GB2144061A - Process for producing aluminium-clad composite materials by roll cladding - Google Patents

Process for producing aluminium-clad composite materials by roll cladding Download PDF

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Publication number
GB2144061A
GB2144061A GB08418872A GB8418872A GB2144061A GB 2144061 A GB2144061 A GB 2144061A GB 08418872 A GB08418872 A GB 08418872A GB 8418872 A GB8418872 A GB 8418872A GB 2144061 A GB2144061 A GB 2144061A
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GB
United Kingdom
Prior art keywords
steel
aluminium
cladding
strip
aluminium alloy
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB08418872A
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GB8418872D0 (en
GB2144061B (en
Inventor
Dr Martin Creydt
Rolf Pfoh
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Kolbenschmidt AG
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Kolbenschmidt AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Application filed by Kolbenschmidt AG filed Critical Kolbenschmidt AG
Publication of GB8418872D0 publication Critical patent/GB8418872D0/en
Publication of GB2144061A publication Critical patent/GB2144061A/en
Application granted granted Critical
Publication of GB2144061B publication Critical patent/GB2144061B/en
Expired legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/22Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded
    • B23K20/227Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded with ferrous layer
    • B23K20/2275Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded with ferrous layer the other layer being aluminium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/04Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by means of a rolling mill

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Sliding-Contact Bearings (AREA)

Abstract

In the process an aluminium layer is bonded to a steel layer by cladding at a temperature of preferably 200 to 400 DEG C. In order to increase the strength of the aluminium alloy, the latter is homogenized at a temperature of 450 to 550 DEG C between 0.5 and 3 hours and is subsequently quenched and then bonded to the steel layer by roll-cladding, the resulting composite material being quenched as soon as it leaves the roll nip.

Description

SPECIFICATION Process for producing aluminium-clad com- posite materials This invention relates to a process for producing aluminium-clad composite materials by roll-cladding an aluminium layer to a steel layer.
It has been known for many years that composite materials can be produced by a roll-cladding process, in which sheet bars of a substrate metal and of a facing metal are jointly rolled so that they are bonded by welding under the rolling pressure. The substrate metal consists usually of plain carbon mild steel, which can easily be welded, or of high-temperature steel. The cladding may consist of copper and various kinds of copper alloys, nickel and nickel alloys, aluminium and aluminium alloys, silver and silver alloys, or of alloy steel. It is known to clad sheet metal elements, strip, tubing, rods, wires and sections whenever it is too expensive to produce these from the cladding metal alone and/or the cladding metal does not have the required mechanical properties. Examples of such products are coin banks, temperature-responsive bimetals or the like.Composite materials consisting of steel which is clad with aluminium alloys have been used for many years mainly in bearings. In such bearings, the aluminium alloy provides the sliding surface and the steel provides a backing (c.f. German Patent Specification No. 706,655). Owing to their high strength, such composite materials can be used in the manufacture of comparatively thin-walled bearing bushings, e.g. for connecing rod bearings, although they are inferior to steel-bronze composite materials made by sintering or casting when relatively high abrading and compressive stresses are to be expected, e.g. owing to the considerably increased power outputs of internal combustion engines per unit of displacement.This less satisfactory behaviour is due to the fact that, after the cladding operation, the aluminium alloy has a relatively low hardness corresponding to a Brinell Hardness Number of 45 to 55. The hardness cannot be increased by a specific heat treatment because the homogenization which has to be effected at a temperature of about 500 C and the succeeding quenching and artificial aging would destroy the frictionwelded joint formed between the aluminium alloy and the steel.
According to the present invention there is provided a process for producing an aluminium-clad composite material, wherein a precipitation-hardenable aluminium alloy strip is homegenized at a temperature of 450 to 550 C for 0.5 hour to 3 hours and is subsequently quenched, wherein the aluminium alloy strip is then bonded to a steel strip by rollcladding and the resulting composite material is quenched as soon as it leaves the roll nip.
With the present process it is possible to provide a process in which the aluminium alloy can be precipitation-hardened after the cladding operation to have properties which are substantially equivalent to the corresponding properties of steel-bronze composite materials whereas this should not adversely affect the strength of the friction-welded joint formed between the aluminium alloy and the steel.
The aluminium alloy strip preferably has a thickness of 0.5 to 5 mm. while the steel strip has a thickness of 0.5 to 10 mm. The rollcladding is conveniently effected at a cladding speed of 1.5 to 5 metres per minute.
It is desirable to use aluminium alloys which are capable of exhibiting high and/or low friction and are preferably of the type AlSill 2CuNiMg, AlZn5PbCuMg, AlSn6Cu, AlSi18NiMg or AlSi21CuNiMg.
Roll cladding is suitably effected at elevated temperatures above 200 C, preferably 200 to 400 C, and more preferably 250 C. Rollcladding may alternatively be effected at ambient temperatures if the fatigue limit of the bonding zone is of minor significance.
In order to facilitate the running-in of bearings made from a composite material which has been made in accordance with the present process, a layer of PbSnCu, AlSn, AlPb or iron phosphate in a thickness of a few microns is applied to the aluminium layer.
By the present process, the hardness of the aluminium alloy which has been clad onto steel can be increased from a Brinell Hardness Number 45 to 55 to a Brinell Hardness Number 65 to 85. This means that the hardness of bronze layers clad onto steel is reached or partly exceeded.
The invention will now be explained in greater detail in the following Example.
Strip steel having a width of 200 mm, and a thickness of 3 mm. is roughened on one side and is heated to about 500 C in an induction coil under a protective gas atmosphere. Thereafter the strip is fed to a roll nip for deforming the strip by roll cladding. An aluminium alloy of Type AlZn5PbCuMg or AlSi12CuNiMg in the form of strip having a thickness of 1.2 mm. and a width of 195 mm. is separately surface-activated and then homogenized at a temperature of 510 C for 2 hours. Thereafter the strip aluminium is quenched and is fed to the roll nip at the same time as the strip steel for deformation by roll cladding. The resulting composite material is quenched as soon as it leaves the roll nip and is subsequently artificially aged at a temperature of 1 85 > C for 10 hours. The aluminium alloy facing had the Brinell Hardness Number 81.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (12)

