The invention discloses a wing anti-icing system test system. A plurality of temperature transmitters and pressure transmitters are additionally arranged on a wing anti-icing system test bed according to process requirements and test requirements; a vortex shedding flowmeter is arranged at the front end of an inlet valve of the whole wing anti-icing system and is used for testing the high-temperature and high-pressure gas flow; the wing anti-icing system exciter collects output parameters of the additionally arranged temperature transmitter and pressure transmitter, and simulates an aircraft flight control system to provide various control signals and alarm signals to the anti-icing system controller on the wing anti-icing system test bed; the industrial personal computer is in real-time communication with the wing anti-icing system exciter through an industrial Ethernet, and test parameters on the wing anti-icing system test bench are displayed on the industrial personal computer through configuration software installed on the industrial personal computer; and the change curve of each parameter is displayed by using a real-time curve graph. The function division is simple and clear, the response speed of the working parameters of the induction anti-icing system is high, and the resolution ratio is high.

    本发明公开了一种机翼防冰系统测试系统。在机翼防冰系统试验台架上根据工艺要求和测试需要,加装多个温度变送器和压力变送器;在整个机翼防冰系统进口活门前端布置涡街流量计,用于测试高温高压气体流量;机翼防冰系统激励器采集加装的温度变送器和压力变送器的输出参数,同时模拟飞机飞控系统提供给机翼防冰系统试验台架上的防冰系统控制器各种控制信号及报警信号;工控机利用工业以太网与机翼防冰系统激励器进行实时通讯,工控机上通过安装的组态软件显示机翼防冰系统试验台架上的试验参数;且用实时曲线图,显示各参数的变化曲线。本发明功能分区简洁明了、感应防冰系统工作参数响应速度快、分辨率高。


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    Titel :

    Wing anti-icing system test system


    Weitere Titelangaben:

    一种机翼防冰系统测试系统


    Beteiligte:
    WANG JIA (Autor:in) / LIAO YOUMING (Autor:in) / TAN YOUAN (Autor:in)

    Erscheinungsdatum :

    2023-06-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen



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