首页> 外国专利> A FIBER REINFORCED/EPOXY MATRIX COMPOSITE HELICOPTER ROTOR MAIN HUB PLATE

A FIBER REINFORCED/EPOXY MATRIX COMPOSITE HELICOPTER ROTOR MAIN HUB PLATE

机译:纤维增强/环氧树脂基复合直升机旋翼主轮毂板

摘要

A helicopter hub main retention plate is described made up of graphite and glass fiber reinforced epoxy resin. The graphite fiber reinforcement is in-plane isotropically laid continuous graphite fibers and the glass fiber reinforcement comprises segments of fiberglass continuously and circumferentially wound around the areas of retention. Such materials and configuration provide crack resistance, damage tolerance, and integrity inspectability to the retention plate.
机译:描述了一种直升机轮毂主固定板,其由石墨和玻璃纤维增​​强的环氧树脂制成。石墨纤维增强物是面内各向同性地铺设的连续石墨纤维,并且玻璃纤维增​​强物包括连续且周向缠绕在保持区域周围的玻璃纤维段。这样的材料和构造为保持板提供了抗裂性,破坏耐受性和完整性检查性。

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