首页 | 本学科首页   官方微博 | 高级检索  
     检索      

涡轮基组合循环发动机分布式控制系统通信网络混合拓扑结构优化方法
引用本文:潘慕绚,梅满,戴冬红,聂聆聪,李岩.涡轮基组合循环发动机分布式控制系统通信网络混合拓扑结构优化方法[J].南京航空航天大学学报,2018,50(4):501-508.
作者姓名:潘慕绚  梅满  戴冬红  聂聆聪  李岩
作者单位:南京航空航天大学能源与动力学院;中国航天科工集团北京动力机械研究所
基金项目:国家自然科学基金(51406084)资助项目;江苏省航空动力系统重点实验室基金(NJ20160020)资助项目。
摘    要:涡轮机组合循环(Turbine based combined cycle,TBCC)发动机控制系统通信网络拓扑结构是其分布式控制系统方案设计的重要部分,优化网络拓扑结构可提高发动机推重比和控制系统可靠性。本文基于智能优化算法提出TBCC分布式控制系统网络拓扑结构优化方法。基于图论建立TBCC几何模型和网格模型,以重量和可靠性为优化性能指标,同时考虑发动机表面高温区域以及控制节点的工作可靠性,分别采用粒子群算法和遗传算法优化星形结构中智能中央节点位置、中央节点的环形拓扑结构,获得星形-环形混合拓扑结构。仿真实例表明,基于本文方法优化所得的混合拓扑结构相较于星形集中式控制结构,系统重量降低了51.9%。

关 键 词:涡轮机组合循环发动机  分布式控制  拓扑结构优化  粒子群算法  遗传算法  混合拓扑结构
收稿时间:2017/12/20 0:00:00
修稿时间:2018/6/15 0:00:00

Topology Optimization of Distributed Control System Communication Network for Turbine Based Combined Cycle Engines
PAN Muxuan,MEI Man,DAI Donghong,NIE Lingcong,LI Yan.Topology Optimization of Distributed Control System Communication Network for Turbine Based Combined Cycle Engines[J].Journal of Nanjing University of Aeronautics & Astronautics,2018,50(4):501-508.
Authors:PAN Muxuan  MEI Man  DAI Donghong  NIE Lingcong  LI Yan
Institution:1. College of Energy and Power Engineering, Nanjing University of Aeronautics & Astronautics, Nanjing, 210016, China;2. Beijing Power Machinery Research Institute, China Aerospace Science and Engineering Group, Beijing, 100074, China
Abstract:A distributed control system (DSC) is critical to improving the thrust-weight ratio and the reliability of turbine based combined cycle (TBCC) engines. A topology of communication network is important for distributed control system(DSC). A topology optimization for TBCC communication networks is proposed based on intelligent algorithms. The engine geometric model and grid model are formed. The optimization index is constructed by system weight and reliability, and constraint conditions are established by considering temperature limitations and reliability of smart nodes. The particle swarm algorithm and the genetic algorithm are employed to optimize positions and the ring topology of central smart nodes, respectively. Finally, a star-ring hybrid topology is obtained. The simulation results show that the new approach reduces the weight of DCS with hybrid topology by 51.9%,compared with that of the centralized control system with a star topology.
Keywords:turbine based combined cycle(TBCC)  distributed control system(DSC)  topology optimization  particle swarm algorithm(PSO)  genetic algorithm(GA)  hybrid topology
本文献已被 CNKI 等数据库收录!
点击此处可从《南京航空航天大学学报》浏览原始摘要信息
点击此处可从《南京航空航天大学学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号