摘要
为保证在目标值下飞机加油车加油系统管径及动力单元输出参数满足各项安全性能指标要求。以双63加油管路原理为例,对飞机加油车管路系统原理及水力计算流程予以介绍。
In order to ensure the aircraft refueling truck, refueling system pipe diameter and power unit output parameters meet the requirements of the safety performance indicators, based on the principle of double 63 filling line as an example, the design of the aircraft refueling truck pipeline hydraulic calculation process was introduced.
出处
《专用汽车》
2015年第12期94-96,共3页
Special Purpose Vehicle
关键词
飞机加油车
管线设计
水力计算
aircraft fuel truck
pipeline design
hydraulic calculation
