RU93032038A - TURBO-REACTIVE ENGINE REVERSOR HAVING A EDGE OF CHANGE OF DIRECTION WITH A CHANGING CURVATURE - Google Patents

TURBO-REACTIVE ENGINE REVERSOR HAVING A EDGE OF CHANGE OF DIRECTION WITH A CHANGING CURVATURE

Info

Publication number
RU93032038A
RU93032038A RU93032038/06A RU93032038A RU93032038A RU 93032038 A RU93032038 A RU 93032038A RU 93032038/06 A RU93032038/06 A RU 93032038/06A RU 93032038 A RU93032038 A RU 93032038A RU 93032038 A RU93032038 A RU 93032038A
Authority
RU
Russia
Prior art keywords
edge
change
reversor
turbo
changing curvature
Prior art date
Application number
RU93032038/06A
Other languages
Russian (ru)
Other versions
RU2069782C1 (en
Inventor
Каримали Феликс
Жан Легра Мишель
Original Assignee
Испано Сюиза
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
Priority claimed from FR9110475A external-priority patent/FR2680547B1/en
Application filed by Испано Сюиза filed Critical Испано Сюиза
Publication of RU93032038A publication Critical patent/RU93032038A/en
Application granted granted Critical
Publication of RU2069782C1 publication Critical patent/RU2069782C1/en

Links

Claims (1)

Реверсор тяги турбореактивного двигателя, имеющий кромку изменения направления с изменяющейся кривизной, содержит трубу инверсии прохождения потока, реверсируемого реверсором тяги турбореактивного двигателя, ограниченную с одной стороны кромкой изменения направления, выполненной заодно с неподвижной частью. Продольные сечения кромки изменения направления имеют изменяющуюся кривизну от одной боковой кромки к другой у трубы инверсии для улучшения управления потоками инвертированного течения.The thrust reverser of a turbojet engine, which has an edge of a change in direction with a varying curvature, contains a flow inversion tube reversed by a thrust reverser of a turbojet engine, bounded on one side by the edge of a change of direction, made integral with the fixed part. The longitudinal sections of the edge of the change of direction have varying curvature from one side edge to the other at the inversion pipe to improve the control of the flow of the inverted flow.
RU9293032038A 1991-08-21 1992-08-19 Thrust reverser of turbojet engine RU2069782C1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR9110475A FR2680547B1 (en) 1991-08-21 1991-08-21 TURBOREACTOR DRIVE INVERTER HAVING A DEVIATION EDGE WITH EVOLUTIVE CURVATURE.
FR9110475 1991-08-21
PCT/FR1992/000802 WO1993004273A1 (en) 1991-08-21 1992-08-19 Turboreactor thrust reverser having a progressive curvature deflecting edge

Publications (2)

Publication Number Publication Date
RU93032038A true RU93032038A (en) 1995-11-10
RU2069782C1 RU2069782C1 (en) 1996-11-27

Family

ID=9416306

Family Applications (1)

Application Number Title Priority Date Filing Date
RU9293032038A RU2069782C1 (en) 1991-08-21 1992-08-19 Thrust reverser of turbojet engine

Country Status (11)

Country Link
US (1) US5297387A (en)
EP (1) EP0530078B1 (en)
AT (1) ATE125595T1 (en)
CA (1) CA2076476C (en)
DE (1) DE69203677T2 (en)
ES (1) ES2075652T3 (en)
FR (1) FR2680547B1 (en)
GR (1) GR3017375T3 (en)
RU (1) RU2069782C1 (en)
UA (1) UA26446C2 (en)
WO (1) WO1993004273A1 (en)

