发明名称 MULTI-SHAFT TYPE VERTICAL TAKEOFF AND LANDING AIRCRAFT AND CONTROL METHOD FOR IT
摘要 PROBLEM TO BE SOLVED: To provide a multi-shaft type vertical takeoff and landing aircraft directly fitted to the side of a high storied building in the levitation state to load and unload the cargo. SOLUTION: This multi-shaft type vertical takeoff and landing aircraft is provided with four variable pitch rotary blades inclined with the fitting angle of the rotary blade ranging from 80 to 90 degrees to a rotating shaft and the fitting angle of the rotating shaft ranging from 40 to 45 degrees. The aircraft is provided with a bearing slide mechanism for varying attack angle of the rotary blade. In order to control the attitude, attack angles of plural rotary blades can be set to be simultaneously varied.
申请公布号 JP2002154486(A) 申请公布日期 2002.05.28
申请号 JP20000396267 申请日期 2000.11.21
申请人 NAKAMURA MIKIO 发明人 NAKAMURA MIKIO
分类号 B64C27/08;B64C27/59;B64C27/80;(IPC1-7):B64C27/08 主分类号 B64C27/08
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