Fuel nozzle with dual-staged main circuit

1. A fuel nozzle apparatus for a gas turbine engine, comprising:

an annular outer body extending parallel to a centerline axis and having an exterior surface extending between forward and aft ends, and having a ring of forward openings passing through the exterior surface, and a ring of aft openings passing through the exterior surface, the ring of aft openings positioned axially aft of the ring of forward openings and circumferentially offset from the ring of forward openings;

an annular main injection ring disposed inside the annular outer body and including:

a forward main fuel gallery extending in a circumferential direction;

an aft main fuel gallery extending in the circumferential direction;

a ring of forward main fuel orifices, each forward main fuel orifice of the ring of forward main fuel orifices communicating with the forward main fuel gallery and aligned with one of the forward openings of the ring of forward openings;

a ring of aft main fuel orifices, each aft main fuel orifice of the ring of aft main fuel orifices communicating with the aft main fuel gallery and aligned with one of the aft openings of the ring of aft openings; and

a pilot fuel injector disposed along the centerline axis,

wherein the annular main injection ring includes an annular array of fuel posts extending radially outward from the annular main injection ring, each fuel post of the annular array of fuel posts being aligned with one of the openings of the ring of forward openings or the ring of aft openings in the annular outer body and separated from the one of the openings of the ring of forward openings or the ring of aft openings by a perimeter gap, the perimeter gap being around each fuel post of the annular array of fuel posts and permitting a purge air to flow through; and

each main fuel orifice of the ring of forward main fuel orifices and the ring of aft main fuel orifices extends through one of the fuel posts of the annular array of fuel posts; and

wherein each fuel post of the annular array of fuel posts is elongated in plan view and includes a perimeter wall defining a lateral surface and a radially-outward-facing floor recessed radially inward from a distal end surface of the perimeter wall to define a spray well; and

wherein the perimeter gap is defined between each opening of the ring of forward openings or the ring of aft openings and each lateral surface of the annular array of fuel posts.

2. The apparatus of claim 1 , wherein a concave fillet is disposed at the junction of each fuel post of the annular array of fuel posts and the annular main injection ring.

3. The apparatus of claim 1 , wherein a convex-curved fillet is formed n the annular outer body adjoining each opening of the ring of forward openings and the ring of aft openings.

4. The apparatus of claim 1 , wherein an assist port is formed in the perimeter wall of each fuel post of the annular array of fuel posts near an intersection of the perimeter wall of each fuel post of the annular array of fuel posts with the radially-outward facing floor of each fuel post of annular array of fuel posts.

5. The apparatus of claim 1 , wherein at least one of the fuel posts of the annular array of fuel posts incorporates a ramp-shaped scarf extending along a line parallel to the distal end surface of the at least one of the fuel posts of the annular array of fuel posts, the ramp-shaped scarf having a maximum radial depth at the spray well of the at least one of the fuel posts of the annular array of fuel posts and tapering outward in radial height, joining the distal end surface of the at least one of the fuel posts of the annular array of fuel posts at a distance away from the spray well of the at least one of the fuel posts of the annular array of fuel posts.

6. The apparatus of claim 1 , wherein the perimeter wall of each fuel post of the annular array of fuel posts is racetrack-shaped in plan view.