[go: up one dir, main page]

US2763058A - Process of producing steel-aluminum bi-metal strip - Google Patents

Process of producing steel-aluminum bi-metal strip Download PDF

Info

Publication number
US2763058A
US2763058A US265356A US26535652A US2763058A US 2763058 A US2763058 A US 2763058A US 265356 A US265356 A US 265356A US 26535652 A US26535652 A US 26535652A US 2763058 A US2763058 A US 2763058A
Authority
US
United States
Prior art keywords
aluminum
strip
steel
strips
aluminum 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.)
Expired - Lifetime
Application number
US265356A
Inventor
William E Mccullough
Wilbur E Wyatt
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bohn Aluminum and Brass Corp
Original Assignee
Bohn Aluminum and Brass Corp
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.)
Filing date
Publication date
Application filed by Bohn Aluminum and Brass Corp filed Critical Bohn Aluminum and Brass Corp
Priority to US265356A priority Critical patent/US2763058A/en
Application granted granted Critical
Publication of US2763058A publication Critical patent/US2763058A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/14Special methods of manufacture; Running-in
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2223/00Surface treatments; Hardening; Coating
    • F16C2223/02Mechanical treatment, e.g. finishing
    • F16C2223/08Mechanical treatment, e.g. finishing shot-peening, blasting
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2223/00Surface treatments; Hardening; Coating
    • F16C2223/30Coating surfaces
    • F16C2223/32Coating surfaces by attaching pre-existing layers, e.g. resin sheets or foils by adhesion to a substrate; Laminating
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2223/00Surface treatments; Hardening; Coating
    • F16C2223/30Coating surfaces
    • F16C2223/70Coating surfaces by electroplating or electrolytic coating, e.g. anodising, galvanising
    • 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
    • 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
    • Y10S428/94Pressure bonding, e.g. explosive
    • 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
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49636Process for making bearing or component thereof
    • Y10T29/49643Rotary bearing
    • Y10T29/49647Plain bearing
    • Y10T29/49668Sleeve or bushing making
    • Y10T29/49671Strip or blank material shaping
    • Y10T29/49673Die-press shaping
    • Y10T29/49675Die-press shaping having inner lining layer

Definitions

  • the present invention is an improvement on the process disclosed in-UJS. Patent N'o.- 2,277 ,023- toSteiner et 'al., whichcovers broadly the. processof rolling-a layer of aluminum bearing alloy to a ferrous baseundercornbined heat and pressure. According to the present invention certain steps are taken to insure a reliable bond between the aluminum alloy and the steel when the process is used on a commercial scale, thus making it a more reliable production process and reducing the percentage of defective material.
  • steel of the type known commercially as SAE 1010 of proper thickness and width for the type of bearing to be made from the completed bi-metal. If the bearings are to be relatively thin and narrow, of the type sometimes called strip bearings, the steel will have corresponding dimensions. If the bi-metal is to be formed into heavier bearings commonly known as the flanged type, the steel strip will of course have to be heavier and wider.
  • the aluminum alloy lining may be of any suitable aluminum alloy having good bearing properties, those containing tin being especially useful for the purpose.
  • An aluminum alloy preferred by us has the following composition; magnesium 2.5%, tin 2.0%, aluminum, balance.
  • the steel strip is first cleaned in any preferred manner to remove grease and dirt.
  • the surface to be bonded to the aluminum is then roughened slightly, as by grit blasting, and is nickel-plated to a thickness of .0003 to .0005 inch.
  • This coating of nickel permits the subsequent formation of an interlayer of nickel between the steel and the aluminum.
  • This interlayer of nickel prevents the formation of the extremely brittle iron-aluminum compound which, if present, impairs the strength of the bond between the steel and the aluminum alloy.
  • the nickel bond is sufliciently ductile to permit bending the edges of the bi-metal strip over into right-angle flanges if necessary.
  • the layer of nickel must be thin, of the size indicated, to give these desired properties.
  • Sttes Patent Prepanationofi aluminum Astiip'ofithealuminum alloy'ofthepproper width and thickness forthepropose'd heating is prepared by brushing with awirebrushto remove'a'luminum oxide.
  • Oxygen should be removed from the gas by converting it to water vapor prior to passing the gas through the electro-dryer.
  • Pressure rolling In order to bond together the steel and aluminum strips, prepared and heated as described above, they are brought into contact with each other and passed through pressure rolls which apply sufficient pressure to cause a reduction of from 33% to 40% in the thickness of the aluminum. This amount of pressure is suflicient to firmly bond the aluminum strip to the nickel-plated steel strip. Ideally the pressure should be applied while the strips are still in the protective atmosphere, but since it is mechanically ditficult to operate high pressure rolls within a chamber containing the protective atmosphere, the rolls should be located as close as possible to the point of exit from the chamber, and preferably the exit from the chamber should be formed with a nose or other device to extend the atmosphere to, or close to, the point of rolling.
  • both the steel and aluminum strips may be in the form of individual pieces of suitable length.
  • both the steel and aluminum strips may be in the form of coils, and the process may be carried out as a continuous process.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Sliding-Contact Bearings (AREA)

