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柱塞泵热力学建模与仿真
引用本文:李成功,焦宗夏.柱塞泵热力学建模与仿真[J].中国航空学报,2006,19(4):354-358.
作者姓名:李成功  焦宗夏
作者单位:School of Automatic Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
基金项目:国家高技术研究发展计划(863计划)
摘    要:针对航空行业广泛应用的柱塞泵的热力学特性,提出了一种分析和建模的方法.应用能量守恒定律推导并建立了集中参数的航空柱塞泵的热力学模型,并针对柱塞泵的内部结构进行了较详细的传热分析.将此建模和分析的方法应用于包含航空柱塞泵的一个典型液压回路.通过对航空柱塞泵的热力学实验与仿真结果的比较证明了建模方法的有效性.

关 键 词:热液压  柱塞泵  温度  建模  thermal-hydraulic  piston  pump  temperature  modelling
文章编号:1000-9361(2006)04-0354-05
收稿时间:2005-12-21
修稿时间:2006-03-07

Thermal-hydraulic Modeling and Simulation of Piston Pump
LI Cheng-gong,JIAO Zong-xia.Thermal-hydraulic Modeling and Simulation of Piston Pump[J].Chinese Journal of Aeronautics,2006,19(4):354-358.
Authors:LI Cheng-gong  JIAO Zong-xia
Institution:School of Automatic Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Abstract:This paper presents a kind of modeling approach to the study of the thermal-hydraulic piston pump which is used in the airplane comprehensively. A set of lumped parameter mathematical models are developed which are based on conservation of energy. Heat transfer analysis for the piston pump is also given in the paper in which the heat flow inside the piston pump is described precisely. The theoretical basis and modeling stratagy are applied in a typical thermal-hydraulic circuit containing the piston pump. Simulation results are presented which show a comparison of model/rig performance and the agreement obtained demonstrates the validity of the modeling approach.
Keywords:thermal-hydraulic  piston pump  temperature  modelling
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