FR2915527B1 - REAR CASTER STRUCTURE FOR REACTOR ENGINE, SUCH AS A PUSH INVERTER - Google Patents
REAR CASTER STRUCTURE FOR REACTOR ENGINE, SUCH AS A PUSH INVERTERInfo
- Publication number
- FR2915527B1 FR2915527B1 FR0703123A FR0703123A FR2915527B1 FR 2915527 B1 FR2915527 B1 FR 2915527B1 FR 0703123 A FR0703123 A FR 0703123A FR 0703123 A FR0703123 A FR 0703123A FR 2915527 B1 FR2915527 B1 FR 2915527B1
- Authority
- FR
- France
- Prior art keywords
- rear caster
- caster structure
- push inverter
- reactor engine
- reactor
- 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
-
- 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
- B64D29/08—Inspection panels for power plants
-
- 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
- B64D29/06—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
- F02K1/64—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
- 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
- F05D2230/00—Manufacture
- F05D2230/80—Repairing, retrofitting or upgrading methods
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (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)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0703123A FR2915527B1 (en) | 2007-04-30 | 2007-04-30 | REAR CASTER STRUCTURE FOR REACTOR ENGINE, SUCH AS A PUSH INVERTER |
PCT/FR2008/000266 WO2008132297A2 (en) | 2007-04-30 | 2008-02-29 | Rear nacelle structure for a jet engine, such as a thrust reverser |
EP08775611A EP2139770A2 (en) | 2007-04-30 | 2008-02-29 | Rear nacelle structure for a jet engine, such as a thrust reverser |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0703123A FR2915527B1 (en) | 2007-04-30 | 2007-04-30 | REAR CASTER STRUCTURE FOR REACTOR ENGINE, SUCH AS A PUSH INVERTER |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2915527A1 FR2915527A1 (en) | 2008-10-31 |
FR2915527B1 true FR2915527B1 (en) | 2009-06-12 |
Family
ID=38800740
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0703123A Expired - Fee Related FR2915527B1 (en) | 2007-04-30 | 2007-04-30 | REAR CASTER STRUCTURE FOR REACTOR ENGINE, SUCH AS A PUSH INVERTER |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP2139770A2 (en) |
FR (1) | FR2915527B1 (en) |
WO (1) | WO2008132297A2 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2967398B1 (en) | 2010-11-16 | 2012-11-02 | Aircelle Sa | STRUCTURE FOR STRENGTHENING A TURBOJET CAPACITY |
FR3033545B1 (en) | 2015-03-12 | 2018-08-10 | Airbus Operations | NACELLE FOR AIRCRAFT ENGINE ASSEMBLY COMPRISING AT LEAST ONE ARTICULATED NACELLE COVER AT ITS FRONT END |
DE102015206093A1 (en) * | 2015-04-02 | 2016-10-06 | Rolls-Royce Deutschland Ltd & Co Kg | Engine cowling of an aircraft gas turbine |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2661213B1 (en) * | 1990-04-19 | 1992-07-03 | Snecma | AVIATION ENGINE WITH VERY HIGH DILUTION RATES AND OF THE SAID TYPE FRONT CONTRAFAN. |
GB9120658D0 (en) * | 1991-09-27 | 1991-11-06 | Short Brothers Plc | Ducted fan turbine engine |
US5350136A (en) * | 1993-05-14 | 1994-09-27 | United Technologies Corporation | Nacelle arrangement |
FR2757823B1 (en) * | 1996-12-26 | 1999-03-12 | Aerospatiale | LAMINARY FLOW TURBOREACTOR BASKET |
US6220546B1 (en) * | 1999-12-29 | 2001-04-24 | The Boeing Company | Aircraft engine and associated aircraft engine cowl |
FR2897339B1 (en) * | 2006-02-16 | 2008-04-11 | Aircelle Sa | NACELLE DE TURBOREACTEUR WITH LATERAL OPENING OF HOODS |
-
2007
- 2007-04-30 FR FR0703123A patent/FR2915527B1/en not_active Expired - Fee Related
-
2008
- 2008-02-29 EP EP08775611A patent/EP2139770A2/en not_active Withdrawn
- 2008-02-29 WO PCT/FR2008/000266 patent/WO2008132297A2/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
EP2139770A2 (en) | 2010-01-06 |
WO2008132297A2 (en) | 2008-11-06 |
WO2008132297A3 (en) | 2008-12-31 |
FR2915527A1 (en) | 2008-10-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20101230 |