BRPI0814497A2 - "nacela de motor a jato, montagem de propulsão e aeronave" - Google Patents

"nacela de motor a jato, montagem de propulsão e aeronave"

Info

Publication number
BRPI0814497A2
BRPI0814497A2 BRPI0814497-4A2A BRPI0814497A BRPI0814497A2 BR PI0814497 A2 BRPI0814497 A2 BR PI0814497A2 BR PI0814497 A BRPI0814497 A BR PI0814497A BR PI0814497 A2 BRPI0814497 A2 BR PI0814497A2
Authority
BR
Brazil
Prior art keywords
jet engine
shell
nacela
aircraft
section
Prior art date
Application number
BRPI0814497-4A2A
Other languages
English (en)
Inventor
Fabrice Provost
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 BRPI0814497A2 publication Critical patent/BRPI0814497A2/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings or cowlings
    • B64D29/06Attaching of nacelles, fairings or cowlings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings or cowlings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Vibration Prevention Devices (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Disintegrating Or Milling (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Vibration Dampers (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)
  • Wind Motors (AREA)
BRPI0814497-4A2A 2007-08-20 2008-07-25 "nacela de motor a jato, montagem de propulsão e aeronave" BRPI0814497A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0705939A FR2920145B1 (fr) 2007-08-20 2007-08-20 Nacelle de turboreacteur a amortisseurs pour demi-coquilles
PCT/EP2008/059760 WO2009024428A1 (fr) 2007-08-20 2008-07-25 Nacelle de turboréacteur à amortisseurs pour demi-coquilles

Publications (1)

Publication Number Publication Date
BRPI0814497A2 true BRPI0814497A2 (pt) 2015-02-03

Family

ID=39271095

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0814497-4A2A BRPI0814497A2 (pt) 2007-08-20 2008-07-25 "nacela de motor a jato, montagem de propulsão e aeronave"

Country Status (11)

Country Link
US (1) US8800299B2 (pt)
EP (1) EP2178757B1 (pt)
CN (1) CN101778763B (pt)
AT (1) ATE502850T1 (pt)
BR (1) BRPI0814497A2 (pt)
CA (1) CA2696709C (pt)
DE (1) DE602008005751D1 (pt)
ES (1) ES2362388T3 (pt)
FR (1) FR2920145B1 (pt)
RU (1) RU2469922C2 (pt)
WO (1) WO2009024428A1 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9221545B2 (en) * 2013-04-03 2015-12-29 The Boeing Company Aircraft nacelle assemblies
FR3007739B1 (fr) * 2013-07-01 2016-02-05 Aircelle Sa Dispositif d’assistance pour la manœuvre d’un capot et nacelle de turboreacteur ainsi equipee
FR3025556B1 (fr) 2014-09-08 2016-09-09 Aircelle Sa Ensemble propulsif pour aeronef et procede d’ouverture d’un capot mobile dudit ensemble propulsif
US10081434B2 (en) * 2015-03-12 2018-09-25 Rohr, Inc. Track mounted hold open rod
CN105508053A (zh) * 2015-12-29 2016-04-20 中国航空工业集团公司沈阳发动机设计研究所 一种内安装边结构的燃汽轮机进气内流道结构
FR3048957B1 (fr) * 2016-03-15 2018-03-09 Airbus Operations Ensemble moteur pour aeronef, comprenant des dispositifs souples de transmission d'efforts agences entre les capots d'inversion de poussee et le moteur
GB201909171D0 (en) * 2019-06-26 2019-08-07 Rolls Royce Plc Gas turbine engine cowl doors
CN110439707B (zh) * 2019-07-26 2021-10-01 中国航发沈阳发动机研究所 一种飞机尾部弹性片组件
CN115248123B (zh) * 2021-04-28 2025-07-25 中国航发商用航空发动机有限责任公司 操作短舱的装置和降低短舱闭合位置剪切力的方法
FR3163350A1 (fr) * 2024-06-13 2025-12-19 Safran Nacelles Ensemble de capots multifonctions et procede d’ouverture de l’ensemble

Family Cites Families (9)

