Research Progress of Z-pin Reinforced Composite Laminate

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Research Progress of Z-pin Reinforced Composite Laminate

更新时间：2025-10-30

- Research Progress of Z-pin Reinforced Composite Laminate
- Aeronautical Manufacturing Technology Vol. 52, Issue 15, Pages: 43-45(2009)
- 作者机构：
  
  南京航空航天大学
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2009.15.012
  CLC：
- Published：2009
- 稿件说明：
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孙涛，李勇，王鹏，马丹，范琳，程培忠，肖军. 层合复合材料Z-pin增强技术研究进展[J]. 航空制造技术, 2009, 52(15): 43-45.

Research Progress of Z-pin Reinforced Composite Laminate[J]. Aeronautical Manufacturing Technology, 2009, 52(15): 43-45.
孙涛，李勇，王鹏，马丹，范琳，程培忠，肖军. 层合复合材料Z-pin增强技术研究进展[J]. 航空制造技术, 2009, 52(15): 43-45. DOI： 10.16080/j.issn1671-833x.2009.15.012.

Research Progress of Z-pin Reinforced Composite Laminate[J]. Aeronautical Manufacturing Technology, 2009, 52(15): 43-45. DOI： 10.16080/j.issn1671-833x.2009.15.012.

摘要

纤维增强复合材料层合板具有良好的面内力学性能和可设计性，但较低的层间强度和层间断裂韧性影响了其工程应用。应用各种Z 向增强技术（包括缝合技术、三维编织、Z - p i n增强技术等）提高层合复合材料抗分层性能是航空复合材料结构技术的重要研究内容。

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