DE69616739T2 - Dichtungsanordnung für schwenkbare Schubumkehrklappe - Google Patents

Dichtungsanordnung für schwenkbare Schubumkehrklappe

Info

Publication number
DE69616739T2
DE69616739T2 DE69616739T DE69616739T DE69616739T2 DE 69616739 T2 DE69616739 T2 DE 69616739T2 DE 69616739 T DE69616739 T DE 69616739T DE 69616739 T DE69616739 T DE 69616739T DE 69616739 T2 DE69616739 T2 DE 69616739T2
Authority
DE
Germany
Prior art keywords
sealing arrangement
thrust reverser
reverser flap
swiveling
swiveling thrust
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
DE69616739T
Other languages
English (en)
Other versions
DE69616739D1 (de
Inventor
Robert Standish
Alain Fournier
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.)
Hurel Hispano Meudon SA
Original Assignee
Societe de Construction des Avions Hurel Dubois
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 Societe de Construction des Avions Hurel Dubois filed Critical Societe de Construction des Avions Hurel Dubois
Publication of DE69616739D1 publication Critical patent/DE69616739D1/de
Application granted granted Critical
Publication of DE69616739T2 publication Critical patent/DE69616739T2/de
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
    • F02K1/78—Other construction of jet pipes
    • F02K1/80—Couplings or connections
    • F02K1/805—Sealing devices therefor, e.g. for movable parts of jet pipes or nozzle flaps
DE69616739T 1996-02-08 1996-02-08 Dichtungsanordnung für schwenkbare Schubumkehrklappe Expired - Lifetime DE69616739T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP96400264A EP0789140B1 (de) 1996-02-08 1996-02-08 Dichtungsanordnung für schwenkbare Schubumkehrklappe

Publications (2)

Publication Number Publication Date
DE69616739D1 DE69616739D1 (de) 2001-12-13
DE69616739T2 true DE69616739T2 (de) 2002-09-05

Family

ID=8225221

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69616739T Expired - Lifetime DE69616739T2 (de) 1996-02-08 1996-02-08 Dichtungsanordnung für schwenkbare Schubumkehrklappe

Country Status (3)

Country Link
US (1) US5934613A (de)
EP (1) EP0789140B1 (de)
DE (1) DE69616739T2 (de)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BR0213262B1 (pt) 2001-10-23 2011-05-31 tubeira de exaustão variável confluente.
US6945031B2 (en) 2003-02-21 2005-09-20 The Nordam Group, Inc. Recessed engine nacelle
US7010905B2 (en) * 2003-02-21 2006-03-14 The Nordam Group, Inc. Ventilated confluent exhaust nozzle
US6971229B2 (en) * 2003-02-26 2005-12-06 The Nordam Group, Inc. Confluent exhaust nozzle
US6966175B2 (en) * 2003-05-09 2005-11-22 The Nordam Group, Inc. Rotary adjustable exhaust nozzle
US7127880B2 (en) * 2003-08-29 2006-10-31 The Nordam Group, Inc. Induction coupled variable nozzle
US8015797B2 (en) 2006-09-21 2011-09-13 Jean-Pierre Lair Thrust reverser nozzle for a turbofan gas turbine engine
FR2914956A1 (fr) * 2007-04-12 2008-10-17 Aircelle Sa Nacelle pour turboreacteur equipee d'un systeme d'inversion de poussee a porte
US7966808B2 (en) * 2007-04-30 2011-06-28 General Electric Company Baffle seal for gas turbine engine thrust reverser
US8052085B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
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
US8052086B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser door
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
GB2464960B (en) * 2008-10-31 2013-03-27 Gen Electric Baffle seal for gas turbine engine thrust reverser
JP5405083B2 (ja) * 2008-10-31 2014-02-05 ゼネラル・エレクトリック・カンパニイ ガスタービンエンジン逆スラスト装置用のバッフルシール
US8549834B2 (en) 2010-10-21 2013-10-08 United Technologies Corporation Gas turbine engine with variable area fan nozzle
US8919784B2 (en) 2011-06-29 2014-12-30 United Technologies Corporation Fan duct blocker actuation tab seal
US9617009B2 (en) 2013-02-22 2017-04-11 United Technologies Corporation ATR full ring sliding nacelle
US9631578B2 (en) 2013-02-22 2017-04-25 United Technologies Corporation Pivot thrust reverser surrounding inner surface of bypass duct
US10247021B2 (en) * 2016-12-07 2019-04-02 Rohr, Inc. High temperature seals for blanketless inner fixed structure

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4005822A (en) * 1975-12-22 1977-02-01 Rohr Industries, Inc. Fan duct thrust reverser
US4182501A (en) * 1977-03-04 1980-01-08 Astech Thrust reverser for jet engine forming active extension of jet tube
FR2486153B1 (fr) * 1980-07-04 1985-10-04 Hurel Dubois Avions Inverseur de poussee pour moteur a reaction, destine notamment a equiper un aeronef
FR2506843B1 (fr) * 1981-05-29 1987-04-24 Hurel Dubois Avions Dispositif d'inversion de poussee pour turboreacteur d'avion
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.
FR2604482B1 (fr) * 1986-09-25 1989-12-15 Fage Etienne Inverseur de poussee pour moteur a reaction d'aeronef et moteur d'aeronef equipe dudit inverseur de poussee
JPH0721316B2 (ja) * 1986-12-09 1995-03-08 本田技研工業株式会社 油圧式伝動装置
US4830519A (en) * 1987-04-06 1989-05-16 United Technologies Corporation Annular seal assembly
FR2618853B1 (fr) * 1987-07-29 1989-11-10 Hispano Suiza Sa Inverseur de poussee de turboreacteur muni d'un deflecteur mobile de porte
GB2212859B (en) * 1987-12-02 1991-03-06 Rolls Royce Plc Ducted fan gas turbine engine with surge controller
US5039171A (en) * 1989-08-18 1991-08-13 Societe Anonyme Dite Hispano-Suiza Multi-panel thrust reverser door
US5243817A (en) * 1990-07-05 1993-09-14 Rohr, Inc. Thrust reverser for fan jet aircraft engines
DE4038623A1 (de) * 1990-12-04 1992-06-11 Bosch Gmbh Robert Handwerkzeugmaschine
FR2683859B1 (fr) * 1991-11-15 1994-02-18 Hispano Suiza Inverseur de poussee de turboreacteur a double flux.
US5224342A (en) * 1992-02-13 1993-07-06 Lair Jean Pierre Latching and sealing arrangement for jet engine thrust reverser
US5209432A (en) * 1992-07-02 1993-05-11 United Technologies Corporation Aircraft reverser port door

Also Published As

Publication number Publication date
EP0789140B1 (de) 2001-11-07
US5934613A (en) 1999-08-10
EP0789140A1 (de) 1997-08-13
DE69616739D1 (de) 2001-12-13

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: HUREL-HISPANO MEUDON, MEUDON-LA-FORET, FR