US3652344A - Aluminum alloy-steel bearing and method of making same - Google Patents

Aluminum alloy-steel bearing and method of making same Download PDF

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Publication number
US3652344A
US3652344A US861196A US3652344DA US3652344A US 3652344 A US3652344 A US 3652344A US 861196 A US861196 A US 861196A US 3652344D A US3652344D A US 3652344DA US 3652344 A US3652344 A US 3652344A
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Prior art keywords
bearing
temperature
percent
bearing material
blanks
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US861196A
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English (en)
Inventor
George R Kingsbury
Raymond L Slater
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JPI Transportation Products Inc
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Clevite Corp
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Assigned to IMPERIAL CLEVITE INC., A CORP. OF PA reassignment IMPERIAL CLEVITE INC., A CORP. OF PA ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: GOULD INC., A CORP. OF DE
Assigned to CLEVITE INDUSTRIES INC., A CORP. OF DE. reassignment CLEVITE INDUSTRIES INC., A CORP. OF DE. MERGER (SEE DOCUMENT FOR DETAILS). Assignors: IMPERIAL CLEVITE INC., A PA. CORP. (MERGED INTO)
Assigned to JPI ACQUISITION, INC., ( JPI"),A CORP. OF MICHIGAN reassignment JPI ACQUISITION, INC., ( JPI"),A CORP. OF MICHIGAN ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: CLEVITE INDUSTRIES INC.,
Assigned to JPI TRANSPORTATION PRODUCTS, INC. reassignment JPI TRANSPORTATION PRODUCTS, INC. MERGER (SEE DOCUMENT FOR DETAILS). Assignors: D.A.B. INDUSTRIES, INC. (MERGED INTO), JPI ACQUISITION, INC. (CHANGE TO)
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Expired - Lifetime legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/02—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers
    • B22F7/04—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers with one or more layers not made from powder, e.g. made from solid metal
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/003—Alloys based on aluminium containing at least 2.6% of one or more of the elements: tin, lead, antimony, bismuth, cadmium, and titanium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C24/00—Coating starting from inorganic powder
    • C23C24/08—Coating starting from inorganic powder by application of heat or pressure and heat
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02—Parts of sliding-contact bearings
    • F16C33/04—Brasses; Bushes; Linings
    • F16C33/06—Sliding surface mainly made of metal
    • F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
    • F16C33/121—Use of special materials
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02—Parts of sliding-contact bearings
    • F16C33/04—Brasses; Bushes; Linings
    • F16C33/06—Sliding surface mainly made of metal
    • F16C33/14—Special methods of manufacture; Running-in
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2220/00—Shaping
    • F16C2220/60—Shaping by removing material, e.g. machining
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2220/00—Shaping
    • F16C2220/80—Shaping by separating parts, e.g. by severing, cracking
    • F16C2220/82—Shaping by separating parts, e.g. by severing, cracking by cutting
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2223/00—Surface treatments; Hardening; Coating
    • F16C2223/10—Hardening, e.g. carburizing, carbo-nitriding
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S384/00—Bearings
    • Y10S384/90—Cooling or heating
    • Y10S384/912—Metallic
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49636—Process for making bearing or component thereof
    • Y10T29/49703—Sealing
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12736—Al-base component
    • Y10T428/1275—Next to Group VIII or IB metal-base component
    • Y10T428/12757—Fe

