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Bearingless tail rotor for helicopters

机译:直升机的无轴承尾桨

摘要

A helicopter tail rotor structure includes a thin, flat, tension- bearing strap of fibers extending spanwise, and is to be centrally secured by a hub to a helicopter tail mast. Flex sections are formed inboard of substantially equally divided portions of said fibers which extend as top and bottom blade spars from the outboard margins of the flex sections. Preferably, the planes of the flex sections and the planes of the spars are oriented at predetermined nose-up twist angles, one relative to the other.
机译:直升飞机的尾桨结构包括一个薄的,扁平的,张紧的纤维拉伸带,它们沿翼展方向延伸,并通过轮毂在中心固定到直升飞机的尾桅杆上。挠曲部分形成在所述纤维的基本上等分的部分的内侧,所述纤维作为挠曲部分的顶部和底部从挠曲部分的外侧边缘延伸。优选地,挠曲部分的平面和翼梁的平面以预定的鼻翼向上扭转角定向,一个相对于另一个。

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