FR2638783B1 - Inverseur de poussee notamment pour moteur a reaction d'aeronef - Google Patents

Inverseur de poussee notamment pour moteur a reaction d'aeronef

Info

Publication number
FR2638783B1
FR2638783B1 FR8814695A FR8814695A FR2638783B1 FR 2638783 B1 FR2638783 B1 FR 2638783B1 FR 8814695 A FR8814695 A FR 8814695A FR 8814695 A FR8814695 A FR 8814695A FR 2638783 B1 FR2638783 B1 FR 2638783B1
Authority
FR
France
Prior art keywords
reaction engine
aircraft reaction
push inverter
inverter
push
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 - Lifetime
Application number
FR8814695A
Other languages
English (en)
Other versions
FR2638783A1 (fr
Inventor
Etienne Fage
Jean-Pierre Lair
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.)
Astech SA
Original Assignee
Astech SA
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 Astech SA filed Critical Astech SA
Priority to FR8814695A priority Critical patent/FR2638783B1/fr
Priority to US07/331,128 priority patent/US5097661A/en
Publication of FR2638783A1 publication Critical patent/FR2638783A1/fr
Application granted granted Critical
Publication of FR2638783B1 publication Critical patent/FR2638783B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime 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
FR8814695A 1988-11-10 1988-11-10 Inverseur de poussee notamment pour moteur a reaction d'aeronef Expired - Lifetime FR2638783B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR8814695A FR2638783B1 (fr) 1988-11-10 1988-11-10 Inverseur de poussee notamment pour moteur a reaction d'aeronef
US07/331,128 US5097661A (en) 1988-11-10 1989-03-31 Jet engine having a planar exit opening

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8814695A FR2638783B1 (fr) 1988-11-10 1988-11-10 Inverseur de poussee notamment pour moteur a reaction d'aeronef

Publications (2)

Publication Number Publication Date
FR2638783A1 FR2638783A1 (fr) 1990-05-11
FR2638783B1 true FR2638783B1 (fr) 1991-04-05

Family

ID=9371767

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8814695A Expired - Lifetime FR2638783B1 (fr) 1988-11-10 1988-11-10 Inverseur de poussee notamment pour moteur a reaction d'aeronef

Country Status (2)

Country Link
US (1) US5097661A (fr)
FR (1) FR2638783B1 (fr)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5176340A (en) * 1991-11-26 1993-01-05 Lair Jean Pierre Thrust reverser with a planar exit opening
US5181676A (en) * 1992-01-06 1993-01-26 Lair Jean Pierre Thrust reverser integrating a variable exhaust area nozzle
IT1257222B (it) * 1992-06-09 1996-01-10 Alenia Aeritalia & Selenia Dispositivo inversore di spinta per motori aeronautici a getto.
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.
FR2727468B1 (fr) 1994-11-30 1996-12-27 Hispano Suiza Sa Inverseur de poussee de turboreacteur a obstacles aval
FR2736390B1 (fr) * 1995-07-05 1997-08-08 Hispano Suiza Sa Inverseur de poussee de turboreacteur a une coquille
US5794433A (en) * 1996-06-18 1998-08-18 The Nordam Group, Inc. Thrust reverser door side fillers
FR2768773B1 (fr) * 1997-09-25 1999-11-05 Hispano Suiza Sa Inverseur de poussee de turboreacteur a coquilles internes
FR2789442B1 (fr) * 1999-02-04 2001-11-09 Snecma Arriere-corps d'ejection a inversion de poussee de turboreacteur
US6938408B2 (en) 2001-04-26 2005-09-06 Propulsion Vectoring, L.P. Thrust vectoring and variable exhaust area for jet engine nozzle
US6845945B1 (en) 2001-07-20 2005-01-25 Aircraft Integration Resources, Inc. Thrust reverser with sliding pivot joints
US8015797B2 (en) * 2006-09-21 2011-09-13 Jean-Pierre Lair Thrust reverser nozzle for a turbofan gas turbine engine
US7665689B2 (en) * 2006-11-24 2010-02-23 The Boeing Company Unconventional integrated propulsion systems and methods for blended wing body aircraft
US8091827B2 (en) 2007-11-16 2012-01-10 The Nordam Group, Inc. Thrust reverser door
US8051639B2 (en) * 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser
US8172175B2 (en) * 2007-11-16 2012-05-08 The Nordam Group, Inc. Pivoting door thrust reverser for a turbofan gas turbine engine
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
US8002217B2 (en) * 2007-11-16 2011-08-23 Spirit Aerosystems, Inc. System for adjustment of thrust reverser pivot door
US8052085B2 (en) * 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
US8127530B2 (en) 2008-06-19 2012-03-06 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
US8959889B2 (en) 2008-11-26 2015-02-24 The Boeing Company Method of varying a fan duct nozzle throat area of a gas turbine engine
US8127532B2 (en) 2008-11-26 2012-03-06 The Boeing Company Pivoting fan nozzle nacelle
WO2011014250A1 (fr) * 2009-07-30 2011-02-03 The Norman Group, Inc. Inverseur de poussee a carenages en coupole
CN102877982B (zh) * 2012-07-24 2015-04-01 中国航空工业集团公司沈阳发动机设计研究所 一种航空发动机反推力装置
US10040563B1 (en) * 2013-04-11 2018-08-07 Geoffrey P. Pinto Dual panel actuator system for jet engines
EP3039275B1 (fr) 2013-08-28 2020-03-04 United Technologies Corporation Ensemble porte coulissante d'inverseur de poussée
US10954888B2 (en) * 2018-03-30 2021-03-23 Rohr, Inc. Hybrid pivot door thrust reversers

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3353355A (en) * 1966-05-31 1967-11-21 United Aircraft Corp Turbofan lightweight thrust reverser
US3579991A (en) * 1970-01-08 1971-05-25 Rohr Corp Thrust reversing apparatus for jet-propelled aircraft
US3604662A (en) * 1970-01-19 1971-09-14 Rohr Corp Thrust-reversing apparatus for jet-propelled aircraft
US4519561A (en) * 1983-05-23 1985-05-28 Rohr Industries, Inc. Aircraft thrust reverser mechanism
GB2168298B (en) * 1984-12-13 1988-01-27 Rolls Royce Thrust reverser
FR2601077B1 (fr) * 1986-07-07 1988-10-21 Hurel Dubois Avions Structure d'ejection des gaz pour moteur a reaction notamment pour reacteur a double flux.

Also Published As

Publication number Publication date
US5097661A (en) 1992-03-24
FR2638783A1 (fr) 1990-05-11

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Legal Events

Date Code Title Description
ST Notification of lapse
RC Opposition against decision of lapse
DA Annulment of decision of lapse
TP Transmission of property
TP Transmission of property