Spline design for the cylinder block within a high-speed electro-hydrostatic actuator pump of aircraft-Reference-Cited by-同舟云学术

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Spline design for the cylinder block within a high-speed electro-hydrostatic actuator pump of aircraft

Published:2017-06-12 Issue:1-2 Volume:53 Page:395-411
ISSN:0025-6455
Container-title:Meccanica
language:en
Short-container-title:Meccanica

Author:

Chao Qun,Zhang Junhui^ORCID,Xu Bing,Chen Yuan,Ge Yaozheng

Funder

National Basic Research Program of China (973 Program)

National Natural Science Foundation of China

Science Fund for Creative Research Groups of the National Natural Science Foundation of China

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Link

http://link.springer.com/article/10.1007/s11012-017-0705-2/fulltext.html

Reference36 articles.

1. Yang HY, Pan M (2015) Engineering research in fluid power: a review. J Zhejiang Univ Sci A 16(6):427–442

2. Habibi S, Goldenberg A (2000) Design of a new high-performance electrohydraulic actuator. IEEE/ASME Trans Mechatron 5(2):158–164

3. Li YH, Ji ZL, Yang LM, Xu B, Zhang JH (2016) Thermal-fluid-structure coupling analysis for valve plate friction pair of axial piston pump in electrohydrostatic actuator (EHA) of aircraft. Appl Math Model. doi: 10.1016/j.apm.2016.08.015

4. Edge KA, Darling J (1989) The pumping dynamics of swash plate piston pumps. J Dyn Syst Meas Control 111(2):307–312

5. Bergada JM, Kumar S, Davies DL, Watton J (2012) A complete analysis of axial piston pump leakage and output flow ripples. Appl Math Model 36(4):1731–1751

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