首页> 外文会议>IEST (Institute of Environmental Sciences and Technology) 46th Annual Technical Meeting amp; Exposition , Apr 30-May 4, 2000, Providence, Rhode Island >Evaluation of the real life vibration regime and its laboratory equivalent for a helicopter carried structure. Part I The real life
【24h】

Evaluation of the real life vibration regime and its laboratory equivalent for a helicopter carried structure. Part I The real life

机译:对直升机携带结构的现实生活振动状况及其实验室等效物的评估。第一部分现实生活

获取原文
获取原文并翻译 | 示例

摘要

This is the first of a two-part paper that describes the results of the analysis of vibration measured on a helicopter-carried structure, consisting of a pylon, launcher, and load installed on the launcher. The analysis was performed to generate a laboratory simulation program for the structure. Hence, the paper considers only measurements on the pylon and launcher. Part I of the paper presents the measurement setup, analysis methods and results, and the methods for generating the simulation program. Part II of the paper presents methods for evaluating the vibration transmission paths, the simulation programs, results of their implementation and the significance of the vibration transmission paths on the configuration of the simulation setup.
机译:这是由两部分组成的论文的第一篇,该论文描述了在直升机运载的结构(包括塔架,发射器和安装在发射器上的负载)上测得的振动分析结果。进行分析以生成该结构的实验室模拟程序。因此,本文仅考虑对塔架和发射器的测量。本文的第一部分介绍了测量设置,分析方法和结果以及生成仿真程序的方法。本文的第二部分介绍了评估振动传递路径的方法,仿真程序,其实现结果以及振动传递路径对仿真装置配置的意义。

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