The Effects of Fluid Preswirl and Swirl Brakes Design on the Performance of Labyrinth Seals

Author:

Untaroiu Alexandrina1,Jin Hanxiang2,Fu Gen2,Hayrapetiau Vahe3,Elebiary Kariem4

Affiliation:

1. Laboratory for Turbomachinery and Components, Department of Biomedical Engineering and Mechanics, Virginia Tech, Norris Hall, Room 324, Virginia Tech 495 Old Turner Street, Blacksburg, VA 24061 e-mail:

2. Laboratory for Turbomachinery and Components, Department of Biomedical Engineering and Mechanics, Virginia Tech, Norris Hall, Room 107, Virginia Tech 495 Old Turner Street, Blacksburg, VA 24061 e-mail:

3. Flowserve Corporation, 2300 E Vernon Avenue, Vernon, CA 90058 e-mail:

4. Flowserve Corporation, 2300 E Vernon Avenue, Vernon, CA 90058, e-mail:

Abstract

In noncontact annular labyrinth seals used in turbomachinery, fluid prerotation in the direction of shaft rotation effectively increases fluid velocity in the circumferential direction and generates fluid forces with potential destabilizing effects to be exerted on the rotor. Swirl brakes are typically employed to reduce the fluid prerotation at the inlet of the seal. The inlet flow separates as it follows the swirl brakes, and the ratio between tangential component of the velocity at the seal, and the velocity of the rotor surface varies consequently. Effective swirl brakes can significantly suppress the destabilizing fluid forces as it is effectively reducing the tangential velocity. The literature shows that leakage rate can also be reduced by using swirl brakes with “negative-swirl.” In this study, a labyrinth seal with inlet swirl brakes is selected from the literature and considered the baseline design. The seal performance is evaluated using ANSYS-cfx. The design of experiments (DOEs) approach is used to investigate the effects of various design variables on the seal performance. The design space consists of the swirl brake's length, width, curvature at the ends, the tilt angle, as well as the number of swirl brakes in the circumferential direction. Simple random sampling method with Euclidean distances for the design matrix is used to generate the design points. Steady-state computational fluid dynamics simulations are then performed for each design point to analyze the performance of the swirl brakes. Quadratic polynomial fitting is used to evaluate the sensitivity of the average circumferential velocity with respect to the design variables, which gives a qualitative estimation for the performance of the swirl brakes. These results assist in creating a better understanding of which design variables are critical and more effective in reduction of the destabilizing forces acting on the rotor, and thus will support the swirl brake design for annular pressure seals.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference19 articles.

1. Benckert, H., and Wachter, J., 1980, “Flow Induced Spring Constants of Labyrinth Seals,” The Second International Conference on Vibrations Rotating Machinery, Cambridge, UK, Sept. 1–4, pp. 53–63.

2. Benckert, H., and Wachter, J., 1980, “Flow Induced Spring Coefficients of Labyrinth Seals for Applications in Rotor Dynamics,” The Rotordynamic Instability Problems in High-Performance Turbomachinery Workshop, College Station, TX, May 12–14, pp. 189–212.https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19800021216.pdf

3. A Test Apparatus and Facility to Identify the Rotordynamic Coefficients of High-Speed Hydrostatic Bearings;ASME J.Tribol.,1994

4. Experimental Test-Results for 4 High-Speed, High-Pressure, Orifice-Compensated Hybrid Bearings;ASME J. Tribol.,1994

5. Moore, J., Walker, S., and Kuzdal, M., 2002, “Rotordynamic Stability Measurement During Full-Load, Full-Pressure Testing of a 6000 Psi Reinjection Centrifugal Compressor,” 31st Turbomachinery Symposium, Houston, TX, pp. 29–38.http://oaktrust.library.tamu.edu/handle/1969.1/163317

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3