TY - JOUR
T1 - Numerical simulation of multi-diversion aero fuel centrifugal pump with ejector
AU - Li, Jia
AU - Li, Hua Cong
AU - Fu, Jiang Feng
AU - Han, Xiao Bao
N1 - Publisher Copyright:
©, 2015, BUAA Press. All right reserved.
PY - 2015/8/1
Y1 - 2015/8/1
N2 - Targeting the multi-diversion aero fuel centrifugal pumps with ejector, the numerical simulation of the centrifugal pump was performed. By comparing the simulation data with test data, the simulation's accuracy was identified by Pumplinx. The inner flow characteristics of the model were calculated by analyzing the pressure of middle axial and middle radial areas. Then cavitation characteristic was simulated in the worst operating conditions; and the gas-liquid two-phase distribution of the pump's full cavitation state was given at its Δh values and Δh-H curve was acquired. Studies have shown that this centrifugal pump's head, efficiency and cavitation characteristic curve of numerical simulation meet the test data. Pressure of inner flow is steady, and could make high pressure at high efficiency under small flow states; meanwhile, it could not produce cavitation within its operating range at the input pressure of 0.018 MPa, less than the input pressure of 0.027 MPa for technical requirements at its full cavitation state.
AB - Targeting the multi-diversion aero fuel centrifugal pumps with ejector, the numerical simulation of the centrifugal pump was performed. By comparing the simulation data with test data, the simulation's accuracy was identified by Pumplinx. The inner flow characteristics of the model were calculated by analyzing the pressure of middle axial and middle radial areas. Then cavitation characteristic was simulated in the worst operating conditions; and the gas-liquid two-phase distribution of the pump's full cavitation state was given at its Δh values and Δh-H curve was acquired. Studies have shown that this centrifugal pump's head, efficiency and cavitation characteristic curve of numerical simulation meet the test data. Pressure of inner flow is steady, and could make high pressure at high efficiency under small flow states; meanwhile, it could not produce cavitation within its operating range at the input pressure of 0.018 MPa, less than the input pressure of 0.027 MPa for technical requirements at its full cavitation state.
KW - Aero oil centrifugal pump
KW - Cavitation characteristic
KW - Ejector
KW - Muti-diversion impeller
KW - Numerical simulation
UR - http://www.scopus.com/inward/record.url?scp=84941089928&partnerID=8YFLogxK
U2 - 10.13224/j.cnki.jasp.2015.08.014
DO - 10.13224/j.cnki.jasp.2015.08.014
M3 - 文章
AN - SCOPUS:84941089928
SN - 1000-8055
VL - 30
SP - 1909
EP - 1917
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 8
ER -