Description

PROCESS OF PRODUCEJG STEEL-ALUMINUM BI-METAL STRIP William E.'McCullough and Wilbur -E. Wyatt, Detroit,
Mich, 'assignors to Bohn Aluminum'and Brass Cor- .poration No -Drawing. ApplicationJaijuary 7, 19 52, -Serial-No.-265,356
s'ciims. 0.29488 I Inthe manufacture"ofprecision type interchangeable bearingsit' is sometimes desired to'produce a bearing in which thef'bearingsu'rfac'e is' a"la'yer"of' aluminum falloy, "with the'alum'im'nnla er su ported by a steelbac'king. The present invention is a process of producing steel -lined with aluminum alloy suitable for forming into bearings. This product will be referred to herein as bi-metal.
The present invention is an improvement on the process disclosed in-UJS. Patent N'o.- 2,277 ,023- toSteiner et 'al., whichcovers broadly the. processof rolling-a layer of aluminum bearing alloy to a ferrous baseundercornbined heat and pressure. According to the present invention certain steps are taken to insure a reliable bond between the aluminum alloy and the steel when the process is used on a commercial scale, thus making it a more reliable production process and reducing the percentage of defective material.
In carrying out the process of the invention we prefer to use steel of the type known commercially as SAE 1010, of proper thickness and width for the type of bearing to be made from the completed bi-metal. If the bearings are to be relatively thin and narrow, of the type sometimes called strip bearings, the steel will have corresponding dimensions. If the bi-metal is to be formed into heavier bearings commonly known as the flanged type, the steel strip will of course have to be heavier and wider.
The aluminum alloy lining may be of any suitable aluminum alloy having good bearing properties, those containing tin being especially useful for the purpose. An aluminum alloy preferred by us has the following composition; magnesium 2.5%, tin 2.0%, aluminum, balance.
Preparation of steel The steel strip is first cleaned in any preferred manner to remove grease and dirt. The surface to be bonded to the aluminum is then roughened slightly, as by grit blasting, and is nickel-plated to a thickness of .0003 to .0005 inch. This coating of nickel permits the subsequent formation of an interlayer of nickel between the steel and the aluminum. This interlayer of nickel prevents the formation of the extremely brittle iron-aluminum compound which, if present, impairs the strength of the bond between the steel and the aluminum alloy. The nickel bond is sufliciently ductile to permit bending the edges of the bi-metal strip over into right-angle flanges if necessary. The layer of nickel must be thin, of the size indicated, to give these desired properties.
It has previously been proposed to use a copper interlayer between steel and aluminum, but it has been found that when a bi-metal piece having a copper bond is held for prolonged periods at elevated temperatures, as in an internal combustion engine (at approximately 400 F.) the copper difiuses into the aluminum, thereby weakening the bond. Under similar circumstances the nickel bond is not adversely afiected.
Sttes Patent Prepanationofi aluminum Astiip'ofithealuminum alloy'ofthepproper width and thickness forthepropose'd heating is prepared by brushing with awirebrushto remove'a'luminum oxide.
:Pre-Jzea-tirzg .the strips The preferredaaluminum alloy mentioned. above .which containsv2%.-tinlrnay.he bonde'dtto the: steel strip. at temgperaturestof :1020rto 1040 F. under vthe: pressures-specified below. Both the steel .andraluminumt strips are heated -to .these temperatures: before subjecting-them" to the-bonding operation.
-Aluminum. al-l-oys containing-higher percentagesof tin amayabe pressure rbonded .at lower. temperatures. Thus, alloys containing approximately 6% ti-nmaybepressure bonded .attemperatur'es craze-940 F.
Protective atmosphere During gthmheating and-bonding operations-the materialsshould be kept-in-a suitable. protective atmosphere to; prevent.thecformation 'OfHOXiClCy-WhiCh interferes .with the formingwofzaygood :bond. From the standpoint of cost, .-ittis of.courseadvisableto use: the cheapest protec- -tive..atmosphereIthatiwill giveuadequate protectionhwith safety. I ItLis, possible .to...use ldissociated ammonia.
