Patent ID: 9016620
Filing Date: 2015-04-28
Classification: B64C,Y02T

Abstract:
1. An aircraft landing gear arrangement comprising a nose landing gear assembly and at least one main landing gear assembly, the nose landing gear assembly having a nose landing gear wheel and a brake apparatus configured for rejected take-off braking, the nose landing gear wheel includes a hub offset relative to a rotational centreline of the wheel in an axial direction, and a rim co-axial with the hub and the brake apparatus fully disposed within the nose landing gear wheel, wherein the nose landing gear wheel comprises a first part and a second part attached to the first part, where the first part includes a cylindrical wall which is deeper than a cylindrical wall of the second part, the main landing gear assembly having a main landing gear wheel with a braking apparatus arranged therein and another main landing gear wheel with a motor arranged therein for driving that main landing gear wheel during taxiing of the aircraft.