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US2238399A - Bearing alloy - Google Patents

Bearing alloy Download PDF

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Publication number
US2238399A
US2238399A US135111A US13511137A US2238399A US 2238399 A US2238399 A US 2238399A US 135111 A US135111 A US 135111A US 13511137 A US13511137 A US 13511137A US 2238399 A US2238399 A US 2238399A
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US
United States
Prior art keywords
alloy
bearing
cadmium
aluminum
silicon
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
US135111A
Inventor
Alfred W Schluchter
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.)
Motors Liquidation Co
Original Assignee
General Motors 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 General Motors Corp filed Critical General Motors Corp
Priority to US135111A priority Critical patent/US2238399A/en
Application granted granted Critical
Publication of US2238399A publication Critical patent/US2238399A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/02Alloys based on aluminium with silicon as the next major constituent
    • 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
    • Y10T29/49709Specific metallic composition

Definitions

  • the invention relates to alloys of the type in which aluminum constitutes the major constituent and is more especially concerned with alloys having properties rendering the alloy suitable for use in bearings.
  • Aluminum and most .of the alloys having a high aluminum content are not at all suitable for use in bearings for machine parts of iron or steel for the reason that aluminum tends to adhere to or combine with the ferrous metal, thereby causing scoring or seizing. found, however, that by a suitable combination of alloying constituents this difliculty may be overcome and an alloy produced having not only high antifriction properties'but other properties especially desirable in a bearing metal.
  • This novel bearing alloy comprises chiefly aluminum but with the addition of silicon preferably within the approximate range of 2-10% by weight of the completed alloy and a relatively small addition of cadmium.
  • This alloy has shown under test excellent antifriction properties so that it did not score or gall in' contact with a steel shaft and neither the bearing nor the shaft showed any appreciable,
  • the -casting may be advantageously carried out in metal molds.
  • the alloy may either be cast in the desired form for use in bearings or it may be cast in ingots, rolled down to strip or sheet material of the desired thickness and bearing liners or other bearing elements formed from the rolled stock.
  • Cast articles in which the structure shows a considerable continuous network of segregated metal compounds may be improved as to fatigue resistance by suitable heat treatment.
  • suitable heat treatment For example, I have found effective a heat treatment at 950 F. for a period of seventeen hours.
  • the specific gravity of the alloy is about onethird that of a tin-bronze bearing alloy, and its much greater resistance to fatigue or to cracking under the pounding action of bearings, such as connecting rod bearings, renders itparticularly suitable for useunder extreme conditions, especially in view of the remarkable absence of wear, either of the bearing or the shaft;
  • said alloy .consisting of aluminum '85-96 /z%, silicon not over approximately 10%
  • the resistance ture may be obtained by casting the alloy from a higher temperature than the melting point. For example, I may fuse the constituents at approximately 1200 F., then raise the temperature of segregated metallic elements.
  • a bearing formed of an alloy principally aluminum and containing lesser amounts of cadmium and silicon, said alloy characterized by high antifriction qualities and fatigue resistance and having a physical structure free from continuous networks of segregated metallic constituents 4.
  • the process of making a bearing comprising fusing a material composed of silicon 2-10%, cadmium 'l -596 and the remainder substantially aluminum, raising the temperature'of the fused disintegration under impact and to attack by acids developed in lubricating oils;

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Sliding-Contact Bearings (AREA)

