JP4555552B2 - ガスタービンエンジンを運転するための方法及び装置 - Google Patents

ガスタービンエンジンを運転するための方法及び装置 Download PDF

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Publication number
JP4555552B2
JP4555552B2 JP2003189147A JP2003189147A JP4555552B2 JP 4555552 B2 JP4555552 B2 JP 4555552B2 JP 2003189147 A JP2003189147 A JP 2003189147A JP 2003189147 A JP2003189147 A JP 2003189147A JP 4555552 B2 JP4555552 B2 JP 4555552B2
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Japan
Prior art keywords
engine
fluid
icing
aircraft
semipermeable membrane
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Expired - Fee Related
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JP2003189147A
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English (en)
Japanese (ja)
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JP2004052764A5 (enExample
JP2004052764A (ja
Inventor
ジョン・フレデリック・アッカーマン
ウィリアム・ケント・ワグナー
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General Electric Co
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General Electric Co
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047Heating to prevent icing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/02De-icing means for engines having icing phenomena

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Separation Using Semi-Permeable Membranes (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
JP2003189147A 2002-07-03 2003-07-01 ガスタービンエンジンを運転するための方法及び装置 Expired - Fee Related JP4555552B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/188,460 US6920748B2 (en) 2002-07-03 2002-07-03 Methods and apparatus for operating gas turbine engines

Publications (3)

Publication Number Publication Date
JP2004052764A JP2004052764A (ja) 2004-02-19
JP2004052764A5 JP2004052764A5 (enExample) 2006-08-17
JP4555552B2 true JP4555552B2 (ja) 2010-10-06

Family

ID=29720422

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003189147A Expired - Fee Related JP4555552B2 (ja) 2002-07-03 2003-07-01 ガスタービンエンジンを運転するための方法及び装置

Country Status (10)

Country Link
US (2) US6920748B2 (enExample)
EP (1) EP1378633A3 (enExample)
JP (1) JP4555552B2 (enExample)
KR (1) KR100836979B1 (enExample)
CN (1) CN100520011C (enExample)
AU (1) AU2003207033B2 (enExample)
BR (1) BR0302379B1 (enExample)
CA (1) CA2432841C (enExample)
RU (1) RU2319023C2 (enExample)
ZA (1) ZA200304719B (enExample)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6920748B2 (en) 2002-07-03 2005-07-26 General Electric Company Methods and apparatus for operating gas turbine engines
US20060204647A1 (en) * 2005-03-09 2006-09-14 Vittorio Calabrese De-icing system for driveways, walkways, sidewalks and other surfaces
US7374404B2 (en) * 2005-09-22 2008-05-20 General Electric Company Methods and apparatus for gas turbine engines
US7429166B2 (en) * 2005-12-20 2008-09-30 General Electric Company Methods and apparatus for gas turbine engines
US8321119B2 (en) * 2008-07-10 2012-11-27 General Electric Company Methods and systems to facilitate over-speed protection
US20100005657A1 (en) * 2008-07-10 2010-01-14 Van Vactor David R Methods and systems to facilitate over-speed protection
US8224552B2 (en) * 2008-07-10 2012-07-17 General Electric Company Methods and systems to facilitate over-speed protection
US8575900B2 (en) 2010-09-03 2013-11-05 Hamilton Sundstrand Corporation Rotor based air gap heating for air driven turbine
US9422063B2 (en) * 2013-05-31 2016-08-23 General Electric Company Cooled cooling air system for a gas turbine
US10156190B2 (en) * 2015-05-20 2018-12-18 Honeywell International Inc. Gas turbine engine uncontrolled high thrust accommodation system and method
US10443497B2 (en) 2016-08-10 2019-10-15 Rolls-Royce Corporation Ice protection system for gas turbine engines
US10801361B2 (en) 2016-09-09 2020-10-13 General Electric Company System and method for HPT disk over speed prevention
US10252808B2 (en) * 2016-09-22 2019-04-09 The Boeing Company Fluid ice protection system flow conductivity sensor
US20180221958A1 (en) * 2017-02-07 2018-08-09 General Electric Company Parts and methods for producing parts using hybrid additive manufacturing techniques
US11365647B2 (en) * 2020-02-28 2022-06-21 Raytheon Technologies Corporation Closed loop fan inlet vane anti icing system
US12428992B2 (en) 2022-11-01 2025-09-30 General Electric Company Gas turbine engine
US12196131B2 (en) 2022-11-01 2025-01-14 General Electric Company Gas turbine engine
US12410753B2 (en) 2022-11-01 2025-09-09 General Electric Company Gas turbine engine
US12392290B2 (en) 2022-11-01 2025-08-19 General Electric Company Gas turbine engine

