Ice may form along the leading edge of an aircraft wing or horizontal and vertical stabilizers. A pneumatic deicer system may be configured to inflate and dislodge ice along the leading edge of lift and control surfaces. The pneumatic deicer system may comprise a laser welded deicing boot attached to the leading edge. The compressed air can be directed to the deicing boot, inflating the deicing boot along inflatable tubes formed by laser welds, which can crack and dislodge the ice. A method of manufacturing a laser welded pneumatic deicer boot is also disclosed.


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    Title :

    LASER WELDED PNEUMATIC DEICER BOOTS FOR AIRCRAFT


    Additional title:

    DEGIVREURS PNEUMATIQUES SOUDES PAR LASER POUR UN AERONEF



    Publication date :

    2023-10-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B23K Löten , SOLDERING OR UNSOLDERING / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS



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