首页> 外文会议>ASME Turbo Expo vol.2; 20050606-09; Reno-Tahoe,NV(US) >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气中燃料浓度和速度场的影响

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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:为了更好地了解工业应用中的受限旋流中的燃料-空气混合,对两个不同的西门子-西屋燃气涡轮混合器的流场进行了实验研究。混合器由环形流动区域组成,使用涡旋叶片实现混合,涡旋叶片的压力侧用于喷射燃料。所研究的两种混合器之间的差异在于旋流叶片赋予旋流的旋流度(45°与55°)。通过分别使用LDV和红外激光吸收技术,获得了非反应性大气压在旋流叶片下游的几个轴向和径向位置处流动的速度(轴向和方位角)和燃料浓度曲线。在这项工作中使用的燃料是甲烷/空气混合物,它的动量通量比与操作条件下的动量通量比相当。结果表明,与速度和燃料浓度曲线相比,对于45°混合器,旋流叶片比55°混合器的流动均匀性更高。这表明45°混合器的混合性能较差。 55°混合器的轴向和方位RMS速度始终较高,这可能是其出色混合性能的原因。高速和燃料浓度梯度对于两种混合器都是常见的,并且存在于旋流叶片附近的近场区域。所获得的数据表明,旋流叶片附近区域中的流动行为强烈影响燃料和空气的混合。燃料浓度数据的频率分析显示,在两个混合器的整个混合区域中都存在一些湍流结构,这表明即使在高度涡旋硬件中,也不会消散一些由涡旋叶片产生的大规模流动特征。最后,计算了两个测试混合器中的不混合度,并与关于它们如何影响NO_x排放水平的讨论进行了比较。

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