The invention discloses a flexible intelligent skin for spacecraft structure health monitoring and a development method, a plurality of sensor arrays such as strain, temperature, acceleration and ultrasound are used, the flexible skin is prepared through an integrated flexible packaging integration method, and the characteristics of being light, thin, flexible, small, special-shaped curved surfaces or narrow and small space conformal are considered. When in use, the device can be attached to the surface of a corresponding spacecraft structure like a band-aid, so that on-orbit state monitoring and space environment sensing of a spacecraft can be realized.

    本发明公开了一种航天器结构健康监测的柔性智能蒙皮及研制方法,使用应变、温度、加速度、超声等多个传感器阵列,通过一体化柔性封装集成的方法制备柔性蒙皮,兼顾轻、薄、柔、小、异型曲面或狭小空间共形的特点。本发明使用时可以像创可贴一样贴合在对应的航天器结构表面,即可实现对航天器在轨状态监测和空间环境感知。


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    Titel :

    Flexible intelligent skin for spacecraft structure health monitoring and development method


    Weitere Titelangaben:

    一种航天器结构健康监测的柔性智能蒙皮及研制方法


    Beteiligte:
    ZHANG YAO (Autor:in) / WANG PENGFEI (Autor:in) / JIA YI (Autor:in) / LI ZHEN (Autor:in) / JI WEI (Autor:in) / LI MENGZHU (Autor:in) / CHENG YANGYANG (Autor:in) / WANG WEIHUA (Autor:in) / FAN YANYAN (Autor:in) / KONG YA (Autor:in)

    Erscheinungsdatum :

    2024-04-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein



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