BRPI0515362A - dispositivo para proteção contra aderência de gelo em motores de aeronave e correspondente método de eliminação de gelo - Google Patents

dispositivo para proteção contra aderência de gelo em motores de aeronave e correspondente método de eliminação de gelo

Info

Publication number
BRPI0515362A
BRPI0515362A BRPI0515362-0A BRPI0515362A BRPI0515362A BR PI0515362 A BRPI0515362 A BR PI0515362A BR PI0515362 A BRPI0515362 A BR PI0515362A BR PI0515362 A BRPI0515362 A BR PI0515362A
Authority
BR
Brazil
Prior art keywords
protection against
ice
aircraft
engine
aircraft engines
Prior art date
Application number
BRPI0515362-0A
Other languages
English (en)
Inventor
Chene Gilles
Jacquet-Francillon Pierre
Original Assignee
Airbus France
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 France filed Critical Airbus France
Publication of BRPI0515362A publication Critical patent/BRPI0515362A/pt

Links

Classifications

    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/48—Control of fuel supply conjointly with another control of the plant
    • 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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
    • B64D15/04—Hot gas application
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/48—Control of fuel supply conjointly with another control of the plant
    • F02C9/50—Control of fuel supply conjointly with another control of the plant with control of working fluid flow
    • F02C9/52—Control of fuel supply conjointly with another control of the plant with control of working fluid flow by bleeding or by-passing the working fluid
    • 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—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Testing Of Engines (AREA)
  • Investigating Or Analyzing Materials By The Use Of Electric Means (AREA)
  • Air-Conditioning For Vehicles (AREA)

Abstract

DISPOSITIVO PARA PROTEçãO CONTRA ADERêNCIA DE GELO EM MOTORES DE AERONAVE E CORRESPONDENTE MéTODO DE ELIMINAçãO DE GELO A invenção refere-se a um dispositivo para proteção contra aderência de gelo em motores de aeronave compreendendo pelo menos uni sensor (1), sensível a uma quantidade de gelo acumulado, disposto na admissão de ar de um motor de aeronave (2), um sistema para medir (3) a referida quantidade e para comparar (4) a referida quantidade com respeito a um predeterminado limite (S) e um sistema de disparo (5) destinado a iniciar uma resposta a uma detecção do predeterminado limite sendo ultrapassado, a resposta pode ser um alarme, uma elevação na potência de motor, retardada por meio do sistema de controle de motor (7) ou pelo retomo de ar quente a montante do motor.
BRPI0515362-0A 2004-09-21 2005-09-12 dispositivo para proteção contra aderência de gelo em motores de aeronave e correspondente método de eliminação de gelo BRPI0515362A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0452110A FR2875542B1 (fr) 2004-09-21 2004-09-21 Dispositif de protection contre le givrage pour moteurs d'aeronefs et procedes de degivrage associe
PCT/FR2005/050733 WO2006032808A1 (fr) 2004-09-21 2005-09-12 Dispositif de protection contre le givrage pour moteurs d'aeronefs et procede de degivrage associe

Publications (1)

Publication Number Publication Date
BRPI0515362A true BRPI0515362A (pt) 2008-07-15

Family

ID=34949529

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0515362-0A BRPI0515362A (pt) 2004-09-21 2005-09-12 dispositivo para proteção contra aderência de gelo em motores de aeronave e correspondente método de eliminação de gelo

Country Status (9)

Country Link
US (1) US7921632B2 (pt)
EP (1) EP1794429B1 (pt)
JP (1) JP4915745B2 (pt)
CN (1) CN100520013C (pt)
BR (1) BRPI0515362A (pt)
CA (1) CA2578408C (pt)
FR (1) FR2875542B1 (pt)
RU (1) RU2349780C2 (pt)
WO (1) WO2006032808A1 (pt)

Families Citing this family (23)

