FIELD: aero-space engineering.
SUBSTANCE: proposed flying vehicle has fuselage, wings mounted in tandem in closed system and provided with control surfaces, vertical fins with rudders, horizontal lifting surface provided with rudder and secured on vertical fins and on fuselage, power plants and quick-detachable attachment units. Each closed system of wings includes fuselage, top, lower and intermediate wings, connecting fin washers at rational parametric convergence of wing dihedral angles and rational parameters of wing V-shaped angles. All together they form rigid flat load-bearing truss in cross-section relative to longitudinal axis of fuselage without excessive rods. Each part of flying vehicle is considered as one rod in said section. Connecting load-bearing articulation units of tips of top and intermediate wings and upper ends of connecting fin washers of each closed system of wings are provided with connecting load-bearing hinges embraced by upper port and starboard nacelles. Connecting load-bearing articulation units of lower wings which are located in tandem and lower tips of connecting fin washers are connected by means of lower starboard and port nacelles.
EFFECT: enhanced efficiency of flying vehicle configuration.
15 cl, 4 dwg
