FIELD: aeronautics.
SUBSTANCE: invention relates to the field of aeronautical vehicles, in particular to unmanned aerial vehicles (UAVs). Aeronautical vehicle includes a multi-copter, a gondola, an automatic control system, a battery compartment, cargo container grips, an orientation and tracking system. In the front part of the ellipsoidal gondola is a capsule with a dome of vision and a parachute system. In the middle of the apparatus there is a solar battery on the gondola body, and in the tail section of the apparatus there are two windmills with vortex transducers, turbines and electric generators. Between the windmills is the battery compartment, under the gondola is the base plate with the grips of the cargo container, and on the multi-copter frame are fixed the instruments of space navigation and orientation on the terrain. In the center of the gondola on the base plate a pneumatic jib for changing the shape of the gondola and controlling the sail of the apparatus is installed.
EFFECT: increase in the carrying capacity, speed and reliability of the aircraft is ensured.
1 cl, 2 dwg
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Authors
Dates
2018-04-25—Published
2017-05-31—Filed