KR100836979B1 - 항공기 엔진의 작동 방법 및 방빙 시스템 - Google Patents

항공기 엔진의 작동 방법 및 방빙 시스템 Download PDF

Info

Publication number
KR100836979B1
KR100836979B1 KR1020030044628A KR20030044628A KR100836979B1 KR 100836979 B1 KR100836979 B1 KR 100836979B1 KR 1020030044628 A KR1020030044628 A KR 1020030044628A KR 20030044628 A KR20030044628 A KR 20030044628A KR 100836979 B1 KR100836979 B1 KR 100836979B1
Authority
KR
South Korea
Prior art keywords
engine
membrane
fluid
aircraft
protection system
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.)
Expired - Fee Related
Application number
KR1020030044628A
Other languages
English (en)
Korean (ko)
Other versions
KR20040004134A (ko
Inventor
아커만존프레더릭
와그너윌리암켄트
Original Assignee
제너럴 일렉트릭 캄파니
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 제너럴 일렉트릭 캄파니 filed Critical 제너럴 일렉트릭 캄파니
Publication of KR20040004134A publication Critical patent/KR20040004134A/ko
Application granted granted Critical
Publication of KR100836979B1 publication Critical patent/KR100836979B1/ko
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

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)
KR1020030044628A 2002-07-03 2003-07-02 항공기 엔진의 작동 방법 및 방빙 시스템 Expired - Fee Related KR100836979B1 (ko)

Applications Claiming Priority (2)

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

Publications (2)

Publication Number Publication Date
KR20040004134A KR20040004134A (ko) 2004-01-13
KR100836979B1 true KR100836979B1 (ko) 2008-06-10

Family

ID=29720422

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020030044628A Expired - Fee Related KR100836979B1 (ko) 2002-07-03 2003-07-02 항공기 엔진의 작동 방법 및 방빙 시스템

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 (20)

* 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
US12392290B2 (en) 2022-11-01 2025-08-19 General Electric Company Gas turbine engine
US12428992B2 (en) 2022-11-01 2025-09-30 General Electric Company Gas turbine engine
US12503980B2 (en) 2022-11-01 2025-12-23 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

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2390093A (en) 1944-03-16 1945-12-04 Garrison Murray Ed Airplane wing deicing means
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
JPS5992300A (ja) * 1982-11-15 1984-05-28 フアイバ−・マテリアルズ・インコ−ポレ−テツド 飛行機の翼の氷結防止装置
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 (22)

* 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
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
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
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

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2390093A (en) 1944-03-16 1945-12-04 Garrison Murray Ed Airplane wing deicing means
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
JPS5992300A (ja) * 1982-11-15 1984-05-28 フアイバ−・マテリアルズ・インコ−ポレ−テツド 飛行機の翼の氷結防止装置
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
JP2004052764A (ja) 2004-02-19
EP1378633A3 (en) 2005-11-09
US6920748B2 (en) 2005-07-26
CA2432841C (en) 2012-08-07
RU2319023C2 (ru) 2008-03-10
US20050039435A1 (en) 2005-02-24
CN100520011C (zh) 2009-07-29
BR0302379B1 (pt) 2011-11-01
CN1470747A (zh) 2004-01-28
CA2432841A1 (en) 2004-01-03
AU2003207033A1 (en) 2004-01-22
EP1378633A2 (en) 2004-01-07
JP4555552B2 (ja) 2010-10-06
US20050144957A1 (en) 2005-07-07
KR20040004134A (ko) 2004-01-13
US7188464B2 (en) 2007-03-13
AU2003207033B2 (en) 2010-07-22
ZA200304719B (en) 2004-04-30
BR0302379A (pt) 2004-08-24

Similar Documents

Publication Publication Date Title
KR100836979B1 (ko) 항공기 엔진의 작동 방법 및 방빙 시스템
US9429072B2 (en) Return fluid air cooler system for turbine cooling with optional power extraction
US7401461B2 (en) Reduced-weight fuel system for gas turbine engine, gas turbine engine having a reduced-weight fuel system, and method of providing fuel to a gas turbine engine using a reduced-weight fuel system
US10654579B2 (en) Cooled cooling air system for a gas turbine
CA2931493C (en) Aircraft environmental control system
CA2479276C (en) Methods and apparatus for operating gas turbine engines
US10823066B2 (en) Thermal management system
US8117827B2 (en) Apparatus for operating gas turbine engines
EP3483414B1 (en) Gas turbine engine having an air-oil heat exchanger
CN113417743B (zh) 用于涡轮发动机的冷却系统
US10323571B2 (en) Method and system for inlet guide vane heating
EP3321489A1 (en) Gas turbine engine bleed configuration
JP2009115092A (ja) フリータービンに流入する空気を加熱する手段を備えるタービンエンジン
US11085312B2 (en) Aircraft incorporating a thrust recovery system using cabin air
US20180149093A1 (en) Turbine engine and method of cooling thereof
US20160160684A1 (en) Turbine engine assembly and method of manufacturing
US7329088B2 (en) Pilot relief to reduce strut effects at pilot interface
US20250172095A1 (en) Turbomachine with axial thrust management
RU2439347C1 (ru) Газотурбинный двигатель с задним расположением винтовентилятора

