Determination of a Numerical Surge Limit by Means of an Enhanced Greitzer Compressor Model

IF 1.3 Q2 ENGINEERING, AEROSPACE
Tobias Haeckel, Dominik Paul, Sebastian Leichtfuß, Heinz-Peter Schiffer, Werner Eißler
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引用次数: 0

Abstract

The surge limit of centrifugal compressors is a key parameter in the design process of modern turbochargers. Numerical methods like steady-state simulations are state-of-the-art methods for predicting the performance of the centrifugal compressor. In contrast to that, the determination of the surge limit with any numerical method is still an unsolved challenge. Since the extensive work of Greitzer and many other researchers in this field, it is well-known that surge is a system-dependent phenomenon. In the case of steady-state simulations, the simulation domain is chosen to be as small as possible due to the numerical cost. This simply implies that there is no system information included in the numerical model. Therefore, it is not possible to determine any system-dependent surge limit with today’s applied numerical methods. To overcome this issue, an enhanced Greitzer surge model, which has been developed at Tu Darmstadt, should act as a link between the simulation and the system in which the compressor will be operated. The focus of this paper will rather be on the methodology of determining the surge limit by means of numerical data than on the surge model itself. The methodology will be validated by experimental data of different systems.
用增强型Greitzer压缩机模型确定喘振数值极限
离心式压气机喘振极限是现代涡轮增压器设计过程中的一个关键参数。稳态模拟等数值方法是预测离心式压缩机性能的最先进方法。相比之下,用任何数值方法确定浪涌极限仍然是一个未解决的挑战。由于格雷策和许多其他研究人员在这一领域的广泛工作,众所周知,激增是一种系统依赖现象。在稳态仿真的情况下,由于数值代价的考虑,选择的仿真域尽可能小。这仅仅意味着数值模型中不包含系统信息。因此,目前应用的数值方法不可能确定任何系统相关的浪涌极限。为了克服这个问题,Tu Darmstadt开发的增强型Greitzer喘振模型应该作为模拟和压缩机运行系统之间的联系。本文的重点将放在利用数值数据确定浪涌极限的方法上,而不是讨论浪涌模型本身。该方法将通过不同系统的实验数据进行验证。
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
2.30
自引率
21.40%
发文量
29
审稿时长
11 weeks
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