GB2063188B - Flexible power take-off system for the gas turbine engine of an aircraft - Google Patents

Flexible power take-off system for the gas turbine engine of an aircraft

Info

Publication number
GB2063188B
GB2063188B GB8036159A GB8036159A GB2063188B GB 2063188 B GB2063188 B GB 2063188B GB 8036159 A GB8036159 A GB 8036159A GB 8036159 A GB8036159 A GB 8036159A GB 2063188 B GB2063188 B GB 2063188B
Authority
GB
United Kingdom
Prior art keywords
aircraft
gas turbine
turbine engine
power take
flexible power
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
GB8036159A
Other languages
English (en)
Other versions
GB2063188A (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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB2063188A publication Critical patent/GB2063188A/en
Application granted granted Critical
Publication of GB2063188B publication Critical patent/GB2063188B/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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Control Of Turbines (AREA)
GB8036159A 1979-11-16 1980-11-11 Flexible power take-off system for the gas turbine engine of an aircraft Expired GB2063188B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2946371A DE2946371C2 (de) 1979-11-16 1979-11-16 Hilfsantriebsanlage für Flugzeughilfsgeräte

Publications (2)

Publication Number Publication Date
GB2063188A GB2063188A (en) 1981-06-03
GB2063188B true GB2063188B (en) 1983-09-28

Family

ID=6086194

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8036159A Expired GB2063188B (en) 1979-11-16 1980-11-11 Flexible power take-off system for the gas turbine engine of an aircraft

Country Status (4)

Country Link
DE (1) DE2946371C2 (enExample)
FR (1) FR2469567A1 (enExample)
GB (1) GB2063188B (enExample)
IT (1) IT1133799B (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3502578A1 (de) * 1985-01-26 1986-07-31 Klöckner-Humboldt-Deutz AG, 5000 Köln Hilfsantrieb fuer ein gasturbinentriebwerk
DE3515770A1 (de) * 1985-05-02 1986-11-06 Klöckner-Humboldt-Deutz AG, 5000 Köln Hilfsantriebsanordnung mit getriebe fuer ein gasturbinentriebwerk
RU2168043C1 (ru) * 1999-12-10 2001-05-27 Открытое акционерное общество "А.Люлька-Сатурн" Способ запуска авиационного газотурбинного двигателя
US7975465B2 (en) * 2003-10-27 2011-07-12 United Technologies Corporation Hybrid engine accessory power system
RU2282736C2 (ru) * 2003-11-14 2006-08-27 Республиканское унитарное предприятие "Головное специальное конструкторско-технологическое бюро гидроаппаратуры с опытно-экспериментальным производством" Устройство для гидравлического запуска газотурбинного двигателя
DE102008018101A1 (de) 2008-04-09 2009-10-15 Rolls-Royce Deutschland Ltd & Co Kg Strahltriebwerk mit mindestens einem Notantrieb

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2863288A (en) * 1954-11-19 1958-12-09 Jack & Heintz Inc Air pressure control means for air turbine drive systems
BE567824A (enExample) * 1957-05-20
GB1212109A (en) * 1968-08-09 1970-11-11 Rolls Royce Engine assembly
US3514945A (en) * 1968-10-04 1970-06-02 Avco Corp Gas turbine accessory power drive unit
US4068470A (en) * 1974-11-08 1978-01-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Gas turbine engine with convertible accessories
DE2519152C2 (de) * 1975-04-30 1982-11-25 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Vorrichtung zum Anlassen von Flugzeugtriebwerken und zum Betreiben von Flugzeughilfsgeräten

Also Published As

Publication number Publication date
FR2469567B3 (enExample) 1982-07-23
GB2063188A (en) 1981-06-03
IT1133799B (it) 1986-07-09
FR2469567A1 (fr) 1981-05-22
IT8025895A0 (it) 1980-11-11
DE2946371C2 (de) 1982-07-08
DE2946371A1 (de) 1981-05-27

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee