发明名称 AIRCRAFT OF LIFTING FUSELAGE AERODYNAMIC CONFIGURATION WITH AERODYNAMIC STALL FENCES
摘要 aviation; passenger and transport aircraft of "lifting fuselage: aerodynamic configuration. SUBSTANCE: aircraft has fuselage in form of lifting surface at low aspect ratio and large relative thickness. Aircraft is provided with cabin for crew and payload, fuel tanks, power plant, control members and alighting gear. Lower surface of fuselage is provided with at least one pair of profiled fences. Profiled fences and control members are so arranged that effect of vortex sheet on control members is taken into account. Profiled fences may be mounted movably relative to fuselage. It is good practice to make fences detachable. Profiled fences may be formed by members of lower part of fuselage. EFFECT: improved stability and controllability; full use of lifting properties and maneuverability of aircraft. 4 cl, 3 dwg
申请公布号 RU2175298(C1) 申请公布日期 2001.10.27
申请号 RU20000126984 申请日期 2000.10.30
申请人 CHIGRIN OLEG RAFAEHLEVICH 发明人 CHIGRIN O.R.;CHIGRIN A.R.;CHIGRIN S.O.
分类号 B64C39/10;(IPC1-7):B64C39/10 主分类号 B64C39/10
代理机构 代理人
主权项
地址