JP2016506335A5 - - Google Patents

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Publication number
JP2016506335A5
JP2016506335A5 JP2015549585A JP2015549585A JP2016506335A5 JP 2016506335 A5 JP2016506335 A5 JP 2016506335A5 JP 2015549585 A JP2015549585 A JP 2015549585A JP 2015549585 A JP2015549585 A JP 2015549585A JP 2016506335 A5 JP2016506335 A5 JP 2016506335A5
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JP
Japan
Prior art keywords
tail boom
tail
surface profile
modified
modifying
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
JP2015549585A
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English (en)
Japanese (ja)
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JP2016506335A (ja
JP6376667B2 (ja
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Publication date
Priority claimed from US13/871,710 external-priority patent/US8991747B2/en
Application filed filed Critical
Publication of JP2016506335A publication Critical patent/JP2016506335A/ja
Publication of JP2016506335A5 publication Critical patent/JP2016506335A5/ja
Application granted granted Critical
Publication of JP6376667B2 publication Critical patent/JP6376667B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2015549585A 2012-12-18 2013-12-17 航空機安定化システム及びそれにより航空機を修正する方法 Active JP6376667B2 (ja)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US201261738663P 2012-12-18 2012-12-18
US61/738,663 2012-12-18
US13/871,710 US8991747B2 (en) 2012-12-18 2013-04-26 Aircraft stabilization systems and methods of modifying an aircraft with the same
US13/871,710 2013-04-26
PCT/US2013/075783 WO2014123627A2 (en) 2012-12-18 2013-12-17 Aircraft stabilization systems and methods of modifying an aircraft with the same

Publications (3)

Publication Number Publication Date
JP2016506335A JP2016506335A (ja) 2016-03-03
JP2016506335A5 true JP2016506335A5 (enExample) 2017-02-09
JP6376667B2 JP6376667B2 (ja) 2018-08-22

Family

ID=50929804

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015549585A Active JP6376667B2 (ja) 2012-12-18 2013-12-17 航空機安定化システム及びそれにより航空機を修正する方法

Country Status (6)

Country Link
US (1) US8991747B2 (enExample)
EP (1) EP2935002B1 (enExample)
JP (1) JP6376667B2 (enExample)
KR (1) KR102144145B1 (enExample)
ES (1) ES2731631T3 (enExample)
WO (1) WO2014123627A2 (enExample)

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* Cited by examiner, † Cited by third party
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FR3023827B1 (fr) * 2014-07-16 2017-12-29 Airbus Helicopters Poutre de queue de giravion, et giravion
CN104859864A (zh) * 2015-04-03 2015-08-26 南京航空航天大学 一种直升机旋翼流场显示介质发生、存储及输运装置
US10279899B2 (en) 2015-07-02 2019-05-07 Blr Aerospace L.L.C. Helicopter with anti-torque system, related kit and methods
CN110654569B (zh) * 2019-09-29 2022-01-07 中国直升机设计研究所 一种直升机尾段疲劳试验载荷模拟简化方法
CN115783323B (zh) * 2022-12-08 2023-10-20 常州大学怀德学院 一种遥感成像的航拍无人机

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