首页> 外国专利> Manufacturing procedure for helicopter tail structure with aperture for tail rotor uses side panels made from composition material with reinforced organic matrix

Manufacturing procedure for helicopter tail structure with aperture for tail rotor uses side panels made from composition material with reinforced organic matrix

机译:带有尾桨孔的直升机尾桨结构的制造程序使用由增强有机基质合成材料制成的侧板

摘要

The procedure for making a helicopter tail structure (43) with a rotor aperture lined by a ring (63) with two end collars or flanges (66, 70) uses two curved side panels (45) made from a composition material with an organic matrix and reinforcing elements, fixed together by solidifying the matrix. The reinforcing elements are pre-impregnated with resin to form side panel pre-forms that are moulded under pressure. The panel preforms are made from thermoplastic resin-impregnated fibres or fabric and are co-hardened to form a shell to receive the rotor ring.
机译:制作直升机尾翼结构(43)的步骤是,转子尾孔由环(63)衬里,该环带有两个端环或凸缘(66、70),其使用两个由带有有机基质的合成材料制成的弯曲侧板(45)和加固元件,通过固化基质固定在一起。增强元件被树脂预浸渍以形成侧板预成型件,其在压力下被模制。面板预成型件由热塑性树脂浸渍的纤维或织物制成,并共同硬化以形成用于容纳转子环的壳体。

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