FR2337258A1 - Equipement inverseur de poussee pour moteurs a double flux - Google Patents

Equipement inverseur de poussee pour moteurs a double flux

Info

Publication number
FR2337258A1
FR2337258A1 FR7619695A FR7619695A FR2337258A1 FR 2337258 A1 FR2337258 A1 FR 2337258A1 FR 7619695 A FR7619695 A FR 7619695A FR 7619695 A FR7619695 A FR 7619695A FR 2337258 A1 FR2337258 A1 FR 2337258A1
Authority
FR
France
Prior art keywords
shutters
jet engine
thrust reverser
engine thrust
operating cylinders
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.)
Granted
Application number
FR7619695A
Other languages
English (en)
Other versions
FR2337258B3 (fr
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.)
Plessey Handel und Investments AG
Original Assignee
Plessey Handel und Investments 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 Plessey Handel und Investments AG filed Critical Plessey Handel und Investments AG
Publication of FR2337258A1 publication Critical patent/FR2337258A1/fr
Application granted granted Critical
Publication of FR2337258B3 publication Critical patent/FR2337258B3/fr
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
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
FR7619695A 1976-01-03 1976-06-29 Equipement inverseur de poussee pour moteurs a double flux Granted FR2337258A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB11176 1976-01-03

Publications (2)

Publication Number Publication Date
FR2337258A1 true FR2337258A1 (fr) 1977-07-29
FR2337258B3 FR2337258B3 (fr) 1979-03-23

Family

ID=9698617

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7619695A Granted FR2337258A1 (fr) 1976-01-03 1976-06-29 Equipement inverseur de poussee pour moteurs a double flux

Country Status (1)

Country Link
FR (1) FR2337258A1 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4533098A (en) * 1983-06-20 1985-08-06 General Electric Company Thrust reverser attachment
US4683717A (en) * 1984-03-07 1987-08-04 Societe Nationale D'etude Et De Construction De Moteur D'aviation "S.N.E.C.M.A." Structural cowlings of twin flow turbo jet engines
FR2715695A1 (fr) * 1994-02-01 1995-08-04 Rolls Royce Plc Inverseur de poussée pour un moteur à turbine à gaz à soufflante canalisée.
US5987880A (en) * 1997-07-08 1999-11-23 Mcdonnell Douglas Corporation Supersonic engine, multi-port thrust reversing system
EP3299609A1 (fr) * 2016-09-27 2018-03-28 The Boeing Company Systèmes et procédés d'inverseur de poussée en cascade à double tour

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4533098A (en) * 1983-06-20 1985-08-06 General Electric Company Thrust reverser attachment
US4683717A (en) * 1984-03-07 1987-08-04 Societe Nationale D'etude Et De Construction De Moteur D'aviation "S.N.E.C.M.A." Structural cowlings of twin flow turbo jet engines
FR2715695A1 (fr) * 1994-02-01 1995-08-04 Rolls Royce Plc Inverseur de poussée pour un moteur à turbine à gaz à soufflante canalisée.
US5987880A (en) * 1997-07-08 1999-11-23 Mcdonnell Douglas Corporation Supersonic engine, multi-port thrust reversing system
EP3299609A1 (fr) * 2016-09-27 2018-03-28 The Boeing Company Systèmes et procédés d'inverseur de poussée en cascade à double tour

Also Published As

Publication number Publication date
FR2337258B3 (fr) 1979-03-23

Similar Documents

Publication Publication Date Title
GB1024952A (en) Diverter valve assembly
GB1345892A (en) Gas turbine engines
SE8107799L (sv) Manovermekanism for stellbara kompressorledskenor och luftavtappningsventil, arbetande i flera plan
GB1534583A (en) Reversal of thrust in gas turbine engines
JPS5248714A (en) Blade rotation device mounted on rear end of moving blade in gas turbine engine
EP0109219A3 (fr) Dispositif d'inversion de jet pour un moteur à turbine à gaz
FR2337258A1 (fr) Equipement inverseur de poussee pour moteurs a double flux
US4047682A (en) Fan cowl translation lock
GB1415679A (en) Gas turbine engine powerplant
FR2379705A1 (fr) Dispositif d'inversion de poussee pour turboreacteur d'avion
GB1252193A (fr)
GB1033583A (en) Thrust reverser for a jet propulsion engine
GB1532850A (en) Axial-flow reversible turbine
JPS5641467A (en) Movable system for propeller blade in fluid velocity variation
FR2349738A1 (fr) Mecanisme d'inversion de poussee
JPS5434117A (en) Auto-stop nozzle
JPS545207A (en) Rotary compressor
GB1064330A (en) Vane operating mechanism for a fluid flow machine such as a gas turbine engine
GB1227157A (fr)
GB978462A (en) Gas turbine by-pass engine
FR2381281A1 (fr) Dispositif de controle du deplacement axial d'un arbre
GB1017831A (en) Air motor having a silencing attachment
GB1507914A (en) Device for preventing foreign matters from being sucked into a gas turbine engine for an aircraft
ES257350A1 (es) Un turbomotor de gas
GB1535598A (en) Turbofan aero engines and propulsion nozzles therefor

Legal Events

Date Code Title Description
ST Notification of lapse