CA1146372A - Structure and method of fabricating a metal composite drive shaft - Google Patents

Structure and method of fabricating a metal composite drive shaft

Info

Publication number
CA1146372A
CA1146372A CA000373994A CA373994A CA1146372A CA 1146372 A CA1146372 A CA 1146372A CA 000373994 A CA000373994 A CA 000373994A CA 373994 A CA373994 A CA 373994A CA 1146372 A CA1146372 A CA 1146372A
Authority
CA
Canada
Prior art keywords
turbine engine
gas turbine
composite shaft
high specific
fabricating
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
CA000373994A
Other languages
English (en)
French (fr)
Inventor
Daniel D. Profant
Jeremy J. Walters
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.)
Avco Corp
Original Assignee
Avco 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 Avco Corp filed Critical Avco Corp
Application granted granted Critical
Publication of CA1146372A publication Critical patent/CA1146372A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F16C3/00—Shafts; Axles; Cranks; Eccentrics
    • F16C3/02—Shafts; Axles
    • 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
    • F16C2360/00—Engines or pumps
    • F16C2360/23—Gas turbine engines

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Ocean & Marine Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
CA000373994A 1980-06-26 1981-03-27 Structure and method of fabricating a metal composite drive shaft Expired CA1146372A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US16303780A 1980-06-26 1980-06-26
US163,037 1980-06-26

Publications (1)

Publication Number Publication Date
CA1146372A true CA1146372A (en) 1983-05-17

Family

ID=22588199

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000373994A Expired CA1146372A (en) 1980-06-26 1981-03-27 Structure and method of fabricating a metal composite drive shaft

Country Status (8)

Country Link
JP (1) JPS5715114A (un)
BR (1) BR8103330A (un)
CA (1) CA1146372A (un)
DE (1) DE3108318A1 (un)
FR (1) FR2485659A1 (un)
GB (1) GB2078338B (un)
IT (1) IT1137947B (un)
SE (1) SE8101237L (un)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3800913A1 (de) * 1988-01-14 1989-08-03 Emitec Emissionstechnologie Mehrschichtenantriebswelle
GB2220595B (en) * 1988-07-13 1992-10-21 Secr Defence Hard surface composite parts.
US5305520A (en) * 1990-09-01 1994-04-26 Rolls-Royce Plc Method of making fibre reinforced metal component
GB2247492B (en) * 1990-09-01 1995-01-11 Rolls Royce Plc A method of making a fibre reinforced metal component
US8225481B2 (en) * 2003-05-19 2012-07-24 Pratt & Whitney Rocketdyne, Inc. Diffusion bonded composite material and method therefor
US6897578B1 (en) * 2003-12-08 2005-05-24 Ingersoll-Rand Energy Systems Corporation Integrated microturbine gearbox generator assembly
GB2438633B (en) * 2006-05-31 2010-12-01 Tisics Ltd Reinforced splines and their manufacture
US20080148708A1 (en) 2006-12-20 2008-06-26 General Electric Company Turbine engine system with shafts for improved weight and vibration characteristic

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1548099A (un) * 1966-12-22 1968-11-29
DE1750523B1 (de) * 1968-05-10 1971-12-09 Augsburg Nuernberg Ag Zweignie Verfahren zur herstellung einer trommel oder welle
US3651661A (en) * 1970-02-02 1972-03-28 United Aircraft Corp Composite shaft with integral end flange
CA1098329A (en) * 1977-12-02 1981-03-31 Richard L. Vanauken Composite tubular element and methods for making same
US4272971A (en) * 1979-02-26 1981-06-16 Rockwell International Corporation Reinforced tubular structure

Also Published As

Publication number Publication date
FR2485659A1 (fr) 1981-12-31
GB2078338B (en) 1983-08-10
DE3108318A1 (de) 1982-01-21
FR2485659B1 (un) 1984-12-28
JPS5715114A (en) 1982-01-26
BR8103330A (pt) 1982-02-16
GB2078338A (en) 1982-01-06
SE8101237L (sv) 1981-12-27
IT1137947B (it) 1986-09-10
IT8122601A0 (it) 1981-06-26

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Legal Events

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