BRPI0906953A2 - Entrada de ar para nacela de aeronave, conjunto compreendendo entrada de ar, conjunto de propulsão para aeronave - Google Patents

Entrada de ar para nacela de aeronave, conjunto compreendendo entrada de ar, conjunto de propulsão para aeronave

Info

Publication number: BRPI0906953A2
Authority: BR; Brazil
Prior art keywords: air intake; assembly; aircraft; nacelle; propulsion assembly
Prior art date: 2008-01-29

Application number

BRPI0906953-4A

Other languages

English (en)

Inventor

Guy Bernard Vauchel

Laurent Georges Valleroy

Stephane Beilliard

Fabien Bravin

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.)

2008-01-29

Filing date

2009-01-21

Publication date

2015-07-14

2009-01-21 Application filed by Aircelle Sa filed Critical Aircelle Sa

2015-07-14 Publication of BRPI0906953A2 publication Critical patent/BRPI0906953A2/pt

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
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
- 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
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0206—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
- 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
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0266—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
- B64D2033/0286—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Aviation & Aerospace Engineering (AREA)
Structures Of Non-Positive Displacement Pumps (AREA)

BRPI0906953-4A 2008-01-29 2009-01-21 Entrada de ar para nacela de aeronave, conjunto compreendendo entrada de ar, conjunto de propulsão para aeronave BRPI0906953A2 (pt)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
FR0800471A FR2926791B1 (fr)	2008-01-29	2008-01-29	Entree d'air pour nacelle d'aeronef, et ensemble propulsif comprenant une telle entree d'air
PCT/FR2009/000061 WO2009109712A1 (fr)	2008-01-29	2009-01-21	Entree d'air pour nacelle d'aeronef, et ensemble propulsif comprenant une telle entree d'air

Publications (1)

Publication Number	Publication Date
BRPI0906953A2 true BRPI0906953A2 (pt)	2015-07-14

Family

ID=39707981

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BRPI0906953-4A BRPI0906953A2 (pt)	2008-01-29	2009-01-21	Entrada de ar para nacela de aeronave, conjunto compreendendo entrada de ar, conjunto de propulsão para aeronave

Country Status (8)

Country	Link
US (1)	US8985506B2 (pt)
EP (1)	EP2238031A1 (pt)
CN (1)	CN101918276B (pt)
BR (1)	BRPI0906953A2 (pt)
CA (1)	CA2708106A1 (pt)
FR (1)	FR2926791B1 (pt)
RU (1)	RU2494015C2 (pt)
WO (1)	WO2009109712A1 (pt)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US7941993B2 (en) *	2003-10-14	2011-05-17	Rolls-Royce Plc	Engine cooling
FR2963469B1 (fr) *	2010-07-27	2012-07-27	Aircelle Sa	Panneau acoustique
GB201120996D0 (en) *	2011-12-07	2012-01-18	Airbus Operations Ltd	Apparatus for attachment of wing panels
FR2997725B1 (fr) *	2012-11-05	2018-03-02	Safran Aircraft Engines	Carter de turbomachine
FR2997726B1 (fr)	2012-11-05	2018-03-02	Safran Aircraft Engines	Carter de turbomachine
FR2998545B1 (fr) *	2012-11-23	2016-10-28	Airbus Operations Sas	Nacelle d'aeronef comprenant une liaison renforcee entre une entree d'air et une motorisation
FR2998547B1 (fr)	2012-11-23	2016-01-29	Airbus Operations Sas	Nacelle d'aeronef comprenant une liaison deformable entre une entree d'air et une motorisation
US10180082B2 (en)	2014-06-05	2019-01-15	Rolls-Royce Corporation	Fan case
US11325717B2 (en) *	2016-10-13	2022-05-10	Airbus Operations Sas	Aircraft nacelle including a link between a conduit of an air inlet and a conduit of an engine
FR3057545A1 (fr) *	2016-10-13	2018-04-20	Airbus Operations	Nacelle d'aeronef comprenant une liaison entre un conduit d'une entree d'air et un conduit d'une motorisation
GB201816990D0 (en) *	2018-10-18	2018-12-05	Rolls Royce Plc	Debris retention
GB201816989D0 (en) *	2018-10-18	2018-12-05	Rolls Royce Plc	Debris retention
FR3092611B1 (fr) *	2019-02-07	2021-02-26	Safran Aircraft Engines	Soufflante de turbomachine

