ES2034710T3 - Inversor de empuje de turborreactor provisto de puertas con minitobera de desviacion del flujo inverso. - Google Patents
Inversor de empuje de turborreactor provisto de puertas con minitobera de desviacion del flujo inverso.Info
- Publication number
- ES2034710T3 ES2034710T3 ES198989403015T ES89403015T ES2034710T3 ES 2034710 T3 ES2034710 T3 ES 2034710T3 ES 198989403015 T ES198989403015 T ES 198989403015T ES 89403015 T ES89403015 T ES 89403015T ES 2034710 T3 ES2034710 T3 ES 2034710T3
- Authority
- ES
- Spain
- Prior art keywords
- turbo
- external
- internal
- mini
- deviation
- 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
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
-
- 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)
- Control Of Turbines (AREA)
- Structure Of Emergency Protection For Nuclear Reactors (AREA)
Abstract
UNA PUERTA BASCULANTE (107) DE UN INVERSOR DE EMPUJE DEL FLUJO SECUNDARIO DE UN TURBORREACTOR DE DOBLE FLUJO CONSTA DE UN PANEL EXTERNO (9) CUYA SUPERFICIE EXTERNA SE UNE AL PERFIL EXTERNO ABARQUILLADO (4) Y DE LA PARTE POSTERIOR FIJA (3) DEL INVERSOR Y UN PANEL INTERNO (111) CUYA SUPERFICIE INTERNA (111A) SE CONFUNDE, EN EMPUJE DIRECTO, CON LA SUPERFICIE TEORICA DE DELIMITACION DEL CANAL DEL FLUJO SECUNDARIO. ENTRE DICHOS PANELES INTERNO (111) Y EXTERNO (9) HAY UN PASO (20) QUE PRESENTA UNA ABERTURA (21,22) A CADA EXTREMO, POR EL LADO INTERNO DE LA PUERTA, Y QUE FORMA, AL PRODUCIRSE EL FUNCIONAMIENTO EN INVERSION DE EMPUJE, UNA MINITUBERIA DE VERTIDO POR DONDE PASA UNA PARTE (15B) DEL FLUJO INVERTIDO (15A), OBTENIENDOSE CON LO CUAL UNA DESVIACION OPTIMA
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8814606A FR2638784B1 (fr) | 1988-11-09 | 1988-11-09 | Inverseur de poussee de turboreacteur muni de portes a mini-tuyere de deviation du flux inverse |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2034710T3 true ES2034710T3 (es) | 1993-04-01 |
Family
ID=9371703
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES198989403015T Expired - Lifetime ES2034710T3 (es) | 1988-11-09 | 1989-11-02 | Inversor de empuje de turborreactor provisto de puertas con minitobera de desviacion del flujo inverso. |
Country Status (6)
Country | Link |
---|---|
US (1) | US5040730A (es) |
EP (1) | EP0368725B1 (es) |
CA (1) | CA2002466C (es) |
DE (1) | DE68902727T2 (es) |
ES (1) | ES2034710T3 (es) |
FR (1) | FR2638784B1 (es) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2669079B1 (fr) * | 1990-11-14 | 1994-12-30 | Hurel Dubois Avions | Amelioration aux inverseurs de poussee a portes pour avion a reaction. |
FR2678026B1 (fr) * | 1991-06-24 | 1993-10-15 | Hurel Dubois Avions | Perfectionnement aux inverseurs de poussee de moteur a reaction. |
US5224342A (en) * | 1992-02-13 | 1993-07-06 | Lair Jean Pierre | Latching and sealing arrangement for jet engine thrust reverser |
FR2687733B1 (fr) * | 1992-02-26 | 1995-08-04 | Hurel Dubois Avions | Inverseur de poussee pour moteur a reaction assurant un guidage du flux devie. |
FR2738597B1 (fr) * | 1995-09-13 | 1997-10-03 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes associees a un panneau primaire |
FR2754565B1 (fr) * | 1996-10-10 | 1999-01-08 | Hispano Suiza Sa | Inverseur de poussee a portes a debit de fuite controle |
FR2760789B1 (fr) * | 1997-03-13 | 2001-09-07 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes a structure externe autoraidie |
FR2764339B1 (fr) * | 1997-06-05 | 1999-07-16 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes formant ecopes associees a une casquette amont mobile |
DE19749576A1 (de) * | 1997-11-10 | 1999-05-12 | Bmw Rolls Royce Gmbh | Schubumkehrvorrichtung eines Flug-Strahltriebwerkes |