Definitions

  • ABSTRACT Bimetallic bearing material comprising aluminum alloys consisting of silicon, cadmium, copper, magnesium, and the balance aluminum, bonded directly on steel backings, are heat treated to efi'ect improved hardness and fatigue resistance.
  • the heat treatment comprises solution heating said bearing material at temperatures ranging from 900 F. to 975 F. for at least 15 seconds but not exceeding 80 seconds, after which it is rapidly quenched in a fluid medium having a maximum temperature of 100 F., followed by precipitation heat treatment at about 350 F. for ten hours.
  • the present invention relates to a bearing comprising aluminum alloy directly bonded on a steel backing. More specifibearings comprising aluminum alloys directly bonded onto steel supports or backings.
  • the aluminum alloy consists of aluminum having small amounts of silicon, cadmium, copper, and magnesium.
  • the steel backing can be any of a number of low carbon steels.
  • solution heat treatments in the order of five minutes and longer are not necessary. in fact, solution heat treatment in the order of 15 seconds is quite satisfactory for obtaining the desired properties of fatigue resistance and strength. Furthermore, heat treatment of finished bearings may be undesirable because of damage to the finely finished bearing surfaces.
  • Another object of the invention is to provide a heat treatment for hearing material, in strip, blank, or semifinished bearing form, thereby improving the strength and fatigue resistance of the finished bearings.
  • a further object of the invention is to provide high quality bearings suitable for use under high loadings and speed conditrons.
  • steel of the type commercially known as SAE 1010 or 1008 may be used as the material for the backing support, though other steel types may be used.
  • Low carbon steel is preferred because it endures a greater rolling reduction which results in an improved bond. Also, it has lower initial hardness and is less subject to cold working during cladding and forming.
  • the aluminum alloy As to the aluminum alloy, it is directly bonded onto the steel backing to form the bearing material in accordance with the method disclosed in U.S. Pat. No.- 3,300,838, assigned to the same assignee of the present invention.
  • the heat-treatment response of the aluminum alloy is related to the copper and magnesium content, as well as the silicon content.
  • Aluminum alloys having silicon 2-8 percent, cadmium 0.5-4 percent, copper 0.05-15 percent, magnesium 0.1-0.2 percent, and the balance aluminum, have proven very satisfactory and the invention contemplates only alloys having the above compositions.
  • the thickness of the layer of aluminum alloy and/or the overall thickness of the composite structure, i.e., the bearing material depend on the intended use of the finished bearing.
  • the bimetallic bearing material can be treated in strip, blank, or semi-finished bearing form.
  • the steel backed clad aluminum strip is attached to a pulling unit leading into a molten lead bath maintained at temperature ranging from 900 to 975 F., preferably about 950 F.
  • the strip is then pulled out at a speed permitting it to be heated at said temperature range for a minimum time of 15 seconds. Heat-up time takes usually about a minute. Thus, total immersion in the lead bath may take about seconds.
  • a fluid medium such as water or oil having a maximum temperature of l00 F preferably about 75 F.
  • the time between removal from the lead bath to quenching should be such that the temperature of the strip is not allowed to drop below 850 F. Intervals in the order of 30 seconds are usually satisfactory. It should be emphasized that the drop in temperature prior to quenching is of important consideration. The short heating cycle is sufficient to cause the copper, magnesium, and a portion of the silicon to go into solid solution with the aluminum under equilibrium conditions and rapid quenching is necessary to preserve a condition of super saturation.
  • the strip After quenching, the strip is air dried and hardened by precipitation heat treatment at 350 F. for about ten hours in a recirculating air furnace, or other heating means. A minimum hardness of 62 on the Rockwell l5 T-scale is obtained for 0.010 inch thick aluminum alloy liner.
  • the strip is then fabricated into bearings and the bearing surface is machined and plated at the bearing surface with an overlay having thickness of 0.0004 to 0.0006 inches.
  • the overlay comprises generally a high lead alloy having copper and tin.
  • the bimetallic strip may be heat treated in the molten lead bath as described above. After quenching, the bearing strip is cut into bearing blanks which are channelled, and roll-formed into shells. The formed bearings are then hardened by precipitation heat treatment in a recirculating air furnace at about 350 F. for 10 hours to a minimum R T 62 hardness for a 0.010 inch thick alloy liner.
  • molten salt baths Other media for solution heat treatment can be utilized such as molten salt baths.
  • the bimetallic strip can be cut into bearing blanks which are then placed in convenient means such as metal baskets which can be lowered into the molten salt bath having a temperature ranging from 900-975 F.
  • the blanks are then maintained at said temperature for a minimum of 15 seconds excluding heat-up time which is usually about one minute.
  • the blanks are then quenched in a fluid medium such as water (maximum temperature F.). Again, keeping in mind that the interval between removing from the molten salt bath and the quenching is such that the temperature of the blanks does not drop below 850 F. Normally, a delay time of up to 30 seconds is satisfactory.
  • the blanks are then dried and precipitation hardened at about 350 F. for ten hours in a recirculating air furnace.
  • Bearings are then fabricated from the hardened blanks as described hereinbefore.
  • the blanks are channelled and rollformed into shells after the solution heat treatment, then they are precipitation hardened at 350 F., as described.
  • the bimetallic strip is annealed at 650 F. for 30 minutes prior to solution heat treatment.
  • EXAMPLE I DIESEL ROD BEARlNG An aluminum alloy having a composition of 3.94 percent silicon, 1.0 percent cadmium, 0.13 percent copper, 0.14 percent magnesium, and the balance aluminum, was directly bonded onto a steel backing (SAE 1010) having a thickness of 0.085 inches to form a bimetallic strip having a thickness of 0.100 inch.
  • SAE 1010 steel backing
  • the strip was cut into blanks which were heated in a neutral molten salt bath at 950 F. for 65 seconds, 50 seconds were required for heat-up time.
  • the blanks were then removed from the bath and rapidly quenched in water at 75 F.
  • the blanks were then precipitation hardened by heating in an air recirculating furnace at 350 F. for 10 hours.
  • the alu- EXAMPLE II An aluminum alloy having a composition of 3.94 percent silicon, 1.0 percent cadmium, 0.13 percent copper, 0.14 percent magnesium, and the balance aluminum, was directly bonded onto a steel backing (SAE 1010) having a thickness of
  • DIESEL MAIN BEARING An aluminum alloy having the composition 3.70 percent silicon, 1.l percent cadmium, 0.15 percent magnesium, 0.10 percent copper, and the balance aluminum, was directly bonded onto an SAE 1010 steel backing (0.139 inch thick) to form a bimetallic bearing strip of 0.166 inch thickness.
  • the strip was cut into blanks which were solution heat treated in a neutral molten salt bath at 950 F as done in Example 1. After precipitation hardening at 350 F. for hours, the average hardness of the aluminum alloy layer measured 69 on R T scale. The blanks were then fabricated into bearings having 0.156 inch wall thickness. Hardness of the aluminum alloy liner had an average of 70 on R ,,T scale. Similar to Example I, the bearing was plated with an over-lay (0.0005 inch thick) having the same composition.
  • EXAMPLE III DIESEL FLANGE MAIN BEARING An aluminum alloy having the same composition of Example II was directly bonded on an SAE 1010 steel backing (0.089 inch thick) to form a bimetallic bearing strip having 0.1 19 inch thickness. The strip was cut into blanks which were solution heat-treated, similar to Examples I and II. The quenched blanks were then formed into flange bearing halfshells which were precipitation hardened, as described in the previous examples. The aluminum alloy layer, was found to have an average hardness of 69 on R T scale. The formed shells were then machined to a wall thickness of 0.102 inch, after which an over-lay of about 0.0005 inch was plated on the bearing surface.
  • a method for making a bimetallic bearing having improved fatigue resistance and strength which comprises the steps of:
  • step (a) the bearing material is made in strip form, in which in step (b) the bearing material is heated in molten lead bath having a temperature range of from 900to 975 F. and m which In step (d) the fluid medium is water having a maximum temperature of 100 F.
  • a method for improving fatigue resistance and strength of a bimetallic bearing which comprises the steps of:
  • step (a) the bearing material is made in strip form; in which in step (c) the bearing material is heated in a medium selected from the group consisting of molten lead and neutral molten salt, and in which in step (e) the fluid medium is water having a maximum temperature of 100 F.
  • a method for improving fatigue resistance and strength of a bimetallic bearing which comprises the steps of:
  • step (d) the bearing blanks are heated in neutral molten salt bath having a temperature range of from 900 to 975 F and in which in step (f) the fluid medium is water having a maximum temperature of 100 F.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Metallurgy (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Composite Materials (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Sliding-Contact Bearings (AREA)
  • Coating With Molten Metal (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
US861196A 1969-09-25 1969-09-25 Aluminum alloy-steel bearing and method of making same Expired - Lifetime US3652344A (en)

