Fuel nozzle structure for air assist injection

• US 10,451,282 B2
• Filed: 12/23/2014
• Issued: 10/22/2019
• Est. Priority Date: 12/23/2013
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Benjamin, Michael Anthony, Mook, Joshua Tyler, Henderson, Sean James, Martinez, Ramon
• Primary Examiner(s): Sung, Gerald L
• Assistant Examiner(s): Cheng, Stephanie
• Application Number:
  US15/107,282
• Publication Number:
  US 20170003030A1
• Time in Patent Office: 1,764 Days
• CPC Class Codes: F23D 11/386 Nozzle cleaning
• CPC Class Codes: F23D 2209/30 Purging
• CPC Class Codes: F23R 2900/00004 Preventing formation of deposits on surfaces of gas turbine components, e.g. coke deposits
• CPC Class Codes: F23R 2900/03343 Pilot burners operating in premixed mode
• CPC Class Codes: F23R 3/14 by using swirl vanes
• CPC Class Codes: F23R 3/283 Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
• CPC Class Codes: F23R 3/286 having fuel-air premixing devices F23R3/30 takes precedence
• CPC Class Codes: F23R 3/34 Feeding into different combustion zones
• CPC Class Codes: F23R 3/343 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 Class Codes: F23R 3/346 for staged combustion

Abstract

A fuel nozzle includes an outer body extending parallel to a centerline axis, having a generally cylindrical exterior surface, forward and aft ends, and a plurality of openings through the exterior surface. The fuel nozzle further includes an inner body inside the outer body, cooperating with the outer body to define an annular space, and a main injection ring inside the annular space, the main injection ring including fuel posts extending therefrom. Each fuel post is aligned with one of the openings and separated from the opening by a perimeter gap which communicates with the annular space. There is a circumferential main fuel gallery in the main injection ring, and a plurality of main fuel orifices, wherein each orifice communicates with the main fuel gallery and extends through one of the fuel posts.

Claims

1. A fuel nozzle apparatus, comprising:

an annular outer body, the outer body extending parallel to a centerline axis, the outer body

having a generally cylindrical exterior surface extending between forward and aft ends, and having a plurality of openings passing through the exterior surface;

an annular inner body disposed inside the outer body, cooperating with the outer body to define an annular space;

an annular main injection ring disposed inside the annular space, the main injection ring including an annular array of fuel posts extending radially outward therefrom;

each fuel post being aligned with one of the openings in the outer body and separated from the opening by a perimeter gap which communicates with the annular space, wherein;

each fuel post 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

the perimeter gap is defined between the opening and the lateral surface;

a main fuel gallery extending within the main injection ring in a circumferential direction; and

a plurality of main fuel orifices, each main fuel orifice communicating with the main fuel gallery and extending through one of the fuel posts.

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

3. The apparatus of claim 1, wherein a convex-curved fillet is formed in the outer body adjoining the opening.

4. The apparatus of claim 1, wherein an assist port is formed in the perimeter wall near an intersection of the perimeter wall with the floor.

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

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

7. The apparatus of claim 1 further including:

an annular venturi including a throat of minimum diameter disposed inside the inner body;

an annular splitter disposed inside the venturi;

an array of outer swirl vanes extending between the venturi and the splitter;

a pilot fuel injector disposed within the splitter; and

an array of inner swirl vanes extending between the splitter and the pilot fuel injector.

8. The apparatus of claim 1 further comprising:

a fuel system operable to supply a flow of liquid fuel at varying flowrates;

a pilot fuel conduit coupled between the fuel system and the pilot fuel injector; and

a main fuel conduit coupled between the fuel system and the main injection ring.