Studies on Performance Deterioration of a Low Bypass Turbofan Engine in Service

Author:

Mishra R. K.,Prakash L.,Srinivasan K.,Saravanan M.

Abstract

The performance deterioration of a low bypass turbofan engine is analyzed to find out its causes. The performance parameters are compared with their limitations for a specific throttle setting. Dirt buildup, soot deposit, de-twisting of turbine blades, malfunction of atomizers and fuel system accessories are found to degrade the engine health and performance before the intended service period. Periodic compressor wash and engine maintenance, cleaning or replacement of fuel filters and good assembly practices are found beneficial in addressing the issues and retaining the engine performance.

Reference18 articles.

1. Rainer Kurz and Klaus Brun., "Degradation of Gas Turbine Performance in Natural Gas Service", Journal of Natural Gas Science and Engineering, Vol.1, 2009, pp.95-102.

2. Nicholas, T., "High Cycle Fatigue Life Management in Gas Turbine Engines", RTO-AVTP Workshop on Qualification of Life Extension Schemes for Engine Components, Corfu, Greece, October 1998, NATO Pub., RTO-MP- 17, AC/323(AVT)TP/7, March 1999, pp.4-114-9.

3. Suresh, S., Fatigue of Materials, 2nd Edn., 2003, Cambridge University Press.

4. Philip P. Walsh and Paul Fletcher., "Gas Turbine Performance", 2004, Blackwell Science Ltd.

5. Mishra, R. K., "TBO Life Extension of a Military Turbojet Engine by Sampling", International Journal of Applied Engineering and Technology, Vol.3 (4), October-December, 2013, pp.23-32.

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