FR2349738A1 - Mecanisme d'inversion de poussee - Google Patents

Mecanisme d'inversion de poussee

Info

Publication number
FR2349738A1
FR2349738A1 FR7712163A FR7712163A FR2349738A1 FR 2349738 A1 FR2349738 A1 FR 2349738A1 FR 7712163 A FR7712163 A FR 7712163A FR 7712163 A FR7712163 A FR 7712163A FR 2349738 A1 FR2349738 A1 FR 2349738A1
Authority
FR
France
Prior art keywords
cascade
blades
exposes
thrust reverser
sliding sleeve
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.)
Withdrawn
Application number
FR7712163A
Other languages
English (en)
Inventor
Augustus Mason Helmintoller
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2349738A1 publication Critical patent/FR2349738A1/fr
Withdrawn legal-status Critical Current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
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
FR7712163A 1976-04-28 1977-04-22 Mecanisme d'inversion de poussee Withdrawn FR2349738A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US68090876A 1976-04-28 1976-04-28

Publications (1)

Publication Number Publication Date
FR2349738A1 true FR2349738A1 (fr) 1977-11-25

Family

ID=24733013

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7712163A Withdrawn FR2349738A1 (fr) 1976-04-28 1977-04-22 Mecanisme d'inversion de poussee

Country Status (5)

Country Link
JP (1) JPS52139816A (fr)
BE (1) BE853946A (fr)
DE (1) DE2718643A1 (fr)
FR (1) FR2349738A1 (fr)
IT (1) IT1203685B (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5211008A (en) * 1990-11-28 1993-05-18 Conception Aeronautique Du Sud Ouest Gas ejection nozzle for a jet engine and a jet engine fitted with this nozzle, in particular an engine of the separate flow type
FR2812035A1 (fr) * 2000-07-24 2002-01-25 Hurel Dubois Avions Perfectionnements aux inverseurs de poussee pour moteurs a reaction, du type a grilles
FR2815672A1 (fr) * 2000-10-19 2002-04-26 Short Brothers Plc Unite de puissance propulsive pour avion
EP1457659A2 (fr) * 2003-02-17 2004-09-15 The Boeing Company Appareil et procédé pour le montage d'un anneau support en cascade sur un inverseur de poussée
WO2008145725A1 (fr) * 2007-06-01 2008-12-04 Airbus France Ensemble moteur pour aeronef a nacelle coulissante
FR3077847A1 (fr) * 2018-02-09 2019-08-16 Safran Nacelles Inverseur de poussee a volets pour ensemble propulsif d’aeronef

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BR112016013122A2 (pt) * 2013-12-23 2017-08-08 Gen Electric Aeronave e sistema de resfriamento de injeção
FR3088373B1 (fr) * 2018-11-09 2021-03-19 Safran Nacelles Joint d’etancheite pour nacelle de turboreacteur d’aeronef

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5211008A (en) * 1990-11-28 1993-05-18 Conception Aeronautique Du Sud Ouest Gas ejection nozzle for a jet engine and a jet engine fitted with this nozzle, in particular an engine of the separate flow type
FR2812035A1 (fr) * 2000-07-24 2002-01-25 Hurel Dubois Avions Perfectionnements aux inverseurs de poussee pour moteurs a reaction, du type a grilles
EP1176302A1 (fr) 2000-07-24 2002-01-30 Hurel-Hispano Meudon Inverseur de poussée pour moteur à réaction
US6438942B2 (en) 2000-07-24 2002-08-27 Societe De Construction Des Avions Hurel-Dubois (Societe Anonyme) Cascade-type reversers for jet engines
FR2815672A1 (fr) * 2000-10-19 2002-04-26 Short Brothers Plc Unite de puissance propulsive pour avion
EP1457659A2 (fr) * 2003-02-17 2004-09-15 The Boeing Company Appareil et procédé pour le montage d'un anneau support en cascade sur un inverseur de poussée
EP1457659A3 (fr) * 2003-02-17 2005-04-13 The Boeing Company Appareil et procédé pour le montage d'un anneau support en cascade sur un inverseur de poussée
WO2008145725A1 (fr) * 2007-06-01 2008-12-04 Airbus France Ensemble moteur pour aeronef a nacelle coulissante
US8226027B2 (en) 2007-06-01 2012-07-24 Airbus Operations (Societe Par Actions Simplifiee) Engine assembly for aircraft with sliding nacelle
RU2472678C2 (ru) * 2007-06-01 2013-01-20 Эрбюс Операсьон Узел двигателя самолета с подвижной гондолой двигателя
FR3077847A1 (fr) * 2018-02-09 2019-08-16 Safran Nacelles Inverseur de poussee a volets pour ensemble propulsif d’aeronef

Also Published As

Publication number Publication date
BE853946A (fr) 1977-08-16
JPS52139816A (en) 1977-11-22
DE2718643A1 (de) 1977-11-10
IT1203685B (it) 1989-02-15

Similar Documents

Publication Publication Date Title
GB1085780A (en) Improvements in thrust reverser
GB1092170A (en) Improvements in thrust reversers for jet propulsion powerplants
GB2045179B (en) Thrust reverser for a long duct fan engine
GB1104764A (en) Improvements in thrust reverters for jet propulsion powerplants
GB1092015A (en) Improvements in thrust reversers for jet propulsion power plants
GB1304212A (fr)
GB1316029A (en) Turbofan engine thrust reversers
GB852829A (en) Improvements in or relating to gas-turbine jet propulsion engines
GB848679A (en) Noise suppressor and thrust reverser for aircraft jet engines
GB1534583A (en) Reversal of thrust in gas turbine engines
GB1181746A (en) Thrust Reverser for Jet Propulsion Plant
GB1083738A (en) Improvements in variable area exhaust nozzle
GB1085619A (en) Gas turbine engine
FR2349738A1 (fr) Mecanisme d'inversion de poussee
GB1147351A (en) Improvements in thrust reverser for jet propulsion engine
GB1211923A (en) Thrust reverser for gas turbine jet propulsion engine
GB1247691A (en) Improvements in or relating to fan ducts for gas turbine ducted fan engines
GB1270434A (en) Turbofan engines
GB925010A (en) Improvements in or relating to turbo-fan units
FR2379705A1 (fr) Dispositif d'inversion de poussee pour turboreacteur d'avion
GB1479149A (en) Variable pitch ducted fan gas turbine power plant
GB1033583A (en) Thrust reverser for a jet propulsion engine
GB1276265A (en) Improvements in or relating to thrust deflectors for gas turbine ducted fan engines
GB976449A (en) Improvements in thrust vectoring and modulating device
GB1166396A (en) Improvements in Power Plant with Thrust Reverser.

Legal Events

Date Code Title Description
ST Notification of lapse