Mechanism of Breakdown of Laboratory Gaps

Upon application of an impulse voltage, of such value as not to cause sparkover, a nonuniform field gap, of the proportions frequently encountered in engineering work, the field at first corresponds to that which would be expected from the conventional electrostatic solution. The fields in the vicinity of the electrodes may exceed the critical field momentarily but when this field is exceeded and a free electron appears in the region of the overstressed field, an electron avalance is triggered that develops into aspace charge. For rod-rod gaps the space charge develops from both electrodes but for rodplate gaps from the rod only. The flow of the charge into the intervening gap is at a rate of about 0.001 c which corresponds approximately to the electron drift; so that for a 10-cm gap the charge has diffused through the entire gap in about 0.3 μsec and for a 200-inch gap in 9 μsec. The current feeding the space charge rises very rapidly and decreases somewhat along an exponential curve so that a substantial portion of the space charge is established in slightly less time than these values. A certain critical average gradient exists for gaps which will produce ultimate sparkover of the gap with prolonged application of the voltage. There is some evidence to indicate that when the space charge is fully developed across the gap the electric gradient in the gap between the electrodes is approximately uniform.

[1]  W. J. Degnan,et al.  Sixty-Cycle and Impulse Sparkover of Large Gap Spacings [includes discussion] , 1952, Transactions of the American Institute of Electrical Engineers. Part III: Power Apparatus and Systems.

[2]  C. F. Wagner,et al.  The lightning stroke , 1958, Electrical Engineering.

[3]  C. F. Wagner A New Approach to the Calculation of the Lightning Performance of Transmission Lines [includes discussion] , 1956, Transactions of the American Institute of Electrical Engineers. Part III: Power Apparatus and Systems.

[4]  C. F. Wagner,et al.  Effects of Corona on Traveling Waves [includes discussion] , 1955, Transactions of the American Institute of Electrical Engineers. Part III: Power Apparatus and Systems.

[5]  P. L. Bellaschi,et al.  Impulse and 60 cycle strength of air , 1934, Electrical Engineering.

[6]  C. F. Wagner,et al.  The Lightning Stroke-II , 1961, Transactions of the American Institute of Electrical Engineers. Part III: Power Apparatus and Systems.

[7]  C. F. Wagner Determination of the Wave Front of Ligktning Stroke Currents from Field Measurements , 1960, Transactions of the American Institute of Electrical Engineers. Part III: Power Apparatus and Systems.

[8]  C. F. Wagner,et al.  A New Approach to the Calculation or the Lightning Perrormance or Transmission Lines III-A Simplified Method: Stroke to Tower , 1960, Transactions of the American Institute of Electrical Engineers. Part III: Power Apparatus and Systems.