BRPI0702056A - motor de tipo turbina a gás e método de operação do mesmo - Google Patents
motor de tipo turbina a gás e método de operação do mesmoInfo
- Publication number
- BRPI0702056A BRPI0702056A BRPI0702056-2A BRPI0702056A BRPI0702056A BR PI0702056 A BRPI0702056 A BR PI0702056A BR PI0702056 A BRPI0702056 A BR PI0702056A BR PI0702056 A BRPI0702056 A BR PI0702056A
- Authority
- BR
- Brazil
- Prior art keywords
- turbine engine
- gas turbine
- air flow
- reversing device
- thrust
- Prior art date
Links
- 230000005465 channeling Effects 0.000 abstract 1
- 230000000694 effects Effects 0.000 abstract 1
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
- F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/02—Power-plant nacelles, fairings, or cowlings associated with wings
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Motor de tipo turbina a gás e método de operação do mesmo. é fornecido um dispositivo reversor do empuxo (100). O dispositivo reversor do empuxo (100) inclui uma primeira pluralidade defletores (180) para canalizar o fluxo de ar do motor a turbina (10) contra a superfície de uma asa (12) de aeronave, de modo a permitir o aumento da sustentação, e uma segunda pluralidade de defletores (182) para canalizar o fluxo de ar do motor a turbina para realizar o empuxo reverso.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/456,666 US20080010969A1 (en) | 2006-07-11 | 2006-07-11 | Gas turbine engine and method of operating same |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0702056A true BRPI0702056A (pt) | 2008-03-04 |
Family
ID=38326477
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0702056-2A BRPI0702056A (pt) | 2006-07-11 | 2007-06-13 | motor de tipo turbina a gás e método de operação do mesmo |
Country Status (7)
Country | Link |
---|---|
US (1) | US20080010969A1 (pt) |
EP (1) | EP1878904A2 (pt) |
JP (1) | JP2008019864A (pt) |
CN (1) | CN101104441A (pt) |
BR (1) | BRPI0702056A (pt) |
CA (1) | CA2592911A1 (pt) |
RU (1) | RU2007126316A (pt) |
Families Citing this family (46)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008045070A1 (en) | 2006-10-12 | 2008-04-17 | United Technologies Corporation | Variable area fan nozzle thrust reverser |
WO2008045072A1 (en) * | 2006-10-12 | 2008-04-17 | United Technologies Corporation | Dual function cascade integrated variable area fan nozzle and thrust reverser |
EP2479414B1 (en) | 2007-08-08 | 2015-06-10 | Rohr, Inc. | 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 |
US9494084B2 (en) | 2007-08-23 | 2016-11-15 | United Technologies Corporation | Gas turbine engine with fan variable area nozzle for low fan pressure ratio |
US9701415B2 (en) | 2007-08-23 | 2017-07-11 | United Technologies Corporation | Gas turbine engine with axial movable fan variable area nozzle |
US10167813B2 (en) | 2007-08-23 | 2019-01-01 | United Technologies Corporation | Gas turbine engine with fan variable area nozzle to reduce fan instability |
US8170771B2 (en) * | 2008-06-30 | 2012-05-01 | Honeywell International Inc. | Fluid-powered thrust reverser actuation system speed control |
FR2936222B1 (fr) * | 2008-09-24 | 2011-04-01 | Aircelle Sa | Nacelle a section de tuyere variable |
FR2938878B1 (fr) * | 2008-11-26 | 2013-11-08 | Aircelle Sa | Inverseur de poussee pour nacelle de turboreacteur a double flux |
FR2944563B1 (fr) * | 2009-04-16 | 2011-04-22 | Aircelle Sa | Dispositif d'inversion de poussee |