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WO2008045065A1 (en) * 2006-10-12 2008-04-17 United Technologies Corporation Controlling ice buildup on aircraft engine and nacelle static and rotating components
US7922121B2 (en) * 2007-10-15 2011-04-12 Rosemount Aerospace Inc. Power distribution architecture for an ice protection system
FR2925878B1 (fr) * 2007-12-28 2010-04-23 Airbus France Ensemble propulsif d'aeronef comprenant des systemes de prelevement d'air chaud
FR2927882B1 (fr) * 2008-02-27 2010-02-12 Aircelle Sa Structure d'entree d'air pour une nacelle d'un aeronef
FR2928346B1 (fr) * 2008-03-05 2011-09-16 Hutchinson Systeme et procede d'antigivrage/degivrage et structure d'aeronef incorporant ce systeme.
FR2938503A1 (fr) * 2008-11-17 2010-05-21 Aircelle Sa Procede de controle d'un systeme de degivrage electrique
FR2941439B1 (fr) * 2009-01-28 2011-01-14 Aircelle Sa Dispositif de degivrage electrique et systeme de controle associe
FR2958622B1 (fr) * 2010-04-09 2013-05-03 Airbus Operations Sas Procede et systeme de controle de la formation de glace sur un aeronef en vol.
FR2961898B1 (fr) * 2010-06-25 2013-01-04 Snecma Procede de detection d'une panne des moyens de degivrage d'une sonde de mesure d'un parametre physique
FR2966531B1 (fr) * 2010-10-26 2012-11-30 Snecma Procede de commande d'une turbomachine
GB201112577D0 (en) * 2011-07-22 2011-08-31 Rolls Royce Plc Method of inhibiting ice accretion within a turbine engine and control system therefor
CN102407942B (zh) * 2011-09-06 2016-05-04 中国商用飞机有限责任公司 结冰条件探测器
CN102490905A (zh) * 2011-12-27 2012-06-13 东南大学 用于飞机翼型的新型防冰除冰装置
JP5843633B2 (ja) * 2012-01-26 2016-01-13 三菱日立パワーシステムズ株式会社 ガスタービンの圧縮機の氷結防止手段およびその制御方法
US9593628B2 (en) * 2012-01-31 2017-03-14 United Technologies Corporation Gas turbine engine variable area fan nozzle with ice management
US8869508B2 (en) 2012-01-31 2014-10-28 United Technologies Corporation Gas turbine engine variable area fan nozzle control
US10421551B2 (en) 2014-12-15 2019-09-24 United Technologies Corporation Aircraft anti-icing system
US10184405B1 (en) * 2016-04-15 2019-01-22 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Aircraft engine icing event avoidance and mitigation through real-time simulation and controls
BE1024951B1 (fr) * 2017-01-25 2018-08-30 Safran Aero Boosters S.A. Dispositif de degivrage pour aube et turbomachine axiale
CN108688824B (zh) * 2017-04-10 2020-07-14 清华大学 发动机进气口除冰系统、内燃发动机及航空器
US11428119B2 (en) 2019-12-18 2022-08-30 Pratt & Whitney Canada Corp. Method and system to promote ice shedding from rotor blades of an aircraft engine
CN111305953B (zh) * 2020-03-18 2021-05-04 中国商用飞机有限责任公司 一种航空涡扇发动机风扇叶片自动脱冰的方法及装置
CN113417891B (zh) * 2021-08-03 2022-08-16 中国航发湖南动力机械研究所 离心压气机防冰引气结构及发动机

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Also Published As

Publication number Publication date
CA2578408C (fr) 2013-11-05
CN101023254A (zh) 2007-08-22
CN100520013C (zh) 2009-07-29
WO2006032808A1 (fr) 2006-03-30
JP2008510913A (ja) 2008-04-10
FR2875542A1 (fr) 2006-03-24
EP1794429B1 (fr) 2017-12-27
RU2007114907A (ru) 2008-10-27
FR2875542B1 (fr) 2009-02-13
US20090294593A1 (en) 2009-12-03
CA2578408A1 (fr) 2006-03-30
RU2349780C2 (ru) 2009-03-20
EP1794429A1 (fr) 2007-06-13
JP4915745B2 (ja) 2012-04-11
US7921632B2 (en) 2011-04-12

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Legal Events

Date Code Title Description
B25A Requested transfer of rights approved

Owner name: AIRBUS OPERATIONS SAS (FR)

Free format text: TRANSFERIDO POR INCORPORACAO DE: AIRBUS FRANCE

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

Free format text: REFERENTE A 10A 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 2323 DE 14-07-2015 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.