流体机械
流體機械
류체궤계
FLUID MACHINERY
2013年
10期
45-48,13
,共5页
倪永燕%刘为民%潘希伟%潘中永
倪永燕%劉為民%潘希偉%潘中永
예영연%류위민%반희위%반중영
多目标泵%设计%模型换算%CFD
多目標泵%設計%模型換算%CFD
다목표빙%설계%모형환산%CFD
multi-objective pump%design%model scaling%CFD
介绍了某项目用泵的2个需求工况点,应用欧拉扬程公式计算单叶轮设计时的叶轮外径,并计算圆盘摩擦损失预估泵效率,初步分析表明单叶轮设计不仅效率极低,而且也无法满足2个设计目标。针对比开发了一种双叶轮双出口组合的新型结构型式,介绍了其工作原理。其中主要过流部件采用模型换算法,应用面积比法计算正导叶外接的首级叶轮蜗壳的第Ⅷ断面面积。根据模型试验数据换算得到该多目标泵的外特性曲线并用现代 CFD 技术进行了数值仿真。发现扬程-流量曲线的模型试验数据与仿真结果曲线一致,满足2个工况点的目标需求。与模型换算数据相比,数值仿真得到的数据最高效率点向大流量方向偏移,这是由于第一级蜗壳是以正导叶为基础采用面积比法设计、过流断面大导致的。
介紹瞭某項目用泵的2箇需求工況點,應用歐拉颺程公式計算單葉輪設計時的葉輪外徑,併計算圓盤摩抆損失預估泵效率,初步分析錶明單葉輪設計不僅效率極低,而且也無法滿足2箇設計目標。針對比開髮瞭一種雙葉輪雙齣口組閤的新型結構型式,介紹瞭其工作原理。其中主要過流部件採用模型換算法,應用麵積比法計算正導葉外接的首級葉輪蝸殼的第Ⅷ斷麵麵積。根據模型試驗數據換算得到該多目標泵的外特性麯線併用現代 CFD 技術進行瞭數值倣真。髮現颺程-流量麯線的模型試驗數據與倣真結果麯線一緻,滿足2箇工況點的目標需求。與模型換算數據相比,數值倣真得到的數據最高效率點嚮大流量方嚮偏移,這是由于第一級蝸殼是以正導葉為基礎採用麵積比法設計、過流斷麵大導緻的。
개소료모항목용빙적2개수구공황점,응용구랍양정공식계산단협륜설계시적협륜외경,병계산원반마찰손실예고빙효솔,초보분석표명단협륜설계불부효솔겁저,이차야무법만족2개설계목표。침대비개발료일충쌍협륜쌍출구조합적신형결구형식,개소료기공작원리。기중주요과류부건채용모형환산법,응용면적비법계산정도협외접적수급협륜와각적제Ⅷ단면면적。근거모형시험수거환산득도해다목표빙적외특성곡선병용현대 CFD 기술진행료수치방진。발현양정-류량곡선적모형시험수거여방진결과곡선일치,만족2개공황점적목표수구。여모형환산수거상비,수치방진득도적수거최고효솔점향대류량방향편이,저시유우제일급와각시이정도협위기출채용면적비법설계、과류단면대도치적。
A certain pump need to be used at two conditions.Euler equation was used to evaluate the impeller diameter for a single impeller design case.Primary analysis showed that one impeller design had too low efficiency and can not reach the two re-quired operating conditions.A new multi-objective pump with two cascade impellers and two discharge flanges was developed and its running principal was introduced.The hydraulic parts were model scaled except that the volute downstream the radial diffuser was designed by area-ratio method.The overall characteristics of the pump were numerically simulated and scaled.The head-flow curve evaluated was agree well with that of model scaled and matched the required conditions.The efficiency-flow curve evaluated has deficiency than that of model scaled and the best efficiency point move to large flow rate area.The former is because of the simple structure of the models causing high efficiency while the latter due to the large section area design of the first stage volute.