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电动静液作动器设计方法综述

付永领 韩旭 杨荣荣 齐海涛 付剑

付永领, 韩旭, 杨荣荣, 等 . 电动静液作动器设计方法综述[J]. 北京航空航天大学学报, 2017, 43(10): 1939-1952. doi: 10.13700/j.bh.1001-5965.2017.0195
引用本文: 付永领, 韩旭, 杨荣荣, 等 . 电动静液作动器设计方法综述[J]. 北京航空航天大学学报, 2017, 43(10): 1939-1952. doi: 10.13700/j.bh.1001-5965.2017.0195
FU Yongling, HAN Xu, YANG Rongrong, et al. Review on design method of electro-hydrostatic actuator[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(10): 1939-1952. doi: 10.13700/j.bh.1001-5965.2017.0195(in Chinese)
Citation: FU Yongling, HAN Xu, YANG Rongrong, et al. Review on design method of electro-hydrostatic actuator[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(10): 1939-1952. doi: 10.13700/j.bh.1001-5965.2017.0195(in Chinese)

电动静液作动器设计方法综述

doi: 10.13700/j.bh.1001-5965.2017.0195
基金项目: 

航空科学基金 20152851020

详细信息
    作者简介:

    付永领, 男, 博士, 教授, 博士生导师。主要研究方向:新型集成一体化功率电传作动技术、液压伺服系统理论与试验研究、特种机器人等

    付剑, 男, 博士。主要研究方向:新型集成一体化功率电传作动技术、复杂机电系统建模与仿真等

    通讯作者:

    付剑, E-mail: fujianbuaa@126.com

  • 中图分类号: TH122;V245.1

Review on design method of electro-hydrostatic actuator

Funds: 

Aeronautical Science Foundation of China 20152851020

More Information
  • 摘要:

    电动静液作动器(EHA)是一种起源于航空领域的新型高性能伺服作动装置,正逐渐成为各类大型装备的通用基础元部件,鉴于其机电液控热多学科耦合较大且要达到的综合指标又高,所以迫切需要一套高效科学的设计方法。从EHA完整设计过程的角度,综述其中的设计方法,为今后EHA产品的设计开发流程提供了基本支撑和多样化的技术手段。总结出基于自动化系统设计和多学科联合详细设计的EHA设计方法,并对其中的综合指标建立、建模仿真、优化设计、控制设计等关键技术进行了分析,给出适合不同设计任务特点的各步骤实现途径。展望了自动化详细设计、基于模型系统工程、3D打印等最新技术在EHA设计中的应用,为后续进一步提升EHA设计水平提供了参考。

     

  • 图 1  机电产品一般开发流程

    Figure 1.  General development process of mechatronic product

    图 2  加入虚拟性能验证的产品设计流程[33]

    Figure 2.  Product design process with virtual performance evaluation[33]

    图 3  EHA设计流程框架

    Figure 3.  EHA design process overview

    图 4  产品设计平台内涵框图[99]

    Figure 4.  Block diagram of product design platform[99]

    图 5  集成于ISIGHT的机电一体化系统优化设计平台[64]

    Figure 5.  Optimal design platform for mechatronic system integrated in ISIGHT[64]

    表  1  用于架构选择的定量与定性矩阵[43]

    Table  1.   Quantitative and qualitative matrix for concept selection[43]

      评价指标 指标值 单位
    定量指标 质量 kg
    可靠性/平均故障间隔时间 flight hour
    一次性成本 $或€
    重复性成本 $或€
    维护费用 $或€
      评价指标 满足或不满足
    定性指标 安装要求
    功能要求
    安全要求
    性能要求
    技术风险
    下载: 导出CSV
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  • 收稿日期:  2017-04-05
  • 录用日期:  2017-05-05
  • 网络出版日期:  2017-10-20

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