Unmanned aerial vehicle with thrust mechanism of amplification and cooling device

具有推力放大机构和冷却装置的无人机

Abstract

本实用新型公开了一种具有推力放大机构和冷却装置的无人机,包括机身、主旋翼、尾旋翼、舵机、发动机和减速箱,所述减速箱与所述发动机连接,所述具有推力放大机构和冷却装置的无人机还包括:推力放大机构,所述推力放大机构与所述舵机连接,以放大所述舵机产生的推力;冷却装置,所述冷却装置与所述减速箱连接。本实用新型解决了现有技术中舵机工作过程中具有能源消耗大的技术缺陷。
The utility model discloses an unmanned aerial vehicle with thrust mechanism of amplification and cooling device, including fuselage, main rotor, the tailspin wing, steering wheel, engine and reducing gear box, the reducing gear box with the engine is connected, unmanned aerial vehicle with thrust mechanism of amplification and cooling device still includes: the thrust mechanism of amplification, the thrust mechanism of amplification with the steering wheel is connected, in order to enlarge the thrust that the steering wheel produced, cooling device, cooling device with the reducing gear box is connected. The utility model provides a prior art centered rudder mechanic have the technical defect that the energy resource consumption is big as the in -process.

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