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    A Review of High-Speed Electro-Hydrostatic Actuator Pumps in Aerospace Applications: Challenges and Solutions

    Source: Journal of Mechanical Design:;2019:;volume( 141 ):;issue: 005::page 50801
    Author:
    Chao, Qun
    ,
    Zhang, Junhui
    ,
    Xu, Bing
    ,
    Huang, Hsinpu
    ,
    Pan, Min
    DOI: 10.1115/1.4041582
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The continued development of electro-hydrostatic actuators (EHAs) in aerospace applications has put forward an increasing demand upon EHA pumps for their high power density. Besides raising the delivery pressure, increasing the rotational speed is another effective way to achieve high power density of the pump, especially when the delivery pressure is limited by the strength of materials. However, high-speed operating conditions can lead to several challenges to the pump design. This paper reviews the current challenges including the cavitation, flow and pressure ripples, tilting motion of rotating group and heat problem, associated with a high-speed rotation. In addition, potential solutions to the challenges are summarized, and their advantages and limitations are analyzed in detail. Finally, future research trends in EHA pumps are suggested. It is hoped that this review can provide a full understanding of the speed limitations for EHA pumps and offer possible solutions to overcome them.
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      A Review of High-Speed Electro-Hydrostatic Actuator Pumps in Aerospace Applications: Challenges and Solutions

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4256860
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    contributor authorChao, Qun
    contributor authorZhang, Junhui
    contributor authorXu, Bing
    contributor authorHuang, Hsinpu
    contributor authorPan, Min
    date accessioned2019-03-17T11:15:42Z
    date available2019-03-17T11:15:42Z
    date copyright1/11/2019 12:00:00 AM
    date issued2019
    identifier issn1050-0472
    identifier othermd_141_05_050801.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4256860
    description abstractThe continued development of electro-hydrostatic actuators (EHAs) in aerospace applications has put forward an increasing demand upon EHA pumps for their high power density. Besides raising the delivery pressure, increasing the rotational speed is another effective way to achieve high power density of the pump, especially when the delivery pressure is limited by the strength of materials. However, high-speed operating conditions can lead to several challenges to the pump design. This paper reviews the current challenges including the cavitation, flow and pressure ripples, tilting motion of rotating group and heat problem, associated with a high-speed rotation. In addition, potential solutions to the challenges are summarized, and their advantages and limitations are analyzed in detail. Finally, future research trends in EHA pumps are suggested. It is hoped that this review can provide a full understanding of the speed limitations for EHA pumps and offer possible solutions to overcome them.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Review of High-Speed Electro-Hydrostatic Actuator Pumps in Aerospace Applications: Challenges and Solutions
    typeJournal Paper
    journal volume141
    journal issue5
    journal titleJournal of Mechanical Design
    identifier doi10.1115/1.4041582
    journal fristpage50801
    journal lastpage050801-13
    treeJournal of Mechanical Design:;2019:;volume( 141 ):;issue: 005
    contenttypeFulltext
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