A We prefer to use partially combusted natural gas, because of its availability and low cost. Care must be taken however, to prevent the formation of carbon in the muffle chamber, since the finely divided carbon will deposit between the steel and aluminum strips, where it impairs the quality of the bond. T o prevent the precipitation of carbon the CO2 content should be sufficiently high to prevent the reaction 2 CO CO2+C. At the temperatures disclosed herein the gas should contain approximately one volume of CO2 for two volumes of CO. Percentagewise, the ratio should be approximately 4 to 5% CO2 and 10% CO.
The presence of moisture at the high temperatures involved would cause oxidation, and hence moisture in the protective atmosphere should be reduced to a minimum, as by the use of an electro-dryer.
Oxygen should be removed from the gas by converting it to water vapor prior to passing the gas through the electro-dryer.
Pressure rolling In order to bond together the steel and aluminum strips, prepared and heated as described above, they are brought into contact with each other and passed through pressure rolls which apply sufficient pressure to cause a reduction of from 33% to 40% in the thickness of the aluminum. This amount of pressure is suflicient to firmly bond the aluminum strip to the nickel-plated steel strip. Ideally the pressure should be applied while the strips are still in the protective atmosphere, but since it is mechanically ditficult to operate high pressure rolls within a chamber containing the protective atmosphere, the rolls should be located as close as possible to the point of exit from the chamber, and preferably the exit from the chamber should be formed with a nose or other device to extend the atmosphere to, or close to, the point of rolling.
In the case of bi-metal for large bearings the steel and aluminum strips may be in the form of individual pieces of suitable length. In the case of thin bi-metal for light bearings, both the steel and aluminum strips may be in the form of coils, and the process may be carried out as a continuous process.
According to the provisions of the patent statutes, we have explained the principles of our invention and have described what we now consider to represent its best embodiment. However, we desire to have it understood that,
within the scope of the appended claims, the invention may be practiced otherwise than asspecifically described.
We claim:
1. The process of producing a bi-metal strip of steel and aluminum alloy suitable for being subsequently fabricated into bearings, said process comprising: plating one side of a steel strip with a thin layer of nickel, mechanically cleaning one side of a strip of aluimnum alloy comprising a small amount of a hardening agent and a small amount of a lubricity agent, pre-heating the two strips in a protective atmosphere substantially free of moisture, oxygen or carbon, bringing the heated strips together with the strip of aluimnum alloy in contact with the nickelplated side of the steel strip, and bonding the two heated strips to each other by pressure which causes a reduction of between 33% to 40% in the thickness of the aluminum strip.
2. The process set forth in claim 1 in which the aluminum alloy contains approximately 2% of a hardening agent, and up to 6% of a lubricity agent.
3. The process of producing a bi-metal strip of steel and aluminum alloy suitable for being subsequently fabricated into bearings, said process comprising: plating one side of a strip of steel with nickel to a thickness of 0.0003 to 0.00005 inch, mechanically cleaning one side of a strip of aluiminum alloy containing approximately 2% of a hardening agent, and approximately 2% of a lubricity agent, pre-heating the two strips to temperatures between 1020 and 1040 F. while maintaining them in a protective atmosphere substantially free of moisture,
oxygen or carbon, bringing the heated strips together with the strip of aluminum alloy in contact with the nickelplated side of the steel strip, and bonding the two heated strips to each other by passing them through pressure rolls which cause a reduction of between 33% to in the thickness of the aluminum strip.
- References Cited in the file of this patent UNITED STATES PATENTS 1,577,171 Brownlee Mar. 16, 1926 1,637,033 Basch July 26,1927 1,667,787 Jaeger May 1, 1928 2,197,622 Sendzimir Apr. 16, 1940 2,473,888 Jordan June 21, 1949 2,490,543 Robertson et al Dec. 6, 1949 2,490,549 Schultz Dec. 6, 1949 2,539,246 Hensel Jan. 23, 1951 2,539,247 Hensel Jan. 23, 1951 2,539,248 Lynch Jan. 23, 1951 2,629,922 Finch Mar. 3, 1953 2,687,565 Schaefer et a1 Aug. 31, 1954 FOREIGN PATENTS 628,197 Great Britain Aug 24, 1949 OTHER REFERENCES Welding Handbook, Third Edition, p. 505, published by American Welding Society, 33 West 39th Street, New York 18, New York.

