Multi-functional fuel nozzle with a dual-orifice atomizer

Patent metadata

Field	Value
Publication number	US-10132240-B2
Application number	US-201415328228-A
Country	US
Kind code	B2
Filing date	Aug 14, 2014
Priority date	Aug 14, 2014
Publication date	Nov 20, 2018
Grant date	Nov 20, 2018

Abstract

A multi-functional fuel nozzle ( 10 ) for a combustion turbine engine is provided. An annular fuel-injecting lance ( 12 ) may include a first fluid circuit ( 14 ) and a second fluid circuit ( 16 ). One of the first and second fluid circuits during a liquid fuel operating mode of the combustion turbine engine may convey a liquid fuel. The other of the first and second fluid circuits may convey a selectable non-fuel fluid. An atomizer ( 30 ) is disposed at the downstream end of the lance. The atomizer may have a first ejection orifice ( 32 ) responsive to the first fluid circuit to form a first atomized ejection cone ( 34 ), and a second ejection orifice ( 36 ) responsive to the second fluid circuit to form a second atomized ejection cone ( 38 ). The first and second ejection cones ( 34, 38 ) formed with the atomizer may be concentric cones that intersect with one another over a predefined angular range.

First claim

What is claimed is:

1. A multi-functional fuel nozzle for a combustion turbine engine, comprising:
an annular fuel-injecting lance comprising a first fluid circuit and a second fluid circuit,
wherein the first fluid circuit is centrally disposed within the lance, wherein the first fluid circuit extends along a longitudinal axis of the lance to convey a first fluid to a downstream end of the lance,
wherein the second fluid circuit is annularly disposed about the first fluid circuit to convey a second fluid to the downstream end of the lance, wherein one of the first and second fluids comprises a liquid fuel conveyed by one of the first and second fluid circuits during a liquid fuel operating mode of the combustion turbine engine,
wherein the other of the first and second fluids conveyed by the other of the first and second fluid circuits comprises a selectable non-fuel fluid; and
an atomizer disposed at the downstream end of the lance, the atomizer having a first ejection orifice responsive to the first fluid circuit to form a first atomized ejection cone, the atomizer further having a second ejection orifice responsive to the second fluid circuit to form a second atomized ejection cone, wherein the first and second ejection orifices of the atomizer are respectively configured so that the first and second ejection cones formed with the atomizer comprise concentric cones that intersect with one another over an angular range of intersection; and
a plurality of gas fuel channels circumferentially disposed about the longitudinal axis of the lance, the plurality of gas fuel channels being positioned circumferentially outwardly relative to the annular lance, wherein, during a gas fuel operating mode of the engine, the selectable non-fuel fluid comprises water, which is conveyed by at least one of the first and second fluid circuits, and wherein at least one of the first and second ejection cones comprises a respective cone formed of atomized water, wherein relatively larger intersecting angular differences between the first and second atomized ejection cones are conducive to enhanced atomization during an ignition event of the liquid fuel and relatively smaller intersecting angular differences between the first and second atomized ejection cones are conducive to enhanced NOx abatement during gas fuel operation.

2. The multi-functional fuel nozzle of claim 1 , wherein in the liquid fuel operating mode of the combustion turbine engine, the first atomized ejection cone comprises one of the liquid fuel or the selectable non-fuel fluid, and the second atomized ejection cone comprises the other of the liquid fuel or the selectable non-fuel fluid.

3. The multi-functional fuel nozzle of claim 1 , wherein, during the ignition event of the liquid fuel, the selectable non-fuel fluid comprises air, which is conveyed by the first fluid circuit, and the first atomized ejection cone comprises a cone of air, and the liquid fuel comprises an oil fuel, which is conveyed by the second fluid circuit, and the second atomized ejection cone comprises a cone of atomized oil fuel, and further wherein, subsequent to the ignition event of the liquid fuel, the selectable non-fuel fluid comprises water, which is conveyed by the first fluid circuit, and the first atomized ejection cone comprises a cone of atomized water.

