JP2019532871A5 - - Google Patents

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Publication number
JP2019532871A5
JP2019532871A5 JP2019523033A JP2019523033A JP2019532871A5 JP 2019532871 A5 JP2019532871 A5 JP 2019532871A5 JP 2019523033 A JP2019523033 A JP 2019523033A JP 2019523033 A JP2019523033 A JP 2019523033A JP 2019532871 A5 JP2019532871 A5 JP 2019532871A5
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Japan
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wing
aerial vehicle
rotor
spin axis
angle
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JP2019523033A
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English (en)
Japanese (ja)
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JP2019532871A (ja
JP7173665B2 (ja
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Priority claimed from PCT/US2017/059809 external-priority patent/WO2018151777A1/en
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Publication of JP2019532871A5 publication Critical patent/JP2019532871A5/ja
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JP2019523033A 2016-11-02 2017-11-02 ロータを使用して空気力学上で一般的な剛体翼として疑似的に機能する垂直離着陸航空機 Active JP7173665B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201662416168P 2016-11-02 2016-11-02
US62/416,168 2016-11-02
PCT/US2017/059809 WO2018151777A1 (en) 2016-11-02 2017-11-02 Vtol aircraft using rotors to simulate rigid wing dynamics

Publications (3)

Publication Number Publication Date
JP2019532871A JP2019532871A (ja) 2019-11-14
JP2019532871A5 true JP2019532871A5 (enExample) 2020-12-17
JP7173665B2 JP7173665B2 (ja) 2022-11-16

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JP2019523033A Active JP7173665B2 (ja) 2016-11-02 2017-11-02 ロータを使用して空気力学上で一般的な剛体翼として疑似的に機能する垂直離着陸航空機

Country Status (11)

Country Link
US (4) US11130566B2 (enExample)
EP (3) EP3535185B1 (enExample)
JP (1) JP7173665B2 (enExample)
KR (1) KR102471407B1 (enExample)
CN (2) CN116714761A (enExample)
AU (1) AU2017399688A1 (enExample)
BR (1) BR112019008925A2 (enExample)
CA (1) CA3042517A1 (enExample)
IL (1) IL266371A (enExample)
MX (1) MX2019005061A (enExample)
WO (1) WO2018151777A1 (enExample)

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