FIELD: aeronautics.
SUBSTANCE: invention relates to the field of aerostats, in particular to pilotless aerial vehicle (PAVs). Aerostat includes a multi-copter, a gondola, ACS capsule, a battery compartment, cargo container grips, an orientation and tracking system. Multicopter consists of several sectacopters connected by locking devices, and a turntable located on the multicopter support frame, the gondola is located below. Body of the nacelle is made in the form of a bellows, with the ability to contract and expand, depending on the flight conditions. Inside the nacelle a pneumatic jack is installed between the gondola support frame and the multicopter support frame, under which the cargo container holds. On top of the multi-copter is an ACS capsule with flight parameters recorders, and above it is an orientation and tracking system. Part of the propellers is used to create a vertical lifting rod, the other part is the horizontal displacement propulsion engines, and the third part is windmills.
EFFECT: provided reduction in energy costs during maneuvering.
1 cl, 2 dwg
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Authors
Dates
2018-04-25—Published
2017-05-16—Filed