首页> 外文会议>ASME Turbo Expo >AN INVESTIGATION OF THE EFFECT OF SWIRL VANE ANGLE ON FUEL CONCENTRATION AND VELOCITY FIELDS IN GAS TURBINE MIXERS
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AN INVESTIGATION OF THE EFFECT OF SWIRL VANE ANGLE ON FUEL CONCENTRATION AND VELOCITY FIELDS IN GAS TURBINE MIXERS

机译:旋流叶片角度对燃气轮机混合器燃料浓度和速度场效果的研究

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The flow fields of two different Siemens-Westinghouse gas turbine mixers were studied experimentally in an effort to better understand fuel-air mixing in confined swirling flows found in industrial applications. The mixers consist of an annular flow region and mixing is achieved using swirl vanes, the pressure side of which is used to inject the fuel. The difference between the two mixers studied is the degree of swirl imparted on the flow by the swirl vanes (45° vs. 55°). Velocity (both axial and azimuthal) and fuel concentration profiles were obtained for non-reacting, atmospheric pressure flows at several axial and radial locations downstream of the swirl vanes by the use of LDV and infrared laser light absorption techniques, respectively. The fuel used in this work was a methane/air mixture, which was injected at a momentum flux ratio comparable to that under operational conditions. Results show that flow uniformity, as evidenced by velocity and fuel concentration profiles, is reached further downstream of the swirl vanes for the 45° mixer than for the 55° mixer. This indicates a lesser mixing performance in the 45° mixer. The axial and azimuthal RMS velocities were consistently higher for the 55° degree mixer and this was a likely contributor to its superior mixing performance. High velocity and fuel concentration gradients are common for both mixers and present in the near-field region close to the swirl vanes. The data obtained indicates that the flow behavior in the region near the swirl vanes strongly influences the mixing of the fuel and air. Frequency analysis of the fuel concentration data shows that some turbulent structures prevail throughout the mixing region in both mixers, revealing that some large scale flow features emanating from the swirl vanes are not dissipated even in the high degree of swirl hardware. Lastly, unmixedness levels in both mixers tested are calculated and compared with a discussion on how they might impact NO_x emission levels.
机译:实验研究了两种不同西门子 - 西屋燃气轮机搅拌机的流场,以便在工业应用中发现的狭窄旋流中更好地了解燃料空气混合。使用旋涡叶片的环形流动区域和混合组成,使用旋流叶片,其压力侧用于喷射燃料。所研究的两个混合器之间的差异是旋流叶片(45°与55°)上施加在流动上的旋涡的程度。在旋流叶片下游的几个轴向和径向位置处,通过使用LDV和红外激光吸收技术,获得速度(轴向和方位角)和燃料浓度剖面的速度(轴向和方位角)和燃料浓度分布。本作作品中使用的燃料是甲烷/空气混合物,其以与运行条件下的动量助熔剂比注入。结果表明,流动均匀性,如速度和燃料浓度型材所证明的,在旋流叶片的进一步下游,对于55°混合器,在旋流叶片的下游比55°混合器更进一步。这表示45°混合器中的混合性能较小。对于55°程度混合器,轴向和方位的速率速度始终较高,这是其优异的混合性能的可能结果。对于两个混合器,高速和燃料浓度梯度常见并且存在于靠近旋流叶片的近场区域中。所获得的数据表明,旋流叶片附近的区域中的流动性强烈影响燃料和空气的混合。燃料浓度数据的频率分析表明,在两个混合器中的整个混合区域中,一些湍流结构占据,揭示了从旋流叶片发出的一些大规模流量,即使在高度的涡流硬件中也不会消散。最后,计算了两种混合器中的解密级别,并与讨论它们如何影响No_X发射水平的讨论进行比较。

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