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发明公开
CN101811571A 封闭式复合材料锥形整流罩整体成型方法 无效 - 撤回

封闭式复合材料锥形整流罩整体成型方法
摘要：
本发明属于复合材料成型技术，涉及一种封闭式复合材料锥形整流罩零件的整体成型方法。成型的步骤如下：模具制造；整体铺层；更换成型工装；封制整体真空袋；固化成型。本发明既满足了整体铺层的要求，又能保证整流罩外表面的质量要求，满足了某型直升机的研制需要。
摘要（英）：

The invention belongs to composite material forming technologies and relates to an integrated forming method of a closed composite material taper fairing. The forming method comprises the steps of: die making, overall layering, formed frock replacing, integral vacuum bag sealing and solidifying and forming. The forming method not only meets the requirement of integral layering, but also reaches the quality requirement of the outer surface of the fairing and satisfies the development requirement of a certain type of helicopter.

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