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FR2730764B1 (en) * 1995-02-21 1997-03-14 Hispano Suiza Sa PUSH INVERTER WITH DOORS ASSOCIATED WITH A DOWNSTREAM PANEL
FR2736682B1 (en) * 1995-07-12 1997-08-14 Hispano Suiza Sa DOUBLE FLOW TURBOMACHINE DRIVE INVERTER WITH DISSYMMETRIC DOORS
US5779454A (en) * 1995-07-25 1998-07-14 Ficht Gmbh & Co. Kg Combined pressure surge fuel pump and nozzle assembly
FR2741910B1 (en) 1995-11-30 1998-01-02 Hispano Suiza Sa DOOR REVERSER OF TURBOJET WITH DOORS WITH ARTICULATED REAR PANEL
FR2748525B1 (en) * 1996-05-09 1998-06-19 Hispano Suiza Sa TURBOREACTOR DRIVE INVERTER WITH DOORS WITH DEFLECTIVE BLADES
FR2748778B1 (en) * 1996-05-15 1998-06-19 Hispano Suiza Sa TURBOREACTOR DRIVE INVERTER WITH DOORS ASSOCIATED WITH A UPSTREAM PANEL
FR2748779B1 (en) * 1996-05-15 1998-06-19 Hispano Suiza Sa TURBOREACTOR DRIVE INVERTER WITH DOORS ASSOCIATED WITH A UPSTREAM PANEL
FR2751377B1 (en) * 1996-07-18 1998-09-04 Hispano Suiza Sa DOOR TURBOREACTOR THRUST CHANGEOVER WITH SLIDING PANEL
FR2752017B1 (en) * 1996-08-01 1998-10-16 Hispano Suiza Sa TURBOREACTOR DRIVE INVERTER WITH SCOOPING DOORS
FR2754313B1 (en) * 1996-10-03 1999-01-08 Hispano Suiza Sa DOOR REVERSER WITH OPTIMIZED CONTROL JACK INSTALLATION
FR2757215B1 (en) * 1996-12-12 1999-01-22 Hispano Suiza Sa DOOR TURBORATOR PUSH INVERTER HAVING DEFLECTIVE VANES ASSOCIATED WITH THE FIXED STRUCTURE
FR2760788B1 (en) * 1997-03-13 1999-05-07 Hispano Suiza Sa PUSH INVERTER WITH TURBO JET WITH PLATED EXTERNAL STRUCTURE
EP0926333A1 (en) * 1997-12-26 1999-06-30 SOCIETE DE CONSTRUCTION DES AVIONS HUREL-DUBOIS (société anonyme) Thrust reverser configuration
FR2813103B1 (en) * 2000-08-17 2003-02-28 Aircelle Sa PUSH-INVERTER WITH DOORS ON BOARD DEVIATION
US8015797B2 (en) * 2006-09-21 2011-09-13 Jean-Pierre Lair Thrust reverser nozzle for a turbofan gas turbine engine
US20080083210A1 (en) * 2006-10-04 2008-04-10 Spirit Aerosystems, Inc Monolithic thrust reverser components
CN101939528B (en) * 2007-08-08 2013-07-24 罗尔股份有限公司 Variable area fan nozzle with bypass flow
US9759087B2 (en) 2007-08-08 2017-09-12 Rohr, Inc. Translating variable area fan nozzle providing an upstream bypass flow exit
US8172175B2 (en) 2007-11-16 2012-05-08 The Nordam Group, Inc. Pivoting door thrust reverser for a turbofan gas turbine engine
US8052085B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
US8052086B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser door
US8051639B2 (en) * 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser
US8091827B2 (en) 2007-11-16 2012-01-10 The Nordam Group, Inc. Thrust reverser door
US7735778B2 (en) 2007-11-16 2010-06-15 Pratt & Whitney Canada Corp. Pivoting fairings for a thrust reverser
US8127530B2 (en) 2008-06-19 2012-03-06 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
US8875486B2 (en) 2010-05-17 2014-11-04 Rohr, Inc. Guide system for nacelle assembly
US8511973B2 (en) 2010-06-23 2013-08-20 Rohr, Inc. Guide system for nacelle assembly
DE102011008918A1 (en) * 2011-01-19 2012-07-19 Rolls-Royce Deutschland Ltd & Co Kg Aircraft gas turbine thrust reverser, has detour elements arranged at peripheral region of cowl, and lever swingably arranged at rear end region of detour elements, where lever enables pivoting doors with displacement of detour elements
US9038367B2 (en) 2011-09-16 2015-05-26 United Technologies Corporation Fan case thrust reverser
FR3007078B1 (en) * 2013-06-12 2015-06-05 Aircelle Sa FASTENER FOR THE ATTACHMENT OF A VERINO OF AN INVERTER WITH DOORS OF A TURBOJET CAPACITY AND A TURBOREACTOR NACELLE
RU2663249C1 (en) 2017-03-16 2018-08-03 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Method for manufacturing sections of a thrust reverser bearing grid

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US2620622A (en) * 1945-05-12 1952-12-09 Svenska Turbinfab Ab Reverse thrust arrangement for braking jet-propelled aircraft
US3599432A (en) * 1970-04-02 1971-08-17 Rohr Corp Thrust reversing apparatus for turbo-fan propulsion unit
US4000610A (en) * 1975-04-28 1977-01-04 General Electric Company Flight maneuverable nozzle for gas turbine engines
US4175385A (en) * 1977-12-12 1979-11-27 General Electric Company Thrust reverser for an asymmetric aircraft exhaust nozzle
GB2075447B (en) * 1980-04-30 1983-10-26 Rolls Royce Thrust deflectors for gas turbine engines
FR2486153B1 (en) * 1980-07-04 1985-10-04 Hurel Dubois Avions DRIVE INVERTER FOR A REACTION ENGINE, IN PARTICULAR FOR EQUIPPING AN AIRCRAFT
FR2506843B1 (en) * 1981-05-29 1987-04-24 Hurel Dubois Avions PUSH-INVERSION DEVICE FOR AIRPLANE TURBOREACTOR
FR2559838B1 (en) * 1984-02-21 1988-05-13 Hurel Dubois Avions PROCESS AND DEVICE FOR CONTROLLING THE REVERSE JET IN A REACTION ENGINE WITH A PUSH INVERTER
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US5046307A (en) * 1988-03-28 1991-09-10 General Electric Company Thrust reverser for high bypass turbofan engine
FR2634251B1 (en) * 1988-07-18 1993-08-13 Hispano Suiza Sa DOUBLE-FLOW TURBOREACTOR DRIVE INVERTER HAVING MOBILE DEVIATION EDGES
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