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.
1. A method for forming a torch igniter, comprising:
providing a torch igniter housing having a combustion chamber therein, the combustion chamber having an upstream area and a downstream area;
forming a first independent path in said housing for supplying a fuel radially into said combustion chamber;
forming a second independent path in said housing for supplying an oxidizer into said combustion chamber, the combustion chamber being of sufficient volume to permit a degree of mixing of said fuel and oxidizer within said combustion chamber; and
further disposing the independent paths relative to the combustion chamber to create first and second recirculation zones within said combustion chamber on opposite longitudinal sides of said first independent path, with at least one of the first and second recirculation zones being in said upstream area, said recirculation zones operating to pilot combustion of said fuel and oxidizer within said combustion chamber, when said mixture is ignited, such that a mixture of said fuel and oxidizer flows through said combustion chamber.
2. The method of claim 1 , further comprising forming said first recirculation zone at an area upstream of said fuel and oxidizer paths, relative to a direction of flow of said fuel and oxidizer mixture in said combustion chamber.
3. The method of claim 1 , further comprising forming said second recirculation zone at an area downstream of said fuel and oxidizer paths, relative to a direction of flow of said fuel and oxidizer mixture in said combustion chamber.
4. The method of claim 1 , further comprising forming the fuel and oxidizer paths at a right angle relative to one another.
5. The method of claim 1 , further comprising forming a pair of fuel flow paths in said housing non-parallel to one another.
6. The method of claim 1 , further forming a pair of oxidizer paths in said housing non-parallel to one another.
7. The method of claim 1 , further forming a plurality of fuel paths and a plurality of oxidizer paths in said housing, and further arranging said paths such that each said fuel path is bordered on opposite sides thereof by a pair of oxidizer paths.
8. The method of claim 1 , further comprising forming said housing as a circumferential housing, and forming a plurality of fuel paths and a plurality of oxidizer paths radially around said housing, said fuel and oxidizer paths further being arranged such that a plurality of pairs of paths each including one fuel path and one oxidizer path are arranged radially around said housing.
9. A method for forming a torch igniter, comprising:
providing a torch igniter housing having a generally circumferential combustion chamber therein, the combustion chamber having an upstream area and a downstream area;
forming a plurality of first independent paths in said housing spaced radially around said housing and communicating with said combustion chamber, for supplying a fuel radially into said combustion chamber;
forming a plurality of second independent paths in said housing spaced radially around said housing and communicating with said combustion chamber, for supplying an oxidizer into said combustion chamber,
further disposing the independent fuel and oxidizer paths to each open into the combustion chamber at an intermediate point along a length of the combustion chamber to create a first recirculation zone upstream of said paths, relative to a direction of flow within said combustion chamber, and a second recirculation zone downstream of said paths, the recirculation zones operating to pilot combustion of said fuel and oxidizer within said combustion chamber, when said mixture is ignited, such that a mixture of said fuel and oxidizer flows through said combustion chamber to an output end thereof.
10. The method of claim 9 , further comprising forming the fuel and oxidizer paths at a right angle relative to one another.
11. The method of claim 9 , further comprising forming said fuel flow paths in said housing such that no two ones of said fuel flow paths extend parallel to one another.
12. The method of claim 9 , further comprising forming said oxidizer flow paths in said housing such that no two ones of said oxidizer paths in said housing extend parallel to one another.
13. The method of claim 9 , further forming said fuel paths and said oxidizer paths in said housing, and further arranging said paths such that each said fuel path is bordered on opposite sides thereof by a pair of said oxidizer paths.
14. The method of claim 9 , further comprising forming said housing to include an igniter disposed at least partially in said housing upstream of said first recirculation zone.
15. A method of igniting a fuel/oxidizer mixture comprising:
injecting a fuel radially into a combustion chamber within a torch igniter housing at a point intermediate first and second ends of said combustion chamber;
injecting an oxidizer into said combustion chamber within a housing at point intermediate said first and second ends;
forming an upstream recirculation zone in said combustion chamber for a portion of fuel and a portion of oxidizer injected into said combustion chamber at an area upstream of said point at which said fuel is injected, relative to a direction of flow through said combustion chamber; and
forming a downstream recirculation zone in said combustion chamber downstream of said upstream recirculation zone, and downstream of said point at which said fuel is injected; and
using said upstream and downstream recirculation zones to cooperatively pilot and stabilize combustion of intermixed fuel and oxidizer within said combustion chamber when said intermixed fuel and oxidizer is ignited by an igniter.
16. The method of claim 15 , further comprising injecting said fuel into said combustion chamber at a plurality of points spaced radially apart from one another.
17. The method of claim 15 , further comprising injecting said oxidizer into said combustion chamber at a plurality of points spaced radially apart from one another.
18. The method of claim 15 , further comprising injecting each of said fuel and oxidizer at a plurality of points spaced radially about said combustion chamber such that each fuel and oxidizer streams are injected into said combustion chamber at alternating points arranged radially about said combustion chamber.
19. The method of claim 15 , further comprising demarcating said upstream and downstream recirculation zones at said points where said fuel and said oxidizer are injected into said combustion chamber.
20. The method of claim 15 , further comprising arranging injecting said fuel and said oxidizer into said combustion chamber within a common plane extending orthogonally to a direction of flow through said combustion chamber.