Patent ID: 8044319

Claim:
A variable arc gap plasma igniter for gas turbine engines, comprising: a cavity having opposed ends thereof, one for receiving a combustion fuel flow injected therein and the other being open and in fluid communication with a combustor, thereby forming a passage for the combustion fuel flow to pass through the cavity; first electrode and a second electrode located at respective opposed sides of the cavity and defining a gap therebetween within the cavity, adapted to generate a plasma arc extending through the gap when an electric voltage is applied across the electrodes to ignite the combustion fuel flow and cause an initiating flame to move through the passage away from the first and second electrodes; an igniter body with which the second electrode is moveably associated, the second electrode being extendable into the cavity while the igniter body remains outside the cavity; means for moving the second electrode relative to the first electrode and relative to the igniter body in a direction substantially perpendicular to the passage during arcing from a first position to a second position, the second position increasing the gap size relative to the first position; and wherein the cavity includes a combustion fuel inlet and a combustion product outlet, the inlet and outlet defined independently of the electrodes.