AU2003207033B2 - Methods and apparatus for operating gas turbine engines - Google Patents

Methods and apparatus for operating gas turbine engines Download PDF

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Publication number
AU2003207033B2
AU2003207033B2 AU2003207033A AU2003207033A AU2003207033B2 AU 2003207033 B2 AU2003207033 B2 AU 2003207033B2 AU 2003207033 A AU2003207033 A AU 2003207033A AU 2003207033 A AU2003207033 A AU 2003207033A AU 2003207033 B2 AU2003207033 B2 AU 2003207033B2
Authority
AU
Australia
Prior art keywords
engine
semi
aircraft
permeable membrane
membrane
Prior art date
Legal status (The legal status 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 status listed.)
Ceased
Application number
AU2003207033A
Other languages
English (en)
Other versions
AU2003207033A1 (en
Inventor
John Frederick Ackerman
William Kent Wagner
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of AU2003207033A1 publication Critical patent/AU2003207033A1/en
Application granted granted Critical
Publication of AU2003207033B2 publication Critical patent/AU2003207033B2/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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
    • 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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/02—De-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)
AU2003207033A 2002-07-03 2003-07-03 Methods and apparatus for operating gas turbine engines Ceased AU2003207033B2 (en)

Applications Claiming Priority (2)

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
US10/188,460 2002-07-03

Publications (2)

Publication Number Publication Date
AU2003207033A1 AU2003207033A1 (en) 2004-01-22
AU2003207033B2 true AU2003207033B2 (en) 2010-07-22

Family

ID=29720422

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2003207033A Ceased AU2003207033B2 (en) 2002-07-03 2003-07-03 Methods and apparatus for operating gas turbine engines

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
US8224552B2 (en) * 2008-07-10 2012-07-17 General Electric Company Methods and systems to facilitate over-speed protection
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
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
US12392290B2 (en) 2022-11-01 2025-08-19 General Electric Company Gas turbine engine
US12410753B2 (en) 2022-11-01 2025-09-09 General Electric Company Gas turbine engine

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
EP0599502A1 (en) * 1992-11-27 1994-06-01 ROLLS-ROYCE plc Porous structure having laminar flow control and contamination protection
US5944287A (en) * 1996-07-02 1999-08-31 Rolls-Royce Plc Ice protection for porous structure

Family Cites Families (25)

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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
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
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
US5143329A (en) 1990-06-01 1992-09-01 General Electric Company Gas turbine engine powered aircraft environmental control system and boundary layer bleed
DE4337674A1 (de) * 1992-11-17 1994-05-19 Elin Energieversorgung Verfahren zur Eisfreihaltung des Frischluft-Ansaugfilters von Gas-Dampfturbinenanlagen
RU2095601C1 (ru) * 1993-12-10 1997-11-10 Юрий Иванович Климнюк Газотурбинная установка с противообледенительным устройством
US6279856B1 (en) 1997-09-22 2001-08-28 Northcoast Technologies Aircraft de-icing system
US5934617A (en) 1997-09-22 1999-08-10 Northcoast Technologies De-ice and anti-ice system and method for aircraft surfaces
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

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
EP0599502A1 (en) * 1992-11-27 1994-06-01 ROLLS-ROYCE plc Porous structure having laminar flow control and contamination protection
US5944287A (en) * 1996-07-02 1999-08-31 Rolls-Royce Plc Ice protection for porous structure

Also Published As

Publication number Publication date
US7188464B2 (en) 2007-03-13
KR20040004134A (ko) 2004-01-13
BR0302379B1 (pt) 2011-11-01
JP2004052764A (ja) 2004-02-19
JP4555552B2 (ja) 2010-10-06
US6920748B2 (en) 2005-07-26
CA2432841C (en) 2012-08-07
EP1378633A2 (en) 2004-01-07
BR0302379A (pt) 2004-08-24
CA2432841A1 (en) 2004-01-03
ZA200304719B (en) 2004-04-30
KR100836979B1 (ko) 2008-06-10
US20050039435A1 (en) 2005-02-24
AU2003207033A1 (en) 2004-01-22
RU2319023C2 (ru) 2008-03-10
CN1470747A (zh) 2004-01-28
US20050144957A1 (en) 2005-07-07
EP1378633A3 (en) 2005-11-09
CN100520011C (zh) 2009-07-29

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Legal Events

Date Code Title Description
FGA Letters patent sealed or granted (standard patent)
MK14 Patent ceased section 143(a) (annual fees not paid) or expired