Legal Events

Date Code Title Description
PA0109 Patent application

St.27 status event code: A-0-1-A10-A12-nap-PA0109

PG1501 Laying open of application

St.27 status event code: A-1-1-Q10-Q12-nap-PG1501

A201 Request for examination
P11-X000 Amendment of application requested

St.27 status event code: A-2-2-P10-P11-nap-X000

P13-X000 Application amended

St.27 status event code: A-2-2-P10-P13-nap-X000

PA0201 Request for examination

St.27 status event code: A-1-2-D10-D11-exm-PA0201

E902 Notification of reason for refusal
PE0902 Notice of grounds for rejection

St.27 status event code: A-1-2-D10-D21-exm-PE0902

P11-X000 Amendment of application requested

St.27 status event code: A-2-2-P10-P11-nap-X000

P13-X000 Application amended

St.27 status event code: A-2-2-P10-P13-nap-X000

E902 Notification of reason for refusal
PE0902 Notice of grounds for rejection

St.27 status event code: A-1-2-D10-D21-exm-PE0902

E13-X000 Pre-grant limitation requested

St.27 status event code: A-2-3-E10-E13-lim-X000

P11-X000 Amendment of application requested

St.27 status event code: A-2-2-P10-P11-nap-X000

P13-X000 Application amended

St.27 status event code: A-2-2-P10-P13-nap-X000

E701 Decision to grant or registration of patent right
PE0701 Decision of registration

St.27 status event code: A-1-2-D10-D22-exm-PE0701

GRNT Written decision to grant
PR0701 Registration of establishment

St.27 status event code: A-2-4-F10-F11-exm-PR0701

PR1002 Payment of registration fee

Fee payment year number: 1

St.27 status event code: A-2-2-U10-U11-oth-PR1002

PG1601 Publication of registration

St.27 status event code: A-4-4-Q10-Q13-nap-PG1601

PR1001 Payment of annual fee

Fee payment year number: 4

St.27 status event code: A-4-4-U10-U11-oth-PR1001

PR1001 Payment of annual fee

Fee payment year number: 5

St.27 status event code: A-4-4-U10-U11-oth-PR1001

FPAY Annual fee payment

Payment date: 20130523

Year of fee payment: 6

PR1001 Payment of annual fee

Fee payment year number: 6

St.27 status event code: A-4-4-U10-U11-oth-PR1001

FPAY Annual fee payment

Payment date: 20140526

Year of fee payment: 7

PR1001 Payment of annual fee

Fee payment year number: 7

St.27 status event code: A-4-4-U10-U11-oth-PR1001

FPAY Annual fee payment

Payment date: 20150522

Year of fee payment: 8

PR1001 Payment of annual fee

Fee payment year number: 8

St.27 status event code: A-4-4-U10-U11-oth-PR1001

R18-X000 Changes to party contact information recorded

St.27 status event code: A-5-5-R10-R18-oth-X000

R18-X000 Changes to party contact information recorded

St.27 status event code: A-5-5-R10-R18-oth-X000

FPAY Annual fee payment

Payment date: 20160525

Year of fee payment: 9

PR1001 Payment of annual fee

Fee payment year number: 9

St.27 status event code: A-4-4-U10-U11-oth-PR1001

FPAY Annual fee payment

Payment date: 20170526

Year of fee payment: 10

PR1001 Payment of annual fee

Fee payment year number: 10

St.27 status event code: A-4-4-U10-U11-oth-PR1001

LAPS Lapse due to unpaid annual fee
PC1903 Unpaid annual fee

Not in force date: 20180604

Payment event data comment text: Termination Category : DEFAULT_OF_REGISTRATION_FEE

St.27 status event code: A-4-4-U10-U13-oth-PC1903

PC1903 Unpaid annual fee

Ip right cessation event data comment text: Termination Category : DEFAULT_OF_REGISTRATION_FEE

Not in force date: 20180604

St.27 status event code: N-4-6-H10-H13-oth-PC1903

R18-X000 Changes to party contact information recorded

St.27 status event code: A-5-5-R10-R18-oth-X000

R18-X000 Changes to party contact information recorded

St.27 status event code: A-5-5-R10-R18-oth-X000

R18-X000 Changes to party contact information recorded

St.27 status event code: A-5-5-R10-R18-oth-X000