期刊文献+

机织物拉伸弹性伸长的理论预测方法 被引量:2

Evaluation of Mathematical Models for Woven Fabric and 2/1 Woven Fabric
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摘要 为了预测机织物的弹性伸长,以Pierce的织物结构模型为出发点,对机织物拉伸过程中单根经纬纱交织点处受力单元进行了理论分析,提出了织物在拉伸过程中的变形主要由弹性变形和几何变形组成的假设。并在这个假设的前提下,依据纱线静力平衡原理及动量矩守恒定理,结合其他弹性力学理论,分别建立了平纹织物和2/1斜纹织物拉伸—伸长的数学模型,并对所建立的数学模型进行了实验验证。 Pierce's rigid-thread model of the woven fabric model has been employed as a starting point, the relationship among strengths which act on the interweave point of the individual warp and weft of fabrics during stretching has been dealt with. Based on the analysis of the Pierce's model, the Newton's law of motion, the law of conservation of momentum, and other mechanical theories, the conclusion that the deformation of fabrics is composed of elastic deformation and geometric deformation has been achieved. And according to the law of equilibrium, the mathematical models for calculating the load -extntion of plain woven fabrics have been set up respectively.
出处 《青岛大学学报(工程技术版)》 CAS 2004年第1期14-17,共4页 Journal of Qingdao University(Engineering & Technology Edition)
关键词 机织物 结构参数 拉伸伸长性能 力学分析 数学模型 静力平衡原理 弹性力学 woven fabric structural parameter tensile function mechanical analysis mathematical model
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参考文献2

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  • 2Pierce F T. Geometrical principles applicable to the design of functional fabrics [J]. Text R J, 1947,17(4):123-147.?A

同被引文献25

  • 1王彦广,李健全,李勇,姚伟.近空间飞行器的特点及其应用前景[J].航天器工程,2007,16(1):50-57. 被引量:63
  • 2顾正铭.平流层飞艇蒙皮材料的研究[J].航天返回与遥感,2007,28(1):62-66. 被引量:50
  • 3林国昌,万志敏,杜星文.机织织物剪切行为研究[J].航空学报,2007,28(4):1005-1008. 被引量:6
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  • 7QNINN J,MCLLHAGGER R,MCLLHAGGER A T.A modified system for design and analysis of 3D woven performs[J].Composites Part A-Applied Science and Manufacturing,2003,34(6):503-509.
  • 8HUANG Z M,FUJIHARA K,RRMAKRISHNA S.Tensile stiffness and strength of regular braid composites:correlation of theory with experiments[J].Journal of Composites Technology & Research,2003,25(1):35-49.
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