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US4293053A (en) *	1979-12-18	1981-10-06	United Technologies Corporation	Sound absorbing structure
SU1793650A1 (ru) *	1991-01-28	1995-03-27	Машиностроительный завод им.П.О.Сухого	Входное устройство силовой установки самолета
US5336044A (en) *	1993-08-06	1994-08-09	General Electric Company	Blade containment system and method
FR2757823B1 (fr) *	1996-12-26	1999-03-12	Aerospatiale	Nacelle de turboreacteur a ecoulement laminaire
FR2767560B1 (fr) *	1997-08-19	1999-11-12	Aerospatiale	Ensemble reducteur de bruit pour turboreacteur d'aeronef
GB9820226D0 (en) *	1998-09-18	1998-11-11	Rolls Royce Plc	Gas turbine engine casing
US6382905B1 (en) *	2000-04-28	2002-05-07	General Electric Company	Fan casing liner support
FR2812911B1 (fr) *	2000-08-11	2002-09-20	Aircelle Sa	Entree d'air pour nacelle de grandes dimensions a transportabilite amelioree
FR2840647B1 (fr) *	2002-06-05	2004-10-29	Airbus France	Dispositif pour le raccordement de deux pieces tubulaires de turboreacteur d'aeronef
FR2856379B1 (fr) *	2003-06-18	2006-11-24	Airbus France	Moteur d'avion dont les capots de soufflante et d'inverseurs de poussee sont separes par un jeu reduit
GB2407134B (en) *	2003-10-16	2008-04-16	Rolls Royce Plc	Aircraft engine mounting assembly
GB0408825D0 (en) *	2004-04-20	2004-05-26	Rolls Royce Plc	A rotor blade containment assembly for a gas turbine engine
FR2869360B1 (fr) *	2004-04-27	2006-07-14	Airbus France Sas	Ensemble reducteur de bruit pour turboreacteur d'aeronef
GB2429043B (en) *	2005-08-13	2008-02-13	Rolls Royce Plc	Clip
FR2898870B1 (fr) *	2006-03-24	2008-05-23	Aircelle Sa	Structure de virole d'entree d'air
US7866440B2 (en) *	2006-07-21	2011-01-11	Rohr, Inc.	System for joining acoustic cellular panel sections in edge-to-edge relation
US7762086B2 (en) *	2008-03-12	2010-07-27	United Technologies Corporation	Nozzle extension assembly for ground and flight testing
US8092169B2 (en) *	2008-09-16	2012-01-10	United Technologies Corporation	Integrated inlet fan case

2008
- 2008-01-29 FR FR0800471A patent/FR2926791B1/fr not_active Expired - Fee Related
2009
- 2009-01-21 EP EP09716599A patent/EP2238031A1/fr not_active Withdrawn
- 2009-01-21 CA CA2708106A patent/CA2708106A1/fr not_active Abandoned
- 2009-01-21 RU RU2010134976/11A patent/RU2494015C2/ru not_active IP Right Cessation
- 2009-01-21 CN CN200980102533.8A patent/CN101918276B/zh not_active Expired - Fee Related
- 2009-01-21 US US12/864,901 patent/US8985506B2/en not_active Expired - Fee Related
- 2009-01-21 WO PCT/FR2009/000061 patent/WO2009109712A1/fr not_active Ceased
- 2009-01-21 BR BRPI0906953-4A patent/BRPI0906953A2/pt not_active IP Right Cessation