Claims (1)

1. THE PROCESS OF PRODUCING A BI-METAL STRIP OF STEEL AND ALUMINUM ALLOY SUITABLE FOR BEING SUBSEQUENTLY FABRICATED INTO BEARINGS, SAID PROCESS COMPRISING: PLATING ONE SIDE OF A STEEL WITH A THIN LAYER OF NICKEL, MECHANICALLY CLEANING ONE SIDE OF A STRIP OF ALUMINUM ALLOY COMPRISING A SMALL AMOUNT OF A HARDENING AGENT AND A SMALL AMOUNT OF A LUBRICITY AGENT, PRE-HEATING THE TWO STRIPS IN A PROTECTIVE ATMOSPHERE SUBSTANTIALLY FREE OF MOISTURE, OXYGEN OR CARBON, BRINGING THE HEATING STRIPS TOGETHER WITH THE STRIP OF ALUMINUM ALLOY IN CONTACT WITH THE NICKELPLATED SIDE OF THE STEEL STRIP, AND BONDING THE TWO HEATED STRIPS TO EACH OTHER BY PRESSURE WHICH CAUSES A REDUCTION OF BETWEEN 33% TO 40% IN THE THICKNESS OF THE ALUMINUM STRIP.
US265356A 1952-01-07 1952-01-07 Process of producing steel-aluminum bi-metal strip Expired - Lifetime US2763058A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US265356A US2763058A (en) 1952-01-07 1952-01-07 Process of producing steel-aluminum bi-metal strip

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US265356A US2763058A (en) 1952-01-07 1952-01-07 Process of producing steel-aluminum bi-metal strip

Publications (1)

Publication Number Publication Date
US2763058A true US2763058A (en) 1956-09-18

Family

ID=23010098

Family Applications (1)

Application Number Title Priority Date Filing Date
US265356A Expired - Lifetime US2763058A (en) 1952-01-07 1952-01-07 Process of producing steel-aluminum bi-metal strip

Country Status (1)