US6938408B2 (en) * | 2001-04-26 | 2005-09-06 | Propulsion Vectoring, L.P. | Thrust vectoring and variable exhaust area for jet engine nozzle |
DE602005026608D1 (de) * | 2004-07-30 | 2011-04-14 | Hill Rom Services Inc | Fortgeschrittenes Gelenksystem und Matratzenauflage für ein Bett |
US8015797B2 (en) * | 2006-09-21 | 2011-09-13 | Jean-Pierre Lair | Thrust reverser nozzle for a turbofan gas turbine engine |
WO2008045048A1 (en) * | 2006-10-12 | 2008-04-17 | United Technologies Corporation | Integrated variable area nozzle and thrust reversing mechanism |
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 |
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 |
US8052085B2 (en) | 2007-11-16 | 2011-11-08 | The Nordam Group, Inc. | 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 |
US8127530B2 (en) | 2008-06-19 | 2012-03-06 | The Nordam Group, Inc. | Thrust reverser for a turbofan gas turbine engine |
FR2965304B1 (fr) * | 2010-09-23 | 2012-10-12 | Airbus Operations Sas | Dispositif de decharge d'air pour turboreacteur d'avion a double flux |
FR2980825B1 (fr) * | 2011-09-29 | 2013-09-13 | Aircelle Sa | Porte d'inverseur de poussee a ouvertures laterales |
US9163583B2 (en) * | 2013-05-01 | 2015-10-20 | Rohr, Inc. | System, apparatus, and method for thrust vectoring |
US9771894B2 (en) | 2013-10-07 | 2017-09-26 | Rohr, Inc. | Radially connected cascade grids |
US9650992B2 (en) * | 2013-10-17 | 2017-05-16 | Rohr, Inc. | Core cowl thrust reverser system and apparatus |
US9964071B2 (en) * | 2015-01-13 | 2018-05-08 | Rohr, Inc. | Decoupled translating sleeve |
DE102016100575A1 (de) | 2016-01-14 | 2017-07-20 | Rolls-Royce Deutschland Ltd & Co Kg | Schubumkehrvorrichtung einer Strömungsmaschine |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2620622A (en) * | 1945-05-12 | 1952-12-09 | Svenska Turbinfab Ab | Reverse thrust arrangement for braking jet-propelled aircraft |
US3601992A (en) * | 1970-06-10 | 1971-08-31 | Rohr Corp | Thrust reversing apparatus |
US4093122A (en) * | 1976-11-03 | 1978-06-06 | Rohr Industries, Inc. | Integrated divergent exhaust nozzle thrust reverser |
FR2506843B1 (fr) * | 1981-05-29 | 1987-04-24 | Hurel Dubois Avions | Dispositif d'inversion de poussee pour turboreacteur d'avion |
FR2618852B1 (fr) * | 1987-07-29 | 1989-11-10 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur muni d'un dispositif redresseur de flux |
FR2621082A1 (fr) * | 1987-09-30 | 1989-03-31 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes munies d'une plaque au profil de veine |
US4922712A (en) * | 1988-03-28 | 1990-05-08 | General Electric Company | Thrust reverser for high bypass turbofan engine |
-
1988
- 1988-11-09 FR FR8814606A patent/FR2638784B1/fr not_active Expired - Lifetime
-
1989
- 1989-11-02 EP EP89403015A patent/EP0368725B1/fr not_active Expired - Lifetime
- 1989-11-02 ES ES198989403015T patent/ES2034710T3/es not_active Expired - Lifetime
- 1989-11-02 DE DE8989403015T patent/DE68902727T2/de not_active Expired - Fee Related
- 1989-11-07 US US07/432,495 patent/US5040730A/en not_active Expired - Lifetime
- 1989-11-08 CA CA002002466A patent/CA2002466C/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US5040730A (en) | 1991-08-20 |
EP0368725A1 (fr) | 1990-05-16 |
DE68902727T2 (de) | 1993-03-25 |
FR2638784A1 (fr) | 1990-05-11 |
CA2002466A1 (en) | 1990-05-09 |
FR2638784B1 (fr) | 1990-12-21 |
DE68902727D1 (de) | 1992-10-08 |
EP0368725B1 (fr) | 1992-09-02 |
CA2002466C (fr) | 1998-11-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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