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基于等概率随机法的航空发动机转子叶片排序优化
引用本文:徐广庆,白彦,孙惠斌,付玄,张纲,彭清,常智勇.基于等概率随机法的航空发动机转子叶片排序优化[J].航空制造技术,2020,63(1):52-56.
作者姓名:徐广庆  白彦  孙惠斌  付玄  张纲  彭清  常智勇
作者单位:中国航发四川燃气涡轮研究院,绵阳 621000,中国航发四川燃气涡轮研究院,绵阳 621000,西北工业大学机电学院,西安 710072,中国航发四川燃气涡轮研究院,绵阳 621000,中国航发四川燃气涡轮研究院,绵阳 621000,中国航发四川燃气涡轮研究院,绵阳 621000,西北工业大学机电学院,西安 710072
基金项目:陕西省重点研发计划;国家科技重大专项;装备预研项目
摘    要:对于盘片分离的航空发动机转子,叶片排序影响初始不平衡量,容易导致振动超限。在转子装配环节,精准、高效的叶片排序优化对于提高装配质量和效率有重要意义。针对此问题,基于单个叶片的质量矩模型,建立单级转子初始不平衡量模型,提出叶片排序优化的目标函数,研究一种基于“等概率随机”的搜索算法,实现在资源、时间消耗和优化效果之间取得平衡。仿真和验证结果表明,该研究方法可以精准、高效地优化叶片装配排序。与传统方法相比,单级转子的初始不平衡量大幅降低,转子的装配品质得到极大提高,已在实际生产中取得显著的应用效益。

关 键 词:航空发动机转子  叶片排序优化  初始不平衡量  等概率随机法  装配

Optimizing Blade Arrangement for Aero-Engine Rotor Based on Random Equiprobability Algorithm
XU Guangqing,BAI Yan,SUN Huibin,FU Xuan,ZHANG Gang,PENG Qing,CHANG Zhiyong.Optimizing Blade Arrangement for Aero-Engine Rotor Based on Random Equiprobability Algorithm[J].Aeronautical Manufacturing Technology,2020,63(1):52-56.
Authors:XU Guangqing  BAI Yan  SUN Huibin  FU Xuan  ZHANG Gang  PENG Qing  CHANG Zhiyong
Institution:(AECC Sichuan Gas Turbine Establishment,Mianyang 621000,China;School of Mechanical Engineering,Northwestern Polytechnical University,Xi’an 710072,China)
Abstract:As to disk-separated aero-engine rotor,blade arrangement affects initial unbalance of the rotor,and leads to vibration.During the rotor assembly process,precise and efficient blade arrangement is believed to improve assembly quality and efficiency.Aiming at this problem,a rotor initial unbalance model is built based on mass moment of a single blade.The fitness function of blade arrangement optimization is put forward.A searching algorithm is designed to make a trade-off between resource,time-consumption and optimization.Simulation and validation verify that blades could be distributed precisely and efficiently by using the proposed method.Compared with traditional methods,the initial unbalance is decreased dramatically,and the assembly quality is improved greatly.The pro-posed method has created valuable benefit in real assembly process.
Keywords:Aero-engine rotor  Blade arrangement optimization  Initial unbalance  Random equiprobability algorithm  Assembly
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