BRPI0814498A2 - "dispositivo de acoplamento, nacele de motor turbojato e aeronave" - Google Patents

"dispositivo de acoplamento, nacele de motor turbojato e aeronave"

Info

Publication number
BRPI0814498A2
BRPI0814498A2 BRPI0814498-2A2A BRPI0814498A BRPI0814498A2 BR PI0814498 A2 BRPI0814498 A2 BR PI0814498A2 BR PI0814498 A BRPI0814498 A BR PI0814498A BR PI0814498 A2 BRPI0814498 A2 BR PI0814498A2
Authority
BR
Brazil
Prior art keywords
nace
aircraft
coupling device
turbojet engine
turbojet
Prior art date
Application number
BRPI0814498-2A2A
Other languages
English (en)
Inventor
Pascal-Marie Paul Marcel Soulier
Aurelie De Sorbay
Original Assignee
Aircelle Sa
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 Aircelle Sa filed Critical Aircelle Sa
Publication of BRPI0814498A2 publication Critical patent/BRPI0814498A2/pt

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
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
    • E05C19/00—Other devices specially designed for securing wings, e.g. with suction cups
    • E05C19/08—Hasps; Hasp fastenings; Spring catches therefor
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
    • E05C7/00—Fastening devices specially adapted for two wings
    • E05C7/04—Fastening devices specially adapted for two wings for wings which abut when closed
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/32—Articulated members
    • Y10T403/32254—Lockable at fixed position
    • Y10T403/32467—Telescoping members

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Wind Motors (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BRPI0814498-2A2A 2007-08-20 2008-07-28 "dispositivo de acoplamento, nacele de motor turbojato e aeronave" BRPI0814498A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0705930A FR2920177B1 (fr) 2007-08-20 2007-08-20 Dispositif de liaison, destine a relier un premier et second elements mobiles l'un par rapport a l'autre
PCT/EP2008/059849 WO2009024431A1 (fr) 2007-08-20 2008-07-28 Dispositif de liaison, destiné à relier un premier et un second éléments mobiles l'un par rapport à l'autre

Publications (1)

Publication Number Publication Date
BRPI0814498A2 true BRPI0814498A2 (pt) 2015-02-03

Family

ID=39247568

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0814498-2A2A BRPI0814498A2 (pt) 2007-08-20 2008-07-28 "dispositivo de acoplamento, nacele de motor turbojato e aeronave"

Country Status (9)

Country Link
US (1) US8573928B2 (pt)
EP (2) EP2178758B1 (pt)
CN (1) CN101784445B (pt)
BR (1) BRPI0814498A2 (pt)
CA (1) CA2696710C (pt)
ES (2) ES2402678T3 (pt)
FR (1) FR2920177B1 (pt)
RU (1) RU2471678C2 (pt)
WO (1) WO2009024431A1 (pt)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2920174A1 (fr) * 2007-08-20 2009-02-27 Aircelle Sa Dispositif de liaison entre les deux demi-coquilles d'une nacelle de moteur d'aeronef, et nacelle equipee d'un tel dispositif
FR2960855A1 (fr) * 2010-06-03 2011-12-09 Aircelle Sa Nacelle pour turboreacteur avec dispositif de reprise d'efforts circonferentiels
CA2812580C (en) 2010-09-24 2018-10-23 Short Brothers Plc Nacelle with hinged cowl doors enabling access to the engine
EP2951090B1 (en) * 2013-01-29 2019-01-16 United Technologies Corporation Cowl with pressure driven latch
US9221545B2 (en) * 2013-04-03 2015-12-29 The Boeing Company Aircraft nacelle assemblies
FR3007805B1 (fr) * 2013-06-28 2019-04-19 Safran Nacelles Procede de controle d’un verin de levage pour nacelle de moteur d’aeronef, systeme de levage a verin mettant en œuvre le procede et nacelle ainsi equipee
US9470107B2 (en) 2014-07-11 2016-10-18 Rohr, Inc. Nacelle compression rods
US10081434B2 (en) * 2015-03-12 2018-09-25 Rohr, Inc. Track mounted hold open rod
FR3037039B1 (fr) * 2015-06-03 2017-06-02 Aircelle Sa Dispositif de verrouillage de capots pivotants d’un inverseur de poussee
FR3075176B1 (fr) * 2017-12-18 2020-11-06 Safran Aircraft Engines Ensemble de capot ouvrant et mecanisme de deploiement
US11453507B2 (en) 2018-10-03 2022-09-27 Rohr, Inc. Thrust reverser compression rod engagement apparatus
US11149564B2 (en) * 2019-06-24 2021-10-19 Rohr, Inc. Nacelle thrust reverser compression rod supporting system
FR3115766B1 (fr) 2020-11-02 2023-03-31 Safran Nacelles Nacelle pour ensemble propulsif d’aéronef, comprenant une bielle de sécurité formant renfort structural
EP4446230A1 (fr) 2023-04-14 2024-10-16 Airbus Operations (S.A.S.) Ensemble propulsif a capot moteur ameliore, et aeronef comprenant un tel ensemble
FR3170434A1 (fr) * 2024-12-20 2026-06-26 Airbus Operations (S.A.S.) Système de motorisation d’aéronef

