摘要
针对给出的飞机地面压力加油系统管路模型,分析得出解决大容量、多吨位飞机加油系统常用吨位加油和最大吨位 加油所需时间之间矛盾的方法,应用遗传算法得到各管路优化的节流孔尺寸,而且计算结果的正确性已经被节流器在该型飞机 地面压力加油系统中的实际应用所证实。
According to the given aircraft ground pressure refuel system pipeline model, we analyze and find the method to solve the contradiction of the refuel time between normal tonnage and maxim tonnage in big capacity and various - tonnage aircrafts' refuel system. We acquire the sizes of optimum orifices in all pipelines with genetic algorithms. The accuracy of the calculating results has been proved by the application of the orifice in the aircraft's ground pressure refuel system.
出处
《机床与液压》
北大核心
2003年第1期131-133,共3页
Machine Tool & Hydraulics
基金
空装科研部科研基金资助(KJ99072)
