风机技术
風機技術
풍궤기술
COMPRESSOR,BLOWER & FAN TECHNOLOGY
2013年
2期
45-48
,共4页
离心风机%最佳蜗壳宽度%理论计算%MATLAB
離心風機%最佳蝸殼寬度%理論計算%MATLAB
리심풍궤%최가와각관도%이론계산%MATLAB
centrifugal fan%optimal volute width%theoretical calculation%MATLAB
通过理论计算分析蜗壳宽度变化对风机效率和声功率级的影响,拟合一优化函数使其同时考虑到蜗壳宽度对风机效率和声功率级的影响.以 T4-72型通风机为研究对象,计算其各函数关系式,并采用 MATLAB 软件将各函数关系式生成曲线,通过分析曲线确定出离心风机的最佳蜗壳宽度.通过上述方法得出结论:对于T4-72型通风机,当蜗壳出口宽度 C 为蜗壳终了截面张开度 A的1.3倍时,最佳蜗壳宽度约为0.481m,此时的风机效率最高,且声功率级最低.
通過理論計算分析蝸殼寬度變化對風機效率和聲功率級的影響,擬閤一優化函數使其同時攷慮到蝸殼寬度對風機效率和聲功率級的影響.以 T4-72型通風機為研究對象,計算其各函數關繫式,併採用 MATLAB 軟件將各函數關繫式生成麯線,通過分析麯線確定齣離心風機的最佳蝸殼寬度.通過上述方法得齣結論:對于T4-72型通風機,噹蝸殼齣口寬度 C 為蝸殼終瞭截麵張開度 A的1.3倍時,最佳蝸殼寬度約為0.481m,此時的風機效率最高,且聲功率級最低.
통과이론계산분석와각관도변화대풍궤효솔화성공솔급적영향,의합일우화함수사기동시고필도와각관도대풍궤효솔화성공솔급적영향.이 T4-72형통풍궤위연구대상,계산기각함수관계식,병채용 MATLAB 연건장각함수관계식생성곡선,통과분석곡선학정출리심풍궤적최가와각관도.통과상술방법득출결론:대우T4-72형통풍궤,당와각출구관도 C 위와각종료절면장개도 A적1.3배시,최가와각관도약위0.481m,차시적풍궤효솔최고,차성공솔급최저.
@@@@Based on theoretically calculating and analyzing the effect of volute width variation on the fan efficiency and acoustic power level, fitting and optimization function is carried out to determine the effect of volute width on fan efficiency and acoustic power level. Take T4-72 type fan as the research object, each function equation is calculated and the function equation curve is generated based on MATLAB software, and the optimal volute width is determinded through the analysis of curve. Through the above methods, for T4-72 type fan,when outlet width of volute C is 1.3 times end section opening A of spiral case, the optimal width is about 0.481m , at the same time the fan efficiency is the highest, and sound power level is the lowest.