Multi-functional fuel nozzle with an atomizer array

Patent metadata

Field	Value
Publication number	US-9958152-B2
Application number	US-201415329639-A
Country	US
Kind code	B2
Filing date	Aug 14, 2014
Priority date	Aug 14, 2014
Publication date	May 1, 2018
Grant date	May 1, 2018

Abstract

A nozzle cap ( 82 ) is disposed at a downstream end of the nozzle. The nozzle cap includes a bore arranged to accommodate a downstream portion of a fluid-injecting lance that extends along a longitudinal axis ( 18 ) of the nozzle. The downstream portion of the fluid-injecting lance includes a centrally-located atomizer ( 80 ) to form a first atomized ejection cone. An array of atomizers ( 84 ) is disposed in the nozzle cap. The array of atomizers is circumferentially disposed about the longitudinal axis of the lance. The array of atomizers may be positioned radially outwardly relative to the centrally-located atomizer to form an array of respective second atomized ejection cones.

First claim

What is claimed is:

1. A multi-functional fuel nozzle for a combustion turbine engine, comprising:
a nozzle cap disposed at a downstream end of the nozzle, wherein the nozzle cap comprises a bore arranged to accommodate a downstream portion of a fluid-injecting lance that ex-tends along a longitudinal axis of the nozzle, the downstream portion of the fluid-injecting lance comprising a centrally-located atomizer to form a first atomized ejection cone; and
an array of atomizers in the nozzle cap, the array of atomizers circumferentially disposed about the longitudinal axis of the fluid-injecting lance, the array of atomizers being positioned radially outwardly relative to the centrally-located atomizer to form an array of respective second atomized ejection cones,
wherein the nozzle cap further comprises a plurality of gas fuel channels circumferentially disposed about the longitudinal axis of the nozzle, the plurality of gas fuel channels being positioned radially outwardly relative to the array of atomizers, wherein the nozzle cap comprises a plurality of castellations circumferentially arranged on a forward face of the nozzle cap, wherein the plurality of gas fuel channels comprise respective outlets arranged at respective top surfaces of the castellations,
wherein the array of atomizers is affixed to the nozzle cap by way of respective threaded connections,
wherein a number of atomizers in the array of atomizers and/or an angular spread of the array of respective second atomized ejection cones is arranged to target a desired zone in a combustion basket,
and wherein, to target a second desired zone, at least some of the atomizers of the array of atomizers are removed and respective spaces previously occupied by the removed atomizers comprise respective plugs to close the respective spaces.

2. The multi-functional fuel nozzle of claim 1 , wherein the array of atomizers comprises an annular array and further wherein the nozzle cap comprises an annular array of atomizer outlets disposed on the forward face of the nozzle cap.

3. The multi-functional fuel nozzle of claim 1 , wherein, during a liquid fuel operating mode of the combustion turbine engine, the centrally-located atomizer is coupled to a first fluid circuit conveying a liquid fuel to form the first atomized ejection cone as an atomized cone of liquid fuel and the array of atomizers is coupled to a second fluid circuit conveying water to form the array of respective second atomized ejection cones as an atomized array of water cones.

4. The multi-functional fuel nozzle of claims 1 wherein, during a liquid fuel operating mode of the combustion turbine engine, the centrally-located atomizer is coupled to a first fluid circuit conveying water to form the first atomized ejection cone as an atomized cone of water and the array of atomizers is coupled to a second fluid circuit conveying a liquid fuel to form the array of respective second atomized ejection cones as an atomized array of liquid fuel cones.

5. The multi-functional fuel nozzle of claim 1 wherein, during a gas fuel operating mode of the combustion turbine engine, the array of atomizers is coupled to a fluid circuit conveying water to form the array of respective second atomized ejection cones as an atomized array of water cones.

6. The multi-functional fuel nozzle of claim 1 wherein, during a gas fuel operating mode of the combustion turbine engine, the centrally-located atomizer is coupled to a fluid circuit conveying water to form the first atomized ejection cone as an atomized cone of water.

7. A method regarding a multi-functional fuel nozzle for a combustion turbine engine, the method comprising:
disposing a nozzle cap at a downstream end of the nozzle, wherein the nozzle cap comprises a bore;
arranging in the bore of the nozzle cap a downstream portion of a fluid-injecting lance that extends along a longitudinal axis of the nozzle;
forming a first atomized ejection cone with a centrally located atomizer in the downstream portion of the fluid-injecting lance;
and circumferentially disposing about the longitudinal axis of the fluid-injecting lance, an array of atomizers;
affixing the array of atomizers to the nozzle cap by way of respective threaded connections;
forming with the array of atomizers an array of respective second atomized ejection cones;
and selecting a number of atomizers from the array of atomizers and/or selecting an angular spread of the respective second atomized ejection cones to target a desired zone in a combustion basket, wherein the selecting of the number of atomizers from the array of atomizers comprises removing at least some of the atomizers from the array of atomizers and plugging respective spaces previously occupied by the removed atomizers to close the respective spaces.

8. The method of claim 7 , wherein, during a liquid fuel operating mode of the combustion turbine engine, the forming of the first atomized ejection cone with the centrally located atomizer comprises forming an atomized cone of liquid fuel and the forming of the array of respective second atomized ejection cones with the array of atomizers comprises forming an atomized array of water cones.

9. The method of claim 7 , wherein, during a liquid fuel operating mode of the combustion turbine engine, the forming of the first atomized ejection cone with the centrally located atomizer comprises forming an atomized cone of water and the forming of the array of respective second atomized ejection cones with the array of atomizers comprises forming an atomized array of liquid fuel cones.

10. The method of claim 7 , wherein, during a gas fuel operating mode of the combustion turbine engine, the forming of the array of respective second atomized ejection cones with the array of atomizers comprises forming atomized cones of water.

11. The method of claim 7 , wherein, during a gas fuel operating mode of the combustion turbine engine, the forming of the first atomized ejection cone with the centrally located atomizer comprises forming an atomized cone of water.

Assignees

• Siemens Ag

Inventors

• Ramier Stephen A
• Barve Vinayak V
• Thackway Richard L
• Polyzopoulos Charalambos
• Abou-Jaoude Khalil Farid

Classifications

• F23C1/08 Primary

  liquid and gaseous fuel · CPC title

• F23L2900/07008

  Injection of water into the combustion chamber · CPC title

• F23L7/002

  Supplying water · CPC title

• F23R3/28

  characterised by the fuel supply (burners F23D) · CPC title

• F23D11/24

  by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space · CPC title