Vented igniter
AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorsWilliam W. Griffin, Jr., Robert M. Pierce
Life of this patent
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Abstract
An improved spark igniter for use in a gas turbine engine wherein vent passages which are in the vicinity of the electrode are placed in communication with the ambient environment external to the engine during the ignition sequence causing fuel-air mixture to flow over the electrode as it is abstracted from the engine, thereby enhancing the probability of ignition.
Claims3
An improved spark igniter for use in a gas turbine engine having a combustion means, said igniter comprising a central electrode, a ceramic insulator surrounding said central electrode and extending beyond the tip thereof, an outer shell positioned around said ceramic insulator and extending over the end surface thereof, said outer shell being spaced from the tip of said central electrode to form an electrode cavity in which a spark gap is formed, at least one vent passage in said outer shell for receiving a fuel-air mixture from within the engine, said vent passage being in communication with an outlet area of lower pressure, and at least one inlet opening in the side wall of the outer shell in the upper portion of the electrode cavity in communication with the vent passage such that the fuel-air mixture entering said opening passes near the tip of the central electrode in the electrode cavity causing the mixture to be ignited when the igniter is activated.
Dependencies are inferred from the claim text.