A New Multi-Stage Turbine Stator Design for Improved Performance Retention

Author:

Jameson Heather K.1,Longley John P.1

Affiliation:

1. University of Cambridge Whittle Laboratory, , 1 J.J. Thomson Avenue, Cambridge CB3 0DY , UK

Abstract

Abstract An experimental and computational investigation has been undertaken into the effects of deterioration of the first-stage rotor-shroud knife-edge seal clearance in a two-stage turbine that has engine-representative cavity geometries. Four values of deterioration were investigated which cover the new-condition to old-condition knife-edge seal clearance. Measurements within the first-stage rotor-shroud cavity show that whilst the leakage mass flowrate increases with deterioration, the angle at which the leakage flow approaches the downstream stator is essentially fixed and independent of the flow coefficient. This agrees with a simple over-tip leakage model. Because of the engine-representative cavity geometry, the over-shroud-leakage flow undergoes little mixing when it re-enters the mainstream and approaches the downstream stator at more than 60-deg negative incidence. Detailed measurements at the exit of the second-stage stator identified two large positive vortices which were not consistent with the horseshoe vortex model for secondary flow. A computational investigation revealed that one vortex originates from the rolling-up within the stator passage of the streamwise vorticity sheet associated with the first-stage rotor over-shroud leakage. This roll-up vortex cannot be eliminated. The second vortex is generated within the stator passage by the separation of the over-shroud-leakage flow at the leading edge due to the large negative incidence. It was hypothesized that this separation vortex might be eliminated by locally redesigning the stator. A new stator was designed, manufactured, and tested. As predicted, the roll-up vortex was still present, but the separation vortex was eliminated. For all the values of deterioration tested, the entropy loss coefficient of the new stator and the unchanged second-stage rotor were reduced. It is estimated that the new stator would improve the lifetime average efficiency by 0.5% compared to the original.

Funder

Rolls-Royce

Publisher

ASME International

Subject

Mechanical Engineering

Reference26 articles.

1. Integrated Turbine Tip Clearance and Gas Turbine Engine Simulation;Chapman,2016

2. Turbine Engine Clearance Control Systems: Current Practices and Future Directions;Lattime,2002

3. IGTI Scholar Lecture: Loss Mechanisms in Turbomachines;Denton;ASME J. Turbomach.,1993

4. The Influence of the Clearance of Shrouded Rotor Blades on the Development of the Flowfield and Losses in the Subsequent Stator;Peters,2000

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