航天无内衬复合材料压力容器结构设计与制备
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上海航天精密机械研究所,上海 201699

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TB332

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Design and Manufacturing of Liner-less Composite Pressure Vessel for Space Application
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Shanghai Spaceflight Precision Machinery Institute,Shanghai 201699

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    摘要:

    随着航天领域竞争愈发激烈,国内外加大了压力容器“皇冠上的明珠”无内衬纤维缠绕复合材料压力容器(Ⅴ型COPV)的开发力度,无内衬结构意味着必须实现复合材料层密封屏蔽/结构承载功能一体化设计,在材料性能和结构设计方面面临巨大挑战。本文针对结构设计进行系统性的梳理,综述了Ⅴ型COPV结构设计的研究进展,主要从功能阻隔层、形貌、接口设计及不同分析优化方法进行了阐述,介绍了基于模块化设计理念的新型V型COPV构型,并对未来航天用Ⅴ型COPV结构设计方面的发展进行了展望。

    Abstract:

    As competition in the aerospace field intensifies,both domestic and international entities have increased their efforts to develop the “crown jewel” of pressure vessels—made of liner-less fiber-wrapped composite materials (Ⅴ-type COPV).The liner-less structure necessitates an integrated design that combines the sealing/shielding function of the composite material layers with structural load-bearing capabilities,presenting significant challenges in terms of material performance and structural design.This paper systematically reviews the structural design of Ⅴ-type COPVs,summerizes the latest research progress in their structural design.It focuses on functional barrier layers,morphology,interface design,and various analysis and optimization methods.The paper introduces a novel Ⅴ-type COPV configuration based on a modular design philosophy and provides insights into the future development of structural design for V-type COPVs in the aerospace industry.

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章轩,王宇飞,王昊,袁杏,叶周军.航天无内衬复合材料压力容器结构设计与制备[J].宇航材料工艺,2025,55(4):1-10.

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  • 收稿日期:2024-05-27
  • 最后修改日期:2025-08-07
  • 录用日期:2024-07-10
  • 在线发布日期: 2025-08-28
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