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高速诱导轮离心泵的汽蚀振荡与控制 被引量:4
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作者 李惠敏 王晓锋 +1 位作者 赵瑞国 陈晖 《导弹与航天运载技术》 CSCD 北大核心 2019年第2期44-48,共5页
为获得更小的质量、更大的推质比,高速诱导轮离心泵中的诱导轮常在潜在汽蚀情况下工作,利用汽穴分割原理进行诱导轮设计方法的研究,实现了诱导轮表面汽穴分布的主动改变,从而达到提高诱导轮离心泵抗汽蚀振荡稳定性的目的。对比试验表明... 为获得更小的质量、更大的推质比,高速诱导轮离心泵中的诱导轮常在潜在汽蚀情况下工作,利用汽穴分割原理进行诱导轮设计方法的研究,实现了诱导轮表面汽穴分布的主动改变,从而达到提高诱导轮离心泵抗汽蚀振荡稳定性的目的。对比试验表明:改进方案离心泵的效率和扬程与原方案相当,改进方案大幅降低泵的压力脉动,使用改进方案改善诱导轮离心泵抗汽蚀振荡稳定性是可行的。 展开更多
关键词 液体火箭发动机 诱导轮离心泵 汽蚀振荡 汽穴分割
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口环间隙对诱导轮离心泵空化流动和性能的影响 被引量:7
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作者 肖丽倩 黎义斌 +2 位作者 刘宜 毕祯 赵伟国 《排灌机械工程学报》 EI CSCD 北大核心 2016年第8期657-664,671,共9页
为了研究口环间隙对前置诱导轮离心泵空化性能的影响,基于RNG k-ε湍流模型和Rayleigh-Plesset方程均相流空化模型,以前置诱导轮离心泵为研究对象,选取口环间隙为0.15,0.25,0.40和0.60 mm这4种方案对其进行空化流动数值计算,并与试验结... 为了研究口环间隙对前置诱导轮离心泵空化性能的影响,基于RNG k-ε湍流模型和Rayleigh-Plesset方程均相流空化模型,以前置诱导轮离心泵为研究对象,选取口环间隙为0.15,0.25,0.40和0.60 mm这4种方案对其进行空化流动数值计算,并与试验结果对比分析.研究结果表明,口环间隙大小对诱导轮离心泵的外特性和空化性能影响较大,随着口环间隙的增大,总扬程效率和叶轮扬程效率均减小,与口环间隙为0.15 mm时相比,总扬程效率和叶轮扬程效率分别降低了0.60%和4.21%,效率分别下降了6.50%和9.32%;而口环间隙的增大使得诱导轮扬程和效率均增大,分别增大了29.86%和28.40%.另外,随着口环间隙的增大,空化性能曲线出现波动现象,间隙越大,波动越明显;离心泵主叶轮工作面靠近前盖板出现云状空泡分布,空化不稳定,间隙越大,空化越不稳定,临界空化数越大.经分析,引起空化不稳定性的因素可能有:口环间隙出口处泄漏高压流体对主流的冲击;口环附近空化的发生以及诱导轮空化引起叶片出口液流角的变化. 展开更多
关键词 诱导轮离心泵 口环间隙 外特性 空化性能 数值模拟
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诱导轮出口参数对高速离心泵性能的影响 被引量:2
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作者 李惠敏 李向阳 +1 位作者 蒋建园 张聃 《火箭推进》 CAS 2020年第1期69-75,共7页
某型号液体火箭发动机用高速诱导轮离心泵存在抗汽蚀性能偏低的问题,而液体火箭发动机对泵的抗汽蚀性能有特别严格的要求,其直接影响发动机的性能和可靠性。为获得更高的效率,按照常规泵设计经验选取较大的诱导轮出口角,而理论分析此时... 某型号液体火箭发动机用高速诱导轮离心泵存在抗汽蚀性能偏低的问题,而液体火箭发动机对泵的抗汽蚀性能有特别严格的要求,其直接影响发动机的性能和可靠性。为获得更高的效率,按照常规泵设计经验选取较大的诱导轮出口角,而理论分析此时诱导轮和离心轮的能量匹配不是最佳,不能获得较好的汽蚀性能。经过理论分析,提出降低诱导轮出口角的改进方案,并对诱导轮离心泵流场进行数值模拟,并在试验室进行了试验验证。仿真及试验表明在相同叶轮外形尺寸条件下,提出适当降低诱导轮出口参数的设计方法,虽然泵的扬程和效率略有降低,但泵的抗汽蚀性能得到大幅提高,该方法提高泵的抗汽蚀性能是可行的。 展开更多
关键词 液体火箭发动机 诱导轮离心泵 变螺距诱导 抗汽蚀性能
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Reliability Improvements to Centrifugal Pump Performance in Conjunction with Inducers, CFD Comparative Study 被引量:1
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作者 Said A. F. Hawash Dalia M. S. EI Gazzar Mohamed A. EI Samanoudy 《Journal of Earth Science and Engineering》 2015年第5期296-305,共10页
In this research, centrifugal pump unit was analysed to study the effects of using inducers on its performance. Hydraulic tests were done to obtain the optimum hydraulic performance before and after using inducer. Two... In this research, centrifugal pump unit was analysed to study the effects of using inducers on its performance. Hydraulic tests were done to obtain the optimum hydraulic performance before and after using inducer. Two types of inducers were used in this work (axial, helical). For this purpose, a test rig was specially designed with a pump system to investigate the parameters under consideration. Plots (H-Q) curves, (B.P.-Q) curves and (q-Q) curves were used to show the effect of pump performance with and without inducers. The present study introduces a simulation of centrifugal pump performance in conjunction with inducers using CFD (Computational Fluid Dynamics), to compare it with experimentally observed values. The model investigates the impact of using inducers on the head and flow of the pump. The results of the CFD model and experimental are correlated well. Furthermore, the results help the decision makers of the pumps for future developments in pump performance assuring safe and reliable running condition of the water pumps. Also it may be used for more applications of larger head and flow pumps. 展开更多
关键词 Centrifugal pump axial helical inducers hydraulic performance CFD simulation NPSH.
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Turbo-pump with Isolated Two Stage Impellers for Future Rocket Engine (Trial to Drive Impellers Independently) 被引量:2
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作者 Toshiaki Kanemoto Makoto Shimojyo +3 位作者 Ryunosuke Kawashima Daisuke Tanaka Akira Inagaki Shin Oba 《Journal of Thermal Science》 SCIE EI CAS CSCD 2008年第1期28-34,共7页
To suppress the cavitation in the impellers and to make the turbo-pump lives longer, the inducer was separated from the main impeller and both impellers were driven independently. The performance of the pump and the f... To suppress the cavitation in the impellers and to make the turbo-pump lives longer, the inducer was separated from the main impeller and both impellers were driven independently. The performance of the pump and the flow conditions around the impellers were investigated experimentally and the following results were obtained. (1)The main impeller contributes to the flow interaction between the inducer and the main impeller. (2)The rotational speeds of both impellers can be controlled independently in order to suppress simultaneously the cavitation not only in the main impeller, but also in the inducer. 展开更多
关键词 Turbo-pump INDUCER IMPELLER Rocket Engine Cavitation NPSH
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