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jimyang2008木虫 (正式写手)
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[求助]
帮忙查询一篇论文EI收录情况 已有1人参与
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谁能帮忙查询一下论文EI收录号，并将收录页面以网页截图或网页（html）形式发送到邮箱：jimyang2008@163.com. 先谢谢大家了！ 论文题目 Study on negative effects on rotational speeds difference caused by turbine fan engine gas path components performance deteriorations 作者 yang xin-yi shen wei,... 发表期刊 journal of propulsion technology vol35. no.6 may 2014 |
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Accession number: 20142217763955 Title: Study on negative effects on rotational speeds difference caused by turbine fan engine gas path components performance deteriorations Authors: Yang, Xin-Yi1; Shen, Wei1; Wang, Yong-Hua1; Zhao, Yong2; Song, Han-Qiang2 Author affiliation: 1 Department of Aerocraft Engineering, Naval Aeronautical and Astronautical University, Yantai 264001, China 2 Graduate Students' Brigade, Naval Aeronautical and Astronautical University, Yantai 264001, China Corresponding author: Yang, X.-Y. Source title: Tuijin Jishu/Journal of Propulsion Technology Abbreviated source title: Tuijin Jishu Volume: 35 Issue: 5 Issue date: May 2014 Publication year: 2014 Pages: 610-617 Language: Chinese ISSN: 10014055 CODEN: TUJIEG Document type: Journal article (JA) Publisher: Journal of Propulsion Technology, P.O. Box 7208-26, Beijing, 100074, China Abstract: Studies on the relationship between turbine fan engine gas path components performance deterioration and the rotational speeds difference (difference between low pressure rotor speeds when afterburner is turned on and off) are necessary but urgently needed. In order to obtain a clear picture on this relationship, the engine model and surface fitting technique were used and the rotational speed difference surfaces interrelating gas path component air flow rate and efficiency parameters were obtained. They were then compared with rotational speed difference threshold and gas path components performance parameter envelops which satisfied the difference threshold requirement were obtained. The study demonstrates that the compressor has more negative effects on rotationed speed difference than turbine and low-pressure compressor affects the most among all the gas path components. For each component, efficiency parameter has more impact than flow rate parameter. The results indicate compressor components deterioration have negative effects on afterburner system performance and need more monitoring. The study also provides theoretical foundation for maintaining good performance and reliable work of the engine afterburner system. Number of references: 16 Main heading: Afterburners (engine) Controlled terms: Afterburners (oven) - Compressors - Deterioration - Engines - Flow rate - Particle swarm optimization (PSO) - Speed - Turbines Uncontrolled terms: Component characteristics - Efficiency parameters - Moving least squares - Performance deterioration - Performance parameters - Quantum-behaved particle swarm optimization - Surface fitting technique - Theoretical foundations Classification code: 951 Materials Science - 931.1 Mechanics - 723 Computer Software, Data Handling and Applications - 642.2 Industrial Furnaces and Components - 631 Fluid Flow - 618.1 Compressors - 612 Engines Database: Compendex |
2楼2014-07-08 18:09:39
jimyang2008
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