BRPI0821930A2 - Conjunto de propulsão para motor turbojato - Google Patents

Conjunto de propulsão para motor turbojato

Info

Publication number
BRPI0821930A2
BRPI0821930A2 BRPI0821930-3A BRPI0821930A BRPI0821930A2 BR PI0821930 A2 BRPI0821930 A2 BR PI0821930A2 BR PI0821930 A BRPI0821930 A BR PI0821930A BR PI0821930 A2 BRPI0821930 A2 BR PI0821930A2
Authority
BR
Brazil
Prior art keywords
turbojet engine
engine propulsion
propulsion kit
kit
turbojet
Prior art date
Application number
BRPI0821930-3A
Other languages
English (en)
Inventor
Guy Bernard Vauchel
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 BRPI0821930A2 publication Critical patent/BRPI0821930A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206—Arrangements 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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266—Arrangements 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—Arrangements 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
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
BRPI0821930-3A 2008-01-29 2008-10-17 Conjunto de propulsão para motor turbojato BRPI0821930A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0800472A FR2926789B1 (fr) 2008-01-29 2008-01-29 Nacelle pour turboreacteur
PCT/FR2008/001464 WO2010000953A1 (fr) 2008-01-29 2008-10-17 Nacelle pour turboreacteur

Publications (1)

Publication Number Publication Date
BRPI0821930A2 true BRPI0821930A2 (pt) 2015-06-16

Family

ID=39713903

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0821930-3A BRPI0821930A2 (pt) 2008-01-29 2008-10-17 Conjunto de propulsão para motor turbojato

Country Status (9)

Country Link
US (1) US9051054B2 (pt)
EP (1) EP2234886B1 (pt)
CN (1) CN101910000B (pt)
BR (1) BRPI0821930A2 (pt)
CA (1) CA2711604A1 (pt)
ES (1) ES2441401T3 (pt)
FR (1) FR2926789B1 (pt)
RU (1) RU2471681C2 (pt)
WO (1) WO2010000953A1 (pt)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2459646B (en) * 2008-04-28 2011-03-30 Rolls Royce Plc A fan assembly
GB0907582D0 (en) 2009-05-05 2009-06-10 Rolls Royce Plc A duct wall for a fan of a gas turbine engine
FR2958980B1 (fr) * 2010-04-14 2013-03-15 Snecma Dispositif redresseur pour turbomachine
FR2975970B1 (fr) * 2011-05-30 2013-05-17 Aircelle Sa Ensemble pour une nacelle d'aeronef
US10907651B2 (en) 2016-01-12 2021-02-02 Rolls-Royce Corporation Fan track liner subassembly angled upturn joint
FR3054527B1 (fr) * 2016-07-29 2019-08-30 Airbus Operations Ensemble pour aeronef comprenant un bouclier de protection contre un eclatement moteur, monte sur le carter d'un module de turbomachine
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
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
FR3082238A1 (fr) * 2018-06-11 2019-12-13 Airbus Operations Tuyere primaire d'un conduit d'ejection primaire d'une turbomachine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5259724A (en) * 1992-05-01 1993-11-09 General Electric Company Inlet fan blade fragment containment shield
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
FR2847304B1 (fr) 2002-11-18 2005-07-01 Airbus France Nacelle de reacteur d'aeronef a attenuation acoustique
FR2862045B1 (fr) * 2003-11-12 2006-05-05 Snecma Moteurs Turboreacteur destine a etre fixe sur le fuselage d'un avion et en particulier sur sa partie arriere
FR2869360B1 (fr) * 2004-04-27 2006-07-14 Airbus France Sas Ensemble reducteur de bruit pour turboreacteur d'aeronef
FR2898870B1 (fr) * 2006-03-24 2008-05-23 Aircelle Sa Structure de virole d'entree d'air
FR2903734B1 (fr) * 2006-07-12 2008-09-12 Airbus France Sas Turbomoteur pour aeronef.
FR2903733B1 (fr) * 2006-07-12 2011-03-04 Airbus France Turbomoteur pour aeronef.

Also Published As

Publication number Publication date
WO2010000953A1 (fr) 2010-01-07
RU2010134974A (ru) 2012-03-10
US9051054B2 (en) 2015-06-09
ES2441401T3 (es) 2014-02-04
RU2471681C2 (ru) 2013-01-10
CN101910000B (zh) 2013-12-25
US20110033286A1 (en) 2011-02-10
CA2711604A1 (fr) 2010-01-07
WO2010000953A8 (fr) 2010-06-24
CN101910000A (zh) 2010-12-08
FR2926789B1 (fr) 2010-05-28
EP2234886B1 (fr) 2013-10-09
EP2234886A1 (fr) 2010-10-06
FR2926789A1 (fr) 2009-07-31

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Legal Events

Date Code Title Description
B08F Application fees: dismissal - article 86 of industrial property law

Free format text: REFERENTE A 8A ANUIDADE.

B08K Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87)

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2385 DE 20-09-2016 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.