FIELD: engine building.
SUBSTANCE: dropping nozzle plug of an air-jet engine of an unmanned aerial vehicle comprises a gas generator, a stopper, assemblies for separation, pipelines and brake aerodynamic shields. Proposed technical solution can be used in aviation as protective devices for nozzles of various types of UAV air-jet engines, intended for protection of inner cavities of nozzles and turbines of engines against ingress of dust, dirt and other foreign objects when using UAV on outer suspension of carrier in operation and especially during taxiing, takeoff and landing roll of carrier.
EFFECT: dropping nozzle plug of an air-jet engine is proposed.
5 cl, 6 dwg
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