GB812030A - Engine gudgeon pin assembly or like article of manufacture - Google Patents

Engine gudgeon pin assembly or like article of manufacture

Info

Publication number
GB812030A
GB812030A GB31614/56A GB3161456A GB812030A GB 812030 A GB812030 A GB 812030A GB 31614/56 A GB31614/56 A GB 31614/56A GB 3161456 A GB3161456 A GB 3161456A GB 812030 A GB812030 A GB 812030A
Authority
GB
United Kingdom
Prior art keywords
core
sleeve
gudgeon pin
article
manufacture
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
GB31614/56A
Inventor
Earl Ginn
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.)
Continental Motors Corp
Original Assignee
Continental 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 Continental Motors Corp filed Critical Continental Motors Corp
Priority to GB31614/56A priority Critical patent/GB812030A/en
Publication of GB812030A publication Critical patent/GB812030A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P11/00—Connecting or disconnecting metal parts or objects by metal-working techniques not otherwise provided for 
    • B23P11/02—Connecting or disconnecting metal parts or objects by metal-working techniques not otherwise provided for  by first expanding and then shrinking or vice versa, e.g. by using pressure fluids; by making force fits
    • B23P11/025—Connecting or disconnecting metal parts or objects by metal-working techniques not otherwise provided for  by first expanding and then shrinking or vice versa, e.g. by using pressure fluids; by making force fits by using heat or cold
    • 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
    • F16C11/00—Pivots; Pivotal connections
    • F16C11/02—Trunnions; Crank-pins
    • 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
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J1/00—Pistons; Trunk pistons; Plungers
    • F16J1/10—Connection to driving members
    • F16J1/14—Connection to driving members with connecting-rods, i.e. pivotal connections
    • F16J1/16—Connection to driving members with connecting-rods, i.e. pivotal connections with gudgeon-pin; Gudgeon-pins

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Abstract

812,030. Making gudgeon pins; jointing by forging. CONTINENTAL MOTORS CORPORATION. Oct. 17, 1956, No. 31614/56. Classes 83 (2) and 83 (4). [Also in Group XXVI] A close fitting assembly of a sleeve 14 and a core 15 of higher thermal expansion than the sleeve is formed by heating the assembled sleeve and core to a predetermined temperature and upsetting both ends of the core on to the sleeve. The invention is described with reference to an engine gudgeon pin 12 wherein the initial core and sleeve are heated to 600‹ F. which is maintained for one hour and the core ends are then upset. After cooling to room temperature the core is machined to a predetermined length calculated from given equations. The core is stated to be tight within the sleeve through a temperature range of - 50‹ F. to 600‹ F.
GB31614/56A 1956-10-17 1956-10-17 Engine gudgeon pin assembly or like article of manufacture Expired GB812030A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB31614/56A GB812030A (en) 1956-10-17 1956-10-17 Engine gudgeon pin assembly or like article of manufacture

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB31614/56A GB812030A (en) 1956-10-17 1956-10-17 Engine gudgeon pin assembly or like article of manufacture

Publications (1)

Publication Number Publication Date
GB812030A true GB812030A (en) 1959-04-15

Family

ID=10325781

Family Applications (1)

Application Number Title Priority Date Filing Date
GB31614/56A Expired GB812030A (en) 1956-10-17 1956-10-17 Engine gudgeon pin assembly or like article of manufacture

Country Status (1)

Country Link
GB (1) GB812030A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1068926A1 (en) * 1999-07-13 2001-01-17 Aerospatiale Matra CCR Process of introducing a metallic ring into a compound material having an organic matrix and element obtained by the method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1068926A1 (en) * 1999-07-13 2001-01-17 Aerospatiale Matra CCR Process of introducing a metallic ring into a compound material having an organic matrix and element obtained by the method
FR2796425A1 (en) * 1999-07-13 2001-01-19 Aerospatiale Matra Ccr METHOD FOR INTRODUCING A METALLIC RING INTO A PART MADE OF COMPOSITE MATERIAL WITH AN ORGANIC MATRIX AND PART OBTAINED BY THIS PROCESS

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