发明名称 UNMANNED AIRCRAFT LANDING AND DEPARTING PERPENDICULARLY BY TILT WING MECHANISM
摘要 PROBLEM TO BE SOLVED: To provide an unmanned aircraft capable of landing and departing perpendicularly by a tilt wing mechanism and achieving advantages of both of a fixed wing aircraft and a helicopter by a simple mechanism because the fixed wing aircraft has high horizontal flight capability, but it requires a runway, thereby limiting its operation and the helicopter has high degree of freedom in its operation, but its cruising performance is inferior to that of the fixed wing aircraft. SOLUTION: This unmanned aircraft achieves horizontal flight capability and perpendicular leaving and departing capability by the simple mechanism by controlling a pair of main wings 2 provided to change their angles of mounting independently on the right and left sides, a main wing propeller 3, and a fuselage propeller 4. COPYRIGHT: (C)2011,JPO&INPIT
申请公布号 JP2010254264(A) 申请公布日期 2010.11.11
申请号 JP20090123582 申请日期 2009.04.24
申请人 YASUDA KENTA 发明人 YASUDA KENTA
分类号 B64C27/26;B64C13/18;B64C39/02 主分类号 B64C27/26
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