JPS6142097B2 - - Google Patents

Info

Publication number
JPS6142097B2
JPS6142097B2 JP56066096A JP6609681A JPS6142097B2 JP S6142097 B2 JPS6142097 B2 JP S6142097B2 JP 56066096 A JP56066096 A JP 56066096A JP 6609681 A JP6609681 A JP 6609681A JP S6142097 B2 JPS6142097 B2 JP S6142097B2
Authority
JP
Japan
Prior art keywords
jet pipe
nozzle
bypass
thrust
area
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
JP56066096A
Other languages
English (en)
Japanese (ja)
Other versions
JPS572449A (en
Inventor
Chaaruzu Hitsuchikotsuku Marukomu
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 1971 Ltd
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 1971 Ltd filed Critical Rolls Royce 1971 Ltd
Publication of JPS572449A publication Critical patent/JPS572449A/ja
Publication of JPS6142097B2 publication Critical patent/JPS6142097B2/ja
Granted 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
    • F02K1/56—Reversing jet main flow
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • 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
    • F02K1/56—Reversing jet main flow
    • F02K1/563—Reversing jet main flow in specified direction, e.g. to obviate its reinjection

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Exhaust Silencers (AREA)
  • Jet Pumps And Other Pumps (AREA)
JP6609681A 1980-04-30 1981-04-30 Gas turbine engine Granted JPS572449A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8014331A GB2075447B (en) 1980-04-30 1980-04-30 Thrust deflectors for gas turbine engines

Publications (2)

Publication Number Publication Date
JPS572449A JPS572449A (en) 1982-01-07
JPS6142097B2 true JPS6142097B2 (en, 2012) 1986-09-19

Family

ID=10513119

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6609681A Granted JPS572449A (en) 1980-04-30 1981-04-30 Gas turbine engine

Country Status (5)