**WARNING** start of CLMS field may overlap end of DESC **. SPECIFICATION Process for producing aluminium-clad com- posite materials This invention relates to a process for producing aluminium-clad composite materials by roll-cladding an aluminium layer to a steel layer. It has been known for many years that composite materials can be produced by a roll-cladding process, in which sheet bars of a substrate metal and of a facing metal are jointly rolled so that they are bonded by welding under the rolling pressure. The substrate metal consists usually of plain carbon mild steel, which can easily be welded, or of high-temperature steel. The cladding may consist of copper and various kinds of copper alloys, nickel and nickel alloys, aluminium and aluminium alloys, silver and silver alloys, or of alloy steel. It is known to clad sheet metal elements, strip, tubing, rods, wires and sections whenever it is too expensive to produce these from the cladding metal alone and/or the cladding metal does not have the required mechanical properties. Examples of such products are coin banks, temperature-responsive bimetals or the like.Composite materials consisting of steel which is clad with aluminium alloys have been used for many years mainly in bearings. In such bearings, the aluminium alloy provides the sliding surface and the steel provides a backing (c.f. German Patent Specification No. 706,655). Owing to their high strength, such composite materials can be used in the manufacture of comparatively thin-walled bearing bushings, e.g. for connecing rod bearings, although they are inferior to steel-bronze composite materials made by sintering or casting when relatively high abrading and compressive stresses are to be expected, e.g. owing to the considerably increased power outputs of internal combustion engines per unit of displacement.This less satisfactory behaviour is due to the fact that, after the cladding operation, the aluminium alloy has a relatively low hardness corresponding to a Brinell Hardness Number of 45 to 55. The hardness cannot be increased by a specific heat treatment because the homogenization which has to be effected at a temperature of about 500 C and the succeeding quenching and artificial aging would destroy the frictionwelded joint formed between the aluminium alloy and the steel. According to the present invention there is provided a process for producing an aluminium-clad composite material, wherein a precipitation-hardenable aluminium alloy strip is homegenized at a temperature of 450 to 550 C for 0.5 hour to 3 hours and is subsequently quenched, wherein the aluminium alloy strip is then bonded to a steel strip by rollcladding and the resulting composite material is quenched as soon as it leaves the roll nip. With the present process it is possible to provide a process in which the aluminium alloy can be precipitation-hardened after the cladding operation to have properties which are substantially equivalent to the corresponding properties of steel-bronze composite materials whereas this should not adversely affect the strength of the friction-welded joint formed between the aluminium alloy and the steel. The aluminium alloy strip preferably has a thickness of 0.5 to 5 mm. while the steel strip has a thickness of 0.5 to 10 mm. The rollcladding is conveniently effected at a cladding speed of 1.5 to 5 metres per minute. It is desirable to use aluminium alloys which are capable of exhibiting high and/or low friction and are preferably of the type AlSill 2CuNiMg, AlZn5PbCuMg, AlSn6Cu, AlSi18NiMg or AlSi21CuNiMg. Roll cladding is suitably effected at elevated temperatures above 200 C, preferably 200 to 400 C, and more preferably 250 C. Rollcladding may alternatively