Three-dimensional optimal design of a cooled turbine considering the coolant-requirement change

Author:

Ba Wei1,Wang Ziyuan1,Li Xuesong1,Gu Chunwei1

Affiliation:

1. Tsinghua University Beijing , Beijing China

Abstract

Abstract Cooling technology is widely applied in modern turbines to protect the turbine blades, and extracting high-pressure cooling air from a compressor exerts a remarkable influence on the gas-turbine performance. However, the three-dimensional optimal design of a turbine in modern industrial practice is usually carried out by pursuing high component efficiency without considering possible changes in coolant requirement; hence, it may not exactly lead to improvement in the gas-turbine cycle efficiency. In this study, the turbine stator was twisted and leaned to achieve higher comprehensive efficiency, which is the cycle-based efficiency definition for a cooled turbine that considers both turbine aerodynamic performance and coolant requirement. First, the influence of twist and compound lean on turbine aerodynamic performance, considering stator-hub leakage, was investigated. Then, a method to predict the coolant requirement for turbines with different stator designs was applied, to evaluate coolant-requirement change at the design condition. The optimized turbines were finally compared to demonstrate the necessity of considering the coolant-requirement change in the optimal design. This indicated that proper twisting to open the throat area in the stator hub and compound lean to the pressure surface side could help improve the cooled-turbine comprehensive efficiency.

Publisher

Walter de Gruyter GmbH

Subject

General Physics and Astronomy

Reference26 articles.

1. Han J. C., Dutta S., Ekkad S., Gas turbine heat transfer and cooling technology, 2012, CRC press, Boca Raton.

2. Öksüz Ö., Akmandor İ. S., Multi-objective aerodynamic optimization of axial turbine blades using a novel multilevel genetic algorithm, Journal of Turbomachinery, 2010, 132(4): 041009.

3. Denton J. D., Xu L., The exploitation of three-dimensional flow in turbomachinery design, Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 1998, 213(2): 125-137.

4. Grant J., Borthwick D., Fully 3D Inviscid Flow Calculations for the Final Stage of a Large, Low-Pressure Steam Turbine, Turbomachinery—Efficiency Prediction and Improvement, 1987: 1987-6.

5. Hourmouziadis J., Hübner N., 3-d design of turbine airfoils, ASME 1985 International Gas Turbine Conference and Exhibit, American Society of Mechanical Engineers, 1985: V001T03A045-V001T03A045.

Cited by 1 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

1. Estimation of cooling flow rate for conceptual design stage of a gas turbine engine;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2021-05-29

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