引用本文:
【打印本页】   【HTML】 【下载PDF全文】   查看/发表评论  【EndNote】   【RefMan】   【BibTex】
←前一篇|后一篇→ 过刊浏览    高级检索
本文已被:浏览 1133次   下载 539 本文二维码信息
码上扫一扫!
分享到: 微信 更多
间隙对半开式离心叶轮性能影响的理论预测
楚武利, 刘志伟
西北工业大学航空动力与热力工程系
摘要:
推导了半开式离心叶轮间隙流动所产生的力及引起的损失,建立了相应的压力损失及效率随间隙变化的模型。在小型试验台上对间隙影响进行了实验研究,得出了间隙对压力、效率的影响规律。实验结果与理论预测相符。
关键词:  涡轮喷气发动机  离心式压缩机  叶轮  间隙  漏泄  能量损失
DOI:
分类号:V235.113
基金项目:航空基金
THEORETICAL PREDICTION OF TIP CLEARANCE EFFECT ON PERFORMANCE OF CENTRIFUGAL IMPELLER
Chu Wuli, Liu Zhiwei
Dept.of Aeroengine,Northwestern Polytechnical Univ ,Xi′an,710072
Abstract:
The flow loss resulted from the tip clearance of half shrouded centrifugal impeller was deduced.The model of the efficiency drop and pressure loss versus the tip clearance was established.The gap effect was tested and the rules of the effect were obtained.The test results are in agreement with the theoretical prediction
Key words:  Turbojet engine  Centrifugal compressor  Impeller  Gap  Leakage  Energy loss