Family Cites Families (14)

* 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
US4585189A (en) * 1984-10-22 1986-04-29 Lockheed Corporation Counterbalanced cowling assembly for a pylon-mounted engine and nacelle therefor
US4629146A (en) * 1985-01-30 1986-12-16 Rohr Industries, Inc. Hold open rod for hinged section of nacelle system
US4825648A (en) * 1987-03-02 1989-05-02 General Electric Company Turbofan engine having a split cowl
FR2622930B1 (fr) * 1987-11-06 1990-03-23 Aerospatiale Capotage pour turboreacteur a double flux
SU1637169A1 (ru) * 1989-12-05 1994-12-15 А.Л. Доброскоков Створка капота летательного аппарата
FR2771710B1 (fr) * 1997-12-03 2000-02-11 Aerospatiale Dispositif d'ouverture commun a deux capots adjacents de nacelle de moteur d'avion
GB0016135D0 (en) * 2000-06-30 2000-08-23 Aerospace Design Facilities Li Safety enhancement method & apparatus
US6629712B2 (en) * 2001-03-30 2003-10-07 Hartwell Corporation Extendable latch
US6495749B2 (en) * 2001-03-30 2002-12-17 Siemens Westinghouse Power Corporation Hybrid combustion power system
GB0124446D0 (en) * 2001-10-11 2001-12-05 Short Brothers Ltd Aircraft propulsive power unit
FR2835870B1 (fr) * 2002-02-14 2005-03-11 Airbus France Systeme de fermeture interpose entre deux elements
US8925979B2 (en) 2006-11-30 2015-01-06 Hartwell Corporation Command latch and pin latch system
FR2920133B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Nacelle de turboreacteur, destinee a equiper un aeronef

Also Published As

Publication number Publication date
FR2920177A1 (fr) 2009-02-27
EP2319762A3 (fr) 2014-05-14
CA2696710A1 (fr) 2009-02-26
WO2009024431A1 (fr) 2009-02-26
ES2402678T3 (es) 2013-05-07
FR2920177B1 (fr) 2009-09-18
CA2696710C (fr) 2014-11-18
CN101784445B (zh) 2013-08-14
US8573928B2 (en) 2013-11-05
EP2319762A2 (fr) 2011-05-11
ES2564012T3 (es) 2016-03-17
EP2178758A1 (fr) 2010-04-28
RU2471678C2 (ru) 2013-01-10
RU2010109805A (ru) 2011-09-27
CN101784445A (zh) 2010-07-21
EP2319762B1 (fr) 2015-12-16
US20110038725A1 (en) 2011-02-17
EP2178758B1 (fr) 2013-01-09

Similar Documents

Publication Publication Date Title
DE502007001624D1 (de) Integriertes Motorkühlsystem
BRPI0720329A2 (pt) " nacela de motor a jato de aeronave "
BRPI0717730A2 (pt) Nacela para motor turbojato de contorno, conjunto de propulsão e avião
TWI346443B (en) Dual-structured aircraft engine starter/generator
DE602007001471D1 (de) Motorsystem
FR2906568B1 (fr) Structure d'entree d'air deposable pour nacelle de turboreacteur.
IL181280A0 (en) Integrated airbreathing and non-airbreathing engine system
EP2061951A4 (en) AIRCRAFT ENGINE WITH PARTICULAR CYCLE
FR2950322B1 (fr) Element d'accrochage d'un moteur d'aeronef, ensemble d'aeronef comprenant cet element et aeronef associe
GB2442337B (en) Turbofan jet engine
FR2920476B1 (fr) Dispositif d'actionnement, systeme de decharge en etant equipe et turboreacteur les comportant
BRPI0821504A2 (pt) nacela para motor de avião
EP1871216A4 (en) THERMAL CAPSULOTOMY TOOL AND SYSTEM
BRPI0813602A2 (pt) "dispositivo de travamento, nacela de turbojato e aeronave"
EP2185804A4 (en) PREMIUM COMBUSTION PROCESSES, DEVICES AND THESE USE MOTORS
FR2917455B1 (fr) Carter d'echappement de turbomachine.
BRPI0813616A2 (pt) "dispositivo de trava, nacela do motor turbojato e aeronave"
BRPI0813043A2 (pt) "nacela de motor a jato de turboventoinha"
DE602006021127D1 (de) Turbinentriebwerk mit verbesserter Kühlung
BRPI0814908A2 (pt) "nacela para motor turbojato e aeronave"
AU315983S (en) Engine shroud
DE602007001094D1 (de) Motoranlassersystem
BRPI0814916A2 (pt) "dispositivo de acoplamento e nacela de aeronave"
ITTO20060865A1 (it) Dispositivo d'avviamento per motori termici e relativo procedimento.
FR2905191B1 (fr) Dispositif de dialogue d'aeronef.

Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]