Supersonic spark gap switch

Electric lamp and discharge devices – With support and/or spacing structure for electrode and/or... – For plural electrodes of discharge device

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Details

313231, 313325, H01J 1704

Patent

active

040271870

ABSTRACT:
The hot gases and discharge products are removed from the space between the electrodes of a spark gap switch after the passage of the discharge by a supersonic air flow in the discharge region created by fabricating the ends of the electrodes to form a DeLaval nozzle. The supersonic air flow clears the switch and provides a switch having a very short grace period.

REFERENCES:
"High Power Spark Gap Switch Development", published by the Air Force Aero Propulsion Laboratory, Air Force Systems Command, Wright-Patterson Air Force Base as technical report AFAPL-TR-75-41.

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