FR3024435B1 - Capot de soufflante pliable guide, pour ensemble moteur d'aeronef - Google Patents
Capot de soufflante pliable guide, pour ensemble moteur d'aeronefInfo
- Publication number
- FR3024435B1 FR3024435B1 FR1457436A FR1457436A FR3024435B1 FR 3024435 B1 FR3024435 B1 FR 3024435B1 FR 1457436 A FR1457436 A FR 1457436A FR 1457436 A FR1457436 A FR 1457436A FR 3024435 B1 FR3024435 B1 FR 3024435B1
- Authority
- FR
- France
- Prior art keywords
- aircraft engine
- engine assembly
- blower hood
- guided folding
- folding blower
- 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
-
- 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
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- 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
-
- 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
-
- 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
- F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
- F02K1/085—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone by transversely deforming an internal member
-
- 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
- F02K1/15—Control or regulation
- F02K1/18—Control or regulation automatic
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
- B64C7/02—Nacelles
-
- 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)
- 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)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1457436A FR3024435B1 (fr) | 2014-07-31 | 2014-07-31 | Capot de soufflante pliable guide, pour ensemble moteur d'aeronef |
US14/811,152 US9783314B2 (en) | 2014-07-31 | 2015-07-28 | Foldable guiding ventilator cover for an aircraft engine assembly |
CN201510456819.3A CN105314119B (zh) | 2014-07-31 | 2015-07-29 | 用于飞行器发动机组件的可折叠的导引通风器盖 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1457436A FR3024435B1 (fr) | 2014-07-31 | 2014-07-31 | Capot de soufflante pliable guide, pour ensemble moteur d'aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3024435A1 FR3024435A1 (fr) | 2016-02-05 |
FR3024435B1 true FR3024435B1 (fr) | 2016-08-26 |
Family
ID=51862437
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1457436A Active FR3024435B1 (fr) | 2014-07-31 | 2014-07-31 | Capot de soufflante pliable guide, pour ensemble moteur d'aeronef |
Country Status (3)
Country | Link |
---|---|
US (1) | US9783314B2 (fr) |
CN (1) | CN105314119B (fr) |
FR (1) | FR3024435B1 (fr) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3036382B1 (fr) * | 2015-05-21 | 2017-06-16 | Airbus Operations Sas | Nacelle d'aeronef comportant au moins un capot monte rotatif autour de l'axe longitudinal de la nacelle |
US10875656B2 (en) | 2017-09-15 | 2020-12-29 | Bell Helicopter Textron Inc. | Bi-folding engine cowl having a plurality of open positions to provide access |
US10875657B2 (en) | 2017-09-15 | 2020-12-29 | Bell Helicopter Textron Inc. | Hold open j-track locking mechanism for cowling |
FR3072908B1 (fr) * | 2017-10-26 | 2021-02-26 | Safran Nacelles | Ensemble propulsif pour aeronef |
FR3075886B1 (fr) | 2017-12-22 | 2019-12-27 | Safran Nacelles | Nacelle de turboreacteur comportant des ouvertures de capots avant d'acces a des points de fixation de la nacelle |
FR3079500A1 (fr) * | 2018-03-29 | 2019-10-04 | Airbus Operations | Nacelle d'aeronef a capot de soufflante rotatif integrant une trappe d'acces |
FR3081837B1 (fr) | 2018-06-05 | 2020-11-27 | Airbus Operations Sas | Ensemble turbomachine d'aeronef comportant un capot articule |
GB201909171D0 (en) * | 2019-06-26 | 2019-08-07 | Rolls Royce Plc | Gas turbine engine cowl doors |
US11718409B2 (en) * | 2020-04-07 | 2023-08-08 | Rohr, Inc. | Nacelle with independent opening thrust reverser section |
FR3113485B1 (fr) | 2020-08-21 | 2022-10-28 | Safran Nacelles | Nacelle pour moteur d’aéronef comportant des capots de soufflante asymétriques |
FR3114849A1 (fr) | 2020-10-02 | 2022-04-08 | Airbus Operations | Turboreacteur double flux d’un aeronef comportant un capot articule en rotation et un systeme de deploiement dudit capot |
EP4001120B1 (fr) * | 2020-11-24 | 2024-03-20 | Airbus Operations (S.A.S.) | Assemblage pour un aéronef comportant un mât et une nacelle comportant une casquette équipée de systèmes de mise en tension et de systèmes de centrage |
CN115218729B (zh) * | 2022-07-06 | 2023-06-09 | 蓝箭航天空间科技股份有限公司 | 一种用于运载火箭整流罩的通风口盖 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2560854B1 (fr) * | 1984-03-07 | 1986-09-12 | Snecma | Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur |
US5213286A (en) * | 1990-10-10 | 1993-05-25 | General Electric Company | Door for aircraft nacelle |
FR2673972B1 (fr) * | 1991-03-12 | 1993-07-23 | Aerospatiale | Porte d'acces, notamment pour nacelle de reacteur d'avion, munie d'un panneau articule a pivotement synchronise. |
US5350136A (en) * | 1993-05-14 | 1994-09-27 | United Technologies Corporation | Nacelle arrangement |
FR2832752B1 (fr) * | 2001-11-27 | 2004-08-06 | Airbus France | Dispositif indicateur de defaut de fermeture d'au moins un mecanisme de verrouillage interpose entre deux elements |
FR2862045B1 (fr) | 2003-11-12 | 2006-05-05 | Snecma Moteurs | Turboreacteur destine a etre fixe sur le fuselage d'un avion et en particulier sur sa partie arriere |
FR2890378B1 (fr) | 2005-09-08 | 2009-01-16 | Airbus France Sas | Capot de nacelle pour turboreacteur et nacelle comportant au moins un tel capot. |
FR2907759B1 (fr) * | 2006-10-31 | 2008-12-12 | Aircelle Sa | Nacelle pour turboreacteur a ouverture laterale |
FR2911372B1 (fr) * | 2007-01-15 | 2009-02-27 | Aircelle Sa | Inverseur de poussee translatable pour moteur a reaction |
FR2933071B1 (fr) * | 2008-06-25 | 2010-06-11 | Snecma | Dispositif de capotage de nacelle d'unite de puissance propulsive d'aeronef |
FR3005453B1 (fr) * | 2013-05-13 | 2016-10-07 | Airbus Operations Sas | Nacelle de turboreacteur d'aeronef |
DE102015206093A1 (de) * | 2015-04-02 | 2016-10-06 | Rolls-Royce Deutschland Ltd & Co Kg | Triebwerksverkleidung einer Fluggasturbine |
-
2014
- 2014-07-31 FR FR1457436A patent/FR3024435B1/fr active Active
-
2015
- 2015-07-28 US US14/811,152 patent/US9783314B2/en active Active
- 2015-07-29 CN CN201510456819.3A patent/CN105314119B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
FR3024435A1 (fr) | 2016-02-05 |
CN105314119A (zh) | 2016-02-10 |
US20160031563A1 (en) | 2016-02-04 |
US9783314B2 (en) | 2017-10-10 |
CN105314119B (zh) | 2020-05-19 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20160205 |
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PLFP | Fee payment |
Year of fee payment: 3 |
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Year of fee payment: 4 |
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Year of fee payment: 5 |
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Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |