The invention relates to the technical field of unmanned aerial vehicle power system heat dissipation, in particular to a rapid heat dissipation power range extender of a turboshaft engine, which comprises a main body component, a power assembly, a water cooling assembly fixed on one side of the power assembly and a transmission assembly sliding on the end face of the water cooling assembly, the heat dissipation assembly is fixed to the end face of the transmission assembly, the track assembly slides on the heat dissipation assembly, and the track assembly is connected with the water cooling assembly; the heat dissipation area and angle of the water cooling assembly and the power assembly can be increased through the transmission assembly, the heat dissipation assembly and the track assembly, so that the heat dissipation effect can be optimized in the limited internal space of the unmanned aerial vehicle shell, and fins are arranged on the outer wall of a heat conduction pipe, so that the contact area of the water cooling assembly is increased; in the operation process of the reinforcing part, cleaning and angle adjusting can be conducted on the heat conduction pipe and the outer walls of the fins, and therefore the heat dissipation efficiency is improved while the heat dissipation effect is kept.
本发明涉及无人机动力系统散热技术领域,尤其是涡轮轴发动机的快速散热动力增程器,包括,主体部件,其包括动力组件,以及固定于所述动力组件一侧的水冷组件,还包括滑移于所述水冷组件端面的传动组件,还包括固定于所述传动组件端面的散热组件,还包括滑移于所述散热组件上的轨道组件,所述轨道组件和水冷组件相连接;加强部件,本发明通过传动组件、散热组件和轨道组件可加大对水冷组件及动力组件的散热面积及角度,由此可在有限的无人机壳体内部空间内优化散热效果,并且通过导热管外壁具有翅片,从而提高了水冷组件的接触面积,在加强部件运作过程中,可对导热管和翅片外壁进行清理和角度调节,从而具有保持散热效果的同时,提高散热效率。
Rapid heat dissipation power range extender of turboshaft engine
一种涡轮轴发动机的快速散热动力增程器
13.05.2025
Patent
Elektronische Ressource
Chinesisch
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