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改进遗传算法的纵列式直升机总体参数优化设计
引用本文:朱清华,张呈林,倪先平,王华明.改进遗传算法的纵列式直升机总体参数优化设计[J].南京航空航天大学学报,2006,38(1):1-5.
作者姓名:朱清华  张呈林  倪先平  王华明
作者单位:南京航空航天大学直升机旋翼动力学国家重点实验室,南京,210016
基金项目:某国防科研计划资助项目
摘    要:研究纵列式双旋翼直升机总体参数的优化设计方法,在分析双旋翼气动干扰对旋翼气动特性影响的基础上,采用改进的遗传算法,以运输效率为目标、以飞行性能和重量效率等参数为约束条件,建立优化设计模型,优化纵列式直升机总体参数。以CH-47D纵列式直升机为优化算例,计算结果表明,本文提出的优化方法是可行的,优化效果良好。

关 键 词:纵列式直升机  总体参数  遗传算法  优化设计
文章编号:1005-2615(2006)01-0001-05
收稿时间:2005-04-19
修稿时间:2005-05-30

General Parameter Optimization of Tandem Helicopter Based on Improved Genetic Algorithm
Zhu Qinghua,Zhang Chenglin,Ni Xianping,Wang Huaming.General Parameter Optimization of Tandem Helicopter Based on Improved Genetic Algorithm[J].Journal of Nanjing University of Aeronautics & Astronautics,2006,38(1):1-5.
Authors:Zhu Qinghua  Zhang Chenglin  Ni Xianping  Wang Huaming
Abstract:By analyzing interference between main rotors and the interference between rotors and the fuselage a intelligent algorithm is developed.General parameter optimization of the tandem helicopter with twin rotors based on the genetic algorithm is presented.To develop a mathematical model for the optimization design, firstly aerodynamic interaction effects of tandem rotors are analyzed.The model is built by considering the transportation efficiency as an objective,flight performances and the weight efficiency as constraints.An improved genetic algorithm is used to optimize general parameters.General parameters of CH-47D tandem helicopter are optimized by a design example.Results indicate that the method is feasible and efficient.
Keywords:tandem helicopter  general parameters  genetic algorithm  optimal design  
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