IMPACT OF THE PURGE FLOW DENSITY RATIO ON THE RIM SEALING EFFECTIVENESS IN HOT GAS INGESTION MEASUREMENTS

IF 1.9 3区 工程技术 Q3 ENGINEERING, MECHANICAL Journal of Turbomachinery-Transactions of the Asme Pub Date : 2023-10-31 DOI:10.1115/1.4063755
Lorenzo Orsini, Alessio Picchi, Bruno Facchini, Alessio Bonini, Luca Innocenti
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Abstract

Abstract The rim seals of gas turbines are used to control the ingestion of hot mainstream gas into the wheel space between the rotor disk and the stationary casing. Sealing air, which is generally used to pressurize the cavity space, flows through the seal clearance and then mixes with the flow path in the annulus. Predicting the correct quantity of purge flow necessary to prevent excessive ingestion of hot gases while, at the same time, minimizing the penalties in terms of engine efficiency and stage aerodynamics represents a great challenge for the designers and a crucial point for the design of reliable engines. Such estimate is governed by unsteady phenomena, and computational fluid dynamics (CFD) approaches are still expensive and time consuming, especially if 3D domains and unsteady conditions have to be simulated. Fundamental test cases, replicating actual engines geometries, are still a valid approach to calibrate correlations or simplified models such as the so-called orifice model. However, most of the experimental studies deal with test rigs at room temperature and do not take into account the effect of the density ratio (DR) between purge and main flows. To fill this gap, the present article reports the impact of the density ratio on the rim sealing effectiveness by performing a nonintrusive diagnostic based on the pressure-sensitive paint (PSP) technique on both the stator side and the rotor side. The analysis was performed on a cold rotating cavity rig, developed for the study of hot gas ingestion, where two different values of density ratios were tested by using N2 (DR = 1) and CO2 (DR = 1.52) as purge flow. The data extracted from the PSP seal effectiveness maps allowed to calibrate the orifice model for the stator side and to fit the coefficients of the buffer ratio model for the rotor surface at different flow conditions where the externally induced ingress is the dominant mechanism for gas ingestion. The results highlighted the impact of the DR on the seal effectiveness and on the low-order models considered for the data analysis. In the end, it is shown that the obtained results can be used to scale experimental data, generally collected at DR close to one, toward more representative engine values where the difference between the density of purge and main flows cannot be neglected.
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吹扫流量密度比对热气体吸入测量中边缘密封效果的影响
摘要燃气轮机的轮缘密封用于控制热主流气体进入转子盘和固定机匣之间的轮空间。密封空气,一般用来给空腔空间加压,通过密封间隙,然后与环空中的流道混合。预测正确的吹扫流量以防止过热气体的过量摄入,同时最大限度地减少发动机效率和级空气动力学方面的损失,这对设计师来说是一个巨大的挑战,也是设计可靠发动机的关键点。这种估计受非定常现象的影响,计算流体动力学(CFD)方法仍然昂贵且耗时,特别是在必须模拟三维区域和非定常条件时。复制实际发动机几何形状的基本测试用例仍然是校准相关性或简化模型(如所谓的孔板模型)的有效方法。然而,大多数实验研究都是在室温下进行的,没有考虑吹扫与主流之间的密度比(DR)的影响。为了填补这一空白,本文通过在定子侧和转子侧进行基于压敏涂料(PSP)技术的非侵入性诊断,报告了密度比对边缘密封有效性的影响。分析是在一个冷旋转腔钻机上进行的,该钻机是为研究热气体吸入而开发的,其中使用N2 (DR = 1)和CO2 (DR = 1.52)作为吹扫流量,测试了两种不同的密度比值。从PSP密封有效性图中提取的数据可以校准定子侧的孔板模型,并在不同的流动条件下拟合转子表面的缓冲比模型系数,其中外部诱导进入是气体吸入的主要机制。结果突出了DR对密封有效性和数据分析中考虑的低阶模型的影响。最后,结果表明,所得结果可用于将通常在DR接近1时收集的实验数据缩放到更具有代表性的发动机值,其中吹扫密度与主流密度之间的差异不容忽视。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
4.70
自引率
11.80%
发文量
168
审稿时长
9 months
期刊介绍: The Journal of Turbomachinery publishes archival-quality, peer-reviewed technical papers that advance the state-of-the-art of turbomachinery technology related to gas turbine engines. The broad scope of the subject matter includes the fluid dynamics, heat transfer, and aeromechanics technology associated with the design, analysis, modeling, testing, and performance of turbomachinery. Emphasis is placed on gas-path technologies associated with axial compressors, centrifugal compressors, and turbines. Topics: Aerodynamic design, analysis, and test of compressor and turbine blading; Compressor stall, surge, and operability issues; Heat transfer phenomena and film cooling design, analysis, and testing in turbines; Aeromechanical instabilities; Computational fluid dynamics (CFD) applied to turbomachinery, boundary layer development, measurement techniques, and cavity and leaking flows.
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