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US86119669A 1969-09-25 1969-09-25

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Country Status (8)

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US (1) US3652344A (de)
JP (1) JPS5144883B1 (de)
BE (1) BE756700A (de)
CA (1) CA922500A (de)
DE (1) DE2043676C3 (de)
FR (1) FR2060705A5 (de)
GB (1) GB1282806A (de)
NL (1) NL7014107A (de)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4881716A (de) * 1972-01-20 1973-11-01
US3871926A (en) * 1972-11-02 1975-03-18 Chace Co W M Process for producing a composite metallic article
US4170469A (en) * 1977-08-09 1979-10-09 Daido Metal Company Ltd. Aluminum base bearing alloy and a composite bearing made of the alloy with a steel backing plate
US4191238A (en) * 1976-04-28 1980-03-04 Ab Volvo Penta Connecting rod or the like and method and mould for producing connecting rods or the like
US5075177A (en) * 1990-04-10 1991-12-24 Daido Metal Company Ltd. Aluminum alloy bearing for use in low-rigidity housing and method of producing same
US5601371A (en) * 1994-02-21 1997-02-11 Miba Gleitlager Aktiengesellschaft Sliding surface bearing
US6596671B2 (en) 2000-11-15 2003-07-22 Federal-Mogul World Wide, Inc. Non-plated aluminum based bearing alloy with performance-enhanced interlayer
US20080025658A1 (en) * 2005-11-14 2008-01-31 Brp-Rotax Gmbh & Co. Kg Friction-bearing assembly for a rotating shaft
US20080169257A1 (en) * 2007-01-17 2008-07-17 Itrec B.V. Hoisting crane with annular bearing structure

