BRPI0906986A2 - Nacela para tubo jato de uma aeronave, turbo jato de duplo fluxo, mastro de suspensão e conjunto de propulsão para aeronave. - Google Patents

Nacela para tubo jato de uma aeronave, turbo jato de duplo fluxo, mastro de suspensão e conjunto de propulsão para aeronave.

Info

Publication number
BRPI0906986A2
BRPI0906986A2 BRPI0906986-0A BRPI0906986A BRPI0906986A2 BR PI0906986 A2 BRPI0906986 A2 BR PI0906986A2 BR PI0906986 A BRPI0906986 A BR PI0906986A BR PI0906986 A2 BRPI0906986 A2 BR PI0906986A2
Authority
BR
Brazil
Prior art keywords
aircraft
jet
nacelle
propulsion assembly
dual flow
Prior art date
Application number
BRPI0906986-0A
Other languages
English (en)
Inventor
Pierre Caruel
Jean-Philippe Joret
Peter Segat
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 BRPI0906986A2 publication Critical patent/BRPI0906986A2/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
    • B64D29/08—Inspection panels for power plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BRPI0906986-0A 2008-01-30 2009-01-21 Nacela para tubo jato de uma aeronave, turbo jato de duplo fluxo, mastro de suspensão e conjunto de propulsão para aeronave. BRPI0906986A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0800501A FR2926790B1 (fr) 2008-01-30 2008-01-30 Systeme de guidage pour la maintenance d'une nacelle d'aeronef
PCT/FR2009/000062 WO2009109713A2 (fr) 2008-01-30 2009-01-21 Système de guidage pour la maintenance d'une nacelle d'aéronef

Publications (1)

Publication Number Publication Date
BRPI0906986A2 true BRPI0906986A2 (pt) 2015-07-21

Family

ID=39739453

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0906986-0A BRPI0906986A2 (pt) 2008-01-30 2009-01-21 Nacela para tubo jato de uma aeronave, turbo jato de duplo fluxo, mastro de suspensão e conjunto de propulsão para aeronave.

Country Status (8)

Country Link
US (1) US8448896B2 (pt)
EP (1) EP2238032A2 (pt)
CN (1) CN101925516B (pt)
BR (1) BRPI0906986A2 (pt)
CA (1) CA2708288A1 (pt)
FR (1) FR2926790B1 (pt)
RU (1) RU2494927C2 (pt)
WO (1) WO2009109713A2 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9783315B2 (en) * 2012-02-24 2017-10-10 Rohr, Inc. Nacelle with longitudinal translating cowling and rotatable sleeves
US9217390B2 (en) * 2012-06-28 2015-12-22 United Technologies Corporation Thrust reverser maintenance actuation system
FR2999155B1 (fr) * 2012-12-12 2014-11-21 Aircelle Sa Ensemble propulsif pour aeronef
US10094286B2 (en) 2013-01-29 2018-10-09 United Technologies Corporation Gas turbine engine with lower bifurcation heat exchanger
US9404507B2 (en) * 2013-04-15 2016-08-02 Mra Systems, Inc. Inner cowl structure for aircraft turbine engine
US8979020B2 (en) * 2013-06-07 2015-03-17 Pratt & Whitney Canada Corp. Mounting system for mounting engine nacelle components and associated method
US9370827B2 (en) * 2013-08-28 2016-06-21 The Boeing Company System and method for forming perforations in a barrel section
US9797271B2 (en) 2014-04-25 2017-10-24 Rohr, Inc. Access panel(s) for an inner nacelle of a turbine engine
DE102015206093A1 (de) * 2015-04-02 2016-10-06 Rolls-Royce Deutschland Ltd & Co Kg Triebwerksverkleidung einer Fluggasturbine
FR3044719B1 (fr) 2015-12-08 2017-12-22 Snecma Ensemble de propulsion d'aeronef equipe de marches permettant a un operateur d'atteindre sa portion superieure
FR3075176B1 (fr) 2017-12-18 2020-11-06 Safran Aircraft Engines Ensemble de capot ouvrant et mecanisme de deploiement
FR3110547B1 (fr) * 2020-05-20 2022-04-22 Safran Nacelles Nacelle pour ensemble propulsif à très grand taux de dilution, comprenant une structure interne avant amovible et structurelle

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU290678A1 (ru) * 1969-08-19 1980-01-15 Предприятие Капот двигател летательного аппарата
FR2622930B1 (fr) * 1987-11-06 1990-03-23 Aerospatiale Capotage pour turboreacteur a double flux
CN1206670A (zh) * 1997-07-29 1999-02-03 王建成 多功能碟形飞行器
US6220546B1 (en) * 1999-12-29 2001-04-24 The Boeing Company Aircraft engine and associated aircraft engine cowl
FR2897339B1 (fr) * 2006-02-16 2008-04-11 Aircelle Sa Nacelle de turboreacteur a ouverture laterale des capots
FR2901244B1 (fr) * 2006-05-16 2009-01-09 Airbus France Sas Dispositif d'articulation de portes d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation
FR2916737B1 (fr) * 2007-06-01 2010-05-28 Airbus France Ensemble moteur pour aeronef a nacelle coulissante.

Also Published As

Publication number Publication date
WO2009109713A3 (fr) 2009-10-29
CN101925516A (zh) 2010-12-22
FR2926790B1 (fr) 2010-02-12
US20100327110A1 (en) 2010-12-30
US8448896B2 (en) 2013-05-28
CN101925516B (zh) 2015-10-21
WO2009109713A2 (fr) 2009-09-11
EP2238032A2 (fr) 2010-10-13
FR2926790A1 (fr) 2009-07-31
RU2010134982A (ru) 2012-03-10
CA2708288A1 (fr) 2009-09-11
RU2494927C2 (ru) 2013-10-10

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 8A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2394 DE 22-11-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.