用声发射技术研究碳/环氧复合材料固化成形中的残余应力

傅焕波;倪荣根;任荣镇;范棠

航空材料学报 ›› 1986, Vol. 6 ›› Issue (2) : 55-61.

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航空材料学报 ›› 1986, Vol. 6 ›› Issue (2) : 55-61.
论文

用声发射技术研究碳/环氧复合材料固化成形中的残余应力

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INVESTIGATIOIN ON THERMAL RESIDUAL STRESSES INTRODUCED DURING CURING OF CARBON/EPOXY COMPOSITES IN ACOUSTIC EMISSION TECHNIQUE

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摘要

运用声发射技术研究了T300/648环氧。BF3MEA体系铺层为[0/].4s(=0,4590)的几种叠层板以四种不同冷却速度(0.5. 1.0. 1.5, 2.0℃/min)固化成形产生的残余应力.结果表明,声发射能够反映固化成形过程中复合材材内部所发生的变化,并能定性地反映固化成形过程中产生成的残余应力的大小.用显微镜观察了叠层板断面,没有发现存在孔隙和裂纹。夸曲和层剪强度受冷却速度的影响不明显。这表明,在本工作范围内,由不同铺层和冷却速度引起的残余应力还不足以引起叠层板内产生裂纹以致显著影响其力学性能。

Abstract

Thermal residual stresses introduced during curing of carbon/epoxy composites were investigated with the use of acoustic emission(AE)technique.The laminates of T300/648 epoxy.BF3MEA with different ply-angle[0/].4scopled at different rates(0.5. 1.0. 1.5, 2.0℃/min)were used as specimens.AE monitoring during curing shows the capability of identifying the structural .changes of composites in the entire curing cycle,It is observed that AE can also be used to determine the residual stresses introduced in the curing cycle qualitatively.Microscopic observations of the cross-sections of the laminates indicate that there is no void and micro-crack in the laminates.The results of flexual and interlaminar shear strength show that the influence of cooling rate on the mechanical properties of laminates is not obvious.Therefore, it can be seen that the residual stresses resulting from different ply-angles and cooling races are not big enough to make cracks in the laminates, so the mechanical properties of the laminates are not remarkably affected by the ply-angle and cooling rate under the condition of this work.

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傅焕波, 倪荣根, 任荣镇, 范棠. 用声发射技术研究碳/环氧复合材料固化成形中的残余应力[J]. 航空材料学报, 1986, 6(2): 55-61
Fu Huanbo, Ni Rong-gen, Ren Rong-zhen, Fan Tang. INVESTIGATIOIN ON THERMAL RESIDUAL STRESSES INTRODUCED DURING CURING OF CARBON/EPOXY COMPOSITES IN ACOUSTIC EMISSION TECHNIQUE[J]. Journal of Aeronautical Materials, 1986, 6(2): 55-61

参考文献

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[5] 张和善等,实验用单向纤维增强塑料平板制备标准方法,北京航空材料研究所,(内部资料)1983。
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