An aircraft landing gear assembly 1 is disclosed. The assembly comprises a wheel 10, a disc brake 20 comprising one or more discs 21, 22 and a filter 30. The disc brake is operable to inhibit rotation of said wheel 10 during a braking event thereby resulti...

A chin ring heat shield for a wheel assembly arranged to provide a shield between convection and radiation heat from braking components and a tyre of the wheel assembly, the chin ring comprising a first, radially extending, flat portion extending from a fi...

The wheel (1) has a brake stop fastened to a rim (2), and a brake disk fastened to the brake stop. Pivotably-supported plate-shaped covering elements (4) for temporary closing rim-sided through holes are provided at the rim. The covering elements are conne...

The device has blades (3) integrated with a tapered ring (31) to form a crown (30) whose symmetrical axis is merged with the rotational axis of a wheel. Inner surface (311) of the ring cooperates with the blades and with the surface of a rim (2), to create...

The wheel (1) for a motor vehicle is equipped with a rotating component (11) which is fitted on the wheel via a center bearing (10) to rotate freely. The rotating component is installed on the outer side of the wheel and is dynamically balanced in its cons...