The invention relates to an aircraft brake temperature measuring system and method. The system comprises an airplane wheel brake infrared thermal imager, a data acquisition memory and ground handheld terminal equipment. By means of the system, temperature field information of the airplane wheel brake assembly can be measured and obtained, the brake temperature information is sent to a cockpit to be displayed, and meanwhile, the brake temperature information can be transmitted to a ground handheld terminal for airplane wheel brake temperature field monitoring.

    本发明涉及一种飞机刹车温度测量系统和方法。该系统包括机轮刹车红外热像仪、数据采集存储器、以及地面手持终端设备。通过该系统,能够测量并获取机轮刹车组件的温度场信息,并将该刹车温度信息发送到驾驶舱进行显示,同时能够传输到地面手持终端进行机轮刹车温度场监测。


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    Title :

    Aircraft brake temperature measuring system and method


    Additional title:

    一种飞机刹车温度测量系统和方法


    Contributors:
    YANG HONG (author) / LI BING (author) / SUN KUI (author)

    Publication date :

    2021-11-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01J Messen der Intensität, der Geschwindigkeit, der spektralen Zusammensetzung, der Polarisation, der Phase oder der Pulscharakteristik von infrarotem, sichtbarem oder ultraviolettem Licht , MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRA-RED, VISIBLE OR ULTRA-VIOLET LIGHT / 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



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