摘要
介绍了一种复合材料球型气瓶的缠绕层设计方法,以某型号球型气瓶为例,分别分析计算了球型气瓶的结构组成、缠绕线型、缠绕角度、缠绕方式和缠绕厚度,为产品后续的仿真与实验提供了必要的理论支持与参考依据,该方法可以推广至后续同类产品。
This paper summarizes a winding layer design method for composite spherical cylinder.Taking a certain type of spherical cylinder as an example,analyzes and calculates the structural composition,winding line shape,winding angle,winding method and winding thickness of the spherical cylinder.This method provides a necessary theoretical support and reference for subsequent simulation and experiment of the product,and the method can be extended to subsequent similar products.
作者
白文怡
廖英强
张宏亮
刘勇琼
Bai Wenyi;Liao Yingqiang;Zhang Hongliang;Liu Yongqiong(Xi’an Aerospace Composites Research Institute,Xi’an 710025)
出处
《航天制造技术》
2020年第1期42-45,57,共5页
Aerospace Manufacturing Technology
关键词
复合材料
球型气瓶
缠绕层设计
composite
spherical cylinder
winding layer design
