JP2013515914A5 - - Google Patents

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Publication number
JP2013515914A5
JP2013515914A5 JP2012547267A JP2012547267A JP2013515914A5 JP 2013515914 A5 JP2013515914 A5 JP 2013515914A5 JP 2012547267 A JP2012547267 A JP 2012547267A JP 2012547267 A JP2012547267 A JP 2012547267A JP 2013515914 A5 JP2013515914 A5 JP 2013515914A5
Authority
JP
Japan
Prior art keywords
power
shaft
flow path
gas turbine
shafts
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
JP2012547267A
Other languages
English (en)
Japanese (ja)
Other versions
JP2013515914A (ja
Filing date
Publication date
Priority claimed from US12/960,779 external-priority patent/US8966911B2/en
Application filed filed Critical
Publication of JP2013515914A publication Critical patent/JP2013515914A/ja
Publication of JP2013515914A5 publication Critical patent/JP2013515914A5/ja
Pending legal-status Critical Current

Links

JP2012547267A 2009-12-29 2010-12-29 高圧パワーオフテイクおよび低圧パワーオフテイクを備えるターボファンエンジン Pending JP2013515914A (ja)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US29072609P 2009-12-29 2009-12-29
US61/290,726 2009-12-29
US12/960,779 US8966911B2 (en) 2009-12-29 2010-12-06 Turbofan engine with HP and LP power off-takes
US12/960,779 2010-12-06
PCT/US2010/062372 WO2011090750A1 (en) 2009-12-29 2010-12-29 Turbofan engine with hp and lp power off-takes

Publications (2)

Publication Number Publication Date
JP2013515914A JP2013515914A (ja) 2013-05-09
JP2013515914A5 true JP2013515914A5 (enExample) 2014-01-23

Family

ID=44185807

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012547267A Pending JP2013515914A (ja) 2009-12-29 2010-12-29 高圧パワーオフテイクおよび低圧パワーオフテイクを備えるターボファンエンジン

Country Status (5)

Country Link
US (1) US8966911B2 (enExample)
EP (1) EP2519722B1 (enExample)
JP (1) JP2013515914A (enExample)
CA (1) CA2785976C (enExample)
WO (1) WO2011090750A1 (enExample)

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US11346427B2 (en) 2019-02-13 2022-05-31 Raytheon Technologies Corporation Accessory gearbox for gas turbine engine with variable transmission
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US11572838B2 (en) * 2020-09-29 2023-02-07 General Electric Company Accessory gearbox for a turbine engine
FR3119373B1 (fr) * 2021-02-01 2023-06-09 Safran Trans Systems Turbomachine pour un aeronef comprenant des machines electriques
US11268453B1 (en) 2021-03-17 2022-03-08 Pratt & Whitney Canada Corp. Lubrication system for aircraft engine reduction gearbox
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