GB850000A - Improvements relating to gas turbine jet propulsion engines - Google Patents

Improvements relating to gas turbine jet propulsion engines

Info

Publication number
GB850000A
GB850000A GB6897/59A GB689759A GB850000A GB 850000 A GB850000 A GB 850000A GB 6897/59 A GB6897/59 A GB 6897/59A GB 689759 A GB689759 A GB 689759A GB 850000 A GB850000 A GB 850000A
Authority
GB
United Kingdom
Prior art keywords
shaft
gas turbine
bevel gear
engine
improvements relating
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
GB6897/59A
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
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 Motors Liquidation Co filed Critical Motors Liquidation Co
Publication of GB850000A publication Critical patent/GB850000A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16Composite ram-jet/turbo-jet engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32Arrangement, mounting, or driving, of auxiliaries

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gear Transmission (AREA)

Abstract

850,000. Engine turning-gear. GENERAL MOTORS CORPORATION. Feb. 27, 1959 [June 2, 1958], No. 6897/59. Class 7(5). [Also in Groups XXV and XXVI] An air turbine 78 which may be supplied with air through a duct 81 either from an external source of compressed air through a valve 86 or from the bypass duct 15 of a gas turbine engine through a valve 87 is connected by a splined shaft 74 to a. bevel gear 122. The bevel gear 122 meshes with a bevel gear 131 integral with a hollow shaft 129 which is coupled to a pinion 113 on the engine shaft by an overrunning clutch mechanism 134. This clutch, which provides a drive from the starter to shaft 29 but disengages when the shaft 29 overruns the starter, comprises inner end outer rings 136, 137 between which are arranged ball bearings and sprag elements or rollers.
GB6897/59A 1958-06-02 1959-02-27 Improvements relating to gas turbine jet propulsion engines Expired GB850000A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US850000XA 1958-06-02 1958-06-02

Publications (1)

Publication Number Publication Date
GB850000A true GB850000A (en) 1960-09-28

Family

ID=22188533

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6897/59A Expired GB850000A (en) 1958-06-02 1959-02-27 Improvements relating to gas turbine jet propulsion engines

Country Status (1)

Country Link
GB (1) GB850000A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1826390A1 (en) * 2006-01-31 2007-08-29 United Technologies Corporation Multipurpose gas generator ramjet/scramjet cold start system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1826390A1 (en) * 2006-01-31 2007-08-29 United Technologies Corporation Multipurpose gas generator ramjet/scramjet cold start system

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