JP4068071B2 - ガスタービンエンジン組立体 - Google Patents

ガスタービンエンジン組立体 Download PDF

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Publication number
JP4068071B2
JP4068071B2 JP2004017793A JP2004017793A JP4068071B2 JP 4068071 B2 JP4068071 B2 JP 4068071B2 JP 2004017793 A JP2004017793 A JP 2004017793A JP 2004017793 A JP2004017793 A JP 2004017793A JP 4068071 B2 JP4068071 B2 JP 4068071B2
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JP
Japan
Prior art keywords
gas turbine
turbine engine
auxiliary power
power unit
bypass duct
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
JP2004017793A
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English (en)
Japanese (ja)
Other versions
JP2004232636A (ja
JP2004232636A5 (enExample
Inventor
ゲーリー・クレイグ・ヴォーレンウェーバー
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
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Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of JP2004232636A publication Critical patent/JP2004232636A/ja
Publication of JP2004232636A5 publication Critical patent/JP2004232636A5/ja
Application granted granted Critical
Publication of JP4068071B2 publication Critical patent/JP4068071B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/12—Plants including a gas turbine driving a compressor or a ducted fan characterised by having more than one gas turbine
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/50—Application for auxiliary power units (APU's)

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
JP2004017793A 2003-01-28 2004-01-27 ガスタービンエンジン組立体 Expired - Fee Related JP4068071B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/352,446 US6968674B2 (en) 2003-01-28 2003-01-28 Methods and apparatus for operating gas turbine engines

Publications (3)

Publication Number Publication Date
JP2004232636A JP2004232636A (ja) 2004-08-19
JP2004232636A5 JP2004232636A5 (enExample) 2007-03-15
JP4068071B2 true JP4068071B2 (ja) 2008-03-26

Family

ID=32655504

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2004017793A Expired - Fee Related JP4068071B2 (ja) 2003-01-28 2004-01-27 ガスタービンエンジン組立体

Country Status (4)

Country Link
US (1) US6968674B2 (enExample)
EP (1) EP1445449A3 (enExample)
JP (1) JP4068071B2 (enExample)
CA (1) CA2455222C (enExample)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7464533B2 (en) * 2003-01-28 2008-12-16 General Electric Company Apparatus for operating gas turbine engines
US7121078B2 (en) * 2003-01-28 2006-10-17 General Electric Company Methods and apparatus for operating gas turbine engines
US8127527B2 (en) * 2004-11-22 2012-03-06 General Electric Company Methods and systems for operating oxidizer systems
US7721554B2 (en) * 2006-02-02 2010-05-25 General Electric Company Aircraft auxiliary gas turbine engine and method for operating
US20070220900A1 (en) * 2006-03-27 2007-09-27 General Electric Company Auxiliary gas turbine engine assembly, aircraft component and controller
US7673459B2 (en) * 2006-04-05 2010-03-09 General Electric Company System and method for providing air to a compressor of an aircraft auxiliary gas turbine engine
US20070240426A1 (en) * 2006-04-12 2007-10-18 General Electric Company Mehtod and controller for operating a gas turbine engine
US20090025393A1 (en) * 2006-10-31 2009-01-29 Karl Edward Sheldon Auxiliary power unit assembly
US7707838B2 (en) * 2006-10-31 2010-05-04 General Electric Company Auxiliary power unit assembly
US7750521B2 (en) * 2006-12-07 2010-07-06 General Electric Company Double-sided starter/generator for aircrafts
US7963098B2 (en) * 2007-06-12 2011-06-21 United Technologies Corporation Composite duct assembly
US8511058B2 (en) * 2007-11-29 2013-08-20 United Technologies Corporation Convertible gas turbine propulsion system
US8061119B2 (en) 2007-11-29 2011-11-22 United Technologies Corporation Actuation mechanism for a convertible gas turbine propulsion system
US8127528B2 (en) * 2008-02-26 2012-03-06 United Technologies Corporation Auxiliary propulsor for a variable cycle gas turbine engine
US20100257837A1 (en) * 2009-04-14 2010-10-14 General Electric Company Systems involving hybrid power plants
US9297304B2 (en) * 2009-12-30 2016-03-29 Rolls-Royce North American Technologies, Inc. Gas turbine engine system with bleed air powered auxiliary engine
US8955335B2 (en) 2010-12-30 2015-02-17 Rolls-Royce Corporation System, propulsion system and vehicle
US8844266B1 (en) * 2011-10-03 2014-09-30 Florida Turbine Technologies, Inc. Variable bypass ratio augmented gas turbine engine
WO2013151909A1 (en) 2012-04-02 2013-10-10 Kraft Robert J Compressed air injection system method and apparatus for gas turbine engines
WO2014055717A1 (en) 2012-10-04 2014-04-10 Kraft Robert J Aero boost - gas turbine energy supplementing systems and efficient inlet cooling and heating, and methods of making and using the same
RU2694600C2 (ru) 2012-10-26 2019-07-16 ПАУЭРФЭЙЗ ЭлЭлСи Системы восполнения энергии и системы подогрева газовых турбин, а также способы их изготовления и использования
FR3004701B1 (fr) * 2013-04-22 2015-04-03 Snecma Dispositif de delestage des alternateurs d'un turboreacteur pendant ses accelerations
WO2016126506A1 (en) 2015-02-08 2016-08-11 Hyperloop Technologies, Inc. Low-pressure environment structures
US9599235B2 (en) 2015-02-08 2017-03-21 Hyperloop Technologies, Inc. Gate valves and airlocks for a transportation system
KR102490998B1 (ko) 2015-02-08 2023-01-26 하이퍼루프 테크놀로지스 인코퍼레이티드 수송 시스템
US9533697B2 (en) 2015-02-08 2017-01-03 Hyperloop Technologies, Inc. Deployable decelerator
WO2016126502A1 (en) * 2015-02-08 2016-08-11 Hyperloop Technologies, Inc Power supply system and method for a movable vehicle within a structure
US20210003072A1 (en) * 2018-12-04 2021-01-07 Look For The Power, Llc Rotary internal combustion engine
US10974844B2 (en) * 2019-01-29 2021-04-13 The Boeing Company Aircraft auxiliary power unit (APU) control system having speed compensation
EP4365426A1 (en) * 2022-11-04 2024-05-08 RTX Corporation Powerplant with multiple integrated gas turbine engines

