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Tail assembly for a rotorcraft, rotorcraft and method of manufacture of a strengthened tail assembly

机译:旋翼飞机的尾翼组件,旋翼飞机和加强尾翼组件的制造方法

摘要

A tail assembly for a rotorcraft. The tail assembly is manufactured to include at least one transition structure provided in the tail assembly. The transition structure is longitudinally arranged between a longitudinal median boom portion and a tail fin. A power transmission shaft of the rotorcraft extends at least partly externally above a longitudinal median boom portion of the tail assembly. The transition structure includes at an entering region a cut-out elevation step, where is made a passing through opening for the power transmission shaft.
机译:旋翼机的尾部组件。尾部组件被制造为包括设置在尾部组件中的至少一个过渡结构。过渡结构沿纵向布置在纵向中间吊杆部分和尾鳍之间。旋翼飞行器的动力传动轴至少部分地在尾部组件的纵向中间吊臂部分上方向外延伸。过渡结构在进入区域包括切去的抬升台阶,在此形成用于动力传递轴的贯通开口。

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