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首页> 外文期刊>The Aeronautical Journal >Non-linear model calibration for off-design performance prediction of gas turbines with experimental data
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Non-linear model calibration for off-design performance prediction of gas turbines with experimental data

机译:基于实验数据的燃气轮机非设计性能预测的非线性模型校准

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摘要

One of the key challenges of the gas turbine community is to empower the condition based maintenance with simulation, diagnostic and prognostic tools which improve the reliability and availability of the engines. Within this context, the inverse adaptive modelling methods have generated much attention for their capability to tune engine models for matching experimental test data and/or simulation data. In this study, an integrated performance adaptation system for estimating the steady-state off-design performance of gas turbines is presented. In the system, a novel method for compressor map generation and a genetic algorithm-based method for engine off-design performance adaptation are introduced. The methods are integrated into PYTHIA gas turbine simulation software, developed at Cranfield University and tested with experimental data of an aero derivative gas turbine. The results demonstrate the promising capabilities of the proposed system for accurate prediction of the gas turbine performance. This is achieved by matching simultaneously a set of multiple off-design operating points. It is proven that the proposed methods and the system have the capability to progressively update and refine gas turbine performance models with improved accuracy, which is crucial for model-based gas path diagnostics and prognostics.
机译:燃气轮机界的主要挑战之一是通过仿真,诊断和预测工具来提高基于状态的维护的能力,从而提高发动机的可靠性和可用性。在这种情况下,逆自适应建模方法因其调整引擎模型以匹配实验测试数据和/或模拟数据的能力而引起了广泛关注。在这项研究中,提出了一种用于评估燃气轮机稳态非设计性能的集成性能自适应系统。在该系统中,介绍了一种用于压缩机图生成的新方法和一种基于遗传算法的发动机偏离设计性能自适应方法。这些方法已集成到由Cranfield大学开发的PYTHIA燃气轮机仿真软件中,并用航空衍生燃气轮机的实验数据进行了测试。结果证明了提出的系统对燃气轮机性能的准确预测的有前途的功能。这是通过同时匹配一组多个非设计工作点来实现的。事实证明,所提出的方法和系统具有以改进的精度逐步更新和完善燃气轮机性能模型的能力,这对于基于模型的气路诊断和预测至关重要。

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