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SE8101237L - DRIVE SHAFT AND SET FOR MANUFACTURING THE SAME - Google Patents

DRIVE SHAFT AND SET FOR MANUFACTURING THE SAME

Info

Publication number
SE8101237L
SE8101237L SE8101237A SE8101237A SE8101237L SE 8101237 L SE8101237 L SE 8101237L SE 8101237 A SE8101237 A SE 8101237A SE 8101237 A SE8101237 A SE 8101237A SE 8101237 L SE8101237 L SE 8101237L
Authority
SE
Sweden
Prior art keywords
mandrel
tube
composite
bonded
manufacturing
Prior art date
Application number
SE8101237A
Other languages
Unknown language ( )
Swedish (sv)
Inventor
D D Profant
J J Walters
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
Publication of SE8101237L publication Critical patent/SE8101237L/en

Links

Classifications

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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Ocean & Marine Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Abstract

A high specific modulus shaft 1 for a gas turbine engine has a metal outer tube 2 to transmit the torque and a metal and high modulus filament composite sleeve 3 bonded to the tube's inner surface. The composite sleeve 3 is fabricated and bonded to the inner diameter of the tube 2 by winding a composite composition tape on a mandrel with the filaments axially aligned. The mandrel is then inserted into the metal outer tube 2. The assembly is encapsulated, evacuated and sealed and the mandrel pressurized at a sufficient temperature to achieve consolidation and diffusion bonding of the wound composite to itself and to the shaft inner surface. <IMAGE>
SE8101237A 1980-06-26 1981-02-25 DRIVE SHAFT AND SET FOR MANUFACTURING THE SAME SE8101237L (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US16303780A 1980-06-26 1980-06-26

Publications (1)

Publication Number Publication Date
SE8101237L true SE8101237L (en) 1981-12-27

Family

ID=22588199

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8101237A SE8101237L (en) 1980-06-26 1981-02-25 DRIVE SHAFT AND SET FOR MANUFACTURING THE SAME

Country Status (8)

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

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3800913A1 (en) * 1988-01-14 1989-08-03 Emitec Emissionstechnologie MULTI-LAYER DRIVE SHAFT
GB2220595B (en) * 1988-07-13 1992-10-21 Secr Defence Hard surface composite parts.
GB2247492B (en) * 1990-09-01 1995-01-11 Rolls Royce Plc A method of making a fibre reinforced metal component
US5305520A (en) * 1990-09-01 1994-04-26 Rolls-Royce Plc Method of making 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 (en) * 1966-12-22 1968-11-29
DE1750523B1 (en) * 1968-05-10 1971-12-09 Augsburg Nuernberg Ag Zweignie METHOD OF MANUFACTURING A DRUM OR SHAFT
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 (en) 1981-12-31
GB2078338B (en) 1983-08-10
IT1137947B (en) 1986-09-10
BR8103330A (en) 1982-02-16
IT8122601A0 (en) 1981-06-26
CA1146372A (en) 1983-05-17
DE3108318A1 (en) 1982-01-21
GB2078338A (en) 1982-01-06
FR2485659B1 (en) 1984-12-28
JPS5715114A (en) 1982-01-26

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