发明名称 Helicopter rotor blade arrangement - has vertical blade-carrying shaft continuously changing position, and blades twisting to keep same thrust direction
摘要 <p>The rotor has a wheel body rotating about a -substantially -vertical axis and carrying two propeller blades. The axis continuously changes position, and the blades are set with respect to each other and to the direction of advance and are controlled (twisted), so that over about three quarters of their rotation-cycle they produce thrust in - substantially - the same direction. The rotor is operable in both a vertical and a horizontal position.</p>
申请公布号 DE3049458(A1) 申请公布日期 1982.07.29
申请号 DE19803049458 申请日期 1980.12.30
申请人 KNOTT,FRANZ JOSEF 发明人 JOSEF KNOTT,FRANZ
分类号 B64C27/32;(IPC1-7):64C27/32 主分类号 B64C27/32
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