TY - GEN
T1 - Research on the optimization design of supersonic swirling separator
AU - Li, Ke Xin
AU - Eri, Qi Tai
AU - Yan, Chen Yang
AU - Ji, Wei An
AU - Su, Pei Ran
PY - 2014
Y1 - 2014
N2 - Supersonic swirling separator had a good ability in separating gas-liquid. In this paper, the Laval-nozzle and straight-tube of the non-central cone supersonic swirling separator were optimized designing. The separation performance of the optimized supersonic swirling separator was researched by CFX. The results show that, with the relative pressure ratio decreasing, the shock waves which occurred in the diffuser moved towards the extraction device, the maximum Mach number decreasing. When the relative pressure ratio down to 1.4, the outlet total pressure recovered to 73% of the inlet total pressure, the flow in the divergent section of Laval-nozzle and the straight-tube was supersonic, the lowest temperature can be down to -84.5°C and the maximum centrifugal acceleration was 261,800g, which provided a swirling and cold environment for the separation of gas-liquid; With the straight-tube's length-diameter ratio increased, a normal shock wave occurred in the straight-tube. Further increased the length-diameter ratio, the normal shock wave moved towards the throat and the strength of the shock wave was increasing, which was a disadvantage to the separation of the gas-liquid.
AB - Supersonic swirling separator had a good ability in separating gas-liquid. In this paper, the Laval-nozzle and straight-tube of the non-central cone supersonic swirling separator were optimized designing. The separation performance of the optimized supersonic swirling separator was researched by CFX. The results show that, with the relative pressure ratio decreasing, the shock waves which occurred in the diffuser moved towards the extraction device, the maximum Mach number decreasing. When the relative pressure ratio down to 1.4, the outlet total pressure recovered to 73% of the inlet total pressure, the flow in the divergent section of Laval-nozzle and the straight-tube was supersonic, the lowest temperature can be down to -84.5°C and the maximum centrifugal acceleration was 261,800g, which provided a swirling and cold environment for the separation of gas-liquid; With the straight-tube's length-diameter ratio increased, a normal shock wave occurred in the straight-tube. Further increased the length-diameter ratio, the normal shock wave moved towards the throat and the strength of the shock wave was increasing, which was a disadvantage to the separation of the gas-liquid.
KW - Gas-liquid separation
KW - Low temperature
KW - Relative pressure ratio
KW - Supersonic swirling
UR - https://www.scopus.com/pages/publications/84887347995
U2 - 10.4028/www.scientific.net/AMM.444-445.332
DO - 10.4028/www.scientific.net/AMM.444-445.332
M3 - 会议稿件
AN - SCOPUS:84887347995
SN - 9783037859063
T3 - Applied Mechanics and Materials
SP - 332
EP - 337
BT - Advances in Computational Modeling and Simulation
T2 - 2nd International Conference on Advances in Computational Modeling and Simulation, ACMS 2013
Y2 - 17 July 2013 through 19 July 2013
ER -