FR2962978B1 - TURBOREACTOR NACELLE - Google Patents
TURBOREACTOR NACELLEInfo
- Publication number
- FR2962978B1 FR2962978B1 FR1056006A FR1056006A FR2962978B1 FR 2962978 B1 FR2962978 B1 FR 2962978B1 FR 1056006 A FR1056006 A FR 1056006A FR 1056006 A FR1056006 A FR 1056006A FR 2962978 B1 FR2962978 B1 FR 2962978B1
- Authority
- FR
- France
- Prior art keywords
- turboreactor
- nacelle
- turboreactor 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.)
- 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
- F02K1/54—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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/06—Attaching of nacelles, fairings or cowlings
-
- 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
- F02K1/76—Control or regulation of thrust reversers
- F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
-
- 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
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/34—Arrangement of components translated
-
- 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
- F05D2250/00—Geometry
- F05D2250/40—Movement of components
- F05D2250/41—Movement of components with one degree of freedom
-
- 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
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1056006A FR2962978B1 (en) | 2010-07-22 | 2010-07-22 | TURBOREACTOR NACELLE |
PCT/FR2011/051649 WO2012010774A2 (en) | 2010-07-22 | 2011-07-12 | Turbojet engine nacelle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1056006A FR2962978B1 (en) | 2010-07-22 | 2010-07-22 | TURBOREACTOR NACELLE |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2962978A1 FR2962978A1 (en) | 2012-01-27 |
FR2962978B1 true FR2962978B1 (en) | 2012-08-03 |
Family
ID=43706336
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1056006A Active FR2962978B1 (en) | 2010-07-22 | 2010-07-22 | TURBOREACTOR NACELLE |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR2962978B1 (en) |
WO (1) | WO2012010774A2 (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2999240B1 (en) * | 2012-12-11 | 2015-01-02 | Aircelle Sa | SYNCHRONIZATION SYSTEM FOR PUSH REVERSING DEVICE |
FR3002785B1 (en) * | 2013-03-01 | 2015-03-27 | Aircelle Sa | TRANSLATANT AND FIXED GRIDS WITH A T / R O-DUCT. |
FR3007800B1 (en) * | 2013-07-01 | 2017-10-20 | Aircelle Sa | THRUST INVERTER OF A TURBOJET NACELLE COMPRISING PARTIALLY INTEGRATED GRIDS IN HOODS |
FR3019229B1 (en) * | 2014-03-31 | 2016-05-06 | Aircelle Sa | THRUST INVERTER OF A TURBOJET NACELLE COMPRISING MOBILE HOOD CONTROL JIGS AND A VARIABLE SECONDARY TUBE |
US10309343B2 (en) * | 2014-11-06 | 2019-06-04 | Rohr, Inc. | Split sleeve hidden door thrust reverser |
US10605197B2 (en) * | 2014-12-02 | 2020-03-31 | United Technologies Corporation | Gas turbine engine and thrust reverser assembly therefore |
US10208708B2 (en) * | 2015-01-29 | 2019-02-19 | Rohr, Inc. | Translating cascade hidden blocker door thrust reverser |
US10428764B2 (en) * | 2016-02-10 | 2019-10-01 | Rohr, Inc. | Deflection limiter for a cascade assembly of a thrust reverser |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2182724B (en) * | 1985-10-08 | 1988-12-07 | Rolls Royce | Gas turbine engine thrust reverser |
FR2622929A1 (en) * | 1987-11-05 | 1989-05-12 | Hispano Suiza Sa | DRIVE INVERTER OF GRID TURBOREACTOR, WITH VARIABLE EJECTION SECTION |
FR2786532B1 (en) * | 1998-11-26 | 2001-09-07 | Snecma | OVERHEAD GRID TURBOREACTOR DRIVE INVERTER |
GB2347126B (en) * | 1999-02-23 | 2003-02-12 | Rolls Royce Plc | Thrust reverser |
FR2922058B1 (en) * | 2007-10-04 | 2009-12-04 | Aircelle Sa | TELESCOPIC LINEAR ACTUATOR FOR MOVING A FIRST AND A SECOND ELEMENTS RELATIVELY TO A FIXED ELEMENT |
-
2010
- 2010-07-22 FR FR1056006A patent/FR2962978B1/en active Active
-
2011
- 2011-07-12 WO PCT/FR2011/051649 patent/WO2012010774A2/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
FR2962978A1 (en) | 2012-01-27 |
WO2012010774A3 (en) | 2012-06-07 |
WO2012010774A2 (en) | 2012-01-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 7 |
|
PLFP | Fee payment |
Year of fee payment: 8 |
|
CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 Owner name: AIRCELLE, FR Effective date: 20170719 |
|
CD | Change of name or company name |
Owner name: SAFRAN NACELLES, FR Effective date: 20180125 Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20180125 |
|
PLFP | Fee payment |
Year of fee payment: 9 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
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PLFP | Fee payment |
Year of fee payment: 14 |