发明名称 AIRCRAFT, HAVING A PAIR OF COUNTER ROTATING ROTORS
摘要 The aircraft has a pair of rotors driven to counterrotate within a housing. Said housing has adjustable air guiding means for the rotor stream and an airfoil-like outer shape to generate lift at horizontal flight. The air guiding means comprise a circulate 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. Said air guiding means allow a precise and easy control of the aircraft maneuvers. 27
申请公布号 CA2014774(A1) 申请公布日期 1990.10.19
申请号 CA19902014774 申请日期 1990.04.18
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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