Country Link
US (1) US4462207A (en, 2012)
JP (1) JPS572449A (en, 2012)
DE (1) DE3114481C2 (en, 2012)
FR (1) FR2481748B1 (en, 2012)
GB (1) GB2075447B (en, 2012)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59136224U (ja) * 1983-02-28 1984-09-11 株式会社アマダ 帯鋸の案内装置
FR2680547B1 (fr) * 1991-08-21 1993-10-15 Hispano Suiza Inverseur de poussee de turboreacteur ayant un bord de deviation a courbure evolutive.
FR2717860B1 (fr) * 1994-03-28 1996-05-31 Sud Ouest Conception Aeronauti Inverseur de poussée doté d'au moins une porte basculante, pour moteur à réaction, notamment d'aéronef, et moteur à réaction équipé de cet inverseur de poussée.
FR2717859B1 (fr) * 1994-03-28 1996-05-31 Sud Ouest Conception Aeronauti Turbomoteur à double flux équipé d'un système d'inversion de poussée et d'un dispositif de restriction du canal d'éjection des gaz froids, et dispositif de restriction équipant un tel turbomoteur.
FR2736390B1 (fr) * 1995-07-05 1997-08-08 Hispano Suiza Sa Inverseur de poussee de turboreacteur a une coquille
FR2736682B1 (fr) * 1995-07-12 1997-08-14 Hispano Suiza Sa Inverseur de poussee de turbomachine a double flux a portes dissymetriques
FR2741114B1 (fr) * 1995-11-15 1997-12-05 Hispano Suiza Sa Inverseur de poussee de turboreacteur a obstacles aval tendant a l'equilibrage
GB2356897B (en) * 1999-12-01 2003-05-14 Secr Defence Improved nozzle
US6526744B2 (en) 2001-04-30 2003-03-04 Honeywell International Inc. System and method for controlling the stowage of jet engine thrust reversers
US6519929B2 (en) 2001-04-30 2003-02-18 Honeywell International, Inc. System and method for controlling the deployment of jet engine thrust reversers
US6439504B1 (en) 2001-06-15 2002-08-27 Honeywell International, Inc. System and method for sustaining electric power during a momentary power interruption in an electric thrust reverser actuation system
US6681559B2 (en) 2001-07-24 2004-01-27 Honeywell International, Inc. Thrust reverser position determination system and method
US6684623B2 (en) * 2002-02-27 2004-02-03 Honeywell International, Inc. Gearless electric thrust reverser actuators and actuation system incorporating same
US6622963B1 (en) 2002-04-16 2003-09-23 Honeywell International Inc. System and method for controlling the movement of an aircraft engine cowl door
US7055329B2 (en) * 2003-03-31 2006-06-06 General Electric Company Method and apparatus for noise attenuation for gas turbine engines using at least one synthetic jet actuator for injecting air
FR2914956A1 (fr) * 2007-04-12 2008-10-17 Aircelle Sa Nacelle pour turboreacteur equipee d'un systeme d'inversion de poussee a porte
US8051639B2 (en) * 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser
US10040563B1 (en) * 2013-04-11 2018-08-07 Geoffrey P. Pinto Dual panel actuator system for jet engines
US9388768B2 (en) * 2013-08-23 2016-07-12 Rohr, Inc. Blocker door actuation system and apparatus
US10125722B2 (en) * 2015-02-13 2018-11-13 United Technologies Corporation Turbine engine with a turbo-compressor
US10100731B2 (en) 2015-02-13 2018-10-16 United Technologies Corporation Turbine engine with a turbo-compressor
US10337401B2 (en) 2015-02-13 2019-07-02 United Technologies Corporation Turbine engine with a turbo-compressor
US20170198658A1 (en) * 2016-01-11 2017-07-13 The Boeing Company Thrust reverser
FR3057620B1 (fr) * 2016-10-18 2020-07-31 Safran Aircraft Engines Ensemble propulsif comprenant un conduit d'alimentation du generateur de gaz dans un carter inter-veine
FR3060660B1 (fr) * 2016-12-20 2019-05-17 Safran Nacelles Nacelle de turboreacteur d'aeronef, ensemble propulsif et aeronef comportant une telle nacelle
FR3075176B1 (fr) * 2017-12-18 2020-11-06 Safran Aircraft Engines Ensemble de capot ouvrant et mecanisme de deploiement
US11408368B2 (en) * 2020-03-31 2022-08-09 Rolls-Royce North American Technologies Inc. Reconfigurable exhaust nozzle for a gas turbine engine
CN114151196B (zh) * 2022-02-09 2022-05-24 南京航空航天大学 一种并联式组合动力进气道的调节机构及设计方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2620622A (en) * 1945-05-12 1952-12-09 Svenska Turbinfab Ab Reverse thrust arrangement for braking jet-propelled aircraft
US2481330A (en) * 1946-08-06 1949-09-06 Gen Electric Variable jet nozzle
US3013386A (en) * 1954-06-01 1961-12-19 United Aircraft Corp Reverse thrust device
GB1002709A (en) * 1964-02-03 1965-08-25 Rolls Royce Improvements in or relating to thrust reversers for jet propulsion engines
GB1150012A (en) * 1966-09-12 1969-04-30 Rolls Royce Fluid Flow Duct Including Thrust Reversing Means
GB1327385A (en) * 1969-12-09 1973-08-22 Secr Defence Jet propulsion apparatus aircraft
US3579991A (en) * 1970-01-08 1971-05-25 Rohr Corp Thrust reversing apparatus for jet-propelled aircraft
US3599432A (en) * 1970-04-02 1971-08-17 Rohr Corp Thrust reversing apparatus for turbo-fan propulsion unit
US3984974A (en) * 1972-11-29 1976-10-12 Rohr Industries, Inc. Thrust spoiling apparatus and method
US3907224A (en) * 1973-06-01 1975-09-23 Boeing Co Variable ramp exhaust nozzle and clamshell reverser
US4073440A (en) * 1976-04-29 1978-02-14 The Boeing Company Combination primary and fan air thrust reversal control systems for long duct fan jet engines
US4182501A (en) * 1977-03-04 1980-01-08 Astech Thrust reverser for jet engine forming active extension of jet tube
US4183478A (en) * 1977-11-25 1980-01-15 The Boeing Company Jet thrust reverser

Also Published As

Publication number Publication date
DE3114481C2 (de) 1983-12-01
DE3114481A1 (de) 1982-02-18
JPS572449A (en) 1982-01-07
GB2075447A (en) 1981-11-18
US4462207A (en) 1984-07-31
FR2481748B1 (fr) 1986-11-21
GB2075447B (en) 1983-10-26
FR2481748A1 (fr) 1981-11-06

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