Design and Experiment of Casing Treatment for a Centrifugal Compressor

Author:

Peng Wenwen1,Zou Xueqi1,Qin Sunde1

Affiliation:

1. China Aviation Powerplant Research Institute , Zhuzhou 412002 , China

Abstract

Abstract Centrifugal compressors have been widely used in light-duty turboshaft engines and automotive turbochargers. One of the essential requirements for centrifugal compressors in these applications is to have adequate stable flow range. As the pressure ratio increases, the stable flow range drops dramatically, and this highlights the importance of stability improvement for centrifugal compressors. This paper first gives a brief review on the measures available for extending the stable flow range, and then focuses on the realization of self-recirculating casing treatment for a centrifugal compressor. The design principles of the casing treatment were introduced. Then the simulations were conducted to design and optimize the geometry of the casing treatment, and finally an optimum case was selected for experimental validation. The experiment results indicate that the designed casing treatment improve the stable flow range by about 5 percent at design speed, while keeping the efficiency almost identical.

Publisher

Walter de Gruyter GmbH

Subject

Aerospace Engineering

Reference73 articles.

1. Krain H. Review of centrifugal compressor’s application and development. J Turbomach. 2005;127:25–34.

2. Ebrahimi M, Huang QQ, He X, Zheng XQ. Effects of variable diffuser vanes on performance of a centrifugal compressor with pressure ratio of 8.0. Energies. 2017;10:682.

3. Zheng XQ, Zhang YJ, Yang MY. Research and development on transonic compressor of high pressure ratio turbocharger for vehicle internal combustion engines. Sci China Ser E-Tech Sci. 2010;53:1817–23.

4. Chen T, Zhang YJ, Zheng XQ, Zhuge WL. Compressor design for multi-point operating conditions of turbocharged gasoline engines. Proceedings of ASME Turbo Expo 2010: Power for Land, Sea and Air, Glasgow, UK, June 14–18 2010, No. GT2010–22283.

5. Rodgers C. The efficiencies of single-stage centrifugal compressors for aircraft applications. International Gas Turbine and Aero-engine Congress and Exposition, Orlando, USA, June 3–6, 1991. No. 91-GT–77, 1991.

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

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