GB1293787A - Gas turbine engine - Google Patents

Gas turbine engine

Info

Publication number
GB1293787A
GB1293787A GB26342/71A GB2634271A GB1293787A GB 1293787 A GB1293787 A GB 1293787A GB 26342/71 A GB26342/71 A GB 26342/71A GB 2634271 A GB2634271 A GB 2634271A GB 1293787 A GB1293787 A GB 1293787A
Authority
GB
United Kingdom
Prior art keywords
casing
gear
compressor
shaft
pinion
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
GB26342/71A
Other languages
English (en)
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
Publication of GB1293787A publication Critical patent/GB1293787A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, 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
    • F02C7/32—Arrangement, 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)
  • General Details Of Gearings (AREA)
GB26342/71A 1970-09-28 1971-04-19 Gas turbine engine Expired GB1293787A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US7601470A 1970-09-28 1970-09-28

Publications (1)

Publication Number Publication Date
GB1293787A true GB1293787A (en) 1972-10-25

Family

ID=22129385

Family Applications (1)

Application Number Title Priority Date Filing Date
GB26342/71A Expired GB1293787A (en) 1970-09-28 1971-04-19 Gas turbine engine

Country Status (6)

Country Link
US (1) US3714779A (enExample)
JP (1) JPS5212323B1 (enExample)
DE (1) DE2118198C3 (enExample)
FR (1) FR2108014B1 (enExample)
GB (1) GB1293787A (enExample)
SE (1) SE368442B (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2162158C1 (ru) * 1999-12-24 2001-01-20 ГОСУДАРСТВЕННОЕ УНИТАРНОЕ ПРЕДПРИЯТИЕ ТУШИНСКОЕ МАШИНОСТРОИТЕЛЬНОЕ КОНСТРУКТОРСКОЕ БЮРО "СОЮЗ" Военно-промышленный комплекс "МАПО" Коробка приводов вспомогательных агрегатов авиационного газотурбинного двигателя

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4566269A (en) * 1983-10-11 1986-01-28 United Technologies Corporation Jet engine removable support assembly
FR2862045B1 (fr) * 2003-11-12 2006-05-05 Snecma Moteurs Turboreacteur destine a etre fixe sur le fuselage d'un avion et en particulier sur sa partie arriere
FR2907167B1 (fr) * 2006-10-13 2011-11-18 Snecma Arbre d'entrainement de boitier a engrenages de machines auxiliaires d'un turboreacteur; machine auxiliaire supplementaire modulaire
US7937949B2 (en) * 2007-07-02 2011-05-10 Honeywell International, Inc. Emergency power engine restart system
US8857192B2 (en) 2010-04-20 2014-10-14 General Electric Company Accessory gearbox with a starter/generator
US8602717B2 (en) * 2010-10-28 2013-12-10 United Technologies Corporation Compression system for turbomachine heat exchanger
US8490410B2 (en) 2010-11-17 2013-07-23 United Technologies Corporation Axial accessory gearbox
US9650964B2 (en) 2010-12-28 2017-05-16 General Electric Company Accessory gearbox with a starter/generator
US9145834B2 (en) * 2011-06-14 2015-09-29 Honeywell International Inc. Transverse mounted accessory gearbox
US9926849B2 (en) 2011-06-14 2018-03-27 Honeywell International Inc. Transverse mounted accessory gearbox
US8973465B2 (en) 2012-07-20 2015-03-10 United Technologies Corporation Gearbox for gas turbine engine
US10107380B2 (en) 2015-06-15 2018-10-23 Regal Beloit America, Inc. Drive assembly, cover and associated kit
US10316898B2 (en) 2016-01-28 2019-06-11 Ge Aviation Systems Llc Method and disconnector for disconnecting a drive shaft
US11572838B2 (en) * 2020-09-29 2023-02-07 General Electric Company Accessory gearbox for a turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2162158C1 (ru) * 1999-12-24 2001-01-20 ГОСУДАРСТВЕННОЕ УНИТАРНОЕ ПРЕДПРИЯТИЕ ТУШИНСКОЕ МАШИНОСТРОИТЕЛЬНОЕ КОНСТРУКТОРСКОЕ БЮРО "СОЮЗ" Военно-промышленный комплекс "МАПО" Коробка приводов вспомогательных агрегатов авиационного газотурбинного двигателя

Also Published As

Publication number Publication date
US3714779A (en) 1973-02-06
JPS5212323B1 (enExample) 1977-04-06
SE368442B (enExample) 1974-07-01
DE2118198A1 (de) 1972-03-30
FR2108014B1 (enExample) 1975-01-17
DE2118198C3 (de) 1975-02-06
FR2108014A1 (enExample) 1972-05-12
DE2118198B2 (de) 1974-06-20

Similar Documents

Publication Publication Date Title
GB1293787A (en) Gas turbine engine
GB1338499A (en) Gas turbine engine
GB1408357A (en) Fan type gas turbine engine
GB1334818A (en) Control of auxiliary energy input to the turbocharger of an internal combustion engine
ES344735A1 (es) Mejoras introducidas en los motores de explosion sobreali- mentados.
SU646931A3 (ru) Двигатель внутреннего сгорани
GB1217555A (en) Improvements in or relating to gearboxes for gas turbine engines
GB206845A (en) Improvements in an internal combustion engine in combination with a gas-turbine driven by the exhaust gases of the engine and driving a compressor
US3490567A (en) Engine with hydrodynamic retarder
US2568473A (en) Combination internal-combustion engine and accessories
GB1212109A (en) Engine assembly
US2172100A (en) Internal combustion engine
US2565060A (en) Transmission mechanism
US4373483A (en) Lubricating oil pump drive for an internal combustion engine
US2185842A (en) Motor vehicle
GB1040047A (en) Improvements in or relating to turbine operated engine starters
GB1136852A (en) Gas turbine engine
US2678037A (en) Transverse accessory drive for engines
US911825A (en) Gas turbine-engine.
US3857378A (en) Oil pump driving arrangement for a separate engine lubricating system of a small-sized internal combustion engine
GB1476328A (en) Power take-off for internal combustion engines
ES484490A1 (es) Un motor de combustion interna de dos tiempos perfeccionado,en especial para vehiculos de dos ruedas
GB1221966A (en) Internal combustion engine
US4061448A (en) Drive for the ignition distributor of an internal combustion engine
GB971690A (en) Gas turbine engine

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee