SINGLE-PILOT SUPERSONIC FIGHTER AIRCRAFT WITH FORWARD-SWEPT WING Russian patent published in 2008 - IPC B64C30/00 B64C3/54 

Abstract RU 2328412 C2

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

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RU 2 328 412 C2

Authors

Sirotin Valerij Nikolaevich

Dates

2008-07-10Published

2005-10-26Filed