FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular to the design of unmanned and remotely piloted aircraft. Aircraft power plant on two-hover suspension comprises external annular circuit with its rotation drive, internal contour in the form of a rod with a drive of its rotation, which is installed inside the outer annular circuit perpendicular to the axis of rotation of the external annular circuit. Engine with rotor is secured on inner circuit. Control unit is connected with rotary drives of external circular and internal circuits and rotor motor. Ends of internal circuit rod are connected via bearings with two diametrically opposite points inside external annular circuit. Engine with rotor is secured on mounting platform located in the middle of internal circuit rod.
EFFECT: possibility of increasing maneuvering characteristics, flight at different angles, fast change of direction of aircraft motion.
9 cl, 8 dwg
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Authors
Dates
2019-09-12—Published
2018-06-26—Filed