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依据试验数据求取航空发动机部件特性的新方法
引用本文:杨欣毅,刘海峰,董可海.依据试验数据求取航空发动机部件特性的新方法[J].航空计算技术,2009,39(3):48-51,55.
作者姓名:杨欣毅  刘海峰  董可海
作者单位:海军航空工程学院,飞行器工程系,山东烟台,264001
摘    要:介绍了通用的依据已知发动机部件特性求取所需部件特性的耦合法,并指出该方法的不足。以压气机部件特性为例提出求取部件特性的新方法。该方法利用发动机试验数据得到转速线与共同工作线的交点,把转速线近似为指数函数曲线,由PSO算法结合所得的交点数据拟合出每条转速曲线。以试验数据为依据,保证了特性的真实和有效性,而PSO算法则提高了特性线拟合的精度。计算结果表明所提出的方法比传统的耦合法更为准确,有利与提高发动机工作过程仿真精度。

关 键 词:航空发动机  粒子群优化算法  部件特性  仿真  拟合  最小二乘法

A New Component Map Generation Method of Aero Engine Based on Experimental Data
YANG Xin-yi,LIU Hai-feng,DONG Ke-hai.A New Component Map Generation Method of Aero Engine Based on Experimental Data[J].Aeronautical Computer Technique,2009,39(3):48-51,55.
Authors:YANG Xin-yi  LIU Hai-feng  DONG Ke-hai
Institution:Department of Aircraft Engineering;Naval Aeronautical and Astronautical University;Yantai 264001;China
Abstract:Traditional scaled method which generates new engine component map according to the known map was introduced.The defect of scaled method was point out.A new component map generation method was proposed with the example of compressor map.First the intersectional points of rotational speed line and common operating line were acquired from experimental data,and then the rotational speed line was set as the exponential function approximately.Every rotational speed line function was fitted using PSO algorithm on...
Keywords:aero engine  particle swarm optimization  component characteristics  simulation  curve fitting  least squares  
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