首页> 外文会议>International Conference on Shock amp; Impact Loads on Structures; 20071017-19; Beijing(CN) >FORMULATING THE CUTTING OF ONE-DIMENSIONAL STRUCTURE UNDER IMPACT LOAD
【24h】

FORMULATING THE CUTTING OF ONE-DIMENSIONAL STRUCTURE UNDER IMPACT LOAD

机译:冲击载荷作用下一维结构的剪裁

获取原文
获取原文并翻译 | 示例

摘要

Under impact loading in middle position, the cutting problem of one-dimensional plane structure (with two fixed edges) is studied in this research. The impact loading is supplied by a flying plane with narrow cut-in edge. After the front cut-in edge goes through the structure, the impact loading is maintained by the friction between the flying plane and the fracture face of structure for a short time. Then the plane is rested in the structure fracturing zone or passes though the structure. In practical problems,it is required to determine the deformation and fracture of structure by the velocity-mass parameter and the geometry of impact load. In this research, the deformation of structure is characterized by the deflection angular in the fracture position. The deformation stress is balanced by the acceleration force of flying plane through the friction coupling. The related impact-fracture equations are formulated in this research. The final equation shows the deflection angular of the structure is completely determined by the mechanical parameters of structure, the mass of flying plane, the friction parameter between the flying plane and the fracturing face of the structure, and the initial velocity of impact. When the friction parameter is taken as one, the equation can be used to evaluate the risk of fracturing for given initial velocity and mass. Generally, the obtained equation is non-linear. For simple case, analytical results are obtained to explain the cutting phenomenon.
机译:在中间位置的冲击载荷作用下,研究了一维平面结构(具有两个固定边)的切削问题。冲击载荷由切入边缘狭窄的飞行飞机提供。在前切入边缘穿过结构后,在短时间内通过飞行平面与结构的断裂面之间的摩擦力来保持冲击载荷。然后,将平面放置在结构破裂区中或穿过结构。在实际问题中,需要通过速度质量参数和冲击载荷的几何形状来确定结构的变形和断裂。在这项研究中,结构的变形以断裂位置的偏转角为特征。变形应力由通过摩擦耦合的飞行平面的加速力平衡。本研究建立了相关的冲击断裂方程。最终方程表明,结构的偏转角完全由结构的力学参数,飞行平面的质量,飞行平面与结构的破裂面之间的摩擦参数以及初始冲击速度决定。当摩擦参数为1时,该方程式可用于评估给定初始速度和质量下的破裂风险。通常,所获得的方程是非线性的。对于简单的情况,将获得分析结果来解释切削现象。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号