Design of a Wide-Range Centrifugal Compressor Stage for Supercritical CO2 Power Cycles

Author:

Pelton Robert1,Jung Sewoong1,Allison Tim2,Smith Natalie2

Affiliation:

1. Hanwha Power Systems Americas, Houston, TX 77079 e-mail:

2. Southwest Research Institute, San Antonio, TX 78238 e-mail:

Abstract

Supercritical carbon dioxide (sCO2) power cycles require high compressor efficiency at both the design point and over a wide operating range. Increasing the compressor efficiency and range helps maximize the power output of the cycle and allows operation over a broader range of transient and part-load operating conditions. For sCO2 cycles operating with compressor inlets near the critical point, large variations in fluid properties are possible with small changes in temperature or pressure. This leads to particular challenges for air-cooled cycles where compressor inlet temperature and associated fluid density are subject to daily and seasonal variations as well as transient events. Design and off-design operating requirements for a wide-range compressor impeller are presented where the impeller is implemented on an integrally geared compressor–expander concept for a high temperature sCO2 recompression cycle. In order to satisfy the range and efficiency requirements of the cycle, a novel compressor stage design incorporating a semi-open impeller concept with a passive recirculating casing treatment is presented that mitigates inducer stall and extends the low flow operating range. The stage design also incorporates splitter blades and a vaneless diffuser to maximize efficiency and operating range. These advanced impeller design features are enabled through the use of direct metal laser sintering (DMLS) manufacturing. The resulting design increases the range from 45% to 73% relative to a conventional closed impeller design while maintaining high design point efficiency.

Funder

Office of Energy Efficiency and Renewable Energy

Publisher

ASME International

Subject

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

Reference22 articles.

1. Wilkes, J., Allison, T., Schmitt, J., Bennett, J., Wygant, K., Pelton, R., and Bosen, W., 2016, “Application of an Integrally Geared Compander to an sCO2 Recompression Brayton Cycle,” Fifth International Symposium—Supercritical CO2 Power Cycles, San Antonio, TX, Mar. 28–31, Paper No. 055.http://www.sco2symposium.com/www2/sco2/papers2016/Turbomachinery/055paper.pdf

2. Cycle Modeling and Optimization of an Integrally Geared sCO2 Compander,2017

3. Centrifugal Compressor Inlet Guide Vanes for Increased Surge;ASME J. Turbomach.,1990

4. Novel IGV Designs for Centrifugal Compressors and Their Interaction With the Impeller;ASME J. Turbomach.,2012

5. Selection of High Performance Low Flow Compressors,1986

Cited by 13 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