Description

Patented Apr. 15, 1941,
' BEARING ALLOY Alfred W. Schluchter, Dearborn, Mich., assignor to General Motors Corporation, Detroit, Micln, a
corporation of Delaware No Drawing. ApplicatibnApril 5, 1937, Serial No. 135,111
7 Claims. (01. 308-242) The invention relates to alloys of the type in which aluminum constitutes the major constituent and is more especially concerned with alloys having properties rendering the alloy suitable for use in bearings.
Aluminum and most .of the alloys having a high aluminum content are not at all suitable for use in bearings for machine parts of iron or steel for the reason that aluminum tends to adhere to or combine with the ferrous metal, thereby causing scoring or seizing. found, however, that by a suitable combination of alloying constituents this difliculty may be overcome and an alloy produced having not only high antifriction properties'but other properties especially desirable in a bearing metal.
This novel bearing alloy comprises chiefly aluminum but with the addition of silicon preferably within the approximate range of 2-10% by weight of the completed alloy and a relatively small addition of cadmium.
It hasbeen generally recognized that the addition of cadmium to aluminum causes brittleness (Patent 1,'75,7'l4 Hybinette). In the presence of silicon, however, I find' that cadmium may be present in amounts up to about 5% without causing brittleness. In fact, the resulting alloy is remarkably resistant to disintegration under impact or "pounding such as occurs in severe bearing service. For most desirable anti- I have friction properties the cadmium content should be withinthe approximate range of lye-5%.
Very satisfactory results have been obtained with an alloy containing constituents by weight as follows:
This alloy has shown under test excellent antifriction properties so that it did not score or gall in' contact with a steel shaft and neither the bearing nor the shaft showed any appreciable,
to approximately 1400 F. or slightly higher and then cast. The -casting may be advantageously carried out in metal molds. The suitable tem-.
perature for castingmay be readily determined by the fact that the cadmium just begins to vaporize or "smoke at that point and it is obviously desirable, in order to avoid loss of cadmium, not to raise the temperature higher. The alloy may either be cast in the desired form for use in bearings or it may be cast in ingots, rolled down to strip or sheet material of the desired thickness and bearing liners or other bearing elements formed from the rolled stock.
Cast articles in which the structure shows a considerable continuous network of segregated metal compounds may be improved as to fatigue resistance by suitable heat treatment. For example, I have found effective a heat treatment at 950 F. for a period of seventeen hours.
'The specific gravity of the alloy is about onethird that of a tin-bronze bearing alloy, and its much greater resistance to fatigue or to cracking under the pounding action of bearings, such as connecting rod bearings, renders itparticularly suitable for useunder extreme conditions, especially in view of the remarkable absence of wear, either of the bearing or the shaft;
,- resistance, said alloy .consisting of aluminum '85-96 /z%, silicon not over approximately 10%,
and cadmium not over approximately 5%.
2. A bearing formed of an alloy comprising silicon and cadmium together amounting to not over approximately 15% and the remainder substantially aluminum, the physical structure of the alloy characterized by a discontinuous network wear after long and severe use. The resistance ture may be obtained by casting the alloy from a higher temperature than the melting point. For example, I may fuse the constituents at approximately 1200 F., then raise the temperature of segregated metallic elements.
3. A bearing formed of an alloy principally aluminum and containing lesser amounts of cadmium and silicon, said alloy characterized by high antifriction qualities and fatigue resistance and having a physical structure free from continuous networks of segregated metallic constituents 4. The process of making a bearing comprising fusing a material composed of silicon 2-10%, cadmium 'l -596 and the remainder substantially aluminum, raising the temperature'of the fused disintegration under impact and to attack by acids developed in lubricating oils;
7. A bearing characterized by high anti-friction properties and high resistance to disintegration under impact and to attack by acids developed in lubricating oils, said bearing consisting essentially of silicon 240%, cadmium 1 -5%, and the balance aluminum and having the physical structure resulting from casting at a temperature higher than the melting point but not above approximately 1400 F., and subsequent heat treatment at approximately 950 F. for a period of approximately seventeen hours.
ALFRED W. SCI-ILUCHTER.
US135111A 1937-04-05 1937-04-05 Bearing alloy Expired - Lifetime US2238399A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2752240A (en) * 1952-12-27 1956-06-26 Gen Motors Corp Aluminum base alloy bearing
US2763546A (en) * 1951-10-06 1956-09-18 Gen Motors Corp Aluminum base bearing
US2766116A (en) * 1951-10-06 1956-10-09 Gen Motors Corp Aluminum base bearing
US2770031A (en) * 1953-04-16 1956-11-13 Gen Motors Corp Bearing
US2807540A (en) * 1952-03-15 1957-09-24 Gen Motors Corp Aluminum base bearing
US2831764A (en) * 1953-04-16 1958-04-22 Gen Motors Corp Bearing
US2894319A (en) * 1954-12-29 1959-07-14 Gen Motors Corp Sintered powdered aluminum base bearing
US3791820A (en) * 1972-06-23 1974-02-12 Atomic Energy Commission Fluxless aluminum brazing

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2763546A (en) * 1951-10-06 1956-09-18 Gen Motors Corp Aluminum base bearing
US2766116A (en) * 1951-10-06 1956-10-09 Gen Motors Corp Aluminum base bearing
US2807540A (en) * 1952-03-15 1957-09-24 Gen Motors Corp Aluminum base bearing
US2752240A (en) * 1952-12-27 1956-06-26 Gen Motors Corp Aluminum base alloy bearing
US2770031A (en) * 1953-04-16 1956-11-13 Gen Motors Corp Bearing
US2831764A (en) * 1953-04-16 1958-04-22 Gen Motors Corp Bearing
US2894319A (en) * 1954-12-29 1959-07-14 Gen Motors Corp Sintered powdered aluminum base bearing
US3791820A (en) * 1972-06-23 1974-02-12 Atomic Energy Commission Fluxless aluminum brazing

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