摘要
利用动态油温计算法,建立了各种液压元件的温度模型,并对飞机液压系统在典型飞行状态下进行温度仿真计算。分析了影响液压系统温度的主要因素和降低油温的措施。
The thermal model of each hydraulic component was built to use the dynamic fluid temperature method,the aircraft hydraulic system thermal simulating calculation was deduced in typical flight status,and the primary influence factors to the temperature of aircraft hydraulic system were analyzed,and how to take reasonable measure to limit the temperature under control was also considered.
出处
《机床与液压》
北大核心
2005年第5期67-68,5,共3页
Machine Tool & Hydraulics
关键词
飞机液压系统
温度模型
温度仿真计算
Aircraft hydraulic system
Thermal model
Thermal simulating calculation
