BRPI0914324A2 - dispositivo de carenagem de nacela para de uma unidade de potência propulsora, e, unidade de potência propulsora - Google Patents

dispositivo de carenagem de nacela para de uma unidade de potência propulsora, e, unidade de potência propulsora

Info

Publication number
BRPI0914324A2
BRPI0914324A2 BRPI0914324A BRPI0914324A BRPI0914324A2 BR PI0914324 A2 BRPI0914324 A2 BR PI0914324A2 BR PI0914324 A BRPI0914324 A BR PI0914324A BR PI0914324 A BRPI0914324 A BR PI0914324A BR PI0914324 A2 BRPI0914324 A2 BR PI0914324A2
Authority
BR
Brazil
Prior art keywords
thrust unit
fairing device
nacelle fairing
nacelle
thrust
Prior art date
Application number
BRPI0914324A
Other languages
English (en)
Inventor
Sébastien Regard
Original Assignee
Snecma
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 Snecma filed Critical Snecma
Publication of BRPI0914324A2 publication Critical patent/BRPI0914324A2/pt
Publication of BRPI0914324B1 publication Critical patent/BRPI0914324B1/pt

Links

Classifications

    • 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
    • B64D29/08—Inspection panels for power plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wind Motors (AREA)
  • Superstructure Of Vehicle (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BRPI0914324 2008-06-25 2009-04-10 dispositivo de carenagem de unidade de potência propulsora, e, unidade de potência propulsora BRPI0914324B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0803554A FR2933071B1 (fr) 2008-06-25 2008-06-25 Dispositif de capotage de nacelle d'unite de puissance propulsive d'aeronef
PCT/FR2009/000423 WO2010007218A1 (fr) 2008-06-25 2009-04-10 Dispositif de capotage de nacelle d'unite de puissance propulsive d'aeronef

Publications (2)

Publication Number Publication Date
BRPI0914324A2 true BRPI0914324A2 (pt) 2015-10-13
BRPI0914324B1 BRPI0914324B1 (pt) 2019-12-03

Family

ID=40228201

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0914324 BRPI0914324B1 (pt) 2008-06-25 2009-04-10 dispositivo de carenagem de unidade de potência propulsora, e, unidade de potência propulsora

Country Status (10)

Country Link
US (1) US8956109B2 (pt)
EP (1) EP2303693B1 (pt)
JP (1) JP2011525874A (pt)
CN (1) CN102076564A (pt)
BR (1) BRPI0914324B1 (pt)
CA (1) CA2728700C (pt)
ES (1) ES2395863T3 (pt)
FR (1) FR2933071B1 (pt)
RU (1) RU2494926C2 (pt)
WO (1) WO2010007218A1 (pt)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2939100B1 (fr) * 2008-12-01 2010-12-31 Airbus France Ensemble moteur pour aeronef comprenant une structure rigide modulaire de mat d'accrochage
EP2971655B1 (en) * 2013-03-14 2017-06-21 United Technologies Corporation Latching actuation mechanism for nacelle mounted latching system
FR3005453B1 (fr) * 2013-05-13 2016-10-07 Airbus Operations Sas Nacelle de turboreacteur d'aeronef
FR3009543B1 (fr) * 2013-08-07 2015-08-07 Airbus Operations Sas Assemblage pour aeronef comprenant un panneau d'acces aux articulations d'un capot de nacelle deplacable par cooperation entre une rampe et un organe d'appui
FR3009542B1 (fr) * 2013-08-07 2015-08-07 Airbus Operations Sas Assemblage pour aeronef comprenant un panneau d'acces aux articulations d'un capot de nacelle monte pivotant sur un dispositif d'accrochage de moteur d'aeronef
FR3024435B1 (fr) * 2014-07-31 2016-08-26 Airbus Operations Sas Capot de soufflante pliable guide, pour ensemble moteur d'aeronef
US10081434B2 (en) * 2015-03-12 2018-09-25 Rohr, Inc. Track mounted hold open rod
DE102015206093A1 (de) * 2015-04-02 2016-10-06 Rolls-Royce Deutschland Ltd & Co Kg Triebwerksverkleidung einer Fluggasturbine
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
US10093429B2 (en) * 2015-07-07 2018-10-09 Rohr, Inc Latch beam deflection support
FR3040044B1 (fr) * 2015-08-12 2019-05-31 Safran Aircraft Engines Capot de nacelle comportant un element de maintien en position solidarise a la paroi interne du capot
CN106741974A (zh) * 2016-12-12 2017-05-31 惠阳航空螺旋桨有限责任公司 一种螺旋桨用复合材料整流罩
US10875657B2 (en) 2017-09-15 2020-12-29 Bell Helicopter Textron Inc. Hold open j-track locking mechanism for cowling
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
FR3075176B1 (fr) * 2017-12-18 2020-11-06 Safran Aircraft Engines Ensemble de capot ouvrant et mecanisme de deploiement
FR3079216A1 (fr) * 2018-03-22 2019-09-27 Airbus Operations Carenage avant d'un mat d'aeronef comprenant au moins un panneau articule et aeronef equipe dudit carenage avant
FR3079500A1 (fr) * 2018-03-29 2019-10-04 Airbus Operations Nacelle d'aeronef a capot de soufflante rotatif integrant une trappe d'acces
FR3085351B1 (fr) * 2018-09-04 2021-12-31 Airbus Operations Sas Carenage central d'un mat d'aeronef comprenant au moins un panneau articule et aeronef equipe dudit carenage central
CN110065639A (zh) * 2019-05-09 2019-07-30 西北工业大学 一种用于无人机快卸对开式动力舱罩
FR3113485B1 (fr) 2020-08-21 2022-10-28 Safran Nacelles Nacelle pour moteur d’aéronef comportant des capots de soufflante asymétriques
US20220136440A1 (en) 2020-10-30 2022-05-05 Raytheon Technologies Corporation Gas turbine engine mounted above wing and with camber

