南京航空航天大学学报（英文版）2003，Vol.20Issue(2)：159-164,6.
基于热动力分析的飞机液压系统数值预测
NUMERICAL PREDICTION OF AIRCRAFT HYDRAULIC SYSTEM BASED ON THERMAL DYNAMIC ANALYSIS
苏向辉 1许锋 1昂海松1
作者信息
- 1. 南京航空航天大学航空宇航学院,南京,210016,中国
- 折叠
摘要
Abstract
A mathematical model of principal elements of the aircraft hydraulic system is presented based on the heat transfer theory. The dynamic heat transfer process of the hydraulic oil and the pump shells within an aircraft hydraulic system are analyzed by the difference method. A kind of means for the prediction to variational trends of the aircraft hydraulic system temperature is provided during operation. The numerical prediction and simulation under the operational conditions are presented for ground trial running and the decelerated operation in flight. Computational results show that there is a good coincidence between the experimental data and the numerical predictions.关键词
液压系统/压力损失/动态热分析/数值预测Key words
hydraulic system/head loss/thermal dynamic analysis/numerical prediction分类
机械制造引用本文复制引用
苏向辉,许锋,昂海松..基于热动力分析的飞机液压系统数值预测[J].南京航空航天大学学报（英文版）,2003,20(2):159-164,6.
