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基于Kriging方法的航空发动机压气机特性元建模
引用本文:尹大伟,李本威,王永华,冯向军.基于Kriging方法的航空发动机压气机特性元建模[J].航空学报,2011,32(1):99-106.
作者姓名:尹大伟  李本威  王永华  冯向军
作者单位:1. 国防科学技术大学航天与材料工程学院,湖南,长沙,410073
2. 海军航空工程学院飞行器工程系,山东烟台,264001
摘    要:针对求解航空发动机数学模型时,使用传统的压气机二维特性曲线进行插值计算精度较差的问题,引入了优化技术中元建模的思想,对压气机特性进行模型重构.根据压气机特性数据空间分布的特点,定义元模型的输入输出维数,采用Kriging算法建立了流量和效率特性的代理模型.以某型涡扇发动机为例进行了压气机特性元建模的仿真计算,设定了满足...

关 键 词:航空发动机  Kriging方法  元建模  压气机特性  代理模型

Aeroengine Compressor Characteristics Metamodeling Using Kriging Method
YIN Dawei,LI Benwei,WANG Yonghua,FENG Xiangjun.Aeroengine Compressor Characteristics Metamodeling Using Kriging Method[J].Acta Aeronautica et Astronautica Sinica,2011,32(1):99-106.
Authors:YIN Dawei  LI Benwei  WANG Yonghua  FENG Xiangjun
Institution:1.College of Aerospace and Material Engineering,National University of Defense Technology, Changsha 410073,China 2.Department of Aerocraft Engineering,Naval Aeronautical and Astronautical Academy, Yantai 264001,China
Abstract:A metamodeling method used in optimization is introduced to reconstruct the characteristics models of an aeroengine compressor, because the traditional 2D compressor characteristics maps used in the interpolation for aeroengine model solving lack sufficient precision. According to the space distribution of the compressor characteristics data, the dimensions of the metamodel inputs and outputs are defined, and the flow and efficiency surrogate models are established using the Kriging method. The simulation on a given turbofan engine is performed as an example, in which the calculation region is set to satisfy its steady work, and then the characteristics of unknown rotational speeds are reconstructed in the new calculation region based on the established Kriging metamodels. The results of model verification and validation show that, the reconstructed characteristics using Kriging surrogate models have high precision, and are better than the linear interpolation method. It can be predicted that the application of compressor characteristics Kriging metamodels will improve the precision of the aeroengine model solution. Therefore, the study is of significant engineering value.
Keywords:aeroengine  Kriging method  metamodeling  compressor characteristics  surrogate model
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