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3347578A (en) * 1964-11-18 1967-10-17 Boeing Co Flush-type safety latch
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
US4428609A (en) * 1980-09-15 1984-01-31 The Boeing Company Latch for flexibly joining trailing edge access doors on an aircraft engine support pylon
US4585189A (en) * 1984-10-22 1986-04-29 Lockheed Corporation Counterbalanced cowling assembly for a pylon-mounted engine and nacelle therefor
US4825648A (en) * 1987-03-02 1989-05-02 General Electric Company Turbofan engine having a split cowl
RU1766020C (ru) * 1989-12-20 1994-08-15 Авиационный комплекс им.С.В.Ильюшина Створка гондолы двигателя летательного аппарата
FR2661213B1 (fr) * 1990-04-19 1992-07-03 Snecma Moteur d'aviation a tres grand taux de dilution et du type dit contrafan avant.
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
US5467941A (en) * 1993-12-30 1995-11-21 The Boeing Company Pylon and engine installation for ultra-high by-pass turbo-fan engines
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
FR2771710B1 (fr) * 1997-12-03 2000-02-11 Aerospatiale Dispositif d'ouverture commun a deux capots adjacents de nacelle de moteur d'avion
US6220546B1 (en) * 1999-12-29 2001-04-24 The Boeing Company Aircraft engine and associated aircraft engine cowl
GB0124446D0 (en) * 2001-10-11 2001-12-05 Short Brothers Ltd Aircraft propulsive power unit
US7090165B2 (en) * 2003-06-02 2006-08-15 Rolls-Royce Plc Aeroengine nacelle
GB0315894D0 (en) * 2003-07-08 2003-08-13 Rolls Royce Plc Aircraft engine arrangement
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
US20080258016A1 (en) * 2007-04-23 2008-10-23 Gukeisen Robert L Nacelle assembly without lower bi-fi splitter

Also Published As

Publication number Publication date
US8956109B2 (en) 2015-02-17
JP2011525874A (ja) 2011-09-29
FR2933071B1 (fr) 2010-06-11
FR2933071A1 (fr) 2010-01-01
US20110091317A1 (en) 2011-04-21
CN102076564A (zh) 2011-05-25
WO2010007218A1 (fr) 2010-01-21
RU2011102573A (ru) 2012-07-27
EP2303693A1 (fr) 2011-04-06
CA2728700C (fr) 2015-10-27
RU2494926C2 (ru) 2013-10-10
BRPI0914324B1 (pt) 2019-12-03
CA2728700A1 (fr) 2010-01-21
EP2303693B1 (fr) 2012-10-31
ES2395863T3 (es) 2013-02-15

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06T Formal requirements before examination [chapter 6.20 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 03/12/2019, OBSERVADAS AS CONDICOES LEGAIS. (CO) 10 (DEZ) ANOS CONTADOS A PARTIR DE 03/12/2019, OBSERVADAS AS CONDICOES LEGAIS