FIELD: aviation.
SUBSTANCE: invention relates to aviation, in particular, to structures of unmanned aerial vehicles (UAV). Modular design of the UAV VTOL includes power element of carrier beam 2, rigidly placed inside main body (1), wing (6), power unit (5), and battery (16). Wing (6) is made solid, on each wing console there are pylons (7) with two lifting screws (8) for vertical take-off and landing. Power unit (5) is designed as main engine with propeller (9), which is located in front of the fuselage. Power composite beam (2), made in the form of a rectangular solid structure, inside which a truss filler is located, is included as a strength element. At the end of the power beam onboard equipment and tail are located.
EFFECT: increased efficiency of an aircraft of modular construction due to expansion of functional capabilities is provided.
1 cl, 4 dwg
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