An aircraft landing gear arrangement comprises a nose landing gear assembly (18) and at least one main landing gear assembly (20). The nose landing gear assembly (18) has a nose landing gear wheel (26) with a high energy brake apparatus therein. The main landing gear assembly has a main landing gear wheel (32b) with a high energy brake apparatus therein and a main landing gear wheel (32a) with a motor (44) therein. The motor is used for driving the main landing wheel during taxiing of the aircraft.


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    Title :

    Aircraft landing gear arrangement


    Contributors:

    Publication date :

    2015-08-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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