Country Link
US (1) US2763058A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3078563A (en) * 1959-10-23 1963-02-26 Federal Mogul Bower Bearings Method of bonding aluminum to steel by roll pressure
US3096577A (en) * 1956-01-12 1963-07-09 Westinghouse Electric Corp Method of making aluminum clad copper wire
US3201862A (en) * 1960-12-28 1965-08-24 Gotoh Kazuo Process for making steel-reinforced aluminum members
US3269004A (en) * 1963-05-06 1966-08-30 Allegheny Ludlum Steel Process of roll bonding stainless steel and aluminum
US3419953A (en) * 1966-01-06 1969-01-07 Aeroquip Corp Method of treating and connecting tube fittings
US3436805A (en) * 1965-08-09 1969-04-08 North American Rockwell Method of joining aluminum and ferrous members
US3436806A (en) * 1967-01-26 1969-04-08 North American Rockwell Method of forming an aluminum-ferrous tubular transition joint
US3468015A (en) * 1966-10-31 1969-09-23 Texas Instruments Inc Process of manufacturing strip contact material by inlaying peripherally clad noble-metal strip
US3532609A (en) * 1965-11-09 1970-10-06 Nippon Kokan Kk Process for the preliminary treatment adapted for the electrolytic formation of aluminum coatings on metallic surfaces in molten salt bath
WO1998034038A1 (en) 1997-02-04 1998-08-06 Federal-Mogul Corporation Laser-welded bearing and method of making same
WO2014059073A1 (en) * 2012-10-10 2014-04-17 Federal-Mogul Corporation Bi-material strip and a method of bonding strips of different materials together
CN109719382A (en) * 2017-10-30 2019-05-07 通用汽车环球科技运作有限责任公司 Welding method and the part manufactured by the welding method

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1577171A (en) * 1915-06-01 1926-03-16 Carbo Oxygen Company Process of metal cutting, welding, or the like
US1637033A (en) * 1925-06-05 1927-07-26 Gen Electric Composite electric conductor
US1667787A (en) * 1925-01-09 1928-05-01 Trierer Walzwerk Ag Method of applying a plating of aluminum to iron and steel sheets and bands
US2197622A (en) * 1937-04-22 1940-04-16 American Rolling Mill Co Process for galvanizing sheet metal
US2473888A (en) * 1947-06-10 1949-06-21 Gen Electric Lead-in wire for electric lamps and similar devices
GB628197A (en) * 1946-03-06 1949-08-24 Gen Motors Corp Improvements relating to composite metallic articles
US2490549A (en) * 1945-07-07 1949-12-06 Gen Motors Corp Method of making composite stock
US2490543A (en) * 1945-06-27 1949-12-06 Gen Motors Corp Method of making composite stock
US2539247A (en) * 1945-07-31 1951-01-23 Mallory & Co Inc P R Method of bonding aluminum to steel
US2539248A (en) * 1945-09-19 1951-01-23 Mallory & Co Inc P R Method of bonding aluminum alloys to steel
US2539246A (en) * 1944-10-07 1951-01-23 Mallory & Co Inc P R Method of making aluminum clad steel
US2629922A (en) * 1950-04-27 1953-03-03 Gen Electric Method of brazing resistor terminals
US2687565A (en) * 1951-02-21 1954-08-31 Clevite Corp Method of bonding aluminum to steel

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1577171A (en) * 1915-06-01 1926-03-16 Carbo Oxygen Company Process of metal cutting, welding, or the like
US1667787A (en) * 1925-01-09 1928-05-01 Trierer Walzwerk Ag Method of applying a plating of aluminum to iron and steel sheets and bands
US1637033A (en) * 1925-06-05 1927-07-26 Gen Electric Composite electric conductor
US2197622A (en) * 1937-04-22 1940-04-16 American Rolling Mill Co Process for galvanizing sheet metal
US2539246A (en) * 1944-10-07 1951-01-23 Mallory & Co Inc P R Method of making aluminum clad steel
US2490543A (en) * 1945-06-27 1949-12-06 Gen Motors Corp Method of making composite stock
US2490549A (en) * 1945-07-07 1949-12-06 Gen Motors Corp Method of making composite stock
US2539247A (en) * 1945-07-31 1951-01-23 Mallory & Co Inc P R Method of bonding aluminum to steel
US2539248A (en) * 1945-09-19 1951-01-23 Mallory & Co Inc P R Method of bonding aluminum alloys to steel
GB628197A (en) * 1946-03-06 1949-08-24 Gen Motors Corp Improvements relating to composite metallic articles
US2473888A (en) * 1947-06-10 1949-06-21 Gen Electric Lead-in wire for electric lamps and similar devices
US2629922A (en) * 1950-04-27 1953-03-03 Gen Electric Method of brazing resistor terminals
US2687565A (en) * 1951-02-21 1954-08-31 Clevite Corp Method of bonding aluminum to steel

