【24h】

Structural analysis of the radar signal simulator back-plane

机译:雷达信号模拟器背板的结构分析

获取原文
获取原文并翻译 | 示例

摘要

LRM (Linear Replaceable Module) structure is a new generation of high-reliability avionics system is based, and in the other comprehensive electronic system design are also beginning to use. In practical applications, according to the structure of RF-based LRM standards for integrated electronic system back-plane radar signal simulator has been designed, but not informed LRM module installation back-plane carrying capacity. In this paper, finite element analysis software module for installation LRM radar signal simulator back-plane structure static analysis, get back the maximum deformation position and the amount of deformation, the maximum stress intensity position and stress values. According to the relevant aviation industry standards, the analysis shows that the back-plane architecture designed to meet the strength requirements of LRM.
机译:LRM(线性可更换模块)结构是新一代高可靠性航空电子系统的基础,并且在其他全面的电子系统设计中也开始使用。在实际应用中,根据基于RF的LRM标准的结构,已经设计了集成电子系统背板雷达信号模拟器,但并未告知LRM模块安装背板的承载能力。本文采用有限元分析软件模块,对安装LRM雷达信号模拟器的背板结构进行静态分析,取回最大变形位置和变形量,最大应力强度位置和应力值。根据相关航空行业标准,分析表明,背板架构旨在满足LRM的强度要求。

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