中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Effects of Nozzle-Strut Integrated Design Concepton on the Subsonic Turbine Stage Flowfield

文献类型:期刊论文

作者Liu Jun; Du Qiang; Liu Guang; Wang Pei; Zhu Junqiang
刊名JOURNAL OF THERMAL SCIENCE
出版日期2014-10-01
卷号23期号:5页码:494-504
关键词Intermediate Turbine Duct Integrated Design Concept Flowfield Analysis Total Pressure Loss Analysis
英文摘要In order to shorten aero-engine axial length, substituting the traditional long chord thick strut design accompanied with the traditional low pressure(LP) stage nozzle, LP turbine is integrated with intermediate turbine duct (ITD). In the current paper, five vanes of the first stage LP turbine nozzle is replaced with loaded struts for supporting the engine shaft, and providing oil pipes circumferentially which fulfilled the areo-engine structure requirement. However, their bulky geometric size represents a more effective obstacle to flow from high pressure (HP) turbine rotor. These five struts give obvious influence for not only the LP turbine nozzle but also the flowfield within the ITD, and hence cause higher loss.
WOS标题词Science & Technology ; Physical Sciences ; Technology
类目[WOS]Thermodynamics ; Engineering, Mechanical
研究领域[WOS]Thermodynamics ; Engineering
关键词[WOS]CLOCKING
收录类别SCI
语种英语
WOS记录号WOS:000341337200012
公开日期2015-12-22
源URL[http://ir.etp.ac.cn/handle/311046/106030]  
专题工程热物理研究所_中国科学院工程热物理所(论文库)_期刊论文(SCI)
作者单位Chinese Acad Sci, Inst Engn Thermophys, Beijing 100190, Peoples R China
推荐引用方式
GB/T 7714
Liu Jun,Du Qiang,Liu Guang,et al. Effects of Nozzle-Strut Integrated Design Concepton on the Subsonic Turbine Stage Flowfield[J]. JOURNAL OF THERMAL SCIENCE,2014,23(5):494-504.
APA Liu Jun,Du Qiang,Liu Guang,Wang Pei,&Zhu Junqiang.(2014).Effects of Nozzle-Strut Integrated Design Concepton on the Subsonic Turbine Stage Flowfield.JOURNAL OF THERMAL SCIENCE,23(5),494-504.
MLA Liu Jun,et al."Effects of Nozzle-Strut Integrated Design Concepton on the Subsonic Turbine Stage Flowfield".JOURNAL OF THERMAL SCIENCE 23.5(2014):494-504.

入库方式: OAI收割

来源:工程热物理研究所

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