For deicing an aircraft, a deicing system includes a base, a plurality of motorized wheel assemblies, a proximal deck and a distal deck, and a plurality of articulated arms. The base may have a length along the longitudinal axis that is substantially equivalent to a specified aircraft. The plurality of motorized wheel assemblies is disposed under the base. A movement direction of each wheel assembly is rotatable about a vertical axis. The plurality of articulated arms is disposed on the proximal deck in the distal deck. A shell is disposed on the end of each articulated arm. The plurality of motorized wheel assemblies moves the deicing system adjacent to the aircraft and the plurality of articulated arms each position a shell adjacent to the aircraft.


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    Title :

    AIRCRAFT DEICING SYSTEM


    Contributors:

    Publication date :

    2018-04-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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