摘要
针对复合材料帽型加筋壁板结构弯曲承载性能差的缺点,采用Z-pin增强技术提高弯曲承载性能。为研究Z-pin直径、体积分数、增强区长度对复合材料帽型加筋壁板弯曲性能的影响,制备了不同参数的Z-pin增强帽型加筋壁板试样并开展三点弯曲试验,对Z-pin增强机理及试样失效机制进行了分析。结果表明:随着体积分数的增加,由于Z-pin的桥联作用,Z-pin增强帽型加筋壁板弯曲性能提高,同时由于Z-pin植入产生的损伤增加,通过理论分析得到当Z-pin体积分数为2.6%时,弯曲峰值力达到最大值6.1kN;Z-pin直径对帽型加筋壁板弯曲峰值力影响不显著;当Z-pin增强区长度为总长度的48%时,Z-pin增强帽型加筋壁板弯曲峰值力与全部植入Z-pin时基本相当。
The Z-pin reinforcing technology is used to improve the less good bending bearing performance of composite hat stiffener wall structure.In order to study the influence of Z-pin volume fraction,Z-pin diameter and Z-pin reinforcing region length on the performance of hat stiffener wall structure polymer composites,the samples reinforced by Z-pin with different parameters are prepared and tested under three-point bending load.The Z-pin reinforcing mechanism and samples' failure mechanism are analyzed.The results show that the bending property of hat stiffener wall structures reinforced by Z-pin is improved with the increase of Z-pin volume fraction due to the bridging role of Z-pin,and the damage caused by Z-pin inserting increases.When the volume fraction of Z-pin is 2.6%,the bending peak load reaches the maximum value 6.1kN through theoretical analysis.The effect of the diameter of Z-pin on the bending load of stiffener wall structures is not obvious.When the length of the Z-pin reinforcing region is 48% of the total length,the bending peak load of hat stiffener wall structure reinforced by Z-pin equals the bending peak load of samples with 100% Z-pin inserting length.
作者
李吻
李勇
还大军
褚奇奕
肖军
LI Wen LI Yong HUAN Dajun CHU Qiyi XIAO Jun(College of Material Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)
出处
《航空学报》
EI
CAS
CSCD
北大核心
2016年第12期3843-3852,共10页
Acta Aeronautica et Astronautica Sinica
基金
航空科学基金(2015ZE52049)
国家"973"计划(2014CB046501)
江苏高校优势学科建设工程~~