Aircraft landing gear forward trunnion support assemblies and related methods are described herein. An example aircraft wing disclosed herein includes a rear spar having a rear side and a front side opposite the rear side and a forward trunnion support assembly. The forward trunnion support assembly includes first and second vertical support fittings coupled to the rear side of the rear spar, anda trunnion housing with a bearing. The trunnion housing is coupled between the first and second vertical support fittings. A central axis of the bearing is perpendicular to the rear side of the rear spar. The forward trunnion support assembly also includes a side load fitting disposed on the rear side of the rear spar. A first end of the side load fitting is coupled to the second vertical supportfitting, and a second end of the side load fitting is coupled to the rear spar.
本文描述了飞机起落架前耳轴支撑组件和相关方法。本文公开的一种实例性飞机机翼包括后翼梁和前耳轴支撑组件,后翼梁具有后侧和与后侧相对的前侧。前耳轴支撑组件包括联接到后翼梁的后侧的第一竖直支撑配件和第二竖直支撑配件,并包括具有轴承的耳轴壳体。耳轴壳体联接在第一竖直支撑配件和第二竖直支撑配件之间。轴承的中心轴线垂直于后翼梁的后侧。前耳轴支撑组件还包括设置在后翼梁的后侧上的侧负载配件。侧负载配件的第一端联接到第二竖直支撑配件,并且侧负载配件的第二端联接到后翼梁。
Aircraft wing and assembly method thereof
飞机机翼及其组装方法
2020-10-27
Patent
Electronic Resource
Chinese