发明名称 |
Vertical takeoff and landing (VTOL) air vehicle |
摘要 |
A flight control apparatus for fixed-wing aircraft includes a first port wing (115) and first starboard wing (120), a first port swash plate (145) coupled between a first port rotor 155) and first port electric motor (135), the first port electric 5 motor (135) coupled to the first port wing (115), and a first starboard swash plate (150) coupled between a first starboard rotor (130) and first starboard electric motor (140), the first starboard electric motor (140) coupled to the first starboard wing (120). |
申请公布号 |
AU2014293617(A1) |
申请公布日期 |
2015.12.03 |
申请号 |
AU20140293617 |
申请日期 |
2014.05.05 |
申请人 |
AEROVIRONMENT, INC. |
发明人 |
TAYLOR, DANA J.;TOKUMARU, PHILLIP T.;HIBBS, BART DEAN;PARKS, WILLIAM MARTIN;GANZER, DAVID WAYNE;FISHER, CHRISTOPHER EUGENE;MUKHERJEE, JASON SIDHARTHADEV;KING, JOSEPH FREDERICK |
分类号 |
B64C27/26;B64C5/02;B64C9/00;B64C25/00;B64C27/54;B64C29/00;B64C39/02;G05D1/08 |
主分类号 |
B64C27/26 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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