CN100520013C - 防止航空器发动机结冰的保护装置和相关的除冰方法 - Google Patents

防止航空器发动机结冰的保护装置和相关的除冰方法 Download PDF

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Publication number
CN100520013C
CN100520013C CNB2005800318314A CN200580031831A CN100520013C CN 100520013 C CN100520013 C CN 100520013C CN B2005800318314 A CNB2005800318314 A CN B2005800318314A CN 200580031831 A CN200580031831 A CN 200580031831A CN 100520013 C CN100520013 C CN 100520013C
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CN
China
Prior art keywords
engine
engine speed
frost
icing
control system
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Expired - Fee Related
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CNB2005800318314A
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English (en)
Chinese (zh)
Other versions
CN101023254A (zh
Inventor
P·雅凯-弗朗西永
G·谢纳
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Airbus Operations SAS
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Airbus Operations SAS
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Publication of CN101023254A publication Critical patent/CN101023254A/zh
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Publication of CN100520013C publication Critical patent/CN100520013C/zh
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Expired - Fee Related legal-status Critical Current

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    • 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—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
    • B64D2033/0233—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid Mechanics (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Investigating Or Analyzing Materials By The Use Of Electric Means (AREA)
  • Air-Conditioning For Vehicles (AREA)
  • Testing Of Engines (AREA)
CNB2005800318314A 2004-09-21 2005-09-12 防止航空器发动机结冰的保护装置和相关的除冰方法 Expired - Fee Related CN100520013C (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0452110 2004-09-21
FR0452110A FR2875542B1 (fr) 2004-09-21 2004-09-21 Dispositif de protection contre le givrage pour moteurs d'aeronefs et procedes de degivrage associe

Publications (2)

Publication Number Publication Date
CN101023254A CN101023254A (zh) 2007-08-22
CN100520013C true CN100520013C (zh) 2009-07-29

Family

ID=34949529

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2005800318314A Expired - Fee Related CN100520013C (zh) 2004-09-21 2005-09-12 防止航空器发动机结冰的保护装置和相关的除冰方法

Country Status (9)

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

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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
US8869508B2 (en) 2012-01-31 2014-10-28 United Technologies Corporation Gas turbine engine variable area fan nozzle control
US9593628B2 (en) * 2012-01-31 2017-03-14 United Technologies Corporation Gas turbine engine variable area fan nozzle with ice management
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
CN116464557A (zh) * 2023-04-20 2023-07-21 中国航发成都发动机有限公司 一种航空发动机防冰自动装置检查仪
US12110825B1 (en) * 2023-08-29 2024-10-08 General Electric Company Systems and method for detecting and responding to icing conditions in gas turbine engines
EP4566946A3 (en) 2023-09-30 2025-06-18 Archer Aviation Inc. Systems and methods for managing ice accretions during flight of aircraft

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DE3333437A1 (de) * 1983-09-16 1985-04-11 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur verdichterregelung von gasturbinentriebwerken
US4782331A (en) * 1986-06-10 1988-11-01 U.S. Philips Corporation Photoelectric icing detector
US6304194B1 (en) * 1998-12-11 2001-10-16 Continuum Dynamics, Inc. Aircraft icing detection system
US6560551B1 (en) * 2000-08-18 2003-05-06 Rosemount Aerospace Inc. Liquid water content measurement apparatus and method

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US5523959A (en) * 1994-04-25 1996-06-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Ice detector and deicing fluid effectiveness monitoring system
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DE3333437A1 (de) * 1983-09-16 1985-04-11 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur verdichterregelung von gasturbinentriebwerken
US4782331A (en) * 1986-06-10 1988-11-01 U.S. Philips Corporation Photoelectric icing detector
US6304194B1 (en) * 1998-12-11 2001-10-16 Continuum Dynamics, Inc. Aircraft icing detection system
US6560551B1 (en) * 2000-08-18 2003-05-06 Rosemount Aerospace Inc. Liquid water content measurement apparatus and method

Also Published As

Publication number Publication date
JP4915745B2 (ja) 2012-04-11
FR2875542A1 (fr) 2006-03-24
US7921632B2 (en) 2011-04-12
JP2008510913A (ja) 2008-04-10
BRPI0515362A (pt) 2008-07-15
US20090294593A1 (en) 2009-12-03
CN101023254A (zh) 2007-08-22
RU2349780C2 (ru) 2009-03-20
WO2006032808A1 (fr) 2006-03-30
RU2007114907A (ru) 2008-10-27
CA2578408C (fr) 2013-11-05
FR2875542B1 (fr) 2009-02-13
EP1794429B1 (fr) 2017-12-27
CA2578408A1 (fr) 2006-03-30
EP1794429A1 (fr) 2007-06-13

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Owner name: AIRBUS OPERATIONS GMBH

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Patentee after: Airbus Operations S.A.S.

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Granted publication date: 20090729

Termination date: 20200912

CF01 Termination of patent right due to non-payment of annual fee