Show simple item record

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


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record