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1+1/2对转涡轮设计及控制方法探索
引用本文:季路成,肖翔,陈江. 1+1/2对转涡轮设计及控制方法探索[J]. 工程热物理学报, 2004, 25(3): 405-407
作者姓名:季路成  肖翔  陈江
作者单位:中国科学院工程热物理研究所,北京,100080;北京航空航天大学,北京,100083
基金项目:国家自然科学基金(No.50376062),中国科学院知识创新工程项目资助(No.KGCX2-301)
摘    要:本文对 1 1/2对转涡轮试验件进行了详细设计,并对其控制问题进行了初步探讨,结果表明所设计 1 1/2对转涡轮基本达到设计要求,其控制问题由高压静叶可调和尾喷管面积调节共同解决。

关 键 词:对转涡轮  设计  叶轮机
文章编号:0253-231X(2004)03-0405-03
修稿时间:2003-12-08

NUMERICAL INVESTIGATIONS ABOUT THE VANELESS COUNTER-ROTATING TURBINE FOR THE COLD-AIR TEST
JI Lu--Cheng,XIAO Xiang,CHEN Jiang Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing ,China Beijing University of Aeronautics and Astronautics,Beijing ,China. NUMERICAL INVESTIGATIONS ABOUT THE VANELESS COUNTER-ROTATING TURBINE FOR THE COLD-AIR TEST[J]. Journal of Engineering Thermophysics, 2004, 25(3): 405-407
Authors:JI Lu--Cheng  XIAO Xiang  CHEN Jiang Institute of Engineering Thermophysics  Chinese Academy of Sciences  Beijing   China Beijing University of Aeronautics  Astronautics  Beijing   China
Affiliation:JI Lu--Cheng,XIAO Xiang,CHEN Jiang Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100080,China Beijing University of Aeronautics and Astronautics,Beijing 100083,China
Abstract:Detailed design and operating method of Vaneless Counter-Rotating Turbine (VCRT) arenumerical investigated in present paper. Results indicate the performance of the VCRT might beproper for practical use. Numerical investigations about the control problem in engines, whicn use thistype of VCRT, show that the engine with VCRT can be operated via combining variable throat vanewith the method of changing engine exhaust nozzle area.
Keywords:counter-rotating turbine  turbomachinery  design  unsteady design
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