航天推进技术研究院主办
[1]严俊峰,陈晖,王文廷.基于比例因子的离心泵圆弧叶片造型研究[J].火箭推进,2016,42(03):45-49.
YAN Junfeng,CHEN Hui,WANG Wenting.Research on shape construction of circular blade in centrifugal pump based on scale factor method[J].Journal of Rocket Propulsion,2016,42(03):45-49.
点击复制
YAN Junfeng,CHEN Hui,WANG Wenting.Research on shape construction of circular blade in centrifugal pump based on scale factor method[J].Journal of Rocket Propulsion,2016,42(03):45-49.
基于比例因子的离心泵圆弧叶片造型研究
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
42
期数:
2016年03期
页码:
45-49
栏目:
研究与设计
出版日期:
2016-06-30
- Title:
- Research on shape construction of circular blade in centrifugal pump based on scale factor method
- Keywords:
- centrifugal pump; circular blade shape construction; scale factor method; parameter of blade profile; performance prediction
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 针对中低比转速离心泵,提出了能够统一各种圆弧叶片造型方法的比例因子法,推导了叶型参数的计算公式,分析了比例因子对叶片安放角、叶片长度等的影响,并采用数值模拟方法对不同比例因子下的泵内流场进行了性能预测.结果表明,不同比例因子下的叶型参数、流动参数及性能参数变化范围很大.比例因子较小时,节流损失较大,泵扬程较低;比例因子较大时,脱流损失较大,泵效率较低,存在较优的比例因子区间[0.15,0.35],使叶片安放角平滑变化,泵的综合性能较优,对应的曲率半径比为1.4～1.9.采用Pfleiderer方法及本文的角度平均法获得的叶片安放角变化较为平稳,可用于离心泵的初步设计.
相似文献/References:
[1]严俊峰,陈 晖,逯婉若.泵-管路系统的汽蚀自激振荡特性分析[J].火箭推进,2015,41(05):29.
YAN Junfeng,CHEN Hui,LU Wanruo.Analysis on characteristics of self-excited cavitation
oscillation in pump-piping system[J].Journal of Rocket Propulsion,2015,41(03):29.
[2]于海力,张 锐,刘海丽,等.高压高扬程固液两相介质离心泵的设计原则[J].火箭推进,2015,41(02):70.
YU Hai-li,ZHANG Rui,LIU Hai-li,et al.Design philosophy of high-pressure & high-lift centrifugal
pump for solid-liquid phase mediums[J].Journal of Rocket Propulsion,2015,41(03):70.
[3]郭 维,白东安.液体火箭发动机用超低比转速离心泵优化设计[J].火箭推进,2011,37(05):19.
GUO Wei,BAI Dong-an.Optimal design of ultra-low specific speed centrifugal pump for LRE[J].Journal of Rocket Propulsion,2011,37(03):19.
[4]郭维,白东安.超低比转速离心泵内流场计算及分析[J].火箭推进,2007,33(02):26.
Guo Wei,Bai Dongan.Inner flow field computation and analysis of super low-specific-speed centrifugal pump[J].Journal of Rocket Propulsion,2007,33(03):26.
[5]严俊峰,陈炜,蒲光荣,等.叶轮盖板侧的流动对离心泵泄漏量的影响[J].火箭推进,2007,33(03):20.
Yan Junfeng,Chen Wei,Pu Guangrong.The effect of flow in the impeller shroud on the leakage rate in a centrifugal pump[J].Journal of Rocket Propulsion,2007,33(03):20.
[6]郑赟韬,蔡国飙,尹贵增,等.液体火箭发动机离心泵叶轮的多目标优化设计[J].火箭推进,2006,32(01):14.
Zheng Yuntao,Cai Guobiao,Yin Guizeng.Multi-objective optimization and design for centrifugal impeller of rocket engine pumps[J].Journal of Rocket Propulsion,2006,32(03):14.
[7]严俊峰,陈炜.基于遗传算法的低比转速高速泵优化设计[J].火箭推进,2006,32(03):1.
Yan Junfeng,Chen Wei.Optimum design of low-specific-speed high-speed centrifugal pump based on genetic algorithm[J].Journal of Rocket Propulsion,2006,32(03):1.
[8]张翠儒,白东安,郭维,等.液体火箭上面级发动机用超低比转数泵研究[J].火箭推进,2005,31(02):17.
Zhang Cuiru,Bai dongan,Guo Wei.Research on ultra-low-specific-speed rotation pump for upper stage engine[J].Journal of Rocket Propulsion,2005,31(03):17.
[9]赵瑞勇,张翠儒,刘军年,等.面积比对变工况泵性能稳定性影响的研究[J].火箭推进,2016,42(04):35.
ZHAO Ruiyong,ZHANG Cuiru,LIU Junnian,et al.Investigation on influence of different area ratio on stability of centrifugal pump with variable working conditions[J].Journal of Rocket Propulsion,2016,42(03):35.
[10]严俊峰,陈晖.可控曲率半径的圆柱形叶片逐点绘型方法[J].火箭推进,2017,43(01):38.
YAN Junfeng,CHEN Hui.Point-by-point drawing method for cylindrical blade with adjustable curvature radius[J].Journal of Rocket Propulsion,2017,43(03):38.
更新日期/Last Update:
1900-01-01