Tolerance design guideline for piston/cylinder interface of electro-hydrostatic actuator (EHA) pumps based on a Thermal-Fluid-Structure model-Reference-Cited by-同舟云学术

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Tolerance design guideline for piston/cylinder interface of electro-hydrostatic actuator (EHA) pumps based on a Thermal-Fluid-Structure model

Published:2024-03 Issue: Volume:191 Page:109208
ISSN:0301-679X
Container-title:Tribology International
language:en
Short-container-title:Tribology International

Author:

Zhang Junhui,Shen Yining,Lyu Fei,Huang Weidi,Xu Bing

Funder

National Natural Science Foundation of China

China Postdoctoral Science Foundation

Publisher

Elsevier BV

Subject

Surfaces, Coatings and Films,Surfaces and Interfaces,Mechanical Engineering,Mechanics of Materials

Reference40 articles.

1. A review of high-speed electro-hydrostatic actuator pumps in aerospace applications: challenges and solutions;Chao;J Mech Des,2019

2. Thermal-fluid-structure coupling analysis for valve plate friction pair of axial piston pump in electrohydrostatic actuator (EHA) of aircraft;Li;Appl Math Modell,2017

3. Challenges and solutions for high-speed aviation piston pumps: a review;Zhang;Aerospace,2021

4. Van Den Bossche D. The A380 flight control electrohydrostatic actuators, achievements and lessons learnt. 25th international congress of the aeronautical sciences: International Council of Aeronautical Sciences (ICAS) Hamburg, Germany; 2006.

5. A new approach for modeling and analysis of the lubricated piston skirt-cylinder system with multi-physics coupling;Zhao;Tribol Int,2022

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