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.
Aircraft landing gear arrangement
2021-11-10
Patent
Electronic Resource
English