| 发明名称 | Aircraft landing gear | ||
| 摘要 | An aircraft landing gear comprising: a shock-absorbing main leg having a sprung part for attachment to an aircraft and an un-sprung part including a slider and an axle carrying at least one wheel, the wheel having a toothed ring gear; a drive transmission mounted externally on the sprung part, or on the un-sprung part, of the main leg, the drive transmission having at least one motor and a drive pinion for meshing with the toothed ring of the wheel; and an actuator for lifting the drive transmission into and out of driving engagement with the toothed ring and for maintaining the driving engagement as the landing gear deflects during a ground taxiing operation. Also, a method of operating the aircraft landing gear. | ||
| 申请公布号 | US9428266(B2) | 申请公布日期 | 2016.08.30 |
| 申请号 | US201414178141 | 申请日期 | 2014.02.11 |
| 申请人 | AIRBUS OPERATIONS LIMITED;MICHELIN RECHERCHE ET TECHNIQUE SA;COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELIN | 发明人 | Wilson Fraser;Bedarrides Jeremy;Platagea Vladimir |
| 分类号 | B64C25/50;B64C25/40 | 主分类号 | B64C25/50 |
| 代理机构 | Hauptman Ham, LLP | 代理人 | Hauptman Ham, LLP |
| 主权项 | 1. An aircraft landing gear comprising: an axle carrying at least one wheel, the wheel having a hub and a toothed ring gear mounted to the hub; a drive transmission having at least one motor and a drive pinion for meshing with the toothed ring of the wheel; and an actuator for lifting via pivoting the drive transmission into and out of driving engagement with the toothed ring. | ||
| 地址 | Bristol GB | ||