Influence of axial clearance on the performance characteristics of a turbopump

被引:5
作者
Li, Deyou [1 ]
Ren, Zhipeng [1 ]
Fan, Rong [1 ]
Chai, Yafei [1 ]
Gong, Ruzhi [1 ]
Wang, Hongjie [1 ]
机构
[1] Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Peoples R China
关键词
Turbopump; Axial clearance; Entropy production; Hydraulic loss; ENTROPY PRODUCTION; INDUCER; PUMP;
D O I
10.1007/s12206-021-0924-2
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
To evaluate the influence of axial clearance on the performance characteristics in turbopumps, numerical simulations of an entire flow passage were carried out. The simulations were validated by performance characteristic experiments. The progress of the reciprocating axial movement in the rotor between the front and back covers was disassembled into five fixed clearances groups. Hump characteristic occurs at the same flow rate under these clearances groups. The hydraulic loss of the inducer-impeller was clearly influenced by the clearances. In particular, the hydraulic loss of the impeller changes significantly at the low flow rate under the +/- 0.3 mm clearance. With the increase of the flow rate, the effect of the clearance change on the flow is weakened. An innovative entropy production analysis was also performed. The distribution of the high local entropy production rate at the impeller inlet under the 0 mm clearance and at the impeller outlet under the -0.15 mm and -0.3 mm clearances overlapped with the vortex caused by flow separation, and the counterpart at the back cover is concentrated around the clearance structures, thereby leading to high hydraulic loss.
引用
收藏
页码:4543 / 4555
页数:13
相关论文
共 23 条
[1]  
Cengel Y.A., 2001, Applied mechanics reviews, V54, pB110, DOI 10.1115/1.1421126
[2]   Numerical simulation of cavitating flow in 2D and 3D inducer geometries [J].
Coutier-Delgosha, O ;
Fortes-Patella, R ;
Reboud, JL ;
Hakimi, N ;
Hirsch, C .
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2005, 48 (02) :135-167
[3]   Application of entropy production theory to hydro-turbine hydraulic analysis [J].
Gong RuZhi ;
Wang HongJie ;
Chen LiXia ;
Li DeYou ;
Zhang HaoChun ;
Wei XianZhu .
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 56 (07) :1636-1643
[4]   Influence of impeller's elastic deformation on the stability of balance piston mechanism of rocket engine turbopump [J].
Hiraki, H. ;
Inoue, T. ;
Yabui, S. .
29TH IAHR SYMPOSIUM ON HYDRAULIC MACHINERY AND SYSTEMS, 2019, 240
[5]  
HO CI CHANG, 2012, [The KSFM Journal of Fluid Machinery, 한국유체기계학회 논문집], V15, P41
[6]  
Horiguchi H, 2009, PROCEEDINGS OF THE ASME FLUIDS ENGINEERING DIVISION SUMMER CONFERENCE, VOL 1, PTS A-C, P243
[7]   Rotordynamic analysis of a high thrust liquid rocket engine fuel (Kerosene) turbopump [J].
Jeon, Seong Min ;
Kwak, Hyun Duck ;
Yoon, Suk Hwan ;
Kim, Jinhan .
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 26 (01) :169-175
[8]  
Jeong E., 2012, CURRENT IND TECHNOLO, V10, P154
[9]   Effective Modes of Axial Balancing of Centrifugal Pump Rotor [J].
Kalinichenko, P. ;
Suprun, A. .
XIIITH INTERNATIONAL SCIENTIFIC AND ENGINEERING CONFERENCE HERMETIC SEALING, VIBRATION RELIABILITY AND ECOLOGICAL SAFETY OF PUMP AND COMPRESSOR MACHINERY-HERVICON-2011, 2012, 39 :111-118
[10]   Effects of inducer tip clearance on the performance and flow characteristics of a pump in a turbopump [J].
Kim, Changhyun ;
Kim, Semi ;
Choi, Chang-Ho ;
Baek, Jehyun .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2017, 231 (05) :398-414