期刊
CHINESE JOURNAL OF AERONAUTICS
卷 34, 期 1, 页码 111-134出版社
ELSEVIER SCIENCE INC
DOI: 10.1016/j.cja.2020.09.030
关键词
Axial piston pump; Cylinder block; valve plate interface; Theoretical model; Test rig; Optimization methods
资金
- Chinese Civil Aircraft Project [MJ2017S49]
- China National Postdoctoral Program for Innovative Talents [BX20200210]
- China Postdoctoral Science Foundation [2019M660086]
Axial piston pumps are widely used in aircraft hydraulic systems, requiring high power density, safety, and reliability. This study comprehensively reviews the latest literature on the cylinder block/valve plate interface, including theoretical models, experimental studies, and structural optimization methods.
Axial piston pumps have been widely used in aircraft hydraulic systems to supply the system with pressurized fluid. The continuous improvement of the aircraft performance has put forward the demand on aviation piston pumps for high power density, safety, and reliability. The lubricating interfaces in axial piston machines are the key design issue that greatly determines the pump performance and service life. The cylinder block/valve plate interface is one of these critical lubricating interfaces and has received considerable attention from many researchers in the last half century. This study aims to review the state-of-the-art literature on the cylinder block/valve plate interface comprehensively and systematically. First, we introduce various theoretical models developed to investigate the lubrication behaviors of the interface and compare them in terms of their assumptions and limitations. Second, the experimental studies on the cylinder block/valve plate interface are presented comprehensively, where the involved test rigs are divided into three types according to their fidelity levels and measurement functionality. Third, we summarize some typical approaches of structure optimization, surface shaping, and surface strengthening, which help improve the load-carrying and anti-wear capacities of the interface under severe operating conditions. Finally, the challenges and future trends of the cylinder block/valve plate interface research are discussed briefly. (c) 2020 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/ licenses/by-nc-nd/4.0/).
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