FR2975971B1 - Nacelle pour un turboreacteur double flux d'un aeronef - Google Patents
Nacelle pour un turboreacteur double flux d'un aeronefInfo
- Publication number
- FR2975971B1 FR2975971B1 FR1154809A FR1154809A FR2975971B1 FR 2975971 B1 FR2975971 B1 FR 2975971B1 FR 1154809 A FR1154809 A FR 1154809A FR 1154809 A FR1154809 A FR 1154809A FR 2975971 B1 FR2975971 B1 FR 2975971B1
- Authority
- FR
- France
- Prior art keywords
- flow path
- annular flow
- mobile flap
- nacelle
- external structure
- 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.)
- Active
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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
-
- 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
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
- F02K1/1207—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure
-
- 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
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
- F02K1/1223—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/50—Kinematic linkage, i.e. transmission of position
- F05D2260/52—Kinematic linkage, i.e. transmission of position involving springs
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/501—Elasticity
-
- 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)
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1154809A FR2975971B1 (fr) | 2011-06-01 | 2011-06-01 | Nacelle pour un turboreacteur double flux d'un aeronef |
CN201280024797.8A CN103732899A (zh) | 2011-06-01 | 2012-05-11 | 用于飞行器旁通涡轮喷气发动机的机舱 |
CA2837635A CA2837635A1 (fr) | 2011-06-01 | 2012-05-11 | Nacelle pour un turboreacteur double flux d'un aeronef |
PCT/FR2012/051045 WO2012164186A1 (fr) | 2011-06-01 | 2012-05-11 | Nacelle pour un turboréacteur double flux d'un aéronef |
RU2013156313/11A RU2013156313A (ru) | 2011-06-01 | 2012-05-11 | Гондола двухконтурного турбореактивного двигателя летательного аппарата |
EP12728656.5A EP2715099A1 (fr) | 2011-06-01 | 2012-05-11 | Nacelle pour un turboréacteur double flux d'un aéronef |
BR112013027959A BR112013027959A2 (pt) | 2011-06-01 | 2012-05-11 | nacela |
US14/093,928 US9279385B2 (en) | 2011-06-01 | 2013-12-02 | Nacelle for an aircraft bypass turbojet engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1154809A FR2975971B1 (fr) | 2011-06-01 | 2011-06-01 | Nacelle pour un turboreacteur double flux d'un aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2975971A1 FR2975971A1 (fr) | 2012-12-07 |
FR2975971B1 true FR2975971B1 (fr) | 2013-05-17 |
Family
ID=46321081
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1154809A Active FR2975971B1 (fr) | 2011-06-01 | 2011-06-01 | Nacelle pour un turboreacteur double flux d'un aeronef |
Country Status (8)
Country | Link |
---|---|
US (1) | US9279385B2 (fr) |
EP (1) | EP2715099A1 (fr) |
CN (1) | CN103732899A (fr) |
BR (1) | BR112013027959A2 (fr) |
CA (1) | CA2837635A1 (fr) |
FR (1) | FR2975971B1 (fr) |
RU (1) | RU2013156313A (fr) |
WO (1) | WO2012164186A1 (fr) |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1424094A (en) * | 1973-05-04 | 1976-02-04 | Rolls Royce | Gas turbine engines |
FR2474592A1 (fr) * | 1980-01-25 | 1981-07-31 | Snecma | Dispositif de tuyere de turboreacteur |
US5141154A (en) * | 1991-04-22 | 1992-08-25 | United Technologies Corporation | Variable throat convergent/divergent nozzle |
EP1509447A4 (fr) * | 2002-05-21 | 2010-07-21 | Nordam Group Inc | Buse de reacteur a double flux bifurquee |
FR2887854B1 (fr) * | 2005-06-30 | 2008-08-08 | Airbus France Sas | Nacelle pour aeronef et aeronef muni d'au moins une telle nacelle |
US7874160B2 (en) * | 2007-08-21 | 2011-01-25 | United Technologies Corporation | Nozzle-area ratio float bias |
US20090090817A1 (en) * | 2007-10-09 | 2009-04-09 | Monka Gary H | Aircraft configuration, gas turbine engine, controller and trim system for neutralizing pitching moments with power changes |
WO2010008641A2 (fr) | 2008-04-09 | 2010-01-21 | Williams International Co., L.L.C. | Système d'injection rotatif de moteur de turbine à gaz et procédé |
FR2929998B1 (fr) * | 2008-04-14 | 2011-08-12 | Aircelle Sa | Nacelle de turboreacteur a double flux |
US7716932B2 (en) * | 2008-07-24 | 2010-05-18 | Spirit Aerosystems, Inc. | Dilating fan duct nozzle |
-
2011
- 2011-06-01 FR FR1154809A patent/FR2975971B1/fr active Active
-
2012
- 2012-05-11 RU RU2013156313/11A patent/RU2013156313A/ru not_active Application Discontinuation
- 2012-05-11 CN CN201280024797.8A patent/CN103732899A/zh active Pending
- 2012-05-11 WO PCT/FR2012/051045 patent/WO2012164186A1/fr active Application Filing
- 2012-05-11 BR BR112013027959A patent/BR112013027959A2/pt not_active IP Right Cessation
- 2012-05-11 CA CA2837635A patent/CA2837635A1/fr not_active Abandoned
- 2012-05-11 EP EP12728656.5A patent/EP2715099A1/fr not_active Withdrawn
-
2013
- 2013-12-02 US US14/093,928 patent/US9279385B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US9279385B2 (en) | 2016-03-08 |
CA2837635A1 (fr) | 2012-12-06 |
US20140086738A1 (en) | 2014-03-27 |
EP2715099A1 (fr) | 2014-04-09 |
WO2012164186A1 (fr) | 2012-12-06 |
RU2013156313A (ru) | 2015-07-20 |
CN103732899A (zh) | 2014-04-16 |
BR112013027959A2 (pt) | 2017-01-17 |
FR2975971A1 (fr) | 2012-12-07 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
|
CD | Change of name or company name |
Owner name: SAFRAN NACELLES, FR Effective date: 20180125 |
|
PLFP | Fee payment |
Year of fee payment: 8 |
|
PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |