首页> 外文会议>Progress in durability analysis of composite systems >Estimation of carrying capacity of aviation engine parts from composite materials
【24h】

Estimation of carrying capacity of aviation engine parts from composite materials

机译:用复合材料估算航空发动机零件的承载能力

获取原文
获取原文并翻译 | 示例

摘要

When analyzed phenomena are changed on distances, comparable to the sizes of structural geterogeneity of composite materials, the mathematical models of higher levels than the homogeneous anisotropic body model are used. In this connection the main relationships of the proposed two-component theory of composite materials linear deformability are discussed. On the basis of proposed approach the estimation of the carrying capacity of the blade root is given and the fatigue damage of the cantilever boraluminium beam at bending vibration on natural frequencies is researched.
机译:当分析的现象在距离上发生变化时,可以与复合材料的结构同质性大小相比较,使用比均质各向异性体模型更高级别的数学模型。在这方面,讨论了所提出的复合材料线性变形的双组分理论的主要关系。在此方法的基础上,给出了叶片根部承载力的估算值,研究了悬臂硼铝梁在固有频率弯曲振动下的疲劳损伤。

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