FR2903454B1 - Nacelle de reacteur d'aeronef et aeronef comprenant une telle nacelle - Google Patents
Nacelle de reacteur d'aeronef et aeronef comprenant une telle nacelleInfo
- Publication number
- FR2903454B1 FR2903454B1 FR0606113A FR0606113A FR2903454B1 FR 2903454 B1 FR2903454 B1 FR 2903454B1 FR 0606113 A FR0606113 A FR 0606113A FR 0606113 A FR0606113 A FR 0606113A FR 2903454 B1 FR2903454 B1 FR 2903454B1
- Authority
- FR
- France
- Prior art keywords
- nacelle
- aircraft
- reactor
- aircraft reactor
- reactor nacelle
- 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 - Fee Related
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
-
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
-
- 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
- F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
-
- 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
- F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
- F02K1/30—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for varying effective area of jet pipe or nozzle
-
- 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
- F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
- F02K1/32—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for reversing thrust
-
- 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
- F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
- F02K1/34—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for attenuating noise
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
-
- 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)
- Wind Motors (AREA)
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0606113A FR2903454B1 (fr) | 2006-07-05 | 2006-07-05 | Nacelle de reacteur d'aeronef et aeronef comprenant une telle nacelle |
FR0752545A FR2903455B1 (fr) | 2006-07-05 | 2007-01-05 | Procede pour inverser la poussee produite par un ensemble propulsif d'un aeronef, dispositif pour sa mise en oeuvre, nacelle equipee dudit dispositif |
CN2007800234892A CN101535622B (zh) | 2006-07-05 | 2007-06-28 | 将飞机推进装置产生的推力反转的方法、实施该方法的装置及装备有该装置的发动机舱 |
PCT/FR2007/051553 WO2008003889A2 (fr) | 2006-07-05 | 2007-06-28 | Procede pour inverser la poussee produite par un ensemble propulsif d ' un aeronef, dispositif pour sa mise en oeuvre, nacelle equipee dudit dispositif et aeronef |
EP07803962.5A EP2035680B1 (fr) | 2006-07-05 | 2007-06-28 | Procédé visant à réduire, annuler ou inverser la poussée générée par au moins un flux d'air sortant d'une nacelle d'un ensemble propulsif d'un aéronef, et dispositif, nacelle et aéronef associés |
JP2009517356A JP2009541659A (ja) | 2006-07-05 | 2007-06-28 | 航空機推進一式装置による発生スラスト反転方法とその実施装置、同装置を装備したエンジン室ならびに航空機 |
US12/307,483 US20090199536A1 (en) | 2006-07-05 | 2007-06-28 | Process for reversing the thrust produced by a propulsion unit of an aircraft, device for its implementation, nacelle equipped with said device |
CA002656279A CA2656279A1 (fr) | 2006-07-05 | 2007-06-28 | Procede pour inverser la poussee produite par un ensemble propulsif d'un aeronef, dispositif pour sa mise en oeuvre, nacelle equipee dudit dispositif |
BRPI0713212-3A BRPI0713212A2 (pt) | 2006-07-05 | 2007-06-28 | processo para reduzir, anular ou inverter o empuxo gerado por pelo menos um fluxo de ar expelido por um conjunto propulsor de uma aeronave, dispositivo para a aplicação do processo, nacela de aeronave e aeronave |
RU2009103777/06A RU2009103777A (ru) | 2006-07-05 | 2007-06-28 | Способ реверсирования тяги, создаваемой силовой установкой летательного аппарата, устройство для его применения, гондола, оборудованная упомянутым устройством |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0606113A FR2903454B1 (fr) | 2006-07-05 | 2006-07-05 | Nacelle de reacteur d'aeronef et aeronef comprenant une telle nacelle |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2903454A1 FR2903454A1 (fr) | 2008-01-11 |
FR2903454B1 true FR2903454B1 (fr) | 2008-08-29 |
Family
ID=37667484
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0606113A Expired - Fee Related FR2903454B1 (fr) | 2006-07-05 | 2006-07-05 | Nacelle de reacteur d'aeronef et aeronef comprenant une telle nacelle |
Country Status (2)
Country | Link |
---|---|
CN (1) | CN101535622B (fr) |
FR (1) | FR2903454B1 (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8006479B2 (en) * | 2007-10-15 | 2011-08-30 | United Technologies Corporation | Thrust reversing variable area nozzle |
CA2918320C (fr) | 2013-07-26 | 2018-05-15 | Mra Systems, Inc. | Mat d'accrochage de moteur pour aeronef |
CA2919124A1 (fr) * | 2013-07-30 | 2015-02-05 | General Electric Company | Systeme inverseur de poussee a ensemble charniere a translation-rotation |
CN113120244B (zh) * | 2021-04-27 | 2022-07-15 | 成都飞机工业(集团)有限责任公司 | 一种提高背负式并列双发双s弯进气道性能的设计方法 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1479705A (fr) * | 1966-05-11 | 1967-05-05 | Bristol Siddeley Engines Ltd | Perfectionnements aux moteurs comportant une turbine à gaz |
GB1357370A (en) * | 1971-09-24 | 1974-06-19 | Rolls Royce | Ducted fan gas turbine jet propulsion engine with thrust control means |
US4978071A (en) * | 1989-04-11 | 1990-12-18 | General Electric Company | Nozzle with thrust vectoring in the yaw direction |
US5713537A (en) * | 1995-12-11 | 1998-02-03 | Northrop Grumman Corporation | Blockerless thrust reverser |
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 |
FR2766522B1 (fr) * | 1997-07-24 | 1999-09-03 | Hispano Suiza Sa | Inverseur de poussee de turbosoufflante a obstacle a guidage axial lies au capot primaire |
FR2776023B1 (fr) * | 1998-03-12 | 2000-04-07 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes formant ecopes associees a une grille mobile |
FR2777043B1 (fr) * | 1998-04-02 | 2000-05-12 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes formant ecopes associees a un capotage externe articule |
-
2006
- 2006-07-05 FR FR0606113A patent/FR2903454B1/fr not_active Expired - Fee Related
-
2007
- 2007-06-28 CN CN2007800234892A patent/CN101535622B/zh not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2903454A1 (fr) | 2008-01-11 |
CN101535622A (zh) | 2009-09-16 |
CN101535622B (zh) | 2013-04-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CA | Change of address |
Effective date: 20110916 |
|
CD | Change of name or company name |
Owner name: AIRBUS HOLDING, FR Effective date: 20110916 |
|
CJ | Change in legal form |
Effective date: 20110916 |
|
TP | Transmission of property |
Owner name: AIRBUS HOLDING, FR Effective date: 20110913 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
|
ST | Notification of lapse |
Effective date: 20210305 |