首页> 外文会议>ASME Turbo Expo: Turbomachinery Technical Conference and Exposition >COMBUSTION INSTABILITIES DAMPING SYSTEM DEVELOPMENT FOR DRY LOW NOX EMISSIONS OPERABILITY ENHANCEMENT OF A HEAVY-DUTY GAS TURBINE
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COMBUSTION INSTABILITIES DAMPING SYSTEM DEVELOPMENT FOR DRY LOW NOX EMISSIONS OPERABILITY ENHANCEMENT OF A HEAVY-DUTY GAS TURBINE

机译:重型燃气轮机干式低NOx排放的可燃性提高的燃烧不稳定性阻尼系统开发

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This paper describes the development phases of a damping system for combustion instability reduction in an annular type combustor for heavy-duty gas turbine applications. As reported by the authors in a previous paper, the full scale annular test rig allowed for an extensive characterization of the combustor with realistic acoustic boundaries at engine-relevant conditions. Emissions and operability assessment over a wide range of load conditions was performed, allowing the evaluation of the response of the system near the thermo-acoustic instability onset. The instability is quantified by its acoustic growth rate. This quantity is a crucial input in the design process of dampers. A methodology has been used to extract these growth rates form measured pulsation data. Experimentally determined growth rates have been evaluated for different fuel flow rate split between the main and the pilot injections, providing input to dampers preliminary design. Given current combustor architecture constraints, a first attempt configuration has been proposed and performances evaluated in the full annular rig. Dampers have been equipped with dynamic sensors and thermocouples with the purpose of measuring the growth rate abatement and the consequent NOx emissions reduction. A dedicated numerical toolbox, in-house developed by GE Power, has been used for both dampers preliminary design and growth rate reduction evaluation. Fine tuning of dampers elements as well as design assumptions adjustments required additional experimental evaluations and design iterations. Encouraged by the successful test in the concept phase, an optimized design for engine implementation was defined, that featured a significant increased damper volume, involving combustor parts re-design. The optimized configuration was finally tested in full annular rig and results demonstrated an important enhancement of operability while maintaining NOx emissions below the target levels.
机译:本文介绍了用于重型燃气轮机应用的环形燃烧器的燃烧系统减震系统的发展阶段。正如作者在以前的论文中所报道的那样,全尺寸环形试验台可以在与发动机相关的条件下对燃烧室进行广泛的表征,并具有真实的声边界。在广泛的负载条件下进行了排放和可操作性评估,从而可以评估热声不稳定开始附近的系统响应。不稳定性通过其声增长率来量化。该数量是风门设计过程中的关键输入。已经使用一种方法从测得的脉动数据中提取这些增长率。对于主喷射和引燃喷射之间的不同燃料流量分配,已经评估了实验确定的增长率,为减震器的初步设计提供了输入。给定当前的燃烧室结构约束,已经提出了首次尝试配置,并在全环形钻机中评估了性能。阻尼器已配备了动态传感器和热电偶,目的是测量增长率的降低和随之而来的NOx排放量的减少。 GE Power内部开发的专用数值工具箱已用于阻尼器的初步设计和增长率降低评估。阻尼器元件的微调以及设计假设的调整需要额外的实验评估和设计迭代。在概念阶段的成功测试的鼓舞下,定义了一种用于发动机实施的优化设计,该设计具有显着增加的风门体积,涉及燃烧器部件的重新设计。最后在全环形钻机上对优化配置进行了测试,结果证明了可操作性的显着提高,同时将NOx排放保持在目标水平以下。

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