FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to unmanned aerial vehicles (UAV) of aircraft type, made in integral layout according to balancing scheme "canard", with high speed and manoeuvring characteristics and low level of radar signature. Unmanned aerial vehicle is made in integral layout according to balancing scheme "canard", containing 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 the same time fuselage is smoothly conjugated with wing of complex shape, which is a combination of delta wing of small aspect ratio and swept wing of moderate elongation, and front and rear edges of swept wing are mechanized. Central fuselage cargo compartment comprises a longitudinal load-bearing wall passing in the middle of the compartment.
EFFECT: aim of the proposed technical solution is to achieve weight perfection of the UAV design.
1 cl, 2 dwg
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Authors
Dates
2025-02-13—Published
2024-05-02—Filed