Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same
View Patent ↗A method of manufacturing gas and/or fuel swirlers for fuel injectors and combustor domes and cone-shaped swirlers so manufactured are disclosed. The disclosed conical swirlers feature cut-through slots on a cone-shaped body. The contour and spacing of the slots are configured and arranged to accommodate a wide range of requirements for fluid flow areas and swirl strengths. Preferably, the cone-shaped swirlers can be manufactured by wire EDM processing. More preferably, multiple cone-shaped swirlers can be manufactured simultaneously by nesting swirler blanks in a stack and wire EDM processing the stack as a unit. The cone-shaped pinwheel swirler fits well into various fuel injector heads, enabling the injectors to reduce the frontal surface area and flat area for minimal potential of carbon formation.
1. A fuel injector comprising:
a) a heat shield defining a longitudinal axis and having a conical outer surface;
b) an air cap located outboard of the heat shield and having a conical inner surface, wherein an axially converging airflow channel is defined between the conical outer surface of the heat shield and the conical inner surface of the air cap; and
c) a conical air swirler disposed within the axially converging airflow channel and having an upstream inlet surface and a downstream outlet surface, wherein the upstream inlet surface of the conical air swirler defines a two-dimensional plane, the conical air swirler having a plurality of axially extending circumferentially spaced apart turning slots located between the upstream inlet surface and the downstream outlet surface, wherein the spaced apart turning slots are bounded in part by the conical outer surface of the heat shield and the conical inner surface of the air cap, and wherein the spaced apart turning slots are further bounded by turning vane walls that are oriented normal to the two-dimensional plane of the upstream inlet surface of conical swirler.
2. A fuel injector as recited in claim 1 , wherein the turning vane walls are planar in relation to the longitudinal axis.
3. A fuel injector as recited in claim 1 , wherein the turning vane walls are curved in relation to the longitudinal axis.
4. A fuel injector as recited in claim 1 , wherein the air cap has an opening with a necking area, wherein the airflow channel is defined between the air cap and the heat shield and wherein the air cap is structured and arranged to provide a converging, radially inward portion upstream of the necking area and a diverging, radially outward portion downstream of the necking area.
5. A fuel injector as recited in claim 4 , wherein the air cap has an inlet opening and an outlet opening, wherein the outlet opening has a necking area that is at least two times the area of the inlet opening at the inlet of the conical swirler.
6. A fuel injector as recited in claim 1 , further comprising a plurality of inner and outer airflow openings structured and arranged to accommodate multiple conical swirlers that are substantially concentric with respect to each other.
7. A fuel injector as recited in claim 1 , further comprising a fuel output portion that is structured and arranged to accommodate a cone-shaped swirler to provide a fuel spray that spreads downstream in a cone-shaped pattern in an axial direction.
8. A fuel injector as recited in claim 1 , further comprising a fuel output portion including a fuel injection device of a type selected from the group consisting of simplex, duplex, dual orifice, and annular pre-filming, wherein the fuel injection device is integrated with the conical swirler in an injector assembly.
9. A fuel injector as recited in claim 1 , further comprising a fuel output portion including a first nozzle to provide a primary fuel output spray, and a second nozzle to provide a secondary fuel output spray.