| 摘要 |
A dynamic bearing 10, 20 for an aircraft landing gear is provided. The bearing 10, 20 comprises a lug 12, 22; a shaft 16, 26 comprising a first material; and a bearing surface 14, 24 comprising a second material that is softer than the first material. The bearing surface 14, 24 defines a bore and is arranged to support the shaft 16, 26 when the shaft is movably housed within the bore in use. The bearing surface is defined by the lug 12 or a coating 24 applied to the lug. Various lubrication conduits 37, 38, 39, 47, 48, 49 may also be incorporated into the bearing for the passage of lubricant to the bearing surface. |
