Fuel lance for liquid and/or gaseous fuels and method for operation thereof

• US 5,487,659 A
• Filed: 06/20/1994
• Issued: 01/30/1996
• Est. Priority Date: 08/10/1993
• Status: Expired due to Term

• Current Assignee: Alstom Technology Ltd. (Alstom SA)
• Original Assignee: ABB Management AG (ABB Limited)
• Inventors: Senior, Peter, Novacek, Peter, Eroglu, Adnan, Joos, Franz
• Primary Examiner(s): Jones, Larry
• Application Number:
  US08/262,454
• Time in Patent Office: 589 Days
• Field of Search: 431/350, 431/183, 431/2, 431/12, 431/8, 60/740, 60/737, 239/405
• US Class Current: 431/350
• CPC Class Codes: F23D 11/101 medium and fuel meeting before the burner outlet
• CPC Class Codes: F23D 14/22 with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
• CPC Class Codes: F23D 14/78 Cooling burner parts
• CPC Class Codes: F23D 17/002 gaseous or liquid fuel

Abstract

A fuel lance for liquid and/or gaseous fuels for use in a combustion chamber includes a liquid fuel pipe extending along a lance center line and defining a liquid fuel passage, a gas pipe surrounding the liquid fuel pipe and forming therebetween a gas passage, and a lance outer shell surrounding the gas pipe and forming an air passage around the gas pipe for cooling air and atomizer air. At least one air/fuel nozzle is provided in a peripheral side of the lance outer shell at a downstream end of the fuel lance for air flow out of the air passage into the combustion chamber. At least one gas nozzle is provided in the gas pipe for gas flow out of the gas passage into the air passage, the gas nozzle is positioned relative to the air/fuel nozzle so that gas from the gas nozzle flows with air from the air passage through the at least one air/fuel nozzle into the combustion chamber. At least one liquid fuel nozzle is provided in the liquid fuel pipe for liquid fuel flow out of the liquid fuel passage, the liquid fuel nozzle being positioned relative to the gas nozzle and air/fuel nozzle so that liquid fuel from the liquid fuel nozzle flows through the air passage and, with the air, through the air/fuel nozzle into the combustion chamber.

Claims

1. A fuel lance for liquid and/or gaseous fuels for use in a combustion chamber, which fuel lance comprises:

(a) a liquid fuel pipe extending along a lance center line and surrounding a liquid fuel passage for carrying a liquid fuel;

(b) a gas pipe surrounding the liquid fuel pipe and forming therebetween a gas passage for carrying a gaseous fuel;

(c) a lance outer shell surrounding the gas pipe and forming an air passage around the gas pipe for carrying cooling air and atomizer air;

(d) at least one air/fuel nozzle provided in a side of the lance outer shell at a downstream end of the fuel lance for air flow out of the air passage into the combustion chamber surrounding the fuel lance;

(e) at least one gas nozzle provided in the gas pipe for gas flow out of the gas passage into the air passage, wherein the at least one gas nozzle is positioned relative to the at least one air/fuel nozzle so that gas from the gas nozzle flows with air from the air passage through the at least one air/fuel nozzle into the combustion chamber; and

(f) at least one liquid fuel nozzle provided in the liquid fuel pipe for liquid fuel flow out of the liquid fuel passage the at least one liquid fuel nozzle being positioned relative to the at least one gas nozzle and at least one air/fuel nozzle so that liquid fuel from the liquid fuel nozzle flows through the air passage and, with the air, through the at least one air/fuel nozzle into the combustion chamber.

2. The fuel lance as claimed in claim 1, wherein the at least one air/fuel nozzle and the at least one gas nozzle are of circular configuration and are positioned on a common nozzle center line, and wherein a diameter of the gas nozzle is smaller than a diameter of the air/fuel nozzle.

3. The fuel lance as claimed in claim 2, further comprising a guide pipe extending from the gas nozzle through the air passage into the air/fuel nozzle, an airflow passage from the air/fuel nozzle surrounding the guide pipe.

4. The fuel lance as claimed in claim 2, wherein the liquid fuel nozzle is positioned on the common nozzle center line, and a diameter of the liquid fuel nozzle is smaller than the diameter of the gas nozzle.

5. The fuel lance as claimed in claim 4, wherein the liquid fuel pipe and the gas pipe are firmly connected to the lance outer shell in the region of the nozzles.

