航天推进技术研究院主办
[1]黄锡龙,杨宝锋,严俊峰,等.基于响应面法的诱导轮多参数水力优化[J].火箭推进,2023,49(05):73-80.
HUANG Xilong,YANG Baofeng,YAN Junfeng,et al.Multi-parameter hydraulic optimization of inducer based on response surface method[J].Journal of Rocket Propulsion,2023,49(05):73-80.
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HUANG Xilong,YANG Baofeng,YAN Junfeng,et al.Multi-parameter hydraulic optimization of inducer based on response surface method[J].Journal of Rocket Propulsion,2023,49(05):73-80.
基于响应面法的诱导轮多参数水力优化
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
49
期数:
2023年05期
页码:
73-80
栏目:
目次
出版日期:
2023-10-25
- Title:
- Multi-parameter hydraulic optimization of inducer based on response surface method
- 文章编号:
- 1672-9374(2023)05-0073-08
- Keywords:
- inducer; multi-parameter; response surface method; penalty function method; hydraulic optimization
- 分类号:
- V434.21
- 文献标志码:
- A
- 摘要:
- 为提高预压泵的水力性能,通过响应面法对高速预压泵的诱导轮进行了多参数水力优化。选取叶片倾角、入口安放角、出口安放角、分流叶片轴向位置、入口轮毂直径和出口轮毂直径这6个结构参数作为影响因素,基于中心复合有界设计原理设计了78组诱导轮方案,并通过数值仿真获得78组诱导轮的扬程和效率。对计算结果进行极差分析,获得各影响因素对诱导轮扬程和效率的影响。结果表明:出口安放角和出口轮毂直径对诱导轮的扬程影响较大,分流叶片轴向位置和入口轮毂直径对扬程的影响较小; 入口安放角对效率的影响最大,出口轮毂直径对效率的影响最小。通过线性回归分别得到扬程系数和效率的响应面模型,以效率大于60%作为约束条件,利用罚函数法对扬程进行寻优,使诱导轮扬程提升15.4%。
- Abstract:
- In order to improve the hydraulic performance of prepressurizing turbopumps, the multi-parameter hydraulic optimization of the inducer was carried out by the response surface method. Six inducer's structural parameters including blade inclination angle, inlet blade angle, outlet blade angle, axial position of splitting vanes, inlet and outlet hub diameters were selected as influencing factors. 78 sets of inducer schemes were designed according to the principle of central composite inscribed design. The head and efficiency of 78 sets of inducers were obtained by numerical simulation. The effects of influence factors on the head and efficiency of inducers were obtained by range analysis of calculation results. The results show that outlet blade angle and outlet hub diameter have more influence on the head of the inducer. Axial position of splitting vanes and inlet hub diameter have little influence on the head. Inlet blade angle has the greatest influence on the efficiency of inducer. Outlet hub diameter has the least influence on the efficiency. The response surface models of head coefficient and efficiency were obtained respectively by linear regression. With the efficiency greater than 60% as the constraint condition, the penalty function method was used to optimize the head of inducer. The results show that the head of the optimized inducer is improved by 15.4%.
参考文献/References:
[1] 廖懂华,林奇燕,叶小明.预压涡轮泵轴流式液力涡轮的流动结构研究[J].导弹与航天运载技术,2018(6):49-54.
[2] 袁伟为,王晓锋,张聃,等.液体火箭发动机预压泵性能优化研究[C]//陕西省宇航学会2018年学术交流会.汉中:陕西省宇航学会,2018.
[3] 陈聿晨,安阳,沈文金.220吨补燃循环发动机氢预压泵诱导轮技术方案研究[C]//第二届中国空天推进技术论坛.西宁:[s.n.],2019.
[4] 王伟,施卫东,蒋小平,等.基于正交试验及 CFD 的多级离心泵叶轮优化设计[J].排灌机械工程学报,2016,34(3):191-197.
[5] 冷洪飞,郝开元.基于权矩阵分析法的微型离心泵多目标正交优化设计[J].流体机械,2018,46(5):35-39.
[6] 童哲铭,陈尧,童水光,等.基于NSGA-Ⅲ算法的低比转速离心泵多目标优化设计[J].中国机械工程,2020,31(18):2239-2246.
[7] 方杰,朱荣生,王秀礼,等.基于二次回归正交组合设计低比转速离心泵叶轮的优化设计[J].水泵技术,2019(1):14-20.
[8] 李惠敏,李向阳,蒋建园,等.诱导轮出口参数对高速离心泵性能的影响[J].火箭推进,2020,46(1):69-75.
LI H M,LI X Y,JIANG J Y,et al.Influence of outlet parameters of inducer on performance of high speed centrifugal pump[J].Journal of Rocket Propulsion,2020,46(1):69-75.
[9] 张亚太,陈晖,项乐,等.基于正交优化设计的诱导轮空化性能研究[J].推进技术,2020,41(2):343-352.
[10] 余璐,张皓晨,陈晖,等.考虑空化不稳定性的诱导轮水力正交优化设计[C]//2018年工程热物理学会西安年会.西安:中国工程热物理学会,2018.
[11] 黄锡龙,陈炜,王文廷,等.前置不同诱导轮的高速离心泵性能[J].火箭推进,2020,46(2):64-70.
HUANG X L,CHEN W,WANG W T,et al.Performance of high-speed centrifugal pump with different pre-positioned inducer[J].Journal of Rocket Propulsion,2020,46(2):64-70.
[12] DERAKHSHAN S,MOHAMMADI B,NOURBAKHSH A.Efficiency improvement of centrifugal reverse pumps[J].Journal of Fluids Engineering,2009,131(2):1-9.
[13] BELLARY S A I,HUSAIN A,SAMAD A.Effectiveness of meta-models for multi-objective optimization of centrifugal impeller[J].Journal of Mechanical Science and Technology,2014,28(12):4947-4957.
[14] PARK H S,MIAO F.Simulation and modeling methodologies,technologies and applications[EB/OL].https://link.springer.com/book/10.1007/978-3-319-11457-6,2015.
[15] 袁寿其,王文杰,裴吉,等.低比转数离心泵的多目标优化设计[J].农业工程学报,2015,31(5):46-52.
[16] 薛城,祝宝山,刘小兵,等.基于叶片载荷分布的离心泵正交优化设计[J].工程热物理学报,2019,40(5):1065-1071.
[17] 张人会,樊家成,杨军虎,等.基于自由曲面变形方法的离心泵叶片载荷优化[J].农业机械学报,2015,46(10):38-43.
[18] 张德胜,梅剑,赵睿杰,等.基于响应曲面法的氟塑料两相流泵优化设计[J].排灌机械工程学报,2020,38(9):898-903.
[19] ZHANG X D,YU S M,GONG Y,et al.Optimization design for turbodrill blades based on response surface method[J].Advances in Mechanical Engineering,2016,8(2):168781401562483.
[20] 方俊涛.响应曲面方法中试验设计与模型估计的比较研究[D].天津:天津大学,2011.
[21] 熊俊涛,乔志德.基于响应面法的跨声速翼型气动优化设计[J].实验流体力学,2005,19(1):104-108.
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备注/Memo
收稿日期:2021-08-14; 修回日期:2022-04-11
基金项目:国家重大基础研究项目(613321)
作者简介:黄锡龙(1995—),男,硕士,研究领域为涡轮泵设计。
更新日期/Last Update:
1900-01-01