The invention belongs to the field of structure health monitoring, and relates to a multi-parameter airborne structure health monitoring system. The multi-parameter airborne structure health monitoring system comprises a power switch, a power module, a main control module, a storage module, a bus communication module, a general electric signal acquisition module, an optical fiber demodulation module, a sensor, a transmission cable and a portable human-computer interface. The system can collect and store multiple bus signals, electric signals and optical signals at the same time, the signals can be downloaded and processed by a portable man-machine interface on the ground through a transmission cable, the problem of mutual reference among parameters is solved through unified processing of multiple parameters, a new solution is provided for health monitoring of an aircraft structure, and the system is suitable for popularization and application. And the external field structure health monitoring efficiency can be obviously improved.

    本发明属于结构健康监测领域,涉及一种多参量机载结构健康监测系统。本发明多参量机载结构健康监测系统包括电源开关、电源模块、主控模块、存储模块、总线通信模块、通用电信号采集模块、光纤解调模块、传感器、传输线缆、便携式人机界面组成。本系统可以同时采集多路总线信号、电信号、光信号并存储,通过传输电缆可由地面的便携式人机界面下载和处理,通过对多参量的统一处理,解决了参量间相互参考的问题,为飞机结构健康监测提供了一种新的解决方案,可显著提高外场结构健康监测效率。


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    Titel :

    Multi-parameter airborne structure health monitoring system


    Weitere Titelangaben:

    一种多参量机载结构健康监测系统


    Beteiligte:
    DU ZHENHUA (Autor:in) / YANG YU (Autor:in) / CHEN XIA (Autor:in) / HUANG BO (Autor:in) / TIAN YUAN (Autor:in) / LIU GUOQIANG (Autor:in)

    Erscheinungsdatum :

    2023-09-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein



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