AIRPLANE, FAST-SPEED ARROW WING AND FUEL SYSTEM Russian patent published in 2010 - IPC B64C39/00 B64C3/10 B64D37/04 

FIELD: air transport.

SUBSTANCE: airplane includes nose, front, central, rear and tail sections and fast-speed arrow wing with jet engines. Fast-speed arrow wing is characterised by change of maximum relative profile thickness, geometric twist angle, angle of lateral V wing under wing semispan and middle surface curvature both along semispan and profile chord. Fuel system includes reservoir of the airplane central section and reservoirs in outer wings near the central section at middle part and at the periphery. The central section is equipped with expandable walls. Fuel system provides initial use of fuel from central section reservoir, then from fuel tanks of outer wings located near central section and then from tanks at the periphery of outer wings, and after all the others - from the middle part of the wing by fuel transfer between tanks.

EFFECT: improvement of aerodynamic characteristics for planes with different weight and hull length.

22 cl, 54 dwg