[go: up one dir, main page]

BRPI0813610A2 - "nacela para um motor turbojato" - Google Patents

"nacela para um motor turbojato"

Info

Publication number
BRPI0813610A2
BRPI0813610A2 BRPI0813610-6A2A BRPI0813610A BRPI0813610A2 BR PI0813610 A2 BRPI0813610 A2 BR PI0813610A2 BR PI0813610 A BRPI0813610 A BR PI0813610A BR PI0813610 A2 BRPI0813610 A2 BR PI0813610A2
Authority
BR
Brazil
Prior art keywords
nacela
turbojet engine
turbojet
engine
Prior art date
Application number
BRPI0813610-6A2A
Other languages
English (en)
Inventor
Gilles Bourdon
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 BRPI0813610A2 publication Critical patent/BRPI0813610A2/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
BRPI0813610-6A2A 2007-08-20 2008-06-12 "nacela para um motor turbojato" BRPI0813610A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0705921A FR2920140B1 (fr) 2007-08-20 2007-08-20 Nacelle de turboreacteur, destinee a equiper un aeronef
PCT/FR2008/000809 WO2009027587A1 (fr) 2007-08-20 2008-06-12 Nacelle de turboréacteur, destinée à équiper un aéronef

Publications (1)

Publication Number Publication Date
BRPI0813610A2 true BRPI0813610A2 (pt) 2014-12-30

Family

ID=39163279

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0813610-6A2A BRPI0813610A2 (pt) 2007-08-20 2008-06-12 "nacela para um motor turbojato"

Country Status (9)

Country Link
US (1) US8783614B2 (pt)
EP (1) EP2188178B1 (pt)
CN (1) CN101778767A (pt)
BR (1) BRPI0813610A2 (pt)
CA (1) CA2696722C (pt)
ES (1) ES2448583T3 (pt)
FR (1) FR2920140B1 (pt)
RU (1) RU2466066C2 (pt)
WO (1) WO2009027587A1 (pt)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2959486B1 (fr) 2010-04-29 2012-04-13 Aircelle Sa Nacelle pour moteur d'aeronef
FR2959487B1 (fr) * 2010-04-29 2012-04-13 Aircelle Sa Nacelle pour moteur d'aeronef
FR3011584B1 (fr) * 2013-10-04 2018-02-23 Safran Aircraft Engines Extension de carter intermediaire
US10309341B2 (en) * 2016-01-15 2019-06-04 The Boeing Company Thrust reverser cascade systems and methods

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU1766020C (ru) * 1989-12-20 1994-08-15 Авиационный комплекс им.С.В.Ильюшина Створка гондолы двигателя летательного аппарата
GB2266080A (en) * 1992-04-16 1993-10-20 Rolls Royce Plc Mounting arrangement for a gas turbine engine.
FR2711733B1 (fr) * 1993-10-22 1996-01-26 Hurel Dubois Avions Inverseur de poussée à portes pour moteur d'avion à réaction équipées d'un volet auxiliaire.
FR2772342B1 (fr) * 1997-12-16 2000-02-18 Aerospatiale Ensemble propulseur a capots de soufflante munis de securites de maintien et de positionnement, pour aeronef
US6260801B1 (en) * 1999-09-17 2001-07-17 The Nordam Group, Inc. Swing pivot thrust reverser
GB2384827A (en) * 2002-01-30 2003-08-06 Rolls Royce Plc A Fastening Between The C-Duct and Core of a Ducted Fan Gas Turbine Engine.
US6688099B2 (en) * 2002-05-21 2004-02-10 The Nordam Group, Inc. Variable area thrust reverser nozzle
US7146796B2 (en) * 2003-09-05 2006-12-12 The Nordam Group, Inc. Nested latch thrust reverser
FR2901245B1 (fr) * 2006-05-22 2008-12-26 Airbus France Sas Dispositif d'articulation d'une porte d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation

Also Published As

Publication number Publication date
RU2010109800A (ru) 2011-09-27
US8783614B2 (en) 2014-07-22
US20110020119A1 (en) 2011-01-27
CA2696722A1 (fr) 2009-03-05
EP2188178B1 (fr) 2013-12-25
FR2920140B1 (fr) 2009-10-30
RU2466066C2 (ru) 2012-11-10
WO2009027587A1 (fr) 2009-03-05
CA2696722C (fr) 2015-03-31
EP2188178A1 (fr) 2010-05-26
ES2448583T3 (es) 2014-03-14
CN101778767A (zh) 2010-07-14
FR2920140A1 (fr) 2009-02-27

Similar Documents

Publication Publication Date Title
BRPI0813042A2 (pt) "nacela para um motor a jato"
BRPI0817204A2 (pt) Fechadura para veículo a motor
BRPI0817123A2 (pt) Motor a diesel
BRPI0821929A2 (pt) Nacela para motor turbojato
BRPI0909595A2 (pt) "arranjo para um motor de combustão sobrecarregado"
EP1879283A4 (en) ENGINE
EP2175116A4 (en) INTERNAL COMBUSTION ENGINE
BRPI0821504A2 (pt) nacela para motor de avião
BRPI0912359A2 (pt) disposição para um motor de combustão supercarregado
EP2061951A4 (en) AIRCRAFT ENGINE WITH PARTICULAR CYCLE
DE602007012259D1 (de) Verbrennungsmotor
EP2341226A4 (en) MOTOR GENERATOR
EP2220352A4 (en) ARRANGEMENT OF A CHARGED INTERNAL COMBUSTION ENGINE
PL2032826T3 (pl) Silnik spalinowy
FR2898641B1 (fr) Habillage de carter dans un turboreacteur
GB0502324D0 (en) A multi-shaft arrangement for a turbine engine
DE602008005797D1 (de) Motor
BRPI0816657A2 (pt) membro de cobertura para motores
DE602007003320D1 (de) Verbrennungsmotor
BRPI0821412A2 (pt) Configuração otimizada de motores para aeronave
BRPI0813049A2 (pt) "inversor de empuxo para nacela de motor a jato"
BRPI0814579A2 (pt) Método para operar um motor à diesel
BRPI0813603A2 (pt) "nacela para um turbojato e aeronave"
BRPI0821930A2 (pt) Conjunto de propulsão para motor turbojato
BRPI0813043A2 (pt) "nacela de motor a jato de turboventoinha"

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 9A ANUIDADE.

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