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对某型机复合材料机翼蒙皮的结构、材料进行分析,制定了某型机机翼蒙皮的铺带制造工艺方案。通过精确铺放控制设计、同向铺带与交叉异向铺带设计、自动铺放与激光投影、自动下料技术配合使用,成功将铺带机技术应用于某型机复合材料机翼蒙皮的制造,制造出的机翼蒙皮,其无损检测内部质量合格,铺带间隙和表面质量满足设计要求,为铺带机技术在复合材料铺带的应用奠定了坚实的基础。
The structure and material of the skin of a composite aircraft wing are analyzed, and the manufacturing scheme of the wing skin of a certain type of machine is established. Through the precise placement control design, the same direction with the tape and the cross-paving design, automatic placement and laser projection, automatic cutting technology with the successful use of tape machine technology applied to a machine composite wing skin , The quality of the non-destructive testing of the inner skin of the fabricated wing skin is met, and the design requirements are met with the clearance and the surface quality, laying a solid foundation for the application of the tape laying technology in the composite material spreading.