跳到主要导航 跳到搜索 跳到主要内容

Aerodynamic design of three-stage vaneless counter-rotating turbine

  • Beihang University
  • China Aviation Industry Corporation

科研成果: 期刊稿件文章同行评审

摘要

An aerodynamic design criterion was discussed for the 1+3/2 counter-rotating turbine by analyzing the velocity triangles. There are 8 key aerodynamic parameters in the criterion, based on the consideration of aerodynamic efficiency and some strength requirements. Then, an aerodynamic design for the 1+3/2 counter-rotating turbine was made according to the criterion, and a three-dimensional simulation was conducted for it. Finally, the conclusions were obtained. The criterion containing 8 key aerodynamic parameters is verified rationally and the efficiency of the turbine reaches 91%. The aerodynamic characteristics of 1+3/2 counter-rotating turbine are mainly decided by the load coefficient, and due to an optimal power distribution coefficient of the low pressure turbine, the efficiency of the low pressure turbine can be best.

源语言英语
页(从-至)1667-1679
页数13
期刊Hangkong Dongli Xuebao/Journal of Aerospace Power
29
7
DOI
出版状态已出版 - 7月 2014

指纹

探究 'Aerodynamic design of three-stage vaneless counter-rotating turbine' 的科研主题。它们共同构成独一无二的指纹。

引用此