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Influence of Weave Structures on the Tribological Properties of Hybrid Kevlar/PTFE Fabric Composites 被引量:14
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作者 GU Dapeng YANG Yulin +2 位作者 QI Xiaowen DENG Wei SHI Lei 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2012年第5期1044-1051,共8页
The existing research of the woven fabric self-lubricating liner mainly focus on the tribological performance improvements and the service life raised by changing different fiber type combinations, adding additive mod... The existing research of the woven fabric self-lubricating liner mainly focus on the tribological performance improvements and the service life raised by changing different fiber type combinations, adding additive modification, and performing fiber surface modification. As fabric composites, the weave structures play an important role in the mechanical and tribological performances of the liners. However, hardly any literature is available on the friction and wear behavior of such composites with different weave structures. In this paper, three weave structures (plain, twill 1/3 and satin 8/5) of hybrid Kevlar/PTFE fabric composites are selected and pin-on-flat linear reciprocating wear studies are done on a CETR tester under different pressures and different frequencies. The relationship between the tensile strength and the wear performance are studied. The morphologies of the worn surfaces under the typical test conditions are analyzed by means of scanning electron microscopy (SEM). The analysis results show that at 10 MPa, satin 8/5 performs the best in friction-reduction and antiwear performance, and plain is the worst. At 30 MPa, however, the antiwear performance is reversed and satin 8/5 does not even complete the 2 h wear test at 16 Hz. There is no clear evidence proving that the tensile strength has an influence on the wear performance. So the different tribological performance of the three weave structures of fabric composites may be attributed to the different PTFE proportions in the fabric surface and the different wear mechanisms. The fabric composites are divided into three regions: the lubrication region, the reinforced region and the bonding region. The major mechanisms are fatigue wear and the shear effects of the friction force in the lubrication region. In the reinforced region fiber-matrix de-bonding and fiber breakage are involved. The proposed research proposes a regional wear model and further indicates the wear process and the wear mechanism of fabric composites. 展开更多
关键词 hybrid kevlar/ptfe fabric composite FRICTION WEAR weave structure scanning electron microscopy
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Sliding Wear of the Hybrid Kevlar/PTFE Fabric Reinforced Phenolic Composite Filled with Nano-titania 被引量:4
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作者 YANG Yulin HUANG Shijun +2 位作者 ZU Dalei ZHANG Ruijun QI Xiaowen 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2011年第1期154-159,共6页
The Kevlar/polytetrafluroethylene(Kevlar/PTFE) fabric composite can be used as a self-lubricating liner of the self-lubricating bearing.Many types of nano-particles can improve the tribological performance of the po... The Kevlar/polytetrafluroethylene(Kevlar/PTFE) fabric composite can be used as a self-lubricating liner of the self-lubricating bearing.Many types of nano-particles can improve the tribological performance of the polymer-based composite.Unfortunately,up to now,published work on the effect of nano-particles on the tribological