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3659422A (en) * 1966-11-04 1972-05-02 North American Rockwell Method and apparatus for aircraft propulsion
US3517509A (en) * 1968-08-26 1970-06-30 North American Rockwell Integrated aircraft propulsion control system
US4192137A (en) 1977-03-04 1980-03-11 Canadian Patents And Development Limited Turboshaft engine
US4222233A (en) 1977-08-02 1980-09-16 General Electric Company Auxiliary lift propulsion system with oversized front fan
GB2161765B (en) * 1978-05-30 1986-07-02 Rolls Royce Gas turbine engine power plant
GB2074654A (en) * 1980-04-16 1981-11-04 Rolls Royce Remote power system for aircraft
US4631914A (en) 1985-02-25 1986-12-30 General Electric Company Gas turbine engine of improved thermal efficiency
US5160080A (en) 1990-10-01 1992-11-03 General Electric Company Gas turbine engine and method of operation for providing increased output shaft horsepower
US6305156B1 (en) * 1999-09-03 2001-10-23 Alliedsignal Inc. Integrated bleed air and engine starting system
JP3120113B1 (ja) * 1999-11-10 2000-12-25 科学技術庁航空宇宙技術研究所長 高速航空機用ジェットエンジン
US6415595B1 (en) * 2000-08-22 2002-07-09 Hamilton Sundstrand Corporation Integrated thermal management and coolant system for an aircraft
CA2329555A1 (en) * 2000-12-22 2002-06-22 Jose Albero Main propulsion engine system integrated with secondary power unit
US6457305B1 (en) 2001-02-07 2002-10-01 James R. Schierbaum Turbo shaft engine with acoustical compression flow amplifying ramjet
US6634596B2 (en) * 2001-02-16 2003-10-21 Jose Albero Aircraft system architecture

Also Published As

Publication number Publication date
CA2455222C (en) 2010-08-10
JP2004232636A (ja) 2004-08-19
US20040144096A1 (en) 2004-07-29
US6968674B2 (en) 2005-11-29
CA2455222A1 (en) 2004-07-28
EP1445449A2 (en) 2004-08-11
EP1445449A3 (en) 2005-04-20

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