The invention discloses a high-speed aircraft waste heat utilization system based on bionic heat pipes, a high-speed aircraft comprises a skin and an exhaust nozzle, bionic heat pipe sets are distributed on the inner surface of the skin and the outer surface of the exhaust nozzle, and each bionic heat pipe set comprises a plurality of bionic heat pipes; the bionic heat pipes fit the inner surface of the skin or the outer surface of the exhaust nozzle in shape, the bionic heat pipes are all connected with the waste heat utilization device, and the waste heat utilization device recovers heat of the skin and the pipe wall of the exhaust nozzle through the bionic heat pipes. Heat of the skin, the exhaust nozzle and the like is absorbed through the bionic heat pipe, waste heat recovery is conducted, heat is effectively recovered while high-temperature components are protected, energy is saved, environment friendliness is achieved, and economic benefits are high.

    本发明公开了一种基于仿生热管的高速飞行器余热利用系统,所述高速飞行器包括蒙皮和尾喷管,所述蒙皮内表面和尾喷管外表面布设有仿生热管组,所述仿生热管组包括若干仿生热管,所述仿生热管的形状贴合蒙皮内表面或尾喷管外表面,所述仿生热管均与余热利用装置连接,余热利用装置通过仿生热管回收蒙皮和尾喷管管壁的热量。通过仿生热管将蒙皮、尾喷管等热量吸收并进行余热回收,实现保护高温部件的同时有效回收热量,节能环保,经济效益高。


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    Titel :

    High-speed aircraft waste heat utilization system based on bionic heat pipe and high-speed aircraft


    Weitere Titelangaben:

    一种基于仿生热管的高速飞行器余热利用系统及高速飞行器


    Beteiligte:
    MAO JUNKUI (Autor:in) / HAN FENG (Autor:in) / ZHANG SHUHAO (Autor:in)

    Erscheinungsdatum :

    2023-12-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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