一种用于飞机的复材连杆及成型方法
本发明公开了一种用于飞机的复材连杆及成型方法。连杆包括基体连杆,基体连杆呈圆柱形结构,其包括依次连接的中间段、两侧段和两端部;中间段为圆环形等截面结构,两侧段为圆环形变截面结构,两端部为耳片结构且耳片结构上开设有通孔。本发明通过整体编织与RTM成型一体化工艺,实现纤维连续分布,既避免传统机械连接的高装配工作量,又提升连接可靠性,解决了现有连杆零件多、装配繁琐或胶接可靠性不足的问题,适用于飞机承受拉压载荷部件的连接。
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