Fuel injectors including gas fuel injection
In accordance with at least one aspect of this disclosure, a fuel injector can include an annular body defining a gas fuel inlet therein, and a structure extending radially outward from the annular body and configured to extend into an air circuit. The structure can include a gas channel defined within the structure at least partially along a radial length of the structure. The gas channel is in fluid communication with the gas fuel inlet where the structure meets the annular body. The structure also includes a slot opening defined at least partially along a radial length of the structure and configured to fluidically connect the gas channel and the air circuit to all gas fuel to effuse into the air circuit.
1. A fuel injector, comprising:
an annular body defining a gas fuel inlet therein; and
a structure extending radially outward from the annular body and configured to extend into an air circuit, the structure defining:
a gas channel defined within the structure, wherein the gas channel is in fluid communication with the gas fuel inlet where the structure meets the annular body;
a slot opening defined within the structure and configured to fluidically connect the gas channel with the air circuit to allow gas fuel to effuse into the air circuit; and
an air shroud attached to or formed from a radially outward end of the structure to define the air circuit, wherein the structure comprises an airfoil shape such that the structure is a vane of an air swirler that is configured to swirl air in the air circuit, wherein the slot opening is disposed proximate to a trailing edge of the vane and is defined through a concave high pressure side of the airfoil shape, wherein the gas channel and the slot opening are defined along the entire radial length of the structure, wherein the slot opening constricts flow from the gas channel.
2. The fuel injector of claim 1 , further comprising a plurality of the structure.
3. The fuel injector of claim 1 , further comprising an additional gas outlet to all gas fuel to effuse from the gas fuel inlet.
4. The fuel injector of claim 3 , wherein the additional gas outlet is defined axially through the annular body.
5. The fuel injector of claim 3 , wherein the additional gas outlet is defined radially outward of the air circuit in the air shroud in fluid communication with the air circuit, wherein the additional gas outlet is in fluid communication with the gas fuel inlet of the annular body through a strut that passes through the air circuit.
6. The fuel injector of claim 1 , further comprising a second air shroud disposed radially outward of the air shroud that is formed from or attached to the structure, wherein the second air shroud defines a second air circuit.
7. The fuel injector of claim 6 , further comprising an additional gas outlet to all gas fuel to effuse from the gas fuel inlet, wherein the additional gas outlet is defined between the air shroud that is formed from or attached to the structure or the second air shroud, wherein the additional gas outlet is in fluid communication with the second air circuit.
8. The fuel injector of claim 1 , further comprising a liquid fuel circuit and/or an inner air flow channel defined by the annular body.
9. The fuel injector of claim 8 , wherein the inner air flow channel includes an inner air swirler.
10. A method for making a fuel injector, comprising:
forming a structure that extends radially outward from an annular body and configured to extend into an air circuit, the structure defining:
a gas channel defined within the structure, wherein the gas channel is in fluid communication with the gas fuel inlet where the structure meets the annular body;
a slot opening defined within the structure and configured to fluidically connect the gas channel with the air circuit to allow gas fuel to effuse into the air circuit; and
an air shroud attached to or formed from a radially outward end of the structure to define the air circuit, wherein the structure comprises an airfoil shape such that the structure is a vane of an air swirler that is configured to swirl air in the air circuit, wherein the slot opening is disposed proximate to a trailing edge of the vane and is defined through a concave high pressure side of the airfoil shape, wherein the gas channel and the slot opening are defined along the entire radial length of the structure, wherein the slot opening constricts flow from the gas channel.