缝合复合材料可用性——环境条件下层合板的冲击后压缩性能

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材料工程 ›› 2004, Vol. 0 ›› Issue (9) : 38-41.

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研究与应用

缝合复合材料可用性——环境条件下层合板的冲击后压缩性能

程小全, 寇长河, 郦正能

作者信息 +

Properties of Stitched Composite LaminatesPost-impact Compression of Laminates Under Different Environment

CHENG Xiao-quan, KOU Chang-he, LI Zheng-neng

Author information +

文章历史 +

摘要

为了解决缝合复合材料在航空航天结构中的应用问题,对国内生产的缝合/树脂膜渗透成型工艺复合材料层合板在三种不同环境条件下的低速冲击后压缩性能进行试验研究.结果表明,缝合改变了含冲击损伤层合板的压缩破坏机理,可以大幅度提高层合板在干态常温下的冲击后剩余压缩强度,但是对湿态高温下层合板的冲击后剩余压缩强度影响不大;缝合方向对冲击损伤面积和剩余压缩强度的影响较小,其中以0°缝合较为有利.

Abstract

In order to solve the application of stitched composites in aircraft structures,experimental studies were carried out on the post-impact compressive properties of internal stitched laminates made by resin film infusion(RFI)process.Three different environments were used in this test.It shows that stitching changes compressive mechanisms of the laminates after low velocity impact.Post-impact compressive strength is improves highly through stitching at dry/normal temperature.But stitching has little influence on residual compressive strength of laminates after low velocity at wet/high temperature.Damage areas and post-impact strength are little affected by stitching directions.Stitching in 0 degree is much better than that in other directions.

导出引用

程小全, 寇长河, 郦正能. 缝合复合材料可用性——环境条件下层合板的冲击后压缩性能[J]. 材料工程, 2004, 0(9): 38-41

CHENG Xiao-quan, KOU Chang-he, LI Zheng-neng. Properties of Stitched Composite LaminatesPost-impact Compression of Laminates Under Different Environment[J]. Journal of Materials Engineering, 2004, 0(9): 38-41

中图分类号： V258+.3

参考文献

[1] DAVIS J G Jr.Overview of the ACT program[R].FAA Report DOT/FAA/CT-92-25(II):577-599.
[2] DELBREY J.Database of mechanical properties of textile composites[R].National Aeronautics and Space Administration,Langley Research Center,Hampton,Virginia 23681-0001,NASA CR-4747,1996.
[3] MASTERS J E,PORTANOVA M A.Standard test methods for textile composites[R].Lockheedmartin Engineering &Sciences Company,NASA CR-4751,1996.
[4] MOURITZ A P,LEONG K H,HERSZBERG I.A review of the effect of stitched on the in-plane mechanical properties of fibre-reinforced polymer composites[J].Composites:Part A,1997,28(12):979-991.
[5] 程小全.复合材料层合板与蜂窝夹芯板低速冲击后压缩性能研究[D].北京:北京航空航天大学,1998.
[6] 桂良进.缝合层合板基本力学性能和抗冲击性能研究[D].北京:北京航空航天大学,2000.
[7] 程小全,赵龙,张怡宁.缝合复合材料可用性-简单层合板的基本性能[J].北京航空航天大学学报,2003,29(11):1001-1005.
[8] 程小全,寇长河,郦正能.低速冲击后复合材料层合板的压缩行为[J].复合材料学报,2001,18(1):115-119.