DRONE Russian patent published in 2024 - IPC B64U10/00 B64U20/70 

FIELD: aviation.

SUBSTANCE: invention relates to unmanned aerial vehicles (UAV) of aircraft type, made in integral layout according to balancing scheme "canard". Unmanned aerial vehicle is made in integral layout according to balancing scheme "canard" and contains fuselage, all-moving front empennage with swept consoles, V-shaped vertical tail unit with trapezoidal keels, power plant in the form of one turbojet engine, ventral air intake, central fuselage cargo compartment, landing gear. At that, fuselage is smoothly conjugated with wing of complex shape, which is a combination of a delta wing of small aspect ratio and a swept wing of a moderate aspect ratio, and swept wing front and rear edges are mechanized. At the same time front empennage is made V-shaped and is installed on fuselage so that distance between the point at the middle of the root chord of the foresail and the point at the middle of the root chord of the swept wing when measured in the horizontal plane is not less than one length of the root chord of the swept wing.

EFFECT: improvement of drone flight characteristics.

2 cl, 2 dwg