FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to unmanned aerial vehicles. Remotely controlled combat device represents an unmanned aerial vehicle with an air propeller. Inside the propeller blade there is a channel open from the peripheral end, which serves as a guide for free movement of bullets along the blade. In the root zone of the blade there is a magazine for bullets and two controlled shutters performing controlled locking of bullets and located between each other at a distance exceeding the length of one bullet. There is also a mechanism for alternate controlled opening of said shutters when the next blade approaches a certain angular position in its rotation.
EFFECT: enabling increase in the total number of rounds of onboard ammunition per unit of take-off weight of an unmanned aerial vehicle with a warhead of a mechanical type, while maintaining optimal energy of destructive action and range.
4 cl, 4 dwg
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