软管式空中加油时受油机响应特性分析  

Analysis of response characteristics of fuel receiver in flexible air refueling

作　　者：郝毓雅[1] 吕旭飞 侯亚东 HAO Yuya;LU Xufei;HOU Yadong

机构地区：[1]中国飞行试验研究院发动机所,陕西西安710089

出　　处：《现代机械》2019年第2期51-53,共3页Modern Machinery

摘　　要：采用无量纲分析方法,对软管式空中加油时对接过程中的受油机纵向操纵响应特性和受油机的俯仰、滚转和偏航操纵特性进行分析,得到对接过程中受油机纵向操纵响应的延迟时间并分析其影响,得到受油机的俯仰、滚转和偏航操纵特点并分析其原因,对后续空中加油的控制系统设计具有参考意义,对后续空中加油的飞行试验具有指导意义。The longitudinal control response characteristics of the receiver and the pitch,roll and yaw control characteristics of the receiver during docking of flexible aerial refueling are analyzed using dimensionless analysis method.We get the characteristics and analyze the causes and effects.It is of reference significance to the subsequent design of control system for aerial refueling,and is of guiding significance to the flight test of aerial refueling.

关 键 词：无量纲分析 空中加油 对接 受油机响应 

分 类 号：V217.1[航空宇航科学与技术—航空宇航推进理论与工程]