GB1174624A - Method of Mechanically-Uniting Sintered Material Parts - Google Patents

Method of Mechanically-Uniting Sintered Material Parts

Info

Publication number
GB1174624A
GB1174624A GB2304967A GB2304967A GB1174624A GB 1174624 A GB1174624 A GB 1174624A GB 2304967 A GB2304967 A GB 2304967A GB 2304967 A GB2304967 A GB 2304967A GB 1174624 A GB1174624 A GB 1174624A
Authority
GB
United Kingdom
Prior art keywords
recesses
parts
projections
portions
coupling
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
GB2304967A
Inventor
John Haller
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.)
Federal Mogul LLC
Original Assignee
Federal Mogul LLC
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 Federal Mogul LLC filed Critical Federal Mogul LLC
Priority to GB2304967A priority Critical patent/GB1174624A/en
Publication of GB1174624A publication Critical patent/GB1174624A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture 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
    • B22F7/06Manufacture 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
    • B22F7/062Manufacture 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 involving the connection or repairing of preformed parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00Supplementary information concerning processes or compositions relating to powder metallurgy

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Powder Metallurgy (AREA)

Abstract

1,174,624. Jointing; riveted joints; brazing. FEDERAL - MOGUL CORP. 18 May, 1967, No. 23049/67. Headings B3R, B3H and B3V. [Also in Division B5] A method of jointing two or more parts 22, 24, Fig. 1, of sintered powdered material, e.g. iron, bronze or nylon, comprising forming the parts with opposed recesses 28, 46, forming a coupling portion 26 alignable with the recess 46, pressing the parts together so that the portion 26 enters the recess 46 and is deformed laterally into interlocking engagement, Fig. 2, with a side 52 of the recess 46. As shown, a pair of annular coupling portions 26, 44 are used which are integral with the parts 22, 24, the coupling portions and recesses being relatively offset laterally and opposed surfaces 32, 56, 38, 50 having different angles so that the surfaces 38, 56 cam the coupling portions 26, 44 laterally as the parts are pressed together. A gap may be left between the parts, Fig. 6, for a layer 70, 72 of bonding material, e.g. brazing metal, inserted e.g. by flowing after the interlocking stage. Alternatively, rings of brazing material (132), Fig. 14 (not shown), may be located at the bottom of the recesses 28, 46. Two or more sets of interlocking projections and recesses may be formed, Fig. 7 (not shown), or annular projections and recesses may be interrupted by radial keys (80), Fig. 8 (not shown), for preventing relative rotation between the parts. In another form, Fig. 10, the coupling portions 96 have recesses 104 engaged by projections 118 in opposed recesses 107. The projections 118 expand the ends of the portions 96, Fig. 11 (not shown), and raised edges 108 surrounding the recesses are cammed inwardly by surfaces 112 surrounding the portions 96. In addition to opposed projections and recesses, frusto-conical washers 216, Fig. 15, may be used which are flattened during the interlocking operation and penetrate the parts, Fig. 17 (not shown). In a further form, Fig. 18, separate coupling members 266 are used which are expanded by projections 280, 282. Toothed coupling members 306, Fig. 21, may be used, the internal teeth 336 of which are contracted and the external teeth 334 expanded by ribs 338, 340. In another form, Fig. 26, a steel coupling member 416 is deformed as it enters sinuous passages 454 in the sintered parts 410, 412 as these are pressed together, Fig. 27 (not shown). The passages may have uniformly tapering portions, Figs. 31 and 33 (not shown).
GB2304967A 1967-05-18 1967-05-18 Method of Mechanically-Uniting Sintered Material Parts Expired GB1174624A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2304967A GB1174624A (en) 1967-05-18 1967-05-18 Method of Mechanically-Uniting Sintered Material Parts

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2304967A GB1174624A (en) 1967-05-18 1967-05-18 Method of Mechanically-Uniting Sintered Material Parts

Publications (1)

Publication Number Publication Date
GB1174624A true GB1174624A (en) 1969-12-17

Family

ID=10189281

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2304967A Expired GB1174624A (en) 1967-05-18 1967-05-18 Method of Mechanically-Uniting Sintered Material Parts

Country Status (1)

Country Link
GB (1) GB1174624A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2127730A (en) * 1982-09-30 1984-04-18 Standard Products Co Attachment of one member to another
EP2821166A1 (en) * 2013-07-04 2015-01-07 Sandvik Intellectual Property AB A method for manufacturing a wear resistant component comprising mechanically interlocked cemented carbide bodies
WO2015039747A1 (en) * 2013-09-23 2015-03-26 Gkn Sinter Metals Holding Gmbh Method for producing a sintered part having a highly precise molded part height and parts set of sintered joining parts
DE102014216848A1 (en) * 2014-08-25 2016-02-25 Schaeffler Technologies AG & Co. KG Rotor for a hydraulic camshaft adjuster and method of manufacturing a rotor for a camshaft adjuster

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2127730A (en) * 1982-09-30 1984-04-18 Standard Products Co Attachment of one member to another
EP2821166A1 (en) * 2013-07-04 2015-01-07 Sandvik Intellectual Property AB A method for manufacturing a wear resistant component comprising mechanically interlocked cemented carbide bodies
WO2015001006A3 (en) * 2013-07-04 2015-03-19 Sandvik Intellectual Property Ab A method for manufacturing a wear resistant component comprising mechanically interlocked cemented carbide bodies
WO2015039747A1 (en) * 2013-09-23 2015-03-26 Gkn Sinter Metals Holding Gmbh Method for producing a sintered part having a highly precise molded part height and parts set of sintered joining parts
CN105705279A (en) * 2013-09-23 2016-06-22 吉凯恩粉末冶金工程有限公司 Method for producing a sintered part having a highly precise molded part height and parts set of sintered joining parts
CN105705279B (en) * 2013-09-23 2018-07-10 吉凯恩粉末冶金工程有限公司 The method of clinkering part of part height and the part group of clinkering assembling parts of the manufacture with precise height molding
US10576586B2 (en) 2013-09-23 2020-03-03 Gkn Sinter Metals Engineering Gmbh Method for producing a sintered part having a highly precise molded part height and parts set of sintered joining parts
DE102014216848A1 (en) * 2014-08-25 2016-02-25 Schaeffler Technologies AG & Co. KG Rotor for a hydraulic camshaft adjuster and method of manufacturing a rotor for a camshaft adjuster
DE102014216848B4 (en) * 2014-08-25 2017-09-14 Schaeffler Technologies AG & Co. KG Rotor for a hydraulic camshaft adjuster and method of manufacturing a rotor for a camshaft adjuster
US10267188B2 (en) 2014-08-25 2019-04-23 Schaeffler Technologies AG & Co. KG Rotor for a hydraulic camshaft adjuster and manufacturing method for a rotor for a camshaft adjuster

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Legal Events

Date Code Title Description
PS Patent sealed
PLNP Patent lapsed through nonpayment of renewal fees