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0PERABILITY AND PERFORMANCE OF CENTRAL (PILOT) STAGE OF AN INDUSTRIAL PROTOTYPE BURNER

机译:0工业原型燃烧器的中央(试点)阶段的性能和性能

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An investigation on the central-pilot stage of a Siemens Industrial Turbomachinery 4th Generation DLE prototype test burner has been performed to understand the emission performance and operability. The core section, which is defined as RPL (Rich premixed lean) plays an important role for full burner combustion operation by stabilizing the main and pilot flames at different operating condition. Optimal fuel-air flow through the RPL is critical for multiple stages mixing and main flame anchoring. Heat and radical production from the central stage provides the ignition source and required heat for burning the main flame downstream of the RPL section. Surrounding the RPL outside wall cooling air has been blown through an annular passage. The cooling air protects the RPL wall from overheating and provides the oxygen source for the secondary combustion downstream of the RPL. At rich operation unburned hydrocarbon/radicals can pass the RPL and burns by the co-flow air entrainment. To determine the flame stabilization and operability, an atmospheric pressure test has been accomplished using methane as a fuel. Primary flame zone can be identified by a thermocouple placed outside the RPL wall and secondary combustion zone at the exit has been examined by chemiluminescence imaging. Emission measurement and LBO (Lean blow out) limits have been determined for different equivalence ratios from 1.8 to LBO limit. Co-flow air temperature was changed from 303 K to 573 K to evaluate the secondary combustion and RPL wall heat transfer effect on flame stability/emission. It is found that equivalence ratio has strong effect on the RPL flame stabilization (primary/secondary flame). Emissions/radical generation were also influenced by the chemical reaction inside the RPL. It can be noticed that co-flow air temperature has a significant role on emission, LBO and flame stabilization for the central-pilot stage burner due to the heat loss from the flame zone and RPL wall. A chemical kinetic network (Chemkin™) and CFD modelling approaches (Fluent) are employed to understand in detail the chemical kinetics, heat transfer effect and flow field inside the RPL (combustion and heat loss inside and emission capability). Experiment shows that the low CO and NOx levels can be achieved at lean and rich condition due to lower flame temperature. Present experimental results by changing equivalence ratio, residence time and co-flow temperature, creates a complete map for the RPL combustion, which is key input for full 4th Generation DLE burner design.
机译:为了了解排放性能和可操作性,已经对西门子工业涡轮机械公司第四代DLE原型测试燃烧器的中试阶段进行了调查。通过将主火焰和引燃火焰稳定在不同的工作条件下,定义为RPL(浓预混稀)的核心部分对于燃烧器的完全燃烧起着重要作用。通过RPL的最佳燃料空气流量对于多级混合和主火焰锚固至关重要。中央阶段产生的热量和自由基产生了点火源,并为燃烧RPL部分下游的主火焰提供了所需的热量。 RPL外壁周围的冷却空气已通过环形通道吹出。冷却空气可防止RPL壁过热,并为RPL下游的二次燃烧提供氧气源。在富油运行时,未燃烧的碳氢化合物/基团可以通过RPL,并通过气流夹带而燃烧。为了确定火焰的稳定性和可操作性,已经使用甲烷作为燃料完成了大气压测试。可以通过放置在RPL壁外侧的热电偶来识别主要火焰区域,并且已经通过化学发光成像检查了出口处的次要燃烧区域。对于从1.8到LBO限值的不同当量比,已经确定了排放量测量值和LBO(精益爆燃)限值。并流空气温度从303 K更改为573 K,以评估二次燃烧和RPL壁传热对火焰稳定性/排放的影响。发现当量比对RPL火焰稳定度(一次/二次火焰)有很强的影响。 RPL内部的化学反应也会影响排放/自由基的产生。可以注意到,由于来自火焰区和RPL壁的热量损失,并流空气温度对中央先导燃烧器的排放,LBO和火焰稳定度具有重要作用。使用化学动力学网络(Chemkin™)和CFD建模方法(Fluent)来详细了解RPL内部的化学动力学,传热效果和流场(内部的燃烧和热损失以及排放能力)。实验表明,由于火焰温度较低,因此在稀薄和浓稠条件下均可实现较低的CO和NOx含量。通过改变当量比,停留时间和同流温度获得的当前实验结果为RPL燃烧创建了完整的映射,这是完整的第四代DLE燃烧器设计的关键输入。

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