FR2946094B1 (fr) * | 2009-06-02 | 2014-04-18 | Aircelle Sa | Inverseur de poussee pour nacelle de turboreacteur double flux. |
EP2278147B1 (en) * | 2009-06-16 | 2014-06-25 | Rohr, Inc. | Translating variable area fan nozzle providing an upstream bypass flow exit |
FR2949141B1 (fr) * | 2009-08-14 | 2011-07-15 | Aircelle Sa | Dispositif d'inversion de poussee |
US8875486B2 (en) | 2010-05-17 | 2014-11-04 | Rohr, Inc. | Guide system for nacelle assembly |
FR2961483B1 (fr) * | 2010-06-18 | 2013-01-18 | Aircelle Sa | Carter de soufflante de turboreacteur d'aeronef |
US8511973B2 (en) | 2010-06-23 | 2013-08-20 | Rohr, Inc. | Guide system for nacelle assembly |
FR2966434B1 (fr) * | 2010-10-21 | 2013-05-31 | Sagem Defense Securite | Systeme d'actionnement pour un ensemble de propulsion d'un avion |
US8727269B2 (en) * | 2011-06-06 | 2014-05-20 | General Electric Company | System and method for mounting an aircraft engine |
GB201112986D0 (en) * | 2011-07-28 | 2011-09-14 | Rolls Royce Plc | Ducted fan gas turbine assembly |
FR2978802B1 (fr) * | 2011-08-05 | 2017-07-14 | Aircelle Sa | Inverseur a grilles mobiles et tuyere variable par translation |
FR2978990A1 (fr) * | 2011-08-08 | 2013-02-15 | Aircelle Sa | Dispositif d'inversion de poussee |
RU2488706C2 (ru) * | 2011-09-20 | 2013-07-27 | Открытое акционерное общество "СТАР" | Способ управления газотурбинным двигателем |
US9151183B2 (en) * | 2011-11-21 | 2015-10-06 | United Technologies Corporation | Retractable exhaust liner segment for gas turbine engines |
DE102012002885A1 (de) * | 2012-02-14 | 2013-08-14 | Rolls-Royce Deutschland Ltd & Co Kg | Fluggasturbinenschubumkehrvorrichtung |
FR2990474B1 (fr) * | 2012-05-10 | 2014-05-02 | Aircelle Sa | Inverseur de poussee a volet de blocage a deploiement controle |
US9371138B2 (en) | 2012-06-07 | 2016-06-21 | Rohr, Inc. | Nacelle |
FR2995637B1 (fr) * | 2012-09-19 | 2018-05-11 | Safran Nacelles | Structure fixe de dispositif d'inversion de poussee |
WO2015080785A2 (en) * | 2013-09-19 | 2015-06-04 | United Technologies Corporation | Extended thrust reverser cascade |
CN103696877A (zh) * | 2013-12-05 | 2014-04-02 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种具有喷管面积调节能力的反推力装置 |
CN104712455B (zh) * | 2013-12-12 | 2017-07-04 | 中航商用航空发动机有限责任公司 | 涡扇发动机的反推力装置和用于该反推力装置的反推叶栅 |
US10161311B2 (en) | 2013-12-23 | 2018-12-25 | General Electric Company | Aircraft with injection cooling system and injection cooling system |
DE102014223109A1 (de) * | 2014-11-12 | 2016-05-12 | Rolls-Royce Deutschland Ltd & Co Kg | Triebwerksverkleidung einer Gasturbine mit Schubumkehrvorrichtung und verstellbarer Ausströmdüse |
DE102015203219A1 (de) * | 2015-02-23 | 2016-08-25 | Rolls-Royce Deutschland Ltd & Co Kg | Triebwerksverkleidung einer Gasturbine mit Schubumkehrvorrichtung und im Querschnitt verstellbarer Ausströmdüse |
DE102015206143A1 (de) * | 2015-04-07 | 2016-10-13 | Rolls-Royce Deutschland Ltd & Co Kg | Vorrichtung zur Beeinflussung von Bodenwirbeln im Ansaugbereich einer Fluggasturbine |
DE102015206985A1 (de) | 2015-04-17 | 2016-10-20 | Rolls-Royce Deutschland Ltd & Co Kg | Triebwerksverkleidung einer Fluggasturbine |
EP3106381B1 (en) * | 2015-06-15 | 2018-10-24 | Airbus Operations, S.L. | Aircraft with a protective shield against an engine blade release |
