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GB1008322A - Gas turbine engine - Google Patents

Gas turbine engine

Info

Publication number
GB1008322A
GB1008322A GB3167064A GB3167064A GB1008322A GB 1008322 A GB1008322 A GB 1008322A GB 3167064 A GB3167064 A GB 3167064A GB 3167064 A GB3167064 A GB 3167064A GB 1008322 A GB1008322 A GB 1008322A
Authority
GB
United Kingdom
Prior art keywords
pressure compressor
engine
high pressure
low pressure
pass
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
GB3167064A
Other languages
English (en)
Inventor
Frederick Freeman
Allen Geoffrey Downhill
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB3167064A priority Critical patent/GB1008322A/en
Priority to DE1965R0041045 priority patent/DE1289364B/de
Publication of GB1008322A publication Critical patent/GB1008322A/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
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/105—Heating the by-pass flow
    • F02K3/11—Heating the by-pass flow by means of burners or combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
GB3167064A 1964-08-04 1964-08-04 Gas turbine engine Expired GB1008322A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB3167064A GB1008322A (en) 1964-08-04 1964-08-04 Gas turbine engine
DE1965R0041045 DE1289364B (de) 1964-08-04 1965-07-08 Verbundtriebwerk zum Antrieb von Flugzeugen

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3167064A GB1008322A (en) 1964-08-04 1964-08-04 Gas turbine engine

Publications (1)

Publication Number Publication Date
GB1008322A true GB1008322A (en) 1965-10-27

Family

ID=10326649

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3167064A Expired GB1008322A (en) 1964-08-04 1964-08-04 Gas turbine engine

Country Status (2)

Country Link
DE (1) DE1289364B (de)
GB (1) GB1008322A (de)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5230603A (en) * 1990-08-22 1993-07-27 Rolls Royce Plc Control of flow instabilities in turbomachines
GB2273318A (en) * 1992-12-09 1994-06-15 Snecma Aircraft engine auxiliary equipment arrangement
EP1619376A2 (de) 2004-07-23 2006-01-25 General Electric Company Schubdüse mit geteiltem Gehäuse
GB2434838A (en) * 2006-02-03 2007-08-08 Stephen Desmond Lewis Supersonic turbofan engine
FR2910056A1 (fr) * 2006-12-18 2008-06-20 Michel Aguilar Turbomachine a compresseur volumique rotatif
JP2013002447A (ja) * 2011-06-17 2013-01-07 General Electric Co <Ge> ジェットエンジンノズルの流れ変更部品をリニア駆動する装置および方法
US20160208737A1 (en) * 2015-01-20 2016-07-21 United Technologies Corporation System for actuating an exhaust cowl

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3911715A1 (de) * 1989-04-10 1990-10-11 Mtu Muenchen Gmbh Absperreinrichtung fuer geblaese-, insbesondere geblaese-staustrahltriebwerke
DE4222947C2 (de) * 1992-07-11 1995-02-02 Deutsche Aerospace Strahltriebwerk
DE10033653A1 (de) * 2000-06-16 2002-03-07 Sandor Nagy Kombinationsantrieb
DE10126632A1 (de) * 2000-08-08 2002-09-12 Sandor Nagy Kombinationsantrieb

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB713783A (en) * 1952-01-02 1954-08-18 Armstrong Siddeley Motors Ltd Gas turbine propulsion units
BE537645A (de) * 1954-06-10
US3102385A (en) * 1957-05-21 1963-09-03 Charles E Lyons Variable area converging-diverging exhaust nozzle for a bypass engine
DE1131467B (de) * 1959-04-30 1962-06-14 Daimler Benz Ag Verbundtriebwerk zum Antrieb von Flugzeugen
DE1143677B (de) * 1959-12-02 1963-02-14 Gen Electric Verbundrueckstosstriebwerk
NL262125A (de) * 1960-04-01

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5230603A (en) * 1990-08-22 1993-07-27 Rolls Royce Plc Control of flow instabilities in turbomachines
GB2273318A (en) * 1992-12-09 1994-06-15 Snecma Aircraft engine auxiliary equipment arrangement
GB2273318B (en) * 1992-12-09 1995-06-21 Snecma Aircraft engine arrangement
EP1619376A2 (de) 2004-07-23 2006-01-25 General Electric Company Schubdüse mit geteiltem Gehäuse
JP2006037949A (ja) * 2004-07-23 2006-02-09 General Electric Co <Ge> 分割シュラウド型排気ノズル
EP1619376A3 (de) * 2004-07-23 2011-12-14 General Electric Company Schubdüse mit geteiltem Gehäuse
JP2012052547A (ja) * 2004-07-23 2012-03-15 General Electric Co <Ge> 分割シュラウド型廃棄ノズル
GB2434838A (en) * 2006-02-03 2007-08-08 Stephen Desmond Lewis Supersonic turbofan engine
FR2910056A1 (fr) * 2006-12-18 2008-06-20 Michel Aguilar Turbomachine a compresseur volumique rotatif
JP2013002447A (ja) * 2011-06-17 2013-01-07 General Electric Co <Ge> ジェットエンジンノズルの流れ変更部品をリニア駆動する装置および方法
US20160208737A1 (en) * 2015-01-20 2016-07-21 United Technologies Corporation System for actuating an exhaust cowl
US10371089B2 (en) * 2015-01-20 2019-08-06 United Technologies Corporation System for actuating an exhaust cowl

Also Published As

Publication number Publication date
DE1289364B (de) 1969-02-13

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