BRPI0907478A2 - flap de admissão de mecanismo propulsor para aplicação à caixa de uma entrada de ar de um mecanismo propulsor de aeronave bem como mecanismo propulsor com flap de admissão de mecanismo propulsor e sistema de aeronave - Google Patents

flap de admissão de mecanismo propulsor para aplicação à caixa de uma entrada de ar de um mecanismo propulsor de aeronave bem como mecanismo propulsor com flap de admissão de mecanismo propulsor e sistema de aeronave

Info

Publication number
BRPI0907478A2
BRPI0907478A2 BRPI0907478A BRPI0907478A BRPI0907478A2 BR PI0907478 A2 BRPI0907478 A2 BR PI0907478A2 BR PI0907478 A BRPI0907478 A BR PI0907478A BR PI0907478 A BRPI0907478 A BR PI0907478A BR PI0907478 A2 BRPI0907478 A2 BR PI0907478A2
Authority
BR
Brazil
Prior art keywords
inlet
engine
inlet flap
flap
base body
Prior art date
Application number
BRPI0907478A
Other languages
English (en)
Inventor
Bolender Lars
Wagnon Sébastian
Original Assignee
Airbus Operations Gmbh
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 Airbus Operations Gmbh filed Critical Airbus Operations Gmbh
Publication of BRPI0907478A2 publication Critical patent/BRPI0907478A2/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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/16—De-icing or preventing icing on exterior surfaces of aircraft by mechanical means
    • 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
    • F02C7/047—Heating to prevent icing
    • 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
    • F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
    • F02C7/055—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles with intake grids, screens or guards
    • 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
    • B64D2033/0213—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for auxiliary power units (APU's)
    • 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
    • B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
    • 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

Abstract

flap de admissão de mecanismo propulsor para aplicação à caixa de uma entrada de ar de um mecanismo propulsor de aeronave bem como mecanismo propulsor com flap de admissão de mecanismo propulsor e sistema de aeronave. a presente invenção refere-se a um flap de admissão de mecanismo propulsor (k) para aplicação a uma caixa de uma entrada de ar ou canal de admissão de ar de um mecanismo propulsor de uma aeronave, com uma primeira extremidade (e1) e uma segunda extremidade (e2) posicionada contrária àquela e distanciada em uma direção longitudinal (l) do flap de admissão, sendo que a direção longitudinal (l) quando o emprego intencionado é dirigida contra a direção aerodinâmica (s) do ar fluindo para dentro do mecanismo propulsor, apresentando: - um corpo de base de flap de admissão (1) com um dispositivo de conexão para uma união articulada para união articulada do corpo de base de flap de admissão (1) na caixa da entrada de ar ou canal de admissão de ar com um eixo de rotação (a) se estendendo ao longo da segunda extremidade (e2), uma parte de prolongamento de flap de admissão (2) estrutura lmente integrada com o corpo de base do flap de admissão (1 ), que apresenta uma primeira e uma segunda partes lateral (5, 6), que se estende respectivamente nas duas bordas laterais (1a, 1b), posicionadas mutuamente contrapostas e se estendendo na direção longitudinal (l), do flap de admissão (k) do corpo de base do flap de admissão (1 ), com uma pluralidade de escoras transversais (11) ou escoras longitudinais, que ficam dispostas na região dianteira do flap de admissão de mecanismo propulsor (k).
BRPI0907478A 2008-02-04 2009-02-04 flap de admissão de mecanismo propulsor para aplicação à caixa de uma entrada de ar de um mecanismo propulsor de aeronave bem como mecanismo propulsor com flap de admissão de mecanismo propulsor e sistema de aeronave BRPI0907478A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US2585708P 2008-02-04 2008-02-04
DE102008007469A DE102008007469A1 (de) 2008-02-04 2008-02-04 Verlängerungsteil für eine Einlaufklappe, Einlaufklappe mit einem solchen Verlängerungsteil und Triebwerk mit einer Einlaufklappe
PCT/EP2009/000753 WO2009098044A1 (de) 2008-02-04 2009-02-04 Triebwerks-einlaufklappe zur anbringung an dem gehäuse eines lufteinlasses eines flugzeug-triebwerks sowie triebwerk mit einer solchen triebwerks-einlaufklappe und flugzeugsystem

Publications (1)

Publication Number Publication Date
BRPI0907478A2 true BRPI0907478A2 (pt) 2019-02-26

Family

ID=40822188

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0907478A BRPI0907478A2 (pt) 2008-02-04 2009-02-04 flap de admissão de mecanismo propulsor para aplicação à caixa de uma entrada de ar de um mecanismo propulsor de aeronave bem como mecanismo propulsor com flap de admissão de mecanismo propulsor e sistema de aeronave

Country Status (10)

Country Link
US (1) US8590832B2 (pt)
EP (1) EP2254795B1 (pt)
JP (1) JP2011514465A (pt)
CN (1) CN101939222B (pt)
AT (1) ATE530441T1 (pt)
BR (1) BRPI0907478A2 (pt)
CA (1) CA2713579A1 (pt)
DE (1) DE102008007469A1 (pt)
RU (1) RU2490178C2 (pt)
WO (1) WO2009098044A1 (pt)

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CN107956609B (zh) * 2017-12-18 2023-07-11 东风商用车有限公司 一种可调挡雨片倾角的引气管控制系统及其控制方法
EP4001119A1 (en) * 2018-01-05 2022-05-25 Rosemount Aerospace Inc. Features to prevent ice accumulation on heated faceplate
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US10877062B2 (en) 2018-05-09 2020-12-29 Rosemount Aerospace Inc. Aft-located heated ramp for ice and water management of angle of attack sensors
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Also Published As

Publication number Publication date
RU2490178C2 (ru) 2013-08-20
CN101939222B (zh) 2013-08-28
US20100307442A1 (en) 2010-12-09
JP2011514465A (ja) 2011-05-06
EP2254795B1 (de) 2011-10-26
US8590832B2 (en) 2013-11-26
EP2254795A1 (de) 2010-12-01
DE102008007469A1 (de) 2009-08-06
CA2713579A1 (en) 2009-08-13
WO2009098044A1 (de) 2009-08-13
ATE530441T1 (de) 2011-11-15
CN101939222A (zh) 2011-01-05
RU2010135968A (ru) 2012-03-20

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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 2513 DE 06-03-2019 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.

B350 Update of information on the portal [chapter 15.35 patent gazette]