发明名称 ROTOR STORAGE TYPE CIRCULAR AEROFOIL AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To provide a high-speed flight aircraft having a simple structure, requiring no complicated mechanism and enabling vertical take-off and landing. SOLUTION: During vertical take-off/landing and low-speed flight, a lift force is obtained by rotors 3 rotated together with a circular aerofoil 2. During high-speed flight, since flight is enabled only by the lift force of the circular aerofoil 2, by storing the rotors 3 inside the circular aerofoil 2, high-speed flight is enabled without being affected by the rotors 3. With such a simple structure as only to change a storage rate of the rotors 3 protruded from the circular aerofoil 2, a complicated mechanism is not required. COPYRIGHT: (C)2009,JPO&INPIT
申请公布号 JP2009190710(A) 申请公布日期 2009.08.27
申请号 JP20080061821 申请日期 2008.02.13
申请人 SAKAMOTO SHOICHI 发明人 SAKAMOTO SHOICHI
分类号 B64C39/06;B64C27/22 主分类号 B64C39/06
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