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针对飞机复合材料机身蒙皮,应用ANSYS12.0建立了碳纤维复合材料层合板胶接修理和胶铆混合修理仿真模型,对比分析两种修理方式对修理效果的影响,并分析铆钉对胶铆混合修理胶层应力分布的影响。
For aircraft composite skin, ANSYS12.0 was used to establish the simulation model of adhesive bonding and plastic composite repair of carbon fiber composite laminates. The effect of the two repairing methods on the repairing effect was analyzed and compared. Repair the influence of the stress distribution of the glue layer.