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Air intake device with resettable plug for an unmanned aerial vehicle with an air-jet engine

机译:用于带有喷气发动机的无人机的带有可复位塞的进气装置

摘要

The utility model relates to aviation technology, to structural elements for unmanned aerial vehicle engines (hereinafter - UAVs), in particular to such as air intake devices and protective devices of various types of air-jet engines - turbojet, direct-flow, etc. Air intake device with a resettable plug for unmanned aerial vehicles an aircraft with an air-jet engine has a resettable plug at the entrance to the air intake device, a pyro-pusher with a gas generator located in metichnoy niche, which is the surface element of the air intake device for fixing the breakable element and the push piston, which end surface coincides with the outer surface of the air intake device. The pyro-pusher gas generator is located in one housing with the pyro-pusher parallel to the longitudinal axis of the pyro-pusher. The proposed technical solution can be used in aviation for air intake devices and protective devices for various types of UAV UAV. 3 n.p. f-ly, 4 ill.
机译:本实用新型涉及航空技术,涉及无人驾驶飞机发动机(以下简称UAV)的结构部件,尤其涉及各种喷气发动机的进气装置和保护装置-涡轮喷气,直流等。用于无人驾驶飞行器的带有可复位塞的进气装置具有喷气发动机的飞机在进气装置的入口处具有可复位塞,位于气孔利基处的带有气体发生器的热推阀是表面元件用于固定易碎元件和推动活塞的进气装置的端部,其端面与进气装置的外表面重合。焦炉气体发生器位于一个外壳内,焦炉平行于焦炉的纵轴。所提出的技术解决方案可以在航空中用于各种类型的无人机的进气装置和保护装置。下午3点F-ly,4病。

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