Supersonic spark gap switch
AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorDouglas C. Rabe
Life of this patent
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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.
Claims3
The improvement in a spark gap switch having a first and a second hollow cylindrical electrode with means for connecting the said electrodes into an electrical circuit, with the said electrodes positioned in axial alignment with the electrode faces of the electrodes in spaced apart relationship providing an annular axial gap therebetween and with an air chamber enclosure connected to an air flow source surrounding the said gap and providing a flow of air through the said gap, the improvement in the said spark gap switch comprising:
- a. the said annular axial gap between the said electrode faces being formed to comprise an annular DeLaval nozzle with the converging side of the nozzle adjacent the said air chamber and the expansion side of the nozzle exhausting into the said hollows of the said electrodes;
- b. means for limiting the discharge region of the said gap to the expansion region of the said annular DeLaval nozzle;
- and
- c. means for providing a supersonic flow of air through the said expansion region of the said gap.
Dependencies are inferred from the claim text.