【24h】

Pressurized Morphing Wing Structures

机译:加压变形机翼结构

获取原文

摘要

The combination of structural material and fluid pressure may result in a morphing structure with integrated shape-change and stiffness functions. In a cellular arrangement, distributed actuation, high control fidelity and a multitude of morphing shapes can also be achieved. The moving isosurface threshold topology optimization method was used to design the cell shapes and the optimal shapes were found to be arch-type structures which elongate or bend for various architecture networks for a NACA 0012 trailing edge. For demonstrative purposes, -3.02/+2.94 deg. deflection was achieved for a 15-cell parallel-type morphing trailing edge prototype.
机译:结构材料和流体压力的组合可能导致具有集成的形状变化和刚度功能的变形结构。在蜂窝布置中,还可以实现分布式致动,高控制保真度和多种变形形状。使用移动等值面阈值拓扑优化方法设计单元格形状,发现最佳形状是拱形结构,对于NACA 0012后缘的各种建筑网络,该弓形结构会伸长或弯曲。出于演示目的,-3.02 / + 2.94度。偏转是实现了15单元并行类型的变形后沿原型。

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