中国航空学报(英文版)2024,Vol.37Issue(3) :391-403.DOI:10.1016/j.cja.2024.01.004

A comparative investigation on wear behaviors of physical and chemical vapor deposited bronze coatings for hydraulic piston pump

Wei HAO Andrews LARBI Hongkang DONG Dongyun WANG Shenghu LI
中国航空学报(英文版)2024,Vol.37Issue(3) :391-403.DOI:10.1016/j.cja.2024.01.004

A comparative investigation on wear behaviors of physical and chemical vapor deposited bronze coatings for hydraulic piston pump

Wei HAO 1Andrews LARBI 1Hongkang DONG 1Dongyun WANG 1Shenghu LI2
扫码查看

作者信息

  • 1. Zhejiang Provincial Key Laboratory of Urban Rail Transit Intelligent Operation and Maintenance Technology and Equipment,Zhejiang Normal University,Jinhua 321004,China;College of Engineering,Zhejiang Normal University,Jinhua 321004,China
  • 2. Hangzhou Lilong Hydraulic Co.,Ltd,Hangzhou 311200,China
  • 折叠

Abstract

The cylinder block/valve plate interface is one of the most critical frictional interfaces of the swashplate-type axial piston pump.However,the poor lubrication interface caused rapid wear and high friction loss in an elastohydrodynamic lubrication system,decreasing the pump lifetime.Wear resistant bronze coatings were fabricated on 38CrMoAl substrate by Physical Vapor Depo-sition(PVD)and Chemical Vapor Deposition(CVD),respectively.Ball-on-disc wear tests were per-formed to comparatively investigate the wear behaviors of the coatings and bulk ductile iron samples.It can be found that the PVD-bronze coating exhibited better wear resistance than the other two samples.This enhanced wear resistance was attributed to the unique composite microstructure and desired mechanical strength,which could resist to mechanical shear and spalla-tion,decreasing friction loss.The appropriate hardness of(1.33±0.07)GPa could be beneficial for enhancing its wear resistance.The PVD-bronze coating possessed a much lower and stable coeffi-cient of friction(about 0.1)and wear rate(about 6000 μm3·N-1·m-1)under the loading forces of about 100 N after 20 min.The wear mechanism was the abrasive wear.

Key words

Aircraft hydraulic pump/Bronze/Coatings/Wear resistance/Mechanisms

引用本文复制引用

基金项目

浙江省重点研发计划(2020C01153)

浙江省重点研发计划(2022C01139)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量43
段落导航相关论文