风机技术
風機技術
풍궤기술
COMPRESSOR,BLOWER & FAN TECHNOLOGY
2014年
1期
31-36
,共6页
离心通风机%叶片型线%数值模拟%双圆弧叶片%等减速叶片
離心通風機%葉片型線%數值模擬%雙圓弧葉片%等減速葉片
리심통풍궤%협편형선%수치모의%쌍원호협편%등감속협편
centrifugal fan%blade profile%numerical simulation%doble-arcblade%uniform deceleration blade
首先对某采用双圆弧叶片的高效离心风机进行实验和数值对比,并在叶轮前盘形状、轮盖和叶片进出口安装角都相同的情况下,分析了采用双圆弧叶片和等减速叶型的模型风机的性能变化。结果表明,使用双圆弧长短叶片风机模型的稳定工况范围更宽、全压更高,等减速模型则在设计流量和小流量下效率更高、流动损失更小。
首先對某採用雙圓弧葉片的高效離心風機進行實驗和數值對比,併在葉輪前盤形狀、輪蓋和葉片進齣口安裝角都相同的情況下,分析瞭採用雙圓弧葉片和等減速葉型的模型風機的性能變化。結果錶明,使用雙圓弧長短葉片風機模型的穩定工況範圍更寬、全壓更高,等減速模型則在設計流量和小流量下效率更高、流動損失更小。
수선대모채용쌍원호협편적고효리심풍궤진행실험화수치대비,병재협륜전반형상、륜개화협편진출구안장각도상동적정황하,분석료채용쌍원호협편화등감속협형적모형풍궤적성능변화。결과표명,사용쌍원호장단협편풍궤모형적은정공황범위경관、전압경고,등감속모형칙재설계류량화소류량하효솔경고、류동손실경소。
In this paper, firstly, a high efficiency centrifugal fan adopting the double-arc blade model was studied experimentally and numerically. And then, the performance distinction between the centrifugal fan with double-arc blade model and that with uniform deceleration blade model was expounded in detail, while keeping the shroud and hub shape, and the inlet and outlet installation angle constant. The results show that double-arc blade model could cover a wide range of operation condition and reach high total pressure. Uniform deceleration blade model could reach higher efficiency and less flow losses under the design flow and small flow conditions.