US2306033A - Bearing - Google Patents

Bearing Download PDF

Info

Publication number
US2306033A
US2306033A US291322A US29132239A US2306033A US 2306033 A US2306033 A US 2306033A US 291322 A US291322 A US 291322A US 29132239 A US29132239 A US 29132239A US 2306033 A US2306033 A US 2306033A
Authority
US
United States
Prior art keywords
bearing
alloys
magnesium
lead
properties
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
US291322A
Inventor
Beck Adolf
Buchmann Walter
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.)
MAGNESIUM DEV CORP
MAGNESIUM DEVELOPMENT Corp
Original Assignee
MAGNESIUM DEV 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 MAGNESIUM DEV CORP filed Critical MAGNESIUM DEV CORP
Application granted granted Critical
Publication of US2306033A publication Critical patent/US2306033A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • 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
    • F16C33/12Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
    • F16C33/121Use of special materials

Definitions

  • the bearing metal alloys of the present invention preferably contain to of lead and/or 7 to 12% of cadmium.
  • Silver, bismuth and tin also may advantageously be present in the foregoing alloys in amounts of up to 12%, but only provided that the total content of alloy formers in the alloys does not exceed about By comparison withhitherto proposed light bearing metal alloys, the bearing metal alloys of the present invention possess more favourable enhanced.
  • the alloys of the present invention are somewhat deficient in re-' spect of fatigue strength and heat strength.
  • cerium in amounts of from about 0.5 to 10%.
  • the amount of the cerium addition depends not only on the intended use, but also on the amount of other alloy formers contained in i the alloy. Thelincrease in strength atelevated temperatures becomes appreciable, for example in the case of alloys having a high lead content, only when the added amount of cerium is high.
  • a bearing made from a magnesium base alloy containing about 18% of lead, the balance being substantially magnesium.
  • a bearing made from a magnesium base said alloy containing between about 1 and about 28 per cent lead, the balance being substantially magnesium.

Landscapes

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

Description

taining aluminium v been used in-the production of bearings, which Patented Dec. 22, 942
BEARING Adolf Beck and Walter Buchmann,
by meme ano s,
Magneaium Development Corporation, a corporation of Delaware No Dra No. 291,322. In
wing. Application August 22, 1939, Serial German August 22, 1938 4 Claims. (Cl. 308-242) This invention relates to bearings.
Certain commercial magnesium base alloys conand zinc have occasionally however have given good results only when subjected to small loads, that is to say, in a limited field of application. Thus for example, the attempt to mount camshafts in crank-cases made of these alloys has been successful. This is due to the fact that even pure magnesium itself has relatively good sliding properties, probably due to its hexagonal crystal'structure. The known commercial magnesium alloys, however, are unsuitable for bearings which are pressures and, in particular, speeds. They lack, in particular, the essential property of being able to form, through running-in, a'bearing surface which is uniformly loaded; in the event of the shaft being tilted, and particularly if lubrication should fail temporarily, local increases in temperature therefore readily occur on the bearing surfaces, rapid destruction of the bearing. The so-called bearings made It has now been ascertained, in accordance with the present invention, that the properties necessary to the more extensive use of magnesium base alloys as hearing metal, are obtained by the use of alloys of magnesium with the metals lead and/or cadmium, both of which form solid solutions with magnesium up to relatively high con--- presence of which not only-does rather increases, the plastic propthe bearing properties of the resultant alloys deteriorate.
The bearing metal alloys of the present invention preferably contain to of lead and/or 7 to 12% of cadmium. Silver, bismuth and tin also may advantageously be present in the foregoing alloys in amounts of up to 12%, but only provided that the total content of alloy formers in the alloys does not exceed about By comparison withhitherto proposed light bearing metal alloys, the bearing metal alloys of the present invention possess more favourable enhanced.
running-in properties, due to their which lead to the present invention provides abearfurther up to about 12% of 50 alloy plastic properties. They are quite generally suitable for bearing purposes for light to medium loads and, in this range of use, are equivalent in respect to their sliding properties to known heavy metal bearing alloys, over which latter they have the important advantage of lower specific gravity;
For heavier loadsfsuch as those occurring in internal combustion engines, the alloys of the present invention are somewhat deficient in re-' spect of fatigue strength and heat strength.
However, these properties can be substantially improved without unduly impairing the plastic properties and the-ability to form good running surfaces, by additionally incorporating with the alloys, cerium in amounts of from about 0.5 to 10%. The amount of the cerium addition depends not only on the intended use, but also on the amount of other alloy formers contained in i the alloy. Thelincrease in strength atelevated temperatures becomes appreciable, for example in the case of alloys having a high lead content, only when the added amount of cerium is high.
The following are examples of bearing metal alloys in accordance-with the invention:
I. 18% of lead, remainder magnesium.
II. 12% of lead, 8% of cadmium, remainder magnesium. i; g
III. 7% of lead, 7%'of cerium, remainder mag- IV.- 10% ofcadmium, 5 magn sium.
We claim:
l. A bearing made from a magnesium base alloy. containing between about 15 and about 20% of lead, the balance be 31m 2.. A hearing from a magnesium base alloy containing between about 1 and about 28% of lead, at least one metal of the group, consisting of silver, bismuth and tin, and between about 0.5 and about 10% of cerium, the total content of the alloying constituents stated not exceeding about 35%, and the balance of cerium, remainder being substantially magnesium.
.3. A bearing made from a magnesium base alloy containing about 18% of lead, the balance being substantially magnesium.
4. A bearing made from a magnesium base said alloy containing between about 1 and about 28 per cent lead, the balance being substantially magnesium.
ADOLF BECK.
WALTER. BUCHMANN.
g substantially magne-
US291322A 1938-08-22 1939-08-22 Bearing Expired - Lifetime US2306033A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2306033X 1938-08-22

