Prototype autonomous deicing system for airplane includes network of electronic and electromechanical modules at various locations in wings and connected to central data-processing unit. Small, integrated solid-state device, using long coils installed under leading edge, exciting small vibrations to detect ice and larger vibrations to knock ice off. In extension of concept, outputs of vibration sensors and other sensors used to detect rivet-line fractures, fatigue cracks, and other potentially dangerous defects.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Autonomous Deicing System For Airplane Wing


    Contributors:

    Published in:

    Publication date :

    1993-10-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Airplane deicing method and deicing device

    GU XINGSHI / LIU QINGLIN / LIU SENYUN et al. | European Patent Office | 2022

    Free access

    Partitioned deicing method and system for airplane

    WANG YUAN / ZHU CHUNLING / ZHU CHENGXIANG et al. | European Patent Office | 2024

    Free access

    Reconfigurable intelligent airplane deicing system and method

    CUI JING / BAI JUAN / YUE MAOCHANG et al. | European Patent Office | 2023

    Free access

    Airplane ground mobile deicing operation mechanism, deicing method and computer equipment

    CHEN BIN / DING YU / LI WENHAO et al. | European Patent Office | 2023

    Free access

    Wing skin deicing device

    SUN XIAOGANG / ZHENG DIANMO / CAI MANYUAN et al. | European Patent Office | 2020

    Free access