JP2019517412A5 - - Google Patents

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Publication number
JP2019517412A5
JP2019517412A5 JP2018562089A JP2018562089A JP2019517412A5 JP 2019517412 A5 JP2019517412 A5 JP 2019517412A5 JP 2018562089 A JP2018562089 A JP 2018562089A JP 2018562089 A JP2018562089 A JP 2018562089A JP 2019517412 A5 JP2019517412 A5 JP 2019517412A5
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Japan
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motor
vtol aircraft
motors
aircraft
starboard
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JP2018562089A
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Japanese (ja)
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JP6825011B2 (ja
JP2019517412A (ja
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Priority claimed from PCT/US2017/035742 external-priority patent/WO2017210595A2/en
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Publication of JP2019517412A5 publication Critical patent/JP2019517412A5/ja
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JP2018562089A 2016-06-03 2017-06-02 補完的な角度がついたロータを有する垂直離着陸用翼付き航空機 Active JP6825011B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201662345618P 2016-06-03 2016-06-03
US62/345,618 2016-06-03
PCT/US2017/035742 WO2017210595A2 (en) 2016-06-03 2017-06-02 Vertical take-off and landing (vtol) winged air vehicle with complementary angled rotors

Publications (3)

Publication Number Publication Date
JP2019517412A JP2019517412A (ja) 2019-06-24
JP2019517412A5 true JP2019517412A5 (enExample) 2020-07-09
JP6825011B2 JP6825011B2 (ja) 2021-02-03

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JP2018562089A Active JP6825011B2 (ja) 2016-06-03 2017-06-02 補完的な角度がついたロータを有する垂直離着陸用翼付き航空機

Country Status (9)

Country Link
US (5) US10370095B2 (enExample)
EP (1) EP3464064B1 (enExample)
JP (1) JP6825011B2 (enExample)
KR (1) KR102415393B1 (enExample)
CN (1) CN109562828A (enExample)
AU (1) AU2017272341B2 (enExample)
CA (1) CA3026260A1 (enExample)
DK (1) DK3464064T3 (enExample)
WO (1) WO2017210595A2 (enExample)

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