JP2016104985A5 - - Google Patents

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Publication number
JP2016104985A5
JP2016104985A5 JP2015226213A JP2015226213A JP2016104985A5 JP 2016104985 A5 JP2016104985 A5 JP 2016104985A5 JP 2015226213 A JP2015226213 A JP 2015226213A JP 2015226213 A JP2015226213 A JP 2015226213A JP 2016104985 A5 JP2016104985 A5 JP 2016104985A5
Authority
JP
Japan
Prior art keywords
coupled
turbine engine
assembly
stationary component
engine assembly
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.)
Pending
Application number
JP2015226213A
Other languages
English (en)
Japanese (ja)
Other versions
JP2016104985A (ja
Filing date
Publication date
Priority claimed from US14/943,653 external-priority patent/US10518891B2/en
Application filed filed Critical
Publication of JP2016104985A publication Critical patent/JP2016104985A/ja
Publication of JP2016104985A5 publication Critical patent/JP2016104985A5/ja
Pending legal-status Critical Current

Links

JP2015226213A 2014-11-21 2015-11-19 タービンエンジン組立体及びその製造方法 Pending JP2016104985A (ja)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US201462082722P 2014-11-21 2014-11-21
US62/082,722 2014-11-21
US14/943,653 US10518891B2 (en) 2014-11-21 2015-11-17 Turbine engine assembly and method of manufacturing thereof
US14/943,653 2015-11-17

Publications (2)

Publication Number Publication Date
JP2016104985A JP2016104985A (ja) 2016-06-09
JP2016104985A5 true JP2016104985A5 (enExample) 2017-11-30

Family

ID=54697477

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015226213A Pending JP2016104985A (ja) 2014-11-21 2015-11-19 タービンエンジン組立体及びその製造方法

Country Status (6)

Country Link
US (2) US10518891B2 (enExample)
EP (1) EP3026213B1 (enExample)
JP (1) JP2016104985A (enExample)
CN (1) CN105715383B (enExample)
BR (1) BR102015029125A2 (enExample)
CA (1) CA2912395C (enExample)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10654577B2 (en) * 2017-02-22 2020-05-19 General Electric Company Rainbow flowpath low pressure turbine rotor assembly
US11156128B2 (en) 2018-08-22 2021-10-26 General Electric Company Embedded electric machine
US11420755B2 (en) * 2019-08-08 2022-08-23 General Electric Company Shape memory alloy isolator for a gas turbine engine
US12149154B2 (en) 2021-07-22 2024-11-19 General Electric Company Electric machine having a hybrid insulative-conductive manifold

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US3632222A (en) * 1970-10-21 1972-01-04 Avco Corp Damping means for differential gas turbine engine
FR2469566A1 (fr) * 1979-11-12 1981-05-22 Snecma Perfectionnements aux dispositifs de fixation de turboreacteurs multiflux
US4829850A (en) 1987-02-25 1989-05-16 Soloy Dual Pac, Inc. Multiple engine drive for single output shaft and combining gearbox therefor
US4875655A (en) * 1987-03-13 1989-10-24 General Electric Company Vibration isolating engine mount
US5390878A (en) * 1993-02-09 1995-02-21 Grumman Aerospace Corporation Strain isolator assembly
GB9305474D0 (en) 1993-03-17 1993-05-05 Jaguar Cars Gearbox mounting
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GB2375513B (en) * 2001-05-19 2005-03-23 Rolls Royce Plc A mounting arrangement for a gas turbine engine
US20030005705A1 (en) * 2001-07-05 2003-01-09 Honeywell International, Inc. Industrial gas turbine multi-axial thermal isolator
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FR2867158B1 (fr) * 2004-03-04 2007-06-08 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
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