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MODEL BASED ACTIVE COMBUSTION CONTROL CONCEPT FOR REDUCTION OF PULSATIONS AND NOX EMISSIONS IN LEAN PREMIXED GAS TURBINE COMBUSTORS

机译:基于模型的基于主动燃烧控制概念,用于减少精益预混燃气轮机燃烧器中的脉动和NOx排放

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Strict environmental regulations demand gas turbine operation at very low equivalence ratios. Premixed gas turbine com-bustors, operated at very lean conditions, are prone to thermoa-coustic instabilities. Thermoacoustic instabilities cause significant performance and reliability problems in gas turbine com-bustors, so their prevention is a general task. Splitting the fuel mass flow between different burner groups, i.e. using a burner group fuel staging technique, is a possibility to control the thermoacoustic instabilities. The resulting combustion perturbations have also effects on the gas turbine NOx emissions making it necessary to find an optimum balance between pulsations and emissions. This paper presents a model based active combustion control concept for the reduction of pulsations and emissions in lean premixed gas turbine combustors. The model is integrated in an observer structure derived from a Luenberger observer. The control logic is based on a PID algorithm allowing either the direct command of the pulsation level with a continuous monitoring and a potential limit setting of the NOx emission level or vice versa. The gas turbine pulsations and emissions are modelled using Gaussian Processes. - Gaussian Processes are stochastic processes related to Neural Networks that can approximate arbitrary-functions. Based on measured gas turbine data they can be implemented in an easy and straightforward manner. The model provides the control system with real time data of the outputs resulting from settings of the staging ratio that is the actuating variable of the system. A model based control concept can significantly alleviate the effects of time delays in the system. The model based control concept allows for fast adaptation of the burner group staging ratio during static and transient operations to achieve an optimum of the pulsation and emission levels. During tests the model based control concept gave good results and proved to be robust even at high disturbance levels.
机译:严格的环境法规要求在非常低的等效比率下燃气涡轮机操作。预混合的燃气轮机Com-Brobors,在非常精益的条件下操作,容易发生Thermo-Coustic Instability。热声无限度导致燃气轮机Com-Bessors中的显着性能和可靠性问题,因此预防是一般的任务。在不同燃烧器组之间分离燃料质量流量,即使用燃烧器组燃料分期技术,是控制热声型稳定性的可能性。由此产生的燃烧扰动也对燃气轮机NOx排放的影响也使得在脉动和排放之间找到最佳平衡。本文介绍了一种基于模型的主动燃烧控制概念,用于减少精益预混燃气轮机燃烧器中的脉动和排放。该模型集成在源自Luenberger观察者的观察者结构中。控制逻辑基于PID算法,允许脉动级的直接命令具有连续监测和NOx发射水平的潜在限制设置,反之亦然。燃气轮机脉动和排放是使用高斯工艺进行建模的。 - 高斯过程是与可以近似任意函数的神经网络相关的随机过程。基于测量的燃气轮机数据,它们可以以简单和简单的方式实现。该模型提供了具有由作为系统的致动变量的分段比的设置产生的输出的实时数据的控制系统。基于模型的控制概念可以显着减轻系统延迟的影响。基于模型的控制概念允许在静态和瞬态操作期间快速适应燃烧器组分级比率,以实现脉动和发射水平的最佳。在测试期间,基于模型的控制概念得到了良好的结果,并且即使在高扰动水平也被证明是坚固的。

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