* 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
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
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
DE10163623A1 (de) * 2001-12-21 2003-07-10 Voith Paper Patent Gmbh Vorrichtung zum Aufwickeln einer Materialbahn
US6622963B1 (en) * 2002-04-16 2003-09-23 Honeywell International Inc. System and method for controlling the movement of an aircraft engine cowl door
US7090165B2 (en) * 2003-06-02 2006-08-15 Rolls-Royce Plc Aeroengine nacelle
FR2890378B1 (fr) * 2005-09-08 2009-01-16 Airbus France Sas Capot de nacelle pour turboreacteur et nacelle comportant au moins un tel capot.
FR2897339B1 (fr) * 2006-02-16 2008-04-11 Aircelle Sa Nacelle de turboreacteur a ouverture laterale des capots

Also Published As

Publication number Publication date
US8800299B2 (en) 2014-08-12
ES2362388T3 (es) 2011-07-04
CN101778763A (zh) 2010-07-14
EP2178757B1 (fr) 2011-03-23
CA2696709A1 (fr) 2009-02-26
RU2469922C2 (ru) 2012-12-20
FR2920145A1 (fr) 2009-02-27
CN101778763B (zh) 2014-04-02
US20110173949A1 (en) 2011-07-21
DE602008005751D1 (de) 2011-05-05
EP2178757A1 (fr) 2010-04-28
ATE502850T1 (de) 2011-04-15
WO2009024428A1 (fr) 2009-02-26
CA2696709C (fr) 2015-04-21
FR2920145B1 (fr) 2009-09-18
RU2010109781A (ru) 2011-09-27

Similar Documents

Publication Publication Date Title
BRPI0814497A2 (pt) "nacela de motor a jato, montagem de propulsão e aeronave"
DE602007003981D1 (de) Strukturgondel
BRPI0813039A2 (pt) "nacela de motor de turbojato, conjunto de propulsão e avião"
FR2921976B1 (fr) Actionneur pour structure mobile de nacelle d'aeronef, et nacelle comprenant au moins un tel actionneur
EP1847457A3 (en) Aeroengine mounting
FR2883256B1 (fr) Attache moteur d'un systeme de montage interpose entre un mat d'accrochage et un moteur d'aeronef
FR2903382B1 (fr) Dispositif d'accrochage d'un moteur d'aeronef comportant deux bielles de reprise de poussee a emboitement transversal
EP2080700A3 (en) Pylon and engine mount configuration
BR112012024647A2 (pt) disposição de haste de ligação de flap de reversor de empuxo sobre a estrutura fixa interna de uma nacela de motor turbojato e nacela de motor turbojato de avião
WO2008093003A8 (fr) Nacelle pour turboréacteur double flux
WO2009112777A3 (fr) Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante
EP2065585A3 (en) Gas turbine engine with pylon mounted accessory drive
WO2008043903A3 (fr) Nacelle pour turboréacteur double flux
BR112012031008A2 (pt) pá em cascata automontada para um reversor de empuxo em cascata para uma nacela de motor turbojato de avião, cascata e montagem da mesma..
BRPI0811239A2 (pt) Conjunto motor para aeronave, e, aeronave
BRPI0813618A2 (pt) "nacela para um motor turbojato e aeronave"
FR2891242B1 (fr) Turboreacteur pour aeronef, aeronef muni d'un tel turboreacteur, et procede de montage d'un tel turboreacteur sur un aeronef
EP2330037A3 (en) Fan cowl support for a turbofan engine
BRPI0813609A2 (pt) "nacela de turbojato projetada para ser ajustada em uma aeronave e aeronave"
ATE423729T1 (de) Triebwerkanordnung für flugzeug
WO2009118470A8 (fr) Dispositif de support et de fixation d'un équipement sur un carter de nacelle ou de moteur d'avion
RU2010109783A (ru) Замок, содержащий телескопическую соединительную тягу, оснащенную возвратным средством
EP2133270A3 (en) Trust struts arrangement for an aircraft engine mount
CN210592395U (zh) 一种用于飞艇推进装置的减振结构
WO2009024661A3 (fr) Dispositif de liaison entre les deux demi-coquilles d'une nacelle de moteur d'aeronef, et nacelle equipee d'un tel dispositif

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]