaic cells
US20060062902A1 (en) * 2004-09-18 2006-03-23 Nanosolar, Inc. Coated nanoparticles and quantum dots for solution-based fabrication of photovoltaic cells
US20080149176A1 (en) * 2004-09-18 2008-06-26 Nanosolar Inc. Coated nanoparticles and quantum dots for solution-based fabrication of photovoltaic cells
US7306823B2 (en) 2004-09-18 2007-12-11 Nanosolar, Inc. Coated nanoparticles and quantum dots for solution-based fabrication of photovoltaic cells
US8809678B2 (en) 2004-09-18 2014-08-19 Aeris Capital Sustainable Ip Ltd. Coated nanoparticles and quantum dots for solution-based fabrication of photovoltaic cells

Also Published As

Publication number Publication date
JPS5077234A (en) 1975-06-24
SE7410901L (en) 1975-03-17
ZA745762B (en) 1975-10-29
SE407428B (en) 1979-03-26
AR200366A1 (en) 1974-10-31
NL7411651A (en) 1975-03-18
FR2244016A1 (en) 1975-04-11
JPS5610992B2 (en) 1981-03-11
BR7407641D0 (en) 1975-07-08
CH592747A5 (en) 1977-11-15
ES429847A1 (en) 1976-12-01
CA1030899A (en) 1978-05-09
IT1020795B (en) 1977-12-30
DE2443884B2 (en) 1977-06-02
DE2443884A1 (en) 1975-04-03
GB1443672A (en) 1976-07-21
FR2244016B1 (en) 1976-06-18

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