be effected at ambient temperatures if the fatigue limit of the bonding zone is of minor significance. In order to facilitate the running-in of bearings made from a composite material which has been made in accordance with the present process, a layer of PbSnCu, AlSn, AlPb or iron phosphate in a thickness of a few microns is applied to the aluminium layer. By the present process, the hardness of the aluminium alloy which has been clad onto steel can be increased from a Brinell Hardness Number 45 to 55 to a Brinell Hardness Number 65 to 85. This means that the hardness of bronze layers clad onto steel is reached or partly exceeded. The invention will now be explained in greater detail in the following Example. Strip steel having a width of 200 mm, and a thickness of 3 mm. is roughened on one side and is heated to about 500 C in an induction coil under a protective gas atmosphere. Thereafter the strip is fed to a roll nip for deforming the strip by roll cladding. An aluminium alloy of Type AlZn5PbCuMg or AlSi12CuNiMg in the form of strip having a thickness of 1.2 mm. and a width of 195 mm. is separately surface-activated and then homogenized at a temperature of 510 C for 2 hours. Thereafter the strip aluminium is quenched and is fed to the roll nip at the same time as the strip steel for deformation by roll cladding. The resulting composite material is quenched as soon as it leaves the roll nip and is subsequently artificially aged at a temperature of 1 85 > C for 10 hours.The aluminium alloy facing had the Brinell Hardness Number 81. CLAIMS
1. A process for producing an aluminiumclad composite material, wherein a precipitation-hardenable aluminium alloy strip is homogenized at a temperature of 450 to 550 C for 0.5 hour for 3 hours and is subsequently quenched, and wherein the aluminium alloy strip is then bonded to a steel strip by rollcladding and the resulting composite material is quenched as soon as it leaves the roll nip.
2. A process as claimed in Claim 1, wherein the aluminium alloy strip has a thickness of 0.5 to 5 mm. and the steel strip has a thickness of 0.5 to 10 mm.
3. A process as claimed in Claim 1 or 2, wherein the roll-cladding is effected at a cladding speed of 1.5 to 5 metres per minute.
4. A process as claimed in any one of Claims 1 to 3, wherein the roll-cladding is effected at a temperature of 200 to 400 C.
5. A process as claimed in any one of Claims 1 to 4, wherein the roll-cladding is effected at a temperarture of 250 C.
6. A process as claimed in any one of Claims 1 to 3, wherein the roll-cladding is effected at ambient temperatures.
7. A process as claimed in any one of Claims 1 to 6, wherein the composite material is artificially aged at a temperature of 150 to 250 C for 2 hours to 10 hours.
8. A process as claimed in any one of Claims 1 to 7, wherein the aluminium alloy is one which is suitable for use as a low friction or bearing alloy.
9. A process as claimed in Claim 9, wherein the aluminium alloy is of the Type AlSil 2CuNiMg, AlZn5PbCuMg, AlSn6Cu, AlSil8NiMg or AlSi21CuNiMg.
10. A process as claimed in any one of Claims 1 to 9, wherein a layer consisting of PbSnCu, AlSn, AlPb or iron phosphate is applied in a thickness of a few micrometers to the aluminium layer.
11. A process for producing an aluminium-clad composite substantially as hereinbefore described in the foregoing Example.
12. An aluminium-clad composite produced by the process claimed in any preceding claim.
GB08418872A 1983-07-30 1984-07-24 Process for producing aluminium-clad composite materials by roll cladding Expired GB2144061B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19833327657 DE3327657A1 (en) 1983-07-30 1983-07-30 METHOD FOR PRODUCING ALUMINUM COMPOSITES

