首页> 外文会议>IEEE International Conference on Aircraft Utility Systems >Electro Hydraulic Actuation (EHA) Systems for Primary Flight Control, Landing Gear and Other Type of Actuation
【24h】

Electro Hydraulic Actuation (EHA) Systems for Primary Flight Control, Landing Gear and Other Type of Actuation

机译:电液驱动(EHA)用于初级飞行控制,着陆装置和其他类型的致动系统

获取原文
获取外文期刊封面目录资料

摘要

This paper provides an overview about different types of Smart Electro Hydraulic Actuators (EHA). The differences between the individual actuator concepts, including strengths and weaknesses, will be described. It will explain the most suitable applications for Electro Hydraulic Actuation as well as the applications for which this technology is not the first choice. Also, it provides examples of EHA applications for primary flight control, landing gear actuation, wind energy and transportation application.
机译:本文概述了有关不同类型的智能电液执行器(EHA)的概述。将描述各个执行器概念,包括强度和弱点之间的差异。它将解释电器液压致动的最合适的应用以及这项技术不是首选的应用。此外,它提供了初级飞行控制,着陆齿轮致动,风能和运输应用的EHA应用的示例。

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