复合材料科学与工程 ›› 2026, Vol. 0 ›› Issue (7): 134-140.DOI: 10.19936/j.cnki.2096-8000.20260728.016

• 设计与工艺 • 上一篇    下一篇

气囊内胀法制备发动机复合壳体的技术研究

李世成1,2, 周琳赟1,2, 史文锋1,2*, 王志远1,2, 李来福1,2   

  1. 1.上海复合材料科技有限公司,上海 201112;
    2.上海航天树脂基复合材料工程技术研究中心,上海 201112
  • 收稿日期:2025-04-29 出版日期:2026-07-28 发布日期:2026-08-06
  • 通讯作者: 史文锋(1983—),男,硕士,研究员,研究方向为树脂基复合材料结构设计与制造,519685828@qq.com。
  • 作者简介:李世成(1987—),男,硕士,高级工程师,研究方向为树脂基复合材料结构设计与制造。

Technical study on preparation of engine composite shell by inflatable bladder molding

LI Shicheng1,2, ZHOU Linyun1,2, SHI Wenfeng1,2*, WANG Zhiyuan1,2, LI Laifu1,2   

  1. 1. Shanghai Composites Science & Technology Co., Ltd., Shanghai 201112, China;
    2. Shanghai Engineering Technology & Research Center of Aerospace Resin Based Composites, Shanghai 201112, China
  • Received:2025-04-29 Online:2026-07-28 Published:2026-08-06

摘要: 为了保证两端收口复合壳体的内部质量,采用斜带平叠螺旋缠绕和气囊内胀法进行制备。通过试验测试黏合后的斜带性能来确定黏合参数,设计斜带缠绕模型并推算斜带变形量来确定缠绕参数,选择不同气囊压力进行试验和测试,对比样件的性能差异。结果表明,斜带黏合的优选时间为1 s,黏合温度为80~90 ℃,缠绕时斜带最大变形量控制在10 mm左右,气囊压力为3 MPa时,制备的内绝热壳体内部质量最优。

关键词: 气囊内胀法, 带缠绕, 复合材料

Abstract: In order to ensure the internal quality of the composite shell with both ends reduced, the method of lap spiral winding and inflatable bladder was used to prepare the composite shell. The bonding parameters were determined by testing the performance of the bonded inclined tape through experiments. The winding mode of the inclined tape was designed and the deformation of the inclined tape was calculated to determine the winding parameters. Different pressures were selected for experiments and tests, and the quality of samples was compared. The results show that the preferred bonding time of the inclined tape is 1 s, the bonding temperature is 80~90 ℃, the maximum deformation of the inclined tape is controlled at about 10 mm during winding, and the pressure of the bladder is 3 MPa, the internal quality of the prepared inner insulated shell is the best.

Key words: inflatable bladder molding, tape winding, composite materials

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