performance of the fabric composite which can be used as a self-lubricating liner is quite scarce.Therefore,for the purpose of exploring a way to significantly improve the tribological performance of the fabric composite,the tribological performance of the Kevlar/PTFE fabric composite filled with nano-titania is evaluated by using the block-on-ring wear tester.The scanning electron microscopy is utilized to observe the morphologies of worn surfaces of the fabric composites and the counterparts.The tensile properties of the composites are evaluated on the universal material testing machine.The test results show that the addition of nano-titania at a proper mass fraction of the matrix resin improves the wear resistance and the tensile strength,decreases the friction coefficient,and makes the wear volume of the composite reach a relative steady state more quickly;plastic deformation and microcutting are important for the wear of the fabric composite;a lubricating layer is formed on the worn surface of the composite during sliding,and the lubricating layer is critical for the tribological performance of the composite;the formation and properties of the lubricating layer are influenced by the nano-titania particles.The proposed study on the effect of nano-titania on the tribological performance of the Kevlar/PTFE fabric composite,especially on the evolution of the worn surface of the composite,provides the basis for further understanding of the influence mechanism of the nano-particles on the tribological performance of the composite and explores a method of improving the tribological performance of the composite. 展开更多
关键词 hybrid kevlar/ptfe fabric composite self-lubricating liner nano-titania friction and wear lubricating layer
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黏接压力对PTFE/Kevlar双层织物摩擦磨损性能的影响 被引量:1
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作者 刘宇飞 尹忠慰 +2 位作者 蒋丹 李虎林 霍亚军 《东华大学学报(自然科学版)》 CAS CSCD 北大核心 2015年第4期433-437,共5页
通过PTFE(聚四氟乙烯)/Kevlar双层织物与GCr15钢制金属盘的黏接试验,研究黏接面经过喷砂处理后,黏接压力对PTFE/Kevlar双层织物摩擦磨损性能的影响.结果表明:黏接压力为0.30 MPa时,PTFE/Kevlar双层织物的摩擦因数和磨损率最低,润滑性能... 通过PTFE(聚四氟乙烯)/Kevlar双层织物与GCr15钢制金属盘的黏接试验,研究黏接面经过喷砂处理后,黏接压力对PTFE/Kevlar双层织物摩擦磨损性能的影响.结果表明:黏接压力为0.30 MPa时,PTFE/Kevlar双层织物的摩擦因数和磨损率最低,润滑性能和耐磨性能最好;同时,与黏接压力为0.10及0.20 MPa时相比,黏接压力为0.30及0.40 MPa时,PTFE/Kevlar双层织物的摩擦因数与磨损率的一致性较好,故适当提高黏接压力有利于提高PTFE/Kevlar双层织物摩擦磨损性能的稳定性. 展开更多
关键词 黏接压力 ptfe/kevlar双层织物 摩擦因数 磨损率
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PTFE/Kevlar接结双层织物的织造研究 被引量:2
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作者 许家骅 赵敏 张继红 《产业用纺织品》 北大核心 2008年第10期9-11,共3页
介绍一种用于航天装备的外防护层产品的织物组织设计和织造工艺,该产品为分别用PTFE和Kevlar两种纱线构成织物正反面的接结双层织物。
关键词 聚四氟乙烯纤维 凯夫拉 组织结构设计 接结双层织物 织造工艺
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紫外辐照对自润滑关节轴承衬垫磨损性能的影响
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作者 叶强 谭德强 +4 位作者 宗法涛 胡月 贺强 杨文锋 周长春 《中国表面工程》 EI CAS CSCD 北大核心 2024年第3期134-144,共11页
PTFE/Kevlar织物材料具有优异自润滑性能,在航空关键部件中广泛应用,但紫外辐照对其影响规律尚不清晰。针对航空器飞行强紫外线暴露的特点,聚焦紫外辐照对航空常用PTFE/Kevlar编织关节轴承衬垫自润滑材料摩擦学性能的影响规律研究。对... PTFE/Kevlar织物材料具有优异自润滑性能,在航空关键部件中广泛应用,但紫外辐照对其影响规律尚不清晰。针对航空器飞行强紫外线暴露的特点,聚焦紫外辐照对航空常用PTFE/Kevlar编织关节轴承衬垫自润滑材料摩擦学性能的影响规律研究。对不同紫外辐照时长的PTFE/Kevlar织物衬垫材料进行往复摩擦试验,并采用多种表征手段对其宏观、微观损伤形貌以及化学状态进行分析。结果表明:PTFE/Kevlar织物衬垫材料的磨损程度随着紫外辐照时间的增加呈现出先降低后升高的趋势,短时辐照(T=100 h和200 h)的磨损最轻微,摩擦损失体积和磨痕最大深度仅为未辐照和长时辐照(T=300 h和500h)的2/3;紫外辐照后,衬垫材料与GCr15轴承钢球之间的磨损行为变化表现为PTFE纤维塑性变形和转移膜形成能力的下降,其主要原因是PTFE纤维结晶度的降低;衬垫材料的磨损机理随辐照时间的延长由疲劳磨损和粘着磨损向磨粒磨损为主转变。研究成果可为PTFE/Kevlar织物衬垫型自润滑材料在紫外辐照后的磨损性能跟踪和研制优化提供参考。 展开更多
关键词 ptfe/kevlar织物 紫外辐照 损伤形貌 转移膜 磨损机理
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