JP2012127344A5 - - Google Patents

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Publication number
JP2012127344A5
JP2012127344A5 JP2011268581A JP2011268581A JP2012127344A5 JP 2012127344 A5 JP2012127344 A5 JP 2012127344A5 JP 2011268581 A JP2011268581 A JP 2011268581A JP 2011268581 A JP2011268581 A JP 2011268581A JP 2012127344 A5 JP2012127344 A5 JP 2012127344A5
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Japan
Prior art keywords
cowl
translational
assembly
operating position
fixed
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JP2011268581A
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English (en)
Japanese (ja)
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JP2012127344A (ja
JP5944153B2 (ja
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Priority claimed from US12/969,258 external-priority patent/US8713911B2/en
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Publication of JP2012127344A publication Critical patent/JP2012127344A/ja
Publication of JP2012127344A5 publication Critical patent/JP2012127344A5/ja
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Publication of JP5944153B2 publication Critical patent/JP5944153B2/ja
Expired - Fee Related legal-status Critical Current
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JP2011268581A 2010-12-15 2011-12-08 ターボファン推進システム用スラストリバーサの操作システム及び方法 Expired - Fee Related JP5944153B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/969,258 2010-12-15
US12/969,258 US8713911B2 (en) 2010-12-15 2010-12-15 System and method for operating a thrust reverser for a turbofan propulsion system

Publications (3)

Publication Number Publication Date
JP2012127344A JP2012127344A (ja) 2012-07-05
JP2012127344A5 true JP2012127344A5 (enExample) 2015-01-29
JP5944153B2 JP5944153B2 (ja) 2016-07-05

Family

ID=45346268

Family Applications (1)

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JP2011268581A Expired - Fee Related JP5944153B2 (ja) 2010-12-15 2011-12-08 ターボファン推進システム用スラストリバーサの操作システム及び方法

Country Status (6)

Country Link
US (1) US8713911B2 (enExample)
EP (1) EP2466101B1 (enExample)
JP (1) JP5944153B2 (enExample)
CN (1) CN102536513B (enExample)
BR (1) BRPI1105033A2 (enExample)
CA (1) CA2760086C (enExample)

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US11834189B2 (en) * 2020-04-09 2023-12-05 Gulfstream Aerospace Corporation Exhaust nozzle assembly, propulsion system employing the exhaust nozzle assembly, and aircraft employing the propulsion system
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