首页> 外文会议>ASME(American Society of Mechanical Engineers) Turbo Expo vol.4; 20060506-11; Barcelona(ES) >Components Map Generation of Gas Turbine Engine Using Genetic Algorithms and Engine Performance Deck Data
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Components Map Generation of Gas Turbine Engine Using Genetic Algorithms and Engine Performance Deck Data

机译:基于遗传算法和发动机性能数据的燃气轮机零部件图生成

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In order to estimate the gas turbine engine performance precisely, the component maps containing their own performance characteristics should be needed. Because the components map is an engine manufacturer's propriety obtained from many experimental tests with high cost, they are not provided to the customer generally. Some scaling methods for gas turbine component maps using experimental data or data partially given by engine manufacturers had been proposed in previous study. Among them the map generation method using experimental data and genetic algorithms (Kong et al., 2004) had showed a possibility composing the component maps from some random test data. However not only this method needs more experimental data to obtain the more realistic component maps but also it requires some more calculation time to treat the additional random test data by component map generation program. Moreover some unnecessary test data may introduce to generate inaccuracy in component maps. And the map generation method called as the system identification method using partially given data from engine manufacturer (Kong et al., 2003) can improve the traditional scaling methods by multiplying the scaling factors at design point to off-design point data of the original performance maps, but some reference map data at off-design points should be needed. In this study a component map generation method which may identify component map conversely from some calculation results of a performance deck provided by engine manufacturer using the Genetic Algorithms was newly proposed to overcome the previous difficulties. As a demonstration example for this study, the PW206C turbo shaft engine for the tilt rotor type Smart UAV (Unmanned Aerial Vehicle) which has been developed by KARI (Korea Aerospace Research Institute) was used. In order to verify the proposed method, steady-state performance analysis results using the newly generated component maps were compared with them performed by EEPP (Estimated Engine Performance Program) deck provided by engine manufacturer. And also the performance results using the identified maps were compared with them using the traditional scaling method. In this investigation, it was found that the newly proposed map generation method would be more effective than the traditional scaling method and the methods explained at the above.
机译:为了精确地估计燃气涡轮发动机的性能,需要包含其自身性能特征的组件图。由于零部件图是发动机制造商从许多实验测试中获得的高成本的专有信息,因此通常不会将其提供给客户。在先前的研究中已经提出了一些使用实验数据或发动机制造商部分给出的数据的燃气轮机部件图的缩放方法。其中,利用实验数据和遗传算法生成图谱的方法(Kong等,2004)显示了由一些随机测试数据组成成分图谱的可能性。然而,这种方法不仅需要更多的实验数据来获得更逼真的分量图,而且还需要更多的计算时间才能通过分量图生成程序处理额外的随机测试数据。此外,可能会引入一些不必要的测试数据以在组件图中生成不准确的数据。利用发动机制造商提供的部分给定数据,称为系统识别方法的地图生成方法(Kong等,2003)可以通过将设计点的比例因子乘以原始性能的非设计点数据来改进传统的比例方法。地图,但在非设计点需要一些参考地图数据。在这项研究中,提出了一种组件图生成方法,该方法可以从发动机制造商使用遗传算法提供的性能甲板的一些计算结果中反过来识别组件图,从而克服了先前的困难。作为该研究的示范示例,使用了由KARI(韩国航空航天研究所)开发的用于倾斜旋翼式Smart UAV(无人机)的PW206C涡轮轴发动机。为了验证所提出的方法,将使用新生成的组件图的稳态性能分析结果与由发动机制造商提供的EEPP(估算的发动机性能程序)平台进行的性能分析结果进行了比较。并且还将使用识别出的地图的性能结果与使用传统缩放方法的性能结果进行比较。在该调查中,发现新提出的地图生成方法将比传统的缩放方法和上面说明的方法更有效。

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