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A NEW TAILPIPE DESIGN FOR GE FRAME TYPE GAS TURBINES TO SUBSTANTIALLY LOWER PRESSURE LOSSES

机译:GE帧型燃气轮机的新尾管设计,以基本较低的压力损失

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Many GE frame gas turbines have a unique 90-degree tailpipe exhaust system that contains struts, diffusers, and turning vanes. As confirmed in a recent report by GE and other authors, it is known in the industry that this tailpipe design has large pressure losses. In this recent report a pressure loss as high as 60 inches of water (0.15 kgs/sqcm) was cited. Due to the flow separations they create, the report indicates that the struts can cause very high-pressure losses in the turbine. The report also states that these pressure losses can vary with different turbine load conditions. Cheng Fluid Systems and Cheng Power Systems have conducted a study aimed at substantially reducing these pressure losses. Flow control technology introduced to the refinery industry, i.e., the Cheng Rotation Vane (CRV) and the Large Angle Diffuser (LAD) can be used to mitigate the flow separation and turbulence that occurs in turns, bends, and large sudden expansions. Specifically the CRV addresses the flow separations in pipe turns, and the LAD addresses the flow problems that occur with large sudden expansion areas. The paper will introduce the past experience of the CRV and LAD, and will then use computer simulations to show the flow characteristics around a new design. First, the study meticulously goes through the entire GE exhaust system, starting with the redesign of the airfoil shape surrounding the struts. This new design has a larger angle of attack and minimizes the flow separations over a much wider operating range. Second, the pros and cons of the concentric turning vanes are studied and it is shown that they are more flow restrictive, rather than flow enhancing. Third, it is shown that the highly turbulent rectangular box type exhaust ducting design, substantially contributes to high noise levels and pressure losses. In this paper a completed design will be shown that incorporates a new airfoil shape for the struts, and by using CRV flow technology in combination with the LAD flow technology, the pressure recovery can be enhanced. If the pressure losses could be reduced by 40 inches of water (0.10 kgs/sqcm), the turbine efficiency could be increased by 5 %, and the power output could be increased by 6 %.
机译:许多GE帧燃气轮机具有独特的90度尾管排气系统,该排气系统包含支柱,漫射器和转动叶片。正如GE和其他作者最近的一份报告中确认,它在该行业中已知这种尾气设计具有大的压力损失。在该近期报告中,引用了高达60英寸水(0.15kgs / sqcm)的压力损失。由于它们创造的流动分离,该报告表明Struts可以在涡轮机中引起非常高压的损失。该报告还指出,这些压力损失可以随着不同的涡轮机负荷条件而变化。程液系统和程力系统已经进行了一项旨在显着降低这些压力损失的研究。引入炼油厂工业的流量控制技术,即程旋转叶片(CRV)和大角度漫射器(LAD)可用于减轻匝数,弯曲和大突然扩展的流动分离和湍流。具体地,CRV地址管道中的流动分离,LAD地址大突然扩展区域发生的流量问题。本文将介绍CRV和LAD的过去经验,然后将使用计算机模拟来显示新设计周围的流动特性。首先,研究精心地通过整个GE排气系统,从围绕支柱围绕翼型形状的重新设计开始。这种新设计具有较大的攻击角度,并最大限度地减少了更宽的工作范围内的流量分离。其次,研究了同心转叶片的优点和缺点,并表明它们更加流动限制,而不是流动增强。第三,示出了高度湍流矩形箱式排气管道设计,基本上有助于高噪声水平和压力损失。在本文中,将显示完成的设计,其包括用于支柱的新型翼型形状,并且通过使用CRV流技术与LAD流程技术结合,可以提高压力恢复。如果压力损失可以减少40英寸的水(0.10kgs / sqcm),则涡轮机效率可以提高5%,功率输出可以增加6%。

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