航空学报 > 2001, Vol. 22 Issue (5): 458-460

复合材料螺接修补参数优化

赵美英, 万小朋, 刘浩   

  1. 西北工业大学飞行器设计与工程系 陕西西安 710072
  • 收稿日期:2000-07-27 修回日期:2001-11-13 出版日期:2001-10-25 发布日期:2001-10-25

OPTIMIZATION OF COMPOSITE PATCH BOLTED REPAIRING PARAMETERS

ZHAO Mei-ying,WAN Xiao-peng,LIU Hao   

  1. Department of Aircraft Engineering, Northwestern Polytechnical University, Xi'an 710072, China
  • Received:2000-07-27 Revised:2001-11-13 Online:2001-10-25 Published:2001-10-25

摘要:

针对复合材料层合板穿透性损伤,采用圆形复合材料补片螺接贴补修理方式,对影响修补效率的多个因素进行了分析计算。修补结构采用“两板—DOF弹簧元”模型,有限元分析运用 NASTRAN软件,所得结论对工程设计具有实用价值。

关键词: 复合材料, 螺接修补, 有限元

Abstract:

For penetrability damaged composite components, composite material rounded patch bolted repairing was used to recover strength. This paper introduced the method to analyze the effect of composite patch bolted repairing parameters. The authors utilized the Double Plate-DOF Spring element in the finite element model to analyze the repair efficiency of the bolted repairing method with MSC/NASTRAN and obtained some valuable conclusions.

Key words: composite, bolted repair ing, finite element