PL415487A1 (pl) * | 2015-12-31 | 2017-07-03 | General Electric Company | Formowana kompozytowa osłona chroniąca przed zużyciem krawędzi dla złącza w postaci wpustu V-kształtnego i łopatki V-kształtnej |
JP2017047898A (ja) * | 2016-08-31 | 2017-03-09 | 元延 深瀬 | エンジンの後方部に揚力板機構を設けたジェット飛行機。 |
FR3074855A1 (fr) * | 2017-12-11 | 2019-06-14 | Airbus Operations | Grille pour la formation d'un flux d'inversion d'un turboreacteur d'aeronef |
CN108501642A (zh) * | 2018-05-03 | 2018-09-07 | 苏龙 | 一种飞行汽车 |
FR3087498B1 (fr) | 2018-10-22 | 2021-03-05 | Airbus Operations Sas | Turboreacteur comportant une nacelle equipee d’un systeme d’inversion de poussee mobile en translation et d’un carter de soufflante equipe de supports |
US11078871B2 (en) * | 2018-12-21 | 2021-08-03 | Rohr, Inc. | Thrust reverser system with cascades |
FR3094956B1 (fr) * | 2019-04-10 | 2021-03-05 | Safran | Systeme propulsif pour un aeronef |
DE102019207742A1 (de) * | 2019-05-27 | 2020-12-03 | MTU Aero Engines AG | Flugzeug mit Mantelstromtriebwerk |
US11613372B2 (en) * | 2020-11-09 | 2023-03-28 | Rohr, Inc. | Ducted fan case attachment structure |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3779010A (en) * | 1972-08-17 | 1973-12-18 | Gen Electric | Combined thrust reversing and throat varying mechanism for a gas turbine engine |
JPS5340996A (en) * | 1973-08-09 | 1978-04-13 | Yoshio Nozaki | Vertical takeoff and landing aeroplane obtaining lift by high speed airflow along upper surface of main wing |
US3920203A (en) * | 1974-12-23 | 1975-11-18 | Boeing Co | Thrust control apparatus for obtaining maximum thrust reversal in minimum time upon landing of an aircraft |
FR2622929A1 (fr) * | 1987-11-05 | 1989-05-12 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a grilles,a section variable d'ejection |
US5655360A (en) * | 1995-05-31 | 1997-08-12 | General Electric Company | Thrust reverser with variable nozzle |
GB9613166D0 (en) * | 1996-06-24 | 1996-08-28 | Short Brothers Plc | Aircraft propulsive power unit |
US5987880A (en) * | 1997-07-08 | 1999-11-23 | Mcdonnell Douglas Corporation | Supersonic engine, multi-port thrust reversing system |
FR2786532B1 (fr) * | 1998-11-26 | 2001-09-07 | Snecma | Inverseur de poussee de turboreacteur a grilles superposables |
GB2347126B (en) * | 1999-02-23 | 2003-02-12 | Rolls Royce Plc | Thrust reverser |
FR2804474B1 (fr) * | 2000-01-27 | 2002-06-28 | Hispano Suiza Sa | Inverseur de poussee a grilles aubagees de deviation a structure arriere fixe |
-
2006
- 2006-07-11 US US11/456,666 patent/US20080010969A1/en not_active Abandoned
-
2007
- 2007-06-13 BR BRPI0702056-2A patent/BRPI0702056A/pt not_active IP Right Cessation
- 2007-06-27 CA CA002592911A patent/CA2592911A1/en not_active Abandoned
- 2007-07-06 EP EP07111927A patent/EP1878904A2/en not_active Withdrawn
- 2007-07-06 JP JP2007177873A patent/JP2008019864A/ja active Pending
- 2007-07-10 RU RU2007126316/06A patent/RU2007126316A/ru not_active Application Discontinuation
- 2007-07-11 CN CNA2007101368792A patent/CN101104441A/zh active Pending
Also Published As
Publication number | Publication date |
---|---|
RU2007126316A (ru) | 2009-01-20 |
CN101104441A (zh) | 2008-01-16 |
US20080010969A1 (en) | 2008-01-17 |
EP1878904A2 (en) | 2008-01-16 |
CA2592911A1 (en) | 2008-01-11 |
JP2008019864A (ja) | 2008-01-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 5A ANUIDADE. |
|
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2161 DE 05/06/2012. |