发明名称 VERTICAL TAKING-OFF/LANDING MACHINE WIN ROTOR (WING ROTARY)
摘要 PROBLEM TO BE SOLVED: To provide an aircraft with a simple structure and inexpensive body production cost in a vertical taking off/landing type aircraft capable of being driven by force of small horsepower and landing at any place. SOLUTION: A shaft is mounted to a front part of a wing and it is fixed to a drive device such as a chain or the like provided at both sides (or a central part) to make a rotary wing. A large number of rotary wings are installed with a distance gap that they are not overlapped and track walls having a bearing or the like for supporting the drive device in the rotatable state and supporting the wing at a rear part of the rotary wing are mounted to both sides (or a central part) of a flying object. A device capable of driving the chain or the like is separately installed at an appropriate position and when the chain is driven, lift by wind force is generated by rotating the respective rotary wings. The aircraft capable of approximately vertically taking off/landing can be provided. COPYRIGHT: (C)2007,JPO&INPIT
申请公布号 JP2006315642(A) 申请公布日期 2006.11.24
申请号 JP20050156343 申请日期 2005.04.26
申请人 IKESHIRO TATSUO 发明人 IKESHIRO TATSUO
分类号 B64C29/00 主分类号 B64C29/00
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