IT1277176B1 - Turbomotore a doppio flusso provvisto di un sistema di inversione di spinta e di un dispositivo di restrizione del canale anulare di - Google Patents

Turbomotore a doppio flusso provvisto di un sistema di inversione di spinta e di un dispositivo di restrizione del canale anulare di

Info

Publication number
IT1277176B1
IT1277176B1 IT95MI000587A ITMI950587A IT1277176B1 IT 1277176 B1 IT1277176 B1 IT 1277176B1 IT 95MI000587 A IT95MI000587 A IT 95MI000587A IT MI950587 A ITMI950587 A IT MI950587A IT 1277176 B1 IT1277176 B1 IT 1277176B1
Authority
IT
Italy
Prior art keywords
turbomotor
double
flow
ring channel
restricting device
Prior art date
Application number
IT95MI000587A
Other languages
English (en)
Inventor
Guy Servanty
Original Assignee
Conception Aeronautique Du Sud
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 Conception Aeronautique Du Sud filed Critical Conception Aeronautique Du Sud
Publication of ITMI950587A0 publication Critical patent/ITMI950587A0/it
Publication of ITMI950587A1 publication Critical patent/ITMI950587A1/it
Application granted granted Critical
Publication of IT1277176B1 publication Critical patent/IT1277176B1/it

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
IT95MI000587A 1994-03-28 1995-03-24 Turbomotore a doppio flusso provvisto di un sistema di inversione di spinta e di un dispositivo di restrizione del canale anulare di IT1277176B1 (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9403919A FR2717859B1 (fr) 1994-03-28 1994-03-28 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.

Publications (3)

Publication Number Publication Date
ITMI950587A0 ITMI950587A0 (it) 1995-03-24
ITMI950587A1 ITMI950587A1 (it) 1996-09-24
IT1277176B1 true IT1277176B1 (it) 1997-11-05

Family

ID=9461695

Family Applications (1)

Application Number Title Priority Date Filing Date
IT95MI000587A IT1277176B1 (it) 1994-03-28 1995-03-24 Turbomotore a doppio flusso provvisto di un sistema di inversione di spinta e di un dispositivo di restrizione del canale anulare di

Country Status (4)

Country Link
US (1) US5495710A (it)
FR (1) FR2717859B1 (it)
GB (1) GB2287921B (it)
IT (1) IT1277176B1 (it)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2755729B1 (fr) * 1996-11-12 1999-01-08 Fage Etienne Turbomoteur a double flux pourvu d'une tuyere confluente et d'un inverseur de poussee
FR2823258B1 (fr) 2001-04-05 2003-09-19 Hispano Suiza Sa Systeme de verrouillage de secours pour porte d'inverseur de poussee
FR2834533B1 (fr) * 2002-01-10 2004-10-29 Hurel Hispano Le Havre Dispositif de refroidissement de la tuyere commune sur une nacelle
FR2920204B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Procede et systeme de commande d'au moins un actionneur de capots d'un inverseur de poussee pour turboreacteur
FR2920197B1 (fr) * 2007-08-20 2013-08-09 Aircelle Sa Ressort pour volet d'inverseur de poussee a grilles pour turboreacteur d'aeronef

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB985192A (en) * 1960-05-13 1965-03-03 Bristol Siddeley Engines Ltd Improvements in aircraft propulsion power plants
US3330115A (en) * 1966-05-31 1967-07-11 United Aircraft Corp Turbofan thrust reverser
FR2126922B1 (it) * 1971-01-20 1975-01-17 Snecma
US4052007A (en) * 1975-11-25 1977-10-04 United Technologies Corporation Flap-type two-dimensional nozzle
FR2456216A1 (fr) * 1979-05-11 1980-12-05 Astech Sa Turbomoteur a double flux equipe d'un inverseur de poussee
GB2075447B (en) * 1980-04-30 1983-10-26 Rolls Royce Thrust deflectors for gas turbine engines
FR2551132B1 (fr) * 1983-05-27 1990-06-08 Astech Turbomoteur a double flux equipe d'une tuyere centrale a melange et d'un inverseur de poussee
FR2602550B1 (fr) * 1986-08-11 1994-02-04 Fage Etienne Turbomoteur a double flux a tuyere confluente variable
US4884748A (en) * 1988-09-02 1989-12-05 United Technologies Corporation Fairing flap arrangement
US5150839A (en) * 1991-03-14 1992-09-29 General Electric Company Nozzle load management
US5224342A (en) * 1992-02-13 1993-07-06 Lair Jean Pierre Latching and sealing arrangement for jet engine thrust reverser
US5370402A (en) * 1993-05-07 1994-12-06 Eg&G Sealol, Inc. Pressure balanced compliant seal device

Also Published As

Publication number Publication date
GB2287921B (en) 1997-12-10
GB2287921A (en) 1995-10-04
US5495710A (en) 1996-03-05
GB9506314D0 (en) 1995-05-17
ITMI950587A1 (it) 1996-09-24
ITMI950587A0 (it) 1995-03-24
FR2717859A1 (fr) 1995-09-29
FR2717859B1 (fr) 1996-05-31

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Legal Events

Date Code Title Description
0001 Granted