JPS5247115A - Gas turbine engine power system with thrust reversing device - Google Patents

Gas turbine engine power system with thrust reversing device

Info

Publication number
JPS5247115A
JPS5247115A JP51119244A JP11924476A JPS5247115A JP S5247115 A JPS5247115 A JP S5247115A JP 51119244 A JP51119244 A JP 51119244A JP 11924476 A JP11924476 A JP 11924476A JP S5247115 A JPS5247115 A JP S5247115A
Authority
JP
Japan
Prior art keywords
gas turbine
power system
turbine engine
engine power
reversing device
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.)
Pending
Application number
JP51119244A
Other languages
English (en)
Japanese (ja)
Inventor
Eritsuku Sumisu Toomasu
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
Publication of JPS5247115A publication Critical patent/JPS5247115A/ja
Pending 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/17—Purpose of the control system to control boundary layer
    • F05D2270/173—Purpose of the control system to control boundary layer by the Coanda effect
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/18—Purpose of the control system using fluidic amplifiers or actuators

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
JP51119244A 1975-10-11 1976-10-04 Gas turbine engine power system with thrust reversing device Pending JPS5247115A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB41751/75A GB1506588A (en) 1975-10-11 1975-10-11 Gas turbine engine power plants for aircraft

Publications (1)

Publication Number Publication Date
JPS5247115A true JPS5247115A (en) 1977-04-14

Family

ID=10421217

Family Applications (1)

Application Number Title Priority Date Filing Date
JP51119244A Pending JPS5247115A (en) 1975-10-11 1976-10-04 Gas turbine engine power system with thrust reversing device

Country Status (6)

Country Link
US (1) US4047381A (OSRAM)
JP (1) JPS5247115A (OSRAM)
DE (1) DE2645349C3 (OSRAM)
FR (1) FR2327411A1 (OSRAM)
GB (1) GB1506588A (OSRAM)
IT (1) IT1068895B (OSRAM)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS54124188A (en) * 1978-03-20 1979-09-26 Hitachi Ltd Building method of reactor container
JPS54149243A (en) * 1978-05-15 1979-11-22 Ohbayashigumi Ltd Method of constructing structure under steel container bottom plate in atomic power plant or the like
JPS5559390A (en) * 1978-10-30 1980-05-02 Tokyo Shibaura Electric Co Method of executing reactor containment device
JPS5674696A (en) * 1979-11-22 1981-06-20 Tokyo Shibaura Electric Co Nuclear reactor building constructing method
JP2010514987A (ja) * 2007-01-02 2010-05-06 エアバス フランス 航空機のジェットエンジンのナセルと該ナセルを備える航空機

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4232516A (en) * 1977-10-05 1980-11-11 Rolls-Royce Limited Flow deflecting devices
US5090196A (en) * 1989-07-21 1992-02-25 The Boeing Company Ducted fan type gas turbine engine power plants
DE4134051C2 (de) * 1991-10-15 1995-02-02 Mtu Muenchen Gmbh Turbinenstrahltriebwerk mit Gebläse
US5435489A (en) * 1994-01-13 1995-07-25 Bell Helicopter Textron Inc. Engine exhaust gas deflection system
GB9613166D0 (en) * 1996-06-24 1996-08-28 Short Brothers Plc Aircraft propulsive power unit
US6696774B1 (en) 2001-06-01 2004-02-24 Steven J. Schneider Magnetohydrodynamic power extraction and flow conditioning in a gas flow turbine
GB0321139D0 (en) * 2003-09-10 2003-10-08 Short Brothers Plc A device
FR2863587B1 (fr) * 2003-12-11 2006-02-24 Hurel Hispano Dispositif de retenue d'un systeme de detection feu
FR2903455B1 (fr) * 2006-07-05 2013-01-18 Airbus France Procede pour inverser la poussee produite par un ensemble propulsif d'un aeronef, dispositif pour sa mise en oeuvre, nacelle equipee dudit dispositif
US8015797B2 (en) * 2006-09-21 2011-09-13 Jean-Pierre Lair Thrust reverser nozzle for a turbofan gas turbine engine
FR2906573B1 (fr) * 2006-09-29 2008-11-21 Airbus France Sas Nacelle de reacteur d'aeronef et aeronef comportant une telle nacelle
US7685805B2 (en) * 2006-11-20 2010-03-30 Pratt & Whitney Canada Corp. Turbofan gas turbine engine and nacelle arrangement
US8091827B2 (en) 2007-11-16 2012-01-10 The Nordam Group, Inc. Thrust reverser door
US8172175B2 (en) 2007-11-16 2012-05-08 The Nordam Group, Inc. Pivoting door thrust reverser for a turbofan gas turbine engine
US8052085B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
US8051639B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser
US7735778B2 (en) 2007-11-16 2010-06-15 Pratt & Whitney Canada Corp. Pivoting fairings for a thrust reverser
US8052086B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser door
US8127530B2 (en) 2008-06-19 2012-03-06 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
US9932121B2 (en) * 2012-06-22 2018-04-03 United Technologies Corporation Turbomachine flow stability enhancement device control
US10145335B2 (en) * 2012-09-28 2018-12-04 United Technologies Corporation Turbomachine thrust reverser
US9670875B2 (en) * 2012-10-31 2017-06-06 The Boeing Company Thrust reversers and methods to provide reverse thrust
CN109484644A (zh) * 2018-12-27 2019-03-19 酷黑科技（北京）有限公司 一种涵道式飞行器及涵道扩散器
GB2584382A (en) * 2019-01-30 2020-12-09 Gregory Smith Anthony Use of Coanda ejector to achieve thrust reversal

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1196067A (fr) * 1958-05-03 1959-11-20 Snecma Dispositif pneumatique supprimant l'interaction du jet dévié d'un réacteur d'avion avec les parties voisines de la cellule
FR1544066A (fr) * 1966-09-12 1968-10-31 Rolls Royce Tuyaux de circulation d'un fluide à renversement de poussée
US3717304A (en) * 1970-05-06 1973-02-20 Rolls Royce Thrust reverser for fluid flow engine
US3605411A (en) * 1970-07-01 1971-09-20 Rohr Corp Thrust reversing apparatus
US3660981A (en) * 1970-10-05 1972-05-09 Us Air Force The s/tol aircraft
GB1319793A (OSRAM) * 1970-11-19 1973-06-06
US3736750A (en) * 1971-03-12 1973-06-05 Rolls Royce Power plant
FR2174672B1 (OSRAM) * 1972-03-06 1975-06-13 Snecma

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS54124188A (en) * 1978-03-20 1979-09-26 Hitachi Ltd Building method of reactor container
JPS54149243A (en) * 1978-05-15 1979-11-22 Ohbayashigumi Ltd Method of constructing structure under steel container bottom plate in atomic power plant or the like
JPS5559390A (en) * 1978-10-30 1980-05-02 Tokyo Shibaura Electric Co Method of executing reactor containment device
JPS5674696A (en) * 1979-11-22 1981-06-20 Tokyo Shibaura Electric Co Nuclear reactor building constructing method
JP2010514987A (ja) * 2007-01-02 2010-05-06 エアバス フランス 航空機のジェットエンジンのナセルと該ナセルを備える航空機

Also Published As

Publication number Publication date
DE2645349A1 (de) 1977-04-21
FR2327411A1 (fr) 1977-05-06
IT1068895B (it) 1985-03-21
FR2327411B1 (OSRAM) 1981-10-16
DE2645349B2 (de) 1978-05-18
GB1506588A (en) 1978-04-05
US4047381A (en) 1977-09-13
DE2645349C3 (de) 1979-01-11

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