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3096577A (en) * 1956-01-12 1963-07-09 Westinghouse Electric Corp Method of making aluminum clad copper wire
US3078563A (en) * 1959-10-23 1963-02-26 Federal Mogul Bower Bearings Method of bonding aluminum to steel by roll pressure
US3201862A (en) * 1960-12-28 1965-08-24 Gotoh Kazuo Process for making steel-reinforced aluminum members
US3269004A (en) * 1963-05-06 1966-08-30 Allegheny Ludlum Steel Process of roll bonding stainless steel and aluminum
US3436805A (en) * 1965-08-09 1969-04-08 North American Rockwell Method of joining aluminum and ferrous members
US3532609A (en) * 1965-11-09 1970-10-06 Nippon Kokan Kk Process for the preliminary treatment adapted for the electrolytic formation of aluminum coatings on metallic surfaces in molten salt bath
US3419953A (en) * 1966-01-06 1969-01-07 Aeroquip Corp Method of treating and connecting tube fittings
US3468015A (en) * 1966-10-31 1969-09-23 Texas Instruments Inc Process of manufacturing strip contact material by inlaying peripherally clad noble-metal strip
US3436806A (en) * 1967-01-26 1969-04-08 North American Rockwell Method of forming an aluminum-ferrous tubular transition joint
WO1998034038A1 (en) 1997-02-04 1998-08-06 Federal-Mogul Corporation Laser-welded bearing and method of making same
EP0958458B1 (en) * 1997-02-04 2005-04-13 Federal-Mogul Corporation Laser-welded bearing and method of making same
WO2014059073A1 (en) * 2012-10-10 2014-04-17 Federal-Mogul Corporation Bi-material strip and a method of bonding strips of different materials together
US9108275B2 (en) 2012-10-10 2015-08-18 Federal-Mogul Corporation Bi-material strip and a method of bonding strips of different materials together
CN109719382A (en) * 2017-10-30 2019-05-07 通用汽车环球科技运作有限责任公司 Welding method and the part manufactured by the welding method

Similar Documents

Publication Publication Date Title
US2763058A (en) Process of producing steel-aluminum bi-metal strip
US2117106A (en) Brazed article
US3078563A (en) Method of bonding aluminum to steel by roll pressure
US2539247A (en) Method of bonding aluminum to steel
US2735170A (en) Method-of producing a multilayer strep
US1840724A (en) Process of bonding cooling fins to cylinders
US2191460A (en) Article of manufacture
CN105316532B (en) Aluminium alloy bimetallic material manufacture method for sandwich construction sliding bearing
US2158461A (en) Method of making bearings
US2392917A (en) Silver cladding
US3386161A (en) Method of making bearing material
US2445858A (en) Laminated structure
JPH07197935A (en) Slide bearing and its manufacture
US1939467A (en) Method of making bearings
US2539248A (en) Method of bonding aluminum alloys to steel
US3350773A (en) Method of making bearings
JP2733735B2 (en) Copper lead alloy bearing
US2693121A (en) Method of making composite aluminum-lined steel-backed bearing material
EP0119036B1 (en) Metal-coating a metallic substrate
US2907105A (en) Method of soldering aluminum
JPS5843460B2 (en) Al alloy for thermal spraying
US2555497A (en) Process of manufacturing bearings
US3513520A (en) Method of making composite metal bearing strips
GB544903A (en) Improvements in methods of making composite metallic articles
US2969590A (en) Production of composite aluminous metal articles