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3327657A1 (de) * 1983-07-30 1985-02-07 Kolbenschmidt AG, 7107 Neckarsulm Verfahren zur herstellung von aluminium-verbundwerkstoffen
DE3843927A1 (de) * 1988-12-24 1990-06-28 Kolbenschmidt Ag Verfahren zur herstellung von lagerungen
DE69021211T2 (de) * 1990-09-05 1995-12-07 Fokker Aircraft Laminat für gebogene Struktur und Verfahren zu ihrer Herstellung.
EP0638736B1 (de) * 1993-08-09 1997-07-16 GLYCO-METALL-WERKE Glyco B.V. & Co. KG In einer Maschine angeordnetes Gleitlager und Verfahren zur Aushärtung
CN102672425B (zh) * 2012-04-28 2014-07-02 重庆市江津区宏盛机械制造有限公司 转盘加工工艺
CN114737091A (zh) * 2022-03-14 2022-07-12 珠海市润星泰电器有限公司 一种用于汽车构件的压铸铝合金及其制备方法

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2807540A (en) * 1952-03-15 1957-09-24 Gen Motors Corp Aluminum base bearing
US3268369A (en) * 1961-04-10 1966-08-23 Gen Motors Corp Process for hardening the aluminum alloy portion of an aluminum alloysteel bearing
US3300838A (en) * 1965-04-30 1967-01-31 Clevite Corp Method of making bimetallic bearing material

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2807540A (en) * 1952-03-15 1957-09-24 Gen Motors Corp Aluminum base bearing
US3268369A (en) * 1961-04-10 1966-08-23 Gen Motors Corp Process for hardening the aluminum alloy portion of an aluminum alloysteel bearing
US3300838A (en) * 1965-04-30 1967-01-31 Clevite Corp Method of making bimetallic bearing material

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Metals Handbook, Vol. 2, 8th Ed., 1964, pages 64 66 *

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4881716A (de) * 1972-01-20 1973-11-01
JPS5638667B2 (de) * 1972-01-20 1981-09-08
US3871926A (en) * 1972-11-02 1975-03-18 Chace Co W M Process for producing a composite metallic article
US4191238A (en) * 1976-04-28 1980-03-04 Ab Volvo Penta Connecting rod or the like and method and mould for producing connecting rods or the like
US4170469A (en) * 1977-08-09 1979-10-09 Daido Metal Company Ltd. Aluminum base bearing alloy and a composite bearing made of the alloy with a steel backing plate
US5075177A (en) * 1990-04-10 1991-12-24 Daido Metal Company Ltd. Aluminum alloy bearing for use in low-rigidity housing and method of producing same
US5601371A (en) * 1994-02-21 1997-02-11 Miba Gleitlager Aktiengesellschaft Sliding surface bearing
US6596671B2 (en) 2000-11-15 2003-07-22 Federal-Mogul World Wide, Inc. Non-plated aluminum based bearing alloy with performance-enhanced interlayer
US20080025658A1 (en) * 2005-11-14 2008-01-31 Brp-Rotax Gmbh & Co. Kg Friction-bearing assembly for a rotating shaft
US20080169257A1 (en) * 2007-01-17 2008-07-17 Itrec B.V. Hoisting crane with annular bearing structure

Also Published As

Publication number Publication date
JPS5144883B1 (de) 1976-12-01
BE756700A (fr) 1971-03-01
NL7014107A (de) 1971-03-29
GB1282806A (en) 1972-07-26
CA922500A (en) 1973-03-13
FR2060705A5 (de) 1971-06-18
DE2043676A1 (de) 1971-04-22
DE2043676C3 (de) 1980-09-11
DE2043676B2 (de) 1980-01-10

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