Also Published As

Publication number	Publication date
US20100320316A1 (en)	2010-12-23
CN101918276A (zh)	2010-12-15
CN101918276B (zh)	2013-10-09
FR2926791B1 (fr)	2010-05-28
CA2708106A1 (fr)	2009-09-11
FR2926791A1 (fr)	2009-07-31
RU2494015C2 (ru)	2013-09-27
US8985506B2 (en)	2015-03-24
EP2238031A1 (fr)	2010-10-13
RU2010134976A (ru)	2012-03-10
WO2009109712A1 (fr)	2009-09-11

Publication	Publication Date	Title
BRPI0906953A2 (pt)	2015-07-14	Entrada de ar para nacela de aeronave, conjunto compreendendo entrada de ar, conjunto de propulsão para aeronave
BRPI0821504A2 (pt)	2016-01-19	nacela para motor de avião
BRPI0812844A2 (pt)	2014-12-09	Estribo de afixação para motor de aeronave, conjunto motor para aeronave, e, aeronave
BRPI0821929A2 (pt)	2015-06-16	Nacela para motor turbojato
BRPI0908079A2 (pt)	2015-08-25	Conjunto motor para aeronave, e, aeronave
GB2469769B (en)	2011-02-23	Aft propeller vane system
BRPI0922745A2 (pt)	2016-01-05	ventoinha para turbomáquina de aeronave e turbomáquina para aeronave.
BRPI0907771A2 (pt)	2015-07-14	Conjunto motor para aeronave, e, aeronave
BRPI0922165A2 (pt)	2015-12-29	sistema de hélices contra-rotativas para turbomáquina de aeronave e turbomáquina para aeronave
BR112012013602A2 (pt)	2017-03-01	conjunto de asinha para aeronave.
BRPI0818168A2 (pt)	2017-05-16	aerogerador com duas hélices sucessivas.
BRPI0717730A2 (pt)	2013-10-22	Nacela para motor turbojato de contorno, conjunto de propulsão e avião
BRPI0911572A2 (pt)	2018-04-03	unidade de propulsão para uma aeronave e estrutura de entrada de ar para a referida unidade de propulsão
EP2256030A4 (en)	2013-10-02	AIRCRAFT ASSEMBLY
BRPI0910935A2 (pt)	2015-10-06	desvio da nacela de motor turbojato e nacela
BRPI0917143A2 (pt)	2018-05-29	avião equipado com motores de turboreator com fluxo duplo
BRPI0820878A2 (pt)	2018-07-17	fuselagem com atenuação acústica para aeronave
BRPI0919451A2 (pt)	2015-12-15	braço projeto para suportar nacela de motor turbojato de avião, nacela de motor turbojato de avião que incorpora um braço, conjunto de propulsão.
BRPI0906171A2 (pt)	2015-06-30	Nacela de aeronave
BRPI1008870A2 (pt)	2016-03-15	sistema de hélices contra-rotativas para turbomáquina de aeronave, e, turbomáquina para aeronave
BRPI0908913A2 (pt)	2018-02-27	aba de entrada de ar para nacela de turbojato
BRPI0917880A2 (pt)	2015-11-24	estrutura de entrada de ar para nacela de motor turbojato tencionada, nacela para um motor turbojato.
BRPI0818497A2 (pt)	2015-04-22	Estrutura de entrada de ar para ser montada a montante de uma estrutura intermediária de nacela para motor de avião, e nacela equipada com tal estrutura de entrada de ar.
BRPI0822363A2 (pt)	2015-06-16	Nacela de motor turbojato
BRPI0821699A2 (pt)	2015-06-16	Nacela de motor turbojato compreendendo sistema de travamento para estrutura de entrada de ar.

Legal Events

Date	Code	Title	Description
2016-11-22	B08F	Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]	Free format text: REFERENTE A 8A ANUIDADE.
2017-03-14	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.