The invention relates to the technical field of aircrafts, in particular to an aircraft flight electronic control system which comprises a system body and a control panel and further comprises a heat dissipation assembly, the heat dissipation assembly comprises a heat dissipation pipeline, a supporting frame, heat dissipation fan blades and a driving component, the heat dissipation pipeline is fixedly connected with the system body, and the supporting frame is fixedly connected with the heat dissipation pipeline. The heat dissipation fan blades are connected with the supporting frame through the driving component, the driving component is arranged on the supporting frame and connected with the heat dissipation fan blades, the heat dissipation fan blades rotate at a high speed so that air with heat generated by operation in the system body can be rapidly discharged through the heat dissipation pipeline, and then a large amount of heat is prevented from being accumulated in the system body; and the influence of heat accumulation on the overall normal operation in the system body is prevented.

    本发明涉及航空器技术领域,具体涉及一种飞机飞行电控系统,包括系统本体和控制面板,还包括散热组件,散热组件包括散热管道、支撑架、散热扇叶和驱动构件,散热管道与系统本体固定连接,支撑架与散热管道固定连接,散热扇叶与支撑架通过驱动构件连接,驱动构件设置在支撑架上,并与散热扇叶连接,通过散热扇叶高速转动能够将系统本体内运行所产生的带有热量的空气通过散热管道快速进行排出,进而避免大量的热量堆积到系统本体内,防止热量堆积对系统本体内整体的正常运行造成影响。


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    Title :

    Airplane flight electronic control system


    Additional title:

    一种飞机飞行电控系统


    Contributors:
    LIU XIJUN (author) / AI HOULONG (author)

    Publication date :

    2023-08-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    H05K PRINTED CIRCUITS , Gedruckte Schaltungen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




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