FR3024435B1 - Capot de soufflante pliable guide, pour ensemble moteur d'aeronef - Google Patents

Capot de soufflante pliable guide, pour ensemble moteur d'aeronef

Info

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
Application number
FR1457436A
Other languages
English (en)
Other versions
FR3024435A1 (fr
Inventor
Olivier Pautis
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1457436A priority Critical patent/FR3024435B1/fr
Priority to US14/811,152 priority patent/US9783314B2/en
Priority to CN201510456819.3A priority patent/CN105314119B/zh
Publication of FR3024435A1 publication Critical patent/FR3024435A1/fr
Application granted granted Critical
Publication of FR3024435B1 publication Critical patent/FR3024435B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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)
FR1457436A 2014-07-31 2014-07-31 Capot de soufflante pliable guide, pour ensemble moteur d'aeronef Active FR3024435B1 (fr)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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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