JP2016121565A5 - - Google Patents

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Publication number
JP2016121565A5
JP2016121565A5 JP2014260582A JP2014260582A JP2016121565A5 JP 2016121565 A5 JP2016121565 A5 JP 2016121565A5 JP 2014260582 A JP2014260582 A JP 2014260582A JP 2014260582 A JP2014260582 A JP 2014260582A JP 2016121565 A5 JP2016121565 A5 JP 2016121565A5
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JP
Japan
Prior art keywords
aircraft
power transmission
transmission unit
fan
rotating shaft
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
JP2014260582A
Other languages
English (en)
Japanese (ja)
Other versions
JP6511265B2 (ja
JP2016121565A (ja
Filing date
Publication date
Application filed filed Critical
Priority to JP2014260582A priority Critical patent/JP6511265B2/ja
Priority claimed from JP2014260582A external-priority patent/JP6511265B2/ja
Priority to PCT/JP2015/005529 priority patent/WO2016103551A1/ja
Priority to US15/539,236 priority patent/US11566566B2/en
Priority to EP15872132.4A priority patent/EP3239499B1/en
Publication of JP2016121565A publication Critical patent/JP2016121565A/ja
Publication of JP2016121565A5 publication Critical patent/JP2016121565A5/ja
Application granted granted Critical
Publication of JP6511265B2 publication Critical patent/JP6511265B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2014260582A 2014-12-24 2014-12-24 航空機用エンジン装置 Active JP6511265B2 (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2014260582A JP6511265B2 (ja) 2014-12-24 2014-12-24 航空機用エンジン装置
PCT/JP2015/005529 WO2016103551A1 (ja) 2014-12-24 2015-11-04 航空機用エンジン装置
US15/539,236 US11566566B2 (en) 2014-12-24 2015-11-04 Aircraft engine power generator disposed inside of a stationary nose cone
EP15872132.4A EP3239499B1 (en) 2014-12-24 2015-11-04 Aircraft engine device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2014260582A JP6511265B2 (ja) 2014-12-24 2014-12-24 航空機用エンジン装置

Publications (3)

Publication Number Publication Date
JP2016121565A JP2016121565A (ja) 2016-07-07
JP2016121565A5 true JP2016121565A5 (enExample) 2018-02-08
JP6511265B2 JP6511265B2 (ja) 2019-05-15

Family

ID=56149628

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014260582A Active JP6511265B2 (ja) 2014-12-24 2014-12-24 航空機用エンジン装置

Country Status (4)

Country Link
US (1) US11566566B2 (enExample)
EP (1) EP3239499B1 (enExample)
JP (1) JP6511265B2 (enExample)
WO (1) WO2016103551A1 (enExample)

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US10883424B2 (en) 2016-07-19 2021-01-05 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine architecture
US11415063B2 (en) 2016-09-15 2022-08-16 Pratt & Whitney Canada Corp. Reverse-flow gas turbine engine
FR3054264B1 (fr) * 2016-07-25 2020-07-03 Safran Aircraft Engines Turbomachine a reducteur a train epicycloidal
US11022042B2 (en) 2016-08-29 2021-06-01 Rolls-Royce North American Technologies Inc. Aircraft having a gas turbine generator with power assist
US11035293B2 (en) 2016-09-15 2021-06-15 Pratt & Whitney Canada Corp. Reverse flow gas turbine engine with offset RGB
US10465611B2 (en) 2016-09-15 2019-11-05 Pratt & Whitney Canada Corp. Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
US10815899B2 (en) 2016-11-15 2020-10-27 Pratt & Whitney Canada Corp. Gas turbine engine accessories arrangement
US10808624B2 (en) 2017-02-09 2020-10-20 Pratt & Whitney Canada Corp. Turbine rotor with low over-speed requirements
US10746188B2 (en) 2017-03-14 2020-08-18 Pratt & Whitney Canada Corp. Inter-shaft bearing connected to a compressor boost system
US10801410B2 (en) * 2018-04-12 2020-10-13 Raytheon Technologies Corporation Thermal management of tail cone mounted generator
EP3587764A1 (en) * 2018-06-27 2020-01-01 Rolls-Royce Deutschland Ltd & Co KG Gas turbine
US11920479B2 (en) 2018-08-08 2024-03-05 Pratt & Whitney Canada Corp. Multi-engine system and method
US11162379B2 (en) * 2019-03-15 2021-11-02 Hamilton Sundstrand Corporation Temperature control device for tail cone mounted generator
US11541990B2 (en) * 2020-09-11 2023-01-03 Textron Innovations Inc. Single spoke spinner support
US11542874B2 (en) * 2020-10-20 2023-01-03 Honda Motor Co., Ltd. Gas turbine system and gas turbine power generator
US11719101B2 (en) 2021-08-14 2023-08-08 Pratt & Whitney Canada Corp. Mechanical drive shaft arrangements for tail cone generators
EP4148250B1 (en) 2021-09-08 2025-08-06 Rolls-Royce plc An improved gas turbine engine
GB2610569A (en) * 2021-09-08 2023-03-15 Rolls Royce Plc An improved gas turbine engine
EP4148263A1 (en) 2021-09-08 2023-03-15 Rolls-Royce plc An improved gas turbine engine
US12055094B1 (en) 2023-02-21 2024-08-06 General Electric Company Engine having an open fan with reduced boundary layer induced distortion
US12292004B1 (en) * 2024-01-12 2025-05-06 Rtx Corporation Component mounting and drive in a geared turbofan architecture

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GB2198791A (en) * 1986-08-20 1988-06-22 Rolls Royce Plc A geared turbofan gas turbine engine with a booster compressor
US4722666A (en) 1987-06-29 1988-02-02 United Technologies Corporation Nose cowl mounted oil lubricating and cooling system
US4934140A (en) 1988-05-13 1990-06-19 United Technologies Corporation Modular gas turbine engine
US6503056B2 (en) * 2001-04-24 2003-01-07 Honeywell International Inc. Heating device and method for deployable ram air turbine
US7448199B2 (en) * 2005-04-29 2008-11-11 General Electric Company Self powdered missile turbojet
DE102006015639A1 (de) * 2006-04-04 2007-10-11 Mtu Aero Engines Gmbh Strahltriebwerk mit Generatoreinheit
GB0821684D0 (en) * 2008-11-28 2008-12-31 Rolls Royce Plc Aeroengine starter/generator arrangement
US8881534B2 (en) * 2008-12-29 2014-11-11 Rolls-Royce Corporation Gas turbine engine shaft coupler
JP4700113B2 (ja) 2009-02-06 2011-06-15 川崎重工業株式会社 航空機用発電装置
US8375695B2 (en) * 2009-06-30 2013-02-19 General Electric Company Aircraft gas turbine engine counter-rotatable generator
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US9765861B2 (en) 2011-04-07 2017-09-19 Kawasaki Jukogyo Kabushiki Kaisha Sealing arrangement of accessory to aircraft engine
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