The invention belongs to the field of aircraft flight tests, and relates to a simulation electric load system for an aircraft engine airborne test. Comprising an air inlet, an air compressor, a motor, a plurality of one-way valves, a plurality of pipelines, an adjustable flow port, a resistance wire, an exhaust port, a display controller and a matched cable, the air inlet is communicated with the exhaust port through a first branch, the first branch comprises the pipelines and the one-way valves, the air inlet is communicated with the exhaust port through a second branch, and the second branch comprises the air compressor, the motor and the one-way valves. An inlet of the air compressor is communicated with the air inlet, an outlet of the air compressor is communicated with the interior of the exhaust port through a pipeline, a one-way valve is arranged on the pipeline where the air compressor is communicated with the interior of the exhaust port, an adjustable throttling port is formed in the pipeline inside the exhaust port, and a resistance wire is arranged in the pipeline inside the exhaust port. The output end of the motor is connected with a driving shaft of the air compressor, and the display controller is connected with the control end of the motor through a matched cable and used for controlling the motor.

    本发明属于飞行器飞行试验领域,涉及一种航空发动机机载试验用模拟电负载系统。包括:进气口、压气机、电动机、多个单向阀、多个管道、可调节流口、电阻丝、排气口、显示控制器、配套线缆,其中,进气口通过第一支路与排气口连通,第一支路包括管道和单向阀,进气口通过第二支路与排气口连通,第二支路包括压气机、电动机、单向阀,其中,压气机的进口与进气口连通,压气机的出口通过管路与排气口内部连通,压气机与排气口内部连通的管路上设置有单向阀,排气口内部管路上设置有可调节流口,排气口内部管路内设置有电阻丝,电动机的输出端与压气机的驱动轴连接,显示控制器与电动机的控制端通过配套线缆连接,用于控制电动机。


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    Title :

    Simulation electric load system for airborne test of aero-engine


    Additional title:

    一种航空发动机机载试验用模拟电负载系统


    Contributors:
    YAN PENGQING (author) / LI QUANXIANG (author) / ZHAO ZHEN (author) / YANG ZEDONG (author) / LYU WENJIE (author) / ZHAO XIAOYU (author)

    Publication date :

    2025-04-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Airborne system of digital electronic controller of aero-engine

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    Aero engine environment simulation

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    Aero engine environment simulation

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