Fuel nozzle with dual-staged main circuit

Patent metadata

Field	Value
Publication number	US-10001281-B2
Application number	US-201514689765-A
Country	US
Kind code	B2
Filing date	Apr 17, 2015
Priority date	Apr 17, 2015
Publication date	Jun 19, 2018
Grant date	Jun 19, 2018

Abstract

A fuel nozzle apparatus for a gas turbine engine includes: an annular outer body extending parallel to a centerline axis and having an exterior surface, and having a ring of forward openings passing through the exterior surface, and a ring of aft openings passing through the exterior surface, the aft openings positioned axially aft of the forward openings; an annular main injection ring disposed inside the outer body and including: a forward main fuel gallery extending in a circumferential direction; an aft main fuel gallery extending in a circumferential direction; a ring of forward main fuel orifices communicating with the forward main fuel gallery and each aligned with one of the forward openings; a ring of aft main fuel orifices, communicating with the aft main fuel gallery and each aligned with one of the aft openings; and a pilot fuel injector disposed along the centerline axis.

First claim

What is claimed is:

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.

Assignees

• Gen Electric

Inventors

• Patel Nayan Vinodbhai
• Thomsen Duane Douglas

Classifications

• F23R3/343

  Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion (ignition in gas-turbine plants F02C7/264; pilot flame igniters F23Q9/00) · CPC title

• F23R3/36

  Supply of different fuels · CPC title

• F23R3/286 Primary

  having fuel-air premixing devices (F23R3/30 takes precedence) · CPC title

• F23R3/14

  by using swirl vanes · CPC title

• F23C7/004

  using vanes · CPC title