1. 南华动力机械研究所
2. 燃气涡轮研究所
3. 沈阳发动机研究所
Published:1989
移动端阅览
Han Jianyuan, Shi Jing, Cheng Xinhua, et al. EFFECT OF VANE AND BLADE NUMBERS ON PERFORMANCE OF TRANSONIC TURBINE STAGE[J]. 1989, 4(4).
DOI:
Han Jianyuan, Shi Jing, Cheng Xinhua, et al. EFFECT OF VANE AND BLADE NUMBERS ON PERFORMANCE OF TRANSONIC TURBINE STAGE[J]. 1989, 4(4). DOI:
导叶叶片数变化对跨音速涡轮性能的影响基本级涡轮A具有动叶47片
导叶29片。为了增大涡轮排气面积
将导叶减为16片
动叶叶片数不变
称涡轮B。将A、B涡轮进行试验对比。
The parameters
such as throat area
trailing edge block ratio and profile turning angle at trailing edge
has been investigated with change of vane and blade number
namely 29
26 vanes and 47
52
42 blades.The results of the effect of the vane and blade numbers on the mass flow
reaction and efficiency of transonic turbine stage are analyzed.
0
Views
13
下载量
CSCD
Publicity Resources
Related Articles
Related Author
Related Institution