Family Cites Families (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2075658A (en) * 1934-04-07 1937-03-30 Ramsbottom John Edwin Ice preventing device
US2098566A (en) * 1934-10-27 1937-11-09 Reed Propeller Co Inc De-icing means for aircraft
US2075659A (en) * 1935-05-08 1937-03-30 Ramsbottom John Edwin Apparatus for preventing ice accumulation on aircraft
US2457031A (en) * 1942-12-05 1948-12-21 Borg Warner Aircraft anti-icing arrangement
GB569301A (en) * 1943-12-15 1945-05-16 Pesco Products Co Improvements in or relating to aircraft anti-icing or de-icing arrangements
US2390093A (en) * 1944-03-16 1945-12-04 Garrison Murray Ed Airplane wing deicing means
GB622554A (en) * 1945-09-24 1949-05-04 Westinghouse Electric Int Co Improvements in or relating to ice detecting apparatus for air compressors
US2812899A (en) * 1949-08-30 1957-11-12 A V Roe Canada Ltd Intake sprinkler for gas turbine engines
GB724019A (en) * 1952-07-15 1955-02-16 Joseph Halbert Improvements relating to means for distributing fluids
GB1094372A (en) * 1964-04-10 1967-12-13 T K S Aircraft De Icing Ltd Improvements relating to means for distributing liquids to the surfaces of aerofoils
US3423052A (en) * 1966-07-21 1969-01-21 Lear Jet Ind Inc De-icing apparatus
US3614038A (en) * 1970-01-08 1971-10-19 Ace Filtercraft Inc Porous metal panel to distribute deicing fluid onto the leading edge of a surface
US4434201A (en) * 1981-11-13 1984-02-28 T.K.S. (Aircraft De-Icing) Limited Porous panel
GB2130158A (en) * 1982-11-15 1984-05-31 Fiber Materials Deicing aircraft surfaces
US5088277A (en) 1988-10-03 1992-02-18 General Electric Company Aircraft engine inlet cowl anti-icing system
US5136837A (en) 1990-03-06 1992-08-11 General Electric Company Aircraft engine starter integrated boundary bleed system
US5143329A (en) 1990-06-01 1992-09-01 General Electric Company Gas turbine engine powered aircraft environmental control system and boundary layer bleed
US5125597A (en) 1990-06-01 1992-06-30 General Electric Company Gas turbine engine powered aircraft environmental control system and boundary layer bleed with energy recovery system
DE4337674A1 (de) * 1992-11-17 1994-05-19 Elin Energieversorgung Verfahren zur Eisfreihaltung des Frischluft-Ansaugfilters von Gas-Dampfturbinenanlagen
GB9224849D0 (en) * 1992-11-27 1993-01-13 Rolls Royce Plc Porous structure having laminar flow control and contamination protection
RU2095601C1 (ru) * 1993-12-10 1997-11-10 Юрий Иванович Климнюк Газотурбинная установка с противообледенительным устройством
GB2314887B (en) * 1996-07-02 2000-02-09 Rolls Royce Plc Ice protection for porous structure
US5934617A (en) 1997-09-22 1999-08-10 Northcoast Technologies De-ice and anti-ice system and method for aircraft surfaces
US6279856B1 (en) 1997-09-22 2001-08-28 Northcoast Technologies Aircraft de-icing system
US6371411B1 (en) 1999-11-23 2002-04-16 The Boeing Company Method and apparatus for aircraft inlet ice protection
JP2001342849A (ja) 2000-05-31 2001-12-14 Honda Motor Co Ltd ガスタービンエンジン
RU21423U1 (ru) * 2001-08-27 2002-01-20 Открытое акционерное общество Омское моторостроительное конструкторское бюро Противообледенительная система газотурбинного двигателя
US6920748B2 (en) 2002-07-03 2005-07-26 General Electric Company Methods and apparatus for operating gas turbine engines
US6990797B2 (en) 2003-09-05 2006-01-31 General Electric Company Methods and apparatus for operating gas turbine engines

Also Published As

Publication number Publication date
CN1470747A (zh) 2004-01-28
EP1378633A3 (en) 2005-11-09
US20050144957A1 (en) 2005-07-07
KR100836979B1 (ko) 2008-06-10
US6920748B2 (en) 2005-07-26
BR0302379A (pt) 2004-08-24
BR0302379B1 (pt) 2011-11-01
US7188464B2 (en) 2007-03-13
CA2432841C (en) 2012-08-07
US20050039435A1 (en) 2005-02-24
CN100520011C (zh) 2009-07-29
ZA200304719B (en) 2004-04-30
AU2003207033A1 (en) 2004-01-22
EP1378633A2 (en) 2004-01-07
KR20040004134A (ko) 2004-01-13
AU2003207033B2 (en) 2010-07-22
JP2004052764A (ja) 2004-02-19
RU2319023C2 (ru) 2008-03-10
CA2432841A1 (en) 2004-01-03

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