首页 | 本学科首页   官方微博 | 高级检索  
     检索      

透平内部非稳态流动试验研究进展
引用本文:邵梓一,李文,张雪辉,陈海生.透平内部非稳态流动试验研究进展[J].推进技术,2019,40(10):2161-2174.
作者姓名:邵梓一  李文  张雪辉  陈海生
作者单位:1.中国科学院工程热物理研究所,北京 100190;2.中国科学院大学 工程科学学院,北京;100049
基金项目:国家自然科学基金 51606188 51522605;“九七三”计划 2015CB251302;中国科学院前沿科学重点研究项目 QYZDB-SSW-JSC023;北京市科技计划项目 D161100004616001 D161100004616002国家自然科学基金(51606188;51522605);“九七三”计划(2015CB251302);中国科学院前沿科学重点研究项目(QYZDB-SSW-JSC023);北京市科技计划项目(D161100004616001;D161100004616002)。
摘    要:为探究透平内部流场的非稳态特性及其演变特征,通过归纳国内外透平内部流动的试验研究,回顾了轴流透平、向心透平采用的试验方法及取得的研究进展,分析总结了试验方案与研究中存在的问题。目前,轴流式透平与平面叶栅的试验数量较多,试验的压力温度较低;向心式透平试验研究还比较少,并且试验多处于高温高压环境;随着接触式测量设备性能的大幅提升,其目前在透平非稳态试验中得到广泛应用,例如气动探针已经能够满足1×106Hz的高频采集要求;上游尾迹以及叶顶泄漏涡扰动下轴流式透平叶表附面层的转捩机制,以及向心式透平盘腔泄漏流与主流流场的非定常掺混等问题还有待进一步研究。

关 键 词:透平  内部流场  试验研究  非稳态流动  动静干涉  二次涡  尾迹  综述
收稿时间:2018/11/11 0:00:00
修稿时间:2019/1/3 0:00:00

Experimental Research Progress on InternalUnsteady Flow of Turbine
SHAO Zi-yi,LI Wen,ZHANG Xue-hui,CHEN Hai-sheng.Experimental Research Progress on InternalUnsteady Flow of Turbine[J].Journal of Propulsion Technology,2019,40(10):2161-2174.
Authors:SHAO Zi-yi  LI Wen  ZHANG Xue-hui  CHEN Hai-sheng
Institution:1.Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China;2.School of Engineering Science,University of Chinese Academy of Sciences,Beijing 100049,China
Abstract:To clarify the unsteadiness and evolution process of internal flow field in turbines, the experimental method and research progress of the axial turbine and radial turbine were reviewed based on domestic and foreign researches, and some disadvantages of present experimental scheme and research were also performed. The results show that experiments, whose pressure and temperature are usually low, in axial turbines and linear cascades have been widely investigated, while relatively less experiments, whose pressure and temperature are relatively high, in radial turbines can be seen in the existing literatures. The contact measurement has been widely used in unsteady experiments of turbines for its increasingly improved performance. For example, the pneumatic probes could meet the requirement of high sampling rate, which may be up to 1×106Hz, very well. However, the transition mechanisms of surface boundary layer under the disturbance of upstream wake and tip leakage vortex in axial turbines are still not fully explained and need further researches, so does the unsteady mixing between the cavity leakage flow and the main flow in radial turbines.
Keywords:Turbine  Internal flow field  Experimental research  Unsteady flow  Rotor-stator interaction  Secondary vortex  Wake  Review
本文献已被 CNKI 等数据库收录!
点击此处可从《推进技术》浏览原始摘要信息
点击此处可从《推进技术》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号