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Simulation and verification of cure-induced deformation by stages for integrated composite structure

  • Tian Jiang
  • , Jifeng Xu
  • , Weiping Liu
  • , Jinrui Ye
  • , Lijie Jia
  • , Boming Zhang*
  • *此作品的通讯作者
  • Beihang University
  • Commercial Aircraft Corporation of China, Ltd.
  • Shanghai Aircraft Manufacturing Co Ltd

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

The developing law of T800/epoxy prepreg property parameters during curing process was analyzed through tests. A finite element analysis (FEA) simulation method of staged cure-induced deformation based on stress transfer was proposed in view of phased molding of composite integrated structures under the autoclave conditions. For I-shaped stiffened structures fabricated in different processes, deformation results predicted by the phased simulation were compared to experimental results and relationships between different manufacture schemes and deformations were also analyzed. The results show that the simulation method proposed in this paper can accurately predict the cure-induced deformations for the integrated structures, deformation is closely correlated with fabrication process, and selecting appropriate fabrication process for special structure and lay-up can effectively reduce the cured-induced deformations of composite structures.

源语言英语
页(从-至)61-66
页数6
期刊Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica
卷30
期5
出版状态已出版 - 10月 2013

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