4. The multi-functional fuel nozzle of claim 1 , wherein, during the ignition event of the liquid fuel, the liquid fuel comprises an oil fuel, which is conveyed by the first circuit, and the first atomized ejection cone comprises a cone of atomized oil fuel, and the selectable non-fuel fluid comprises air, which is conveyed by the second circuit, and the second atomized ejection cone comprises a cone of air, and further wherein, subsequent to the ignition event of the liquid fuel, the selectable non-fuel fluid comprises water, which is conveyed by the second fluid circuit, and the second atomized ejection cone comprises a cone formed of atomized water, which is mixed with the cone of atomized oil fuel.

5. The multi-functional fuel nozzle of claim 4 , wherein, during the gas fuel operating mode of the engine, the selectable non-fuel fluid comprises water, which is conveyed by at least one of the first and second fluid circuits, and wherein at least one of the first and second ejection cones comprises a respective cone formed of atomized water.

6. The multi-functional fuel nozzle of claim 1 , wherein, during the gas fuel operating mode of the engine, at least some of the plurality of gas fuel channels convey water mixed with fuel gas.

7. The multi-functional fuel nozzle of claim 1 , wherein, during the gas fuel operating mode of the engine, at least some of the plurality of gas fuel channels convey water mixed with fuel gas.

8. The multi-functional fuel nozzle of claim 1 , wherein an angular range of the first atomized ejection cone extends from approximately 80 degrees to approximately 120 degrees.

9. The multi-functional fuel nozzle of claim 8 , wherein an angular range of the first atomized ejection cone extends from approximately 90 degrees to approximately 115 degrees.

10. The multi-functional fuel nozzle of claim 9 , wherein an angular range of the first atomized ejection cone extends from approximately 104 degrees to approximately 110 degrees.

11. The multi-functional fuel nozzle of claim 1 , wherein an angular range of the second atomized ejection cone extends from approximately 40 degrees to approximately 90 degrees.

12. The multi-functional fuel nozzle of claim 11 , wherein an angular range of the second atomized ejection cone extends from approximately 60 degrees to approximately 80 degrees.

13. A method regarding a multi-functional fuel nozzle for a combustion turbine engine, the method comprising:
centrally disposing a first fluid circuit within an annular fuel-injecting lance, wherein the first fluid circuit extends along a longitudinal axis of the lance to convey a first fluid to a downstream end of the lance;
annularly disposing a second fluid circuit about the first fluid circuit to convey a second fluid to the downstream end of the lance;
circumferentially disposing about the longitudinal axis of the lance a plurality of gas fuel channels, and positioning the plurality of gas fuel channels circumferentially outwardly relative to the annular lance;
during a liquid fuel operating mode of the engine, one of the first and second fluids comprising a liquid fuel, conveying the liquid fuel with one of the first and second fluid circuits;
the other of the first and second fluids comprising a selectable non-fuel fluid, conveying the selectable non-fuel fluid with the other of the first and second circuits;
disposing a dual orifice atomizer at the downstream end of the lance;
coupling the dual orifice atomizer to the first fluid circuit to form a first atomized ejection cone and to the second fluid circuit to form a second atomized ejection cone; and
arranging the first and the second ejection cones to intersect with one another over an intersecting angular range, wherein relatively larger intersecting angular differences between the first and second atomized ejection cones are conducive to enhanced atomization during an ignition event of the liquid fuel and relatively smaller intersecting angular differences between the first and second atomized ejection cones are conducive to enhanced NOx abatement during gas fuel operation.

14. The method of claim 13 , further comprising defining an angular range of the first ejection cone to extend from approximately 80 degrees to approximately 120 degrees.

15. The method of claim 14 , wherein

Assignees

• Siemens Ag

Inventors

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

Classifications

• F23R3/286

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

• F02C3/30 Primary

  Adding water, steam or other fluids {for influencing combustion, e.g. to obtain cleaner exhaust gases (F02C7/141, F02C7/30, F01D21/00, F01K21/04, F23D11/10 take precedence)} · CPC title

• F23R3/36

  Supply of different fuels · CPC title

• F23D17/002

  gaseous or liquid fuel · CPC title

• F02C7/22

  Fuel supply systems · CPC title