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An improved torch igniter for use in devices such as thrust augmenters, gas turbine engines, ramjets, combined-cycle engines and industrial burners. The torch igniter includes a housing with a combustion chamber. Fuel and oxidizer are delivered into the combustion chamber and ignited by an electroni

An improved torch igniter for use in devices such as thrust augmenters, gas turbine engines, ramjets, combined-cycle engines and industrial burners. The torch igniter includes a housing with a combustion chamber. Fuel and oxidizer are delivered into the combustion chamber and ignited by an electronic ignition source, such as a plasma jet igniter or a spark igniter, so that an upstream recirculation zone and a downstream recirculation zone are created. The upstream recirculation zone stabilizes and pilots combustion within the combustion chamber, while the downstream recirculation zone augments the combustion event. Byproducts of the combustion event within the torch igniter provide a high mass flux with high thermal energy and strong ignition source radicals that are discharged through a neck portion of the housing and are thereafter employed to initiate a primary combustion event in a primary combustor.

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1. A torch igniter comprising: a housing defining a combustion chamber, at least one fuel conduit and at least one oxidizer conduit, the at least one fuel conduit intersecting the combustion chamber forwardly of an end wall and being configured to dispense at least one stream of fuel into the comb

1. A torch igniter comprising: a housing defining a combustion chamber, at least one fuel conduit and at least one oxidizer conduit, the at least one fuel conduit intersecting the combustion chamber forwardly of an end wall and being configured to dispense at least one stream of fuel into the combustion chamber, the at least one oxidizer conduit intersecting the combustion chamber forwardly of the end wall and being configured to dispense at least one stream of oxidizer into the combustion chamber, the at least one stream of fuel mixing with the at least one stream of oxidizer to produce a fuel/oxidizer mixture; and an electronic ignition source coupled to the housing and generating an ignition kernel that is dispensed into the combustion chamber rearwardly of the fuel and oxidizer conduits, the ignition kernel initially igniting the fuel/oxidizer mixture in the combustion chamber; wherein the fuel and oxidizer conduits are positioned relative to the combustion chamber to create an upstream recirculation zone and a downstream recirculation zone, the upstream and downstream recirculation zones cooperating to stabilize and pilot combustion within the combustion chamber. 2. The torch igniter of claim 1, wherein the electronic ignition source is selected from a group consisting of plasma jet igniters and spark igniters.3. The torch igniter of claim 1, wherein each of the fuel conduits is spaced about the combustion chamber between two oxidizer conduits.4. The torch igniter of claim 1, wherein each of the oxidizer conduits is spaced about the combustion chamber between two fuel conduits.5. The torch igniter of claim 1, wherein the housing further comprises an ignition source mounting portion that is disposed rearwardly of an end wall of the combustion chamber, the end wall including an aperture into which a tip portion of the electronic ignition source extends, the kernel being ejected through the tip portion.6. The torch igniter of claim 1, wherein the housing further comprises a neck portion that is disposed on a side of the combustion chamber opposite the electronic ignition source, the neck portion having a neck barrel that is in fluid communication with the combustion chamber, wherein combustion byproducts that are generated from combustion of the fuel/oxidizer mixture in the combustion chamber are discharged through the neck barrel and out of the housing.7. The torch igniter of claim 6, wherein the housing further comprises a tip that is coupled to the neck portion on a side opposite the combustion chamber, the tip having at least one orifice formed therein, the at least one orifice being in fluid communication with the neck barrel.8. The torch igniter of claim 7, wherein the tip includes a first orifice and a second orifice, the first orifice being disposed generally perpendicular to the second orifice.9. The torch igniter of claim 8, wherein the first orifice is disposed substantially coincident along a longitudinal axis of the neck barrel.10. The torch igniter of claim 7, wherein the tip is fixedly coupled to the neck portion.11. The torch igniter of claim 1, wherein at least one of the streams of fuel and oxidizer impinges on another one of the streams of fuel and oxidizer.12. The torch igniter of claim 11, wherein all of the streams of fuel and oxidizer impinge upon one another about a common point.13. A torch igniter comprising: a torch housing having an igniter mounting portion, a combustion chamber portion and a neck portion, the igniter mounting portion terminating at an end wall that is located at a first end of the combustion chamber portion, the combustion chamber portion defining a combustion chamber, at least one fuel conduit and at least one oxidizer conduit, each fuel conduit being configured to dispense a stream of fuel into the combustion chamber, each oxidizer conduit being configured to dispense a stream of oxidizer into the combustion chamber, the fuel and oxidizer conduits being spaced between the first end of the combustion chamber portion and a second end of the combustion chamber portion that is opposite the first end, the fuel and oxidizer conduits being positioned relative one another such that the streams of fuel and oxidizer impinge on one another to form a fuel/oxidizer mixture, the neck portion defining a neck barrel that is in fluid communication with the combustion chamber, the neck barrel having a lateral cross-section that is smaller than a lateral cross-section of the combustion chamber; and an electronically actuated ignition source at least partially housed in the igniter mounting portion, the electronically actuated ignition source having a tip portion for generating an ignition kernel in the combustion chamber, the ignition kernel generating a combustion event in which the fuel/oxidizer mixture combusts; wherein byproducts produced by combustion of the fuel/oxidizer mixture are ejected through the neck barrel. 14. The torch igniter of claim 13, wherein the electronic ignition source is selected from a group consisting of plasma jet igniters and spark igniters.15. The torch igniter of claim 13, wherein each of the fuel conduits is spaced about the combustion chamber between two oxidizer conduits.16. The torch igniter of claim 13, wherein each of the oxidizer conduits is spaced about the combustion chamber between two fuel conduits.17. The torch igniter of claim 13, wherein the housing further comprises a tip that is coupled to the neck portion on a side opposite the combustion chamber, the tip having at least one orifice formed therein, the at least one orifice being in fluid communication with the neck barrel.18. The torch igniter of claim 17, wherein the tip includes a first orifice and a second orifice, the first orifice being disposed generally perpendicular to the second orifice.19. The torch igniter of claim 18, wherein the first orifice is disposed substantially coincident a longitudinal axis of the neck barrel.20. The torch igniter of claim 17, wherein the tip is fixedly coupled to the neck portion.