发明名称 AIRCRAFT WITH A PAIR OF CONTRA-ROTATING PROPELLERS
摘要 The aircraft has a pair of rotors driven to counter-rotate within a housing. The housing has adjustable air guiding discuss for the rotor stream and a airfoil-like outer shape to generate lift at horizontal flight. The air guiding devices include a circular arrangement of a plurality of individual sectors having tangentially extending blades arranged in a zone below the rotors. In each sector the blades are adjustable in their position relative to the rotor stream. In at least some of the sectors, the blades are arranged in pairs for an adjusting movement in opposite relative sense. The air guiding devices allow precise and easy control of the aircraft maneuvers.
申请公布号 EP0393410(A3) 申请公布日期 1991.07.03
申请号 EP19900106212 申请日期 1990.03.31
申请人 BUCHER, FRANZ 发明人 BUCHER, FRANZ
分类号 B64C27/20;B64C27/10;B64C29/00;B64C39/00 主分类号 B64C27/20
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