Publications (1)

Publication Number Publication Date
US2306033A true US2306033A (en) 1942-12-22

Family

ID=7994348

Family Applications (1)

Application Number Title Priority Date Filing Date
US291322A Expired - Lifetime US2306033A (en) 1938-08-22 1939-08-22 Bearing

Country Status (1)

Country Link
US (1) US2306033A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2461229A (en) * 1944-07-11 1949-02-08 Magnesium Elektron Ltd Method of producing magnesium base alloys
US3148952A (en) * 1961-10-18 1964-09-15 Dow Chemical Co Composite metallic body and method of preparation

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2461229A (en) * 1944-07-11 1949-02-08 Magnesium Elektron Ltd Method of producing magnesium base alloys
US3148952A (en) * 1961-10-18 1964-09-15 Dow Chemical Co Composite metallic body and method of preparation

Similar Documents

Publication Publication Date Title
US1947121A (en) Aluminum base alloys
US4153756A (en) Aluminum-base bearing alloy and composite
US2306033A (en) Bearing
US2802733A (en) Process for manufacturing brass and bronze alloys containing lead
US2373352A (en) Method of making bearings
US3567436A (en) Compression resistant zinc base alloy
US2288656A (en) Bearing
US2357106A (en) Bearing construction
US2870008A (en) Zinc-aluminium alloys and the method for producing same
JPS582578B2 (en) aluminum bearing alloy
US2288655A (en) Metal alloy
US2375224A (en) Silver-thallium bearing
US3215513A (en) Bearing material
US3514286A (en) Wear-resisting aluminum alloys
US1568224A (en) Bearing metal
US2357451A (en) Aluminum alloy
US2070474A (en) Zinc alloy
US2076281A (en) Aluminium alloy and article made therefrom
SU406931A1 (en) ALLOY BASED ON ALUMINUM
US3031298A (en) Bearing alloys
US2341550A (en) Bearing
JPS6055582B2 (en) aluminum bearing material
US2246067A (en) Alloy
US2357449A (en) Aluminum alloy
US2075091A (en) Aluminum alloy