FR1371981A - Improvements made to friction linings, in particular those for aviation brakes, and the processes for their development - Google Patents

Improvements made to friction linings, in particular those for aviation brakes, and the processes for their development

Info

Publication number
FR1371981A
FR1371981A FR943374A FR943374A FR1371981A FR 1371981 A FR1371981 A FR 1371981A FR 943374 A FR943374 A FR 943374A FR 943374 A FR943374 A FR 943374A FR 1371981 A FR1371981 A FR 1371981A
Authority
FR
France
Prior art keywords
aviation
brakes
development
processes
particular those
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
Application number
FR943374A
Other languages
French (fr)
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.)
Hispano Suiza Lallemant SA
Original Assignee
Hispano Suiza Lallemant SA
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 Hispano Suiza Lallemant SA filed Critical Hispano Suiza Lallemant SA
Priority to FR943374A priority Critical patent/FR1371981A/en
Priority to GB3354863A priority patent/GB1034686A/en
Application granted granted Critical
Publication of FR1371981A publication Critical patent/FR1371981A/en
Priority to US465696A priority patent/US3306741A/en
Expired legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C33/00—Making ferrous alloys
    • C22C33/02—Making ferrous alloys by powder metallurgy
    • C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
    • C22C33/0278—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
    • C22C33/0292—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5% with more than 5% preformed carbides, nitrides or borides
    • 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
    • B22F7/06—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 workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/08—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 workpieces or articles from parts, e.g. to form tipped tools with one or more parts not made from powder
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • C22C29/02—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
    • C22C29/06—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds
    • C22C29/062—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds based on B4C
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C32/00—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/0047—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents
    • C22C32/0052—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents only carbides
    • C22C32/0057—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with carbides, nitrides, borides or silicides as the main non-metallic constituents only carbides based on B4C
    • 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
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
    • F16D69/02—Compositions of linings; Methods of manufacturing
    • F16D69/027—Compositions based on metals or inorganic oxides
FR943374A 1962-09-12 1963-07-31 Improvements made to friction linings, in particular those for aviation brakes, and the processes for their development Expired FR1371981A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR943374A FR1371981A (en) 1963-07-31 1963-07-31 Improvements made to friction linings, in particular those for aviation brakes, and the processes for their development
GB3354863A GB1034686A (en) 1963-07-31 1963-08-23 Improvements in or relating to the production of friction linings, more particularlyfor aircraft brakes
US465696A US3306741A (en) 1962-09-12 1965-06-21 Friction linings and processes for the production of such linings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR943374A FR1371981A (en) 1963-07-31 1963-07-31 Improvements made to friction linings, in particular those for aviation brakes, and the processes for their development

Publications (1)

Publication Number Publication Date
FR1371981A true FR1371981A (en) 1964-09-11

Family

ID=8809646

Family Applications (1)

Application Number Title Priority Date Filing Date
FR943374A Expired FR1371981A (en) 1962-09-12 1963-07-31 Improvements made to friction linings, in particular those for aviation brakes, and the processes for their development

Country Status (2)

Country Link
FR (1) FR1371981A (en)
GB (1) GB1034686A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2362097A1 (en) * 1976-08-16 1978-03-17 Arabei Boris Heat absorbing material for aircraft disc brakes - comprises boron carbide, silicon carbide, copper, titanium diobride and carbon
FR2441100A2 (en) * 1978-11-10 1980-06-06 Abex Pagid Equip Pad for disc brake - is made by hot-pressing of liner onto support which includes metal reinforcement

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2362097A1 (en) * 1976-08-16 1978-03-17 Arabei Boris Heat absorbing material for aircraft disc brakes - comprises boron carbide, silicon carbide, copper, titanium diobride and carbon
FR2441100A2 (en) * 1978-11-10 1980-06-06 Abex Pagid Equip Pad for disc brake - is made by hot-pressing of liner onto support which includes metal reinforcement

Also Published As

Publication number Publication date
GB1034686A (en) 1966-06-29

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