Publications (3)

Publication Number Publication Date
GB8418872D0 GB8418872D0 (en) 1984-08-30
GB2144061A true GB2144061A (en) 1985-02-27
GB2144061B GB2144061B (en) 1986-01-02

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DE (1) DE3327657A1 (en)
FR (1) FR2549758A1 (en)
GB (1) GB2144061B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20170014941A1 (en) * 2014-04-01 2017-01-19 Toyo Kohan Co., Ltd. Method for producing metal laminate material
US10392687B2 (en) * 2010-03-12 2019-08-27 Centre National De La Recherche Scientifique (Cnrs) Method for manufacturing a metal assembly having a sheet of thermally treated aluminum to obtain alpha alumina and another sheet having surface irregularities that become embedded in said surface during roll bonding
GB2602039A (en) * 2020-12-16 2022-06-22 Mahle Engine Systems Uk Ltd Method of manufacturing a strip for a bearing

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3412779C1 (en) * 1984-04-05 1985-11-07 Kolbenschmidt AG, 7107 Neckarsulm Method of making a synchronizer ring
AT400174B (en) * 1994-02-21 1995-10-25 Miba Gleitlager Ag BEARINGS
DE102007049383A1 (en) 2007-10-15 2009-04-16 Wickeder Westfalenstahl Gmbh Composite material, in particular friction composite material and method for producing a composite material

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3340597A (en) * 1963-06-28 1967-09-12 Reynolds Metals Co Method of bonding
US3481023A (en) * 1965-08-26 1969-12-02 Texas Instruments Inc Method of making a composite metal product
BE756700A (en) * 1969-09-25 1971-03-01 Clevite Corp STEEL BUSHINGS WITH ALUMINUM SURFACE AND METHOD FOR MANUFACTURING THEM
US3732083A (en) * 1970-08-13 1973-05-08 Federal Mogul Corp Composite article

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10392687B2 (en) * 2010-03-12 2019-08-27 Centre National De La Recherche Scientifique (Cnrs) Method for manufacturing a metal assembly having a sheet of thermally treated aluminum to obtain alpha alumina and another sheet having surface irregularities that become embedded in said surface during roll bonding
US20170014941A1 (en) * 2014-04-01 2017-01-19 Toyo Kohan Co., Ltd. Method for producing metal laminate material
US10259073B2 (en) * 2014-04-01 2019-04-16 Toyo Kohan Co., Ltd. Method for producing metal laminate material
GB2602039A (en) * 2020-12-16 2022-06-22 Mahle Engine Systems Uk Ltd Method of manufacturing a strip for a bearing
EP4015854A1 (en) * 2020-12-16 2022-06-22 Mahle Engine Systems UK Limited Method of manufacturing a strip for a bearing
GB2602039B (en) * 2020-12-16 2024-04-24 Mahle Engine Systems Uk Ltd Method of manufacturing a strip for a bearing
US12055182B2 (en) 2020-12-16 2024-08-06 Mahle International Gmbh Method of manufacturing a strip for a bearing

Also Published As

Publication number Publication date
FR2549758A1 (en) 1985-02-01
GB8418872D0 (en) 1984-08-30
DE3327657A1 (en) 1985-02-07
GB2144061B (en) 1986-01-02

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