发明名称 SINGLE-PILOT SUPERSONIC FIGHTER AIRCRAFT WITH FORWARD-SWEPT WING
摘要 FIELD: aviation. ^ SUBSTANCE: fighter features fuselage, undercarriage, two wings, power plant with two vectored-thrust turbojet engines, each of which is attached to the stabiliser fin wing with rearward-facing nozzle. Each wing is attached to the aircraft fuselage and consists of mobile sections retractable horizontally inside the fuselage along the axis parallel to the axial axis of fuselage. Fighter aircraft has also front stabiliser fin rotating horizontally along the fuselage axis, stabiliser fin with ailerons acting as a wing, rudder fin and cockpit with ejecting seat. ^ EFFECT: improved flight stability. ^ 2 cl, 16 dwg
申请公布号 RU2328412(C2) 申请公布日期 2008.07.10
申请号 RU20050132858 申请日期 2005.10.26
申请人 SIROTIN VALERIJ NIKOLAEVICH 发明人 SIROTIN VALERIJ NIKOLAEVICH
分类号 B64C30/00;B64C3/54 主分类号 B64C30/00
代理机构 代理人
主权项
地址