JP2008132973A5 - - Google Patents

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Publication number
JP2008132973A5
JP2008132973A5 JP2007278709A JP2007278709A JP2008132973A5 JP 2008132973 A5 JP2008132973 A5 JP 2008132973A5 JP 2007278709 A JP2007278709 A JP 2007278709A JP 2007278709 A JP2007278709 A JP 2007278709A JP 2008132973 A5 JP2008132973 A5 JP 2008132973A5
Authority
JP
Japan
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
JP2007278709A
Other languages
Japanese (ja)
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JP2008132973A (ja
JP5325411B2 (ja
Filing date
Publication date
Priority claimed from US11/590,114 external-priority patent/US7707838B2/en
Application filed filed Critical
Publication of JP2008132973A publication Critical patent/JP2008132973A/ja
Publication of JP2008132973A5 publication Critical patent/JP2008132973A5/ja
Application granted granted Critical
Publication of JP5325411B2 publication Critical patent/JP5325411B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2007278709A 2006-10-31 2007-10-26 補助動力装置組立体 Expired - Fee Related JP5325411B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/590,114 2006-10-31
US11/590,114 US7707838B2 (en) 2006-10-31 2006-10-31 Auxiliary power unit assembly

Publications (3)

Publication Number Publication Date
JP2008132973A JP2008132973A (ja) 2008-06-12
JP2008132973A5 true JP2008132973A5 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 2010-12-02
JP5325411B2 JP5325411B2 (ja) 2013-10-23

Family

ID=39027573

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2007278709A Expired - Fee Related JP5325411B2 (ja) 2006-10-31 2007-10-26 補助動力装置組立体

Country Status (6)

Country Link
US (1) US7707838B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
EP (1) EP1918200B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP (1) JP5325411B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
CN (1) CN101172520B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
CA (1) CA2606739C (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE602007009347D1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

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US7721554B2 (en) * 2006-02-02 2010-05-25 General Electric Company Aircraft auxiliary gas turbine engine and method for operating
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
US8015826B2 (en) * 2007-04-05 2011-09-13 Siemens Energy, Inc. Engine brake for part load CO reduction
US8480460B2 (en) * 2007-10-01 2013-07-09 United Technologies Corporation Cabin air supercharged aircraft internal combustion engine
CA2762184A1 (en) 2009-05-12 2010-11-18 Icr Turbine Engine Corporation Gas turbine energy storage and conversion system
US8866334B2 (en) 2010-03-02 2014-10-21 Icr Turbine Engine Corporation Dispatchable power from a renewable energy facility
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
CA2813680A1 (en) 2010-09-03 2012-03-08 Icr Turbine Engine Corporation Gas turbine engine configurations
US8256571B1 (en) 2010-10-29 2012-09-04 Butler Boyd L Frequency-modifying muffler
US8746401B2 (en) 2010-10-29 2014-06-10 Boyd L. Butler Frequency-modifying muffler
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
FR2986780B1 (fr) * 2012-02-13 2014-11-14 Motorisations Aeronautiques Dispositif d’alimentation en air d’un groupe auxiliaire de puissance d’un aeronef, aeronef
GB201202990D0 (en) * 2012-02-22 2012-04-04 Rolls Royce Plc An auxiliary power system
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
FR3001441B1 (fr) * 2013-01-29 2016-05-13 Microturbo Architecture d'alimentation en air d'un groupe auxiliaire de puissance dans un aeronef
FR3001442B1 (fr) * 2013-01-29 2016-05-20 Microturbo Architecture de fourniture de puissance electrique de secours amelioree dans un aeronef
US10208672B2 (en) 2015-02-09 2019-02-19 United Technologies Corporation Accumulator assisted gas turbine engine start system and methods therefor
GB201506517D0 (en) 2015-04-17 2015-06-03 Rolls Royce Plc Convergent-divergent nozzle
GB2541185A (en) * 2015-08-07 2017-02-15 Rolls Royce Plc Auxiliary power unit assembly and a method of using the same
US10823078B2 (en) 2017-06-28 2020-11-03 General Electric Company Systems and methods for starting a turbine engine
GB201712993D0 (en) * 2017-08-14 2017-09-27 Rolls Royce Plc Gas turbine engine
US10988262B2 (en) 2018-03-14 2021-04-27 Honeywell International Inc. Cabin pressure control system architecture using cabin pressure air for inlet to APU core compressor
US10951095B2 (en) 2018-08-01 2021-03-16 General Electric Company Electric machine arc path protection
US11332256B2 (en) 2018-08-21 2022-05-17 General Electric Company Fault tolerant hybrid electric propulsion system for an aerial vehicle
US11015480B2 (en) 2018-08-21 2021-05-25 General Electric Company Feed forward load sensing for hybrid electric systems
FR3085447B1 (fr) * 2018-09-04 2020-09-11 Safran Aircraft Engines Carter de soufflante pour une turbomachine d'aeronef integrant directement des portions abradable et ayant des proprietes acoustiques
US11027719B2 (en) 2018-12-03 2021-06-08 General Electric Company Distributed power generation for a vehicle system
US10988266B2 (en) * 2019-01-29 2021-04-27 The Boeing Company Aircraft auxiliary power unit (APU) control system having speed compensation
US11982239B2 (en) 2021-12-17 2024-05-14 Rolls-Royce North American Technologies Inc. Gas turbine engine system with mixed flow auxiliary power unit
CN116104647B (zh) * 2022-09-15 2023-09-08 南京航空航天大学 基于可调频的振荡型Ramp式涡流发生器的进气道设计方法

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US4118926A (en) * 1977-02-28 1978-10-10 United Technologies Corporation Automatic stall recovery system
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US20070220900A1 (en) * 2006-03-27 2007-09-27 General Electric Company Auxiliary gas turbine engine assembly, aircraft component and controller
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US7707838B2 (en) * 2006-10-31 2010-05-04 General Electric Company Auxiliary power unit assembly

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