| 发明名称 | Nose landing gear arrangement for aircraft and method of assembly | ||
| 摘要 | A nose landing gear arrangement for an aircraft and a method of assembling the nose landing gear arrangement are disclosed herein. The nose landing gear arrangement includes, but is not limited to, a wheel assembly, a shock strut extending upwards from the wheel assembly towards a fuselage of the aircraft, and a torque arm assembly coupled to the wheel assembly and to the shock strut. The torque arm assembly is configured to transmit torque to the wheel assembly. The torque arm assembly is disposed forward of the shock strut with respect to a direction of travel of the aircraft. | ||
| 申请公布号 | US9302767(B2) | 申请公布日期 | 2016.04.05 |
| 申请号 | US201213674303 | 申请日期 | 2012.11.12 |
| 申请人 | Gulfstream Aerospace Corporation | 发明人 | Cook Brian G.;Louis John;Ven Thomas Van de;Vieito Robert M. |
| 分类号 | B64C25/00;B64C25/16;B64C25/14 | 主分类号 | B64C25/00 |
| 代理机构 | Ingrassia, Fisher & Lorenz PC | 代理人 | Ingrassia, Fisher & Lorenz PC |
| 主权项 | 1. A nose landing gear arrangement for an aircraft, the nose landing gear arrangement comprising: a wheel assembly configured for use with the nose landing gear arrangement; a shock strut extending upwards from the wheel assembly towards a fuselage of the aircraft; and a torque arm assembly coupled to the wheel assembly and to the shock strut, the torque arm assembly configured to transmit torque to the wheel assembly, the torque arm assembly being disposed forward of the shock strut with respect to a direction of travel of the aircraft, the torque arm assembly having a width that tapers along a substantial length of the torque arm assembly, the torque arm assembly having a concave cross-section with respect to a direction opposite the direction of travel of the aircraft, and the shock strut being disposed at least partially within a recess formed by the concave cross-section. | ||
| 地址 | Savannah GA US | ||