发明名称 Twin fuselage V/STOL aircraft
摘要 The V/STOL aircraft incorporates an engine in which the drive unit is an airscrew drive (5a). The airscrew drive has two sets of coaxial counter-running cyclically and collectively adjustable rotary blades.The airscrew drive can also have two coaxial counter-running propellers. The wing (3) between the two fuselages (1) can tilt until the propeller axis is vertical. It has control flaps arranged in the plane of the wing and control flaps arranged vertically to the plane of the wing. In addition, stabiliser fins are joined to the wing.
申请公布号 DE4443731(A1) 申请公布日期 1996.06.13
申请号 DE19944443731 申请日期 1994.12.08
申请人 DORNIER, CONRADO, 82229 SEEFELD, DE 发明人 DORNIER, CONRADO, 82229 SEEFELD, DE
分类号 B64C3/42;B64C29/00;B64C39/04;(IPC1-7):B64C29/00 主分类号 B64C3/42
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