DocumentCode :
1435298
Title :
Investigation of the effects of pressure ratios on arc behavior in a supersonic nozzle
Author :
Zhang, Jin Ling ; Yan, Jiu Dun ; Fang, Michael T C
Author_Institution :
Dept. of Electr. Eng. & Electron., Liverpool Univ., UK
Volume :
28
Issue :
5
fYear :
2000
fDate :
10/1/2000 12:00:00 AM
Firstpage :
1725
Lastpage :
1734
Abstract :
Supersonic nozzles are commonly used in modern high voltage circuit breakers. The thermodynamic and electrical behavior of arcs burning in such nozzles is closely related to the nozzle geometry and the pressures at the nozzle inlet and exit. Computational investigation has been carried out on the thermal interruption capability of a supersonic nozzle at different inlet stagnation pressures and at different exit pressure to inlet stagnation pressure ratios (referred to as pressure ratios). The critical rate of rise of recovery voltage (RRRV), which is the most important parameter determining the thermal interruption capability of a circuit breaker, was predicted for five pressure ratios at three inlet stagnation pressures. The predicted RRRV values are compared with the test results of Campbell et al. (1976)
Keywords :
Navier-Stokes equations; circuit-breaking arcs; nozzles; plasma devices; plasma flow; plasma pressure; plasma theory; plasma thermodynamics; stagnation flow; supersonic flow; arc behavior; arcs; burning arcs; circuit breaker; computational investigation; critical rate; electrical behavior; exit pressure; high voltage circuit breakers; inlet stagnation pressure; inlet stagnation pressures; nozzle exit; nozzle geometry; nozzle inlet; pressure ratios; pressures; recovery voltage; supersonic nozzle; test results; thermal interruption capability; thermodynamic behavior; Arc discharges; Circuit breakers; Circuit testing; Electric shock; Equations; Geometry; Interrupters; Solids; Thermodynamics; Voltage;
fLanguage :
English
Journal_Title :
Plasma Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0093-3813
Type :
jour
DOI :
10.1109/27.901260
Filename :
901260
Link To Document :
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