JP2004232636A5 - - Google Patents

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Publication number
JP2004232636A5
JP2004232636A5 JP2004017793A JP2004017793A JP2004232636A5 JP 2004232636 A5 JP2004232636 A5 JP 2004232636A5 JP 2004017793 A JP2004017793 A JP 2004017793A JP 2004017793 A JP2004017793 A JP 2004017793A JP 2004232636 A5 JP2004232636 A5 JP 2004232636A5
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JP
Japan
Prior art keywords
gas turbine
turbine engine
auxiliary power
exhaust port
power unit
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.)
Granted
Application number
JP2004017793A
Other languages
English (en)
Japanese (ja)
Other versions
JP2004232636A (ja
JP4068071B2 (ja
Filing date
Publication date
Priority claimed from US10/352,446 external-priority patent/US6968674B2/en
Application filed filed Critical
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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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 true JP2004232636A5 (enExample) 2007-03-15
JP4068071B2 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

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