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 |
| 卷 | 29 |
| 期 | 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
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