An aircraft landing gear arrangement (1, 101) is provided, comprising a wheel (2, 22), a brake (6) operable to inhibit rotation of said wheel, one or more fan blades (7a, 7b) rotatable to cool the brake, and a brushless DC motor (8) operable to rotate the one or more fan blades. An aircraft (100) comprising such a landing gear arrangement (1, 101) and a method (50) of cooling an aircraft landing gear brake are also provided.


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    Title :

    Aircraft landing gear arrangement


    Publication date :

    2021-11-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



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