6. The fuel lance as claimed in claim 2, wherein the liquid fuel nozzle is positioned relative to the gas nozzle out of the nozzle center line, and the gas pipe is firmly connected to the lance outer shell in the region of the nozzles.

7. The fuel lance as claimed in claim 5, wherein, at a downstream end of the fuel lance, the gas pipe merges into a rounded, closed pipe end which is surrounded by the air passage and the lance outer shell and is fastened to the lance outer shell by a plurality of connecting webs which cross the air passage.

8. The fuel lance as claimed in claim 1, wherein the gas pipe and the liquid fuel pipe end, in a flow direction, before the at least one air/fuel nozzle, wherein the gas nozzle is positioned at the end of the gas pipe and the liquid fuel nozzle is positioned at the end of the liquid fuel pipe and the gas nozzle and liquid fuel nozzle are directed parallel to the lance center line and wherein a vane-shaped guide plate is provided for the at least one air/fuel nozzle, the guide plate positioned for deflecting gas and liquid flows emerging from the gas and liquid fuel nozzles by approximately 90°

and the gas and liquid flows into the air/fuel nozzle.

9. The fuel lance as claimed in claim 8, wherein, in the region of the air/fuel nozzle, the guide plate ends in a closed sheet-metal ring whose diameter is smaller than the diameter of the air/fuel nozzle so that the deflected gas and liquid fuel flows are jacketed by an airflow on emergence from the air/fuel nozzle.

10. The fuel lance as claimed in claim 8, wherein a guide pipe is fitted into the gas nozzle and wherein the guide plate is firmly connected to the lance outer shell in the region of the at least one air/fuel nozzle.

11. The fuel lance as claimed in claim 1, wherein a plurality of fuel/air nozzles is distributed over a periphery of the fuel lance.

12. The fuel lance as claimed in claim 1, wherein the lance outer shell and air passage extend along the lance centerline to form a downstream end of the fuel lance, and at least one auxiliary nozzle directed substantially parallel to the lance center line is provided in the lance outer shell at the downstream end for flow out of the air passage through the auxiliary nozzle into the combustion chamber.

13. The fuel lance as claimed in claim 1, wherein the fuel lance is fastened on a casing surrounding the combustion chamber by a side support arm having a streamlined profile and wherein the liquid fuel and gas pipes extend through the support arm to the fuel lance.

14. The fuel lance as claimed in claim 1, wherein, in the flow direction, the at least one gas nozzle is positioned upstream of the air/fuel nozzle and liquid fuel nozzle.

15. The fuel lance as claimed in claim 14, wherein the lance outer shell has at least one auxiliary nozzle directed substantially parallel to the lance center line at the downstream end of the fuel lance for air flow out of the air passage into the combustion chamber and wherein air pipes are disposed in the air passage to guide fuel-free cooling air past the gas nozzle to the auxiliary nozzle.

16. A method of operating a fuel lance, including a liquid fuel pipe extending along a lance center line and defining a liquid fuel passage and having at least one liquid fuel nozzle for liquid fuel flow out of the liquid fuel passage, a gas pipe surrounding the liquid fuel pipe and forming therebetween a gas passage and having at least one gas nozzle for gas flow out of the gas passage into the air passage, and a lance outer shell Surrounding the gas pipe and forming an air passage around the gas pipe for cooling air and atomizer air and having at least one air/fuel nozzle in a peripheral side of the lance outer shell at a downstream end of the fuel lance for air flow out of the air passage into the combustion chamber, wherein the gas nozzle is positioned relative to the air/fuel nozzle so that gas from the gas nozzle flows with air from the air passage through the at least one air/fuel nozzle into the combustion chamber and the liquid fuel nozzle is positioned relative to the gas nozzle and air/fuel nozzle so that liquid fuel from the liquid fuel nozzle flows through the air passage and with the air, through the air/fuel nozzle into the combustion chamber the method comprising the steps of:

directing air through the air passage to the air/fuel nozzle to cool the fuel lance and distribute fuel and

wherein the air is blown through the air/fuel nozzle into the combustion chamber as a flow jacketing the fuel flow.

17. The method as claimed in claim 16, wherein gas fuel is directed through the gas passage and the gas nozzle to the air/fuel nozzle and mixes the airflow, wherein the liquid fuel passage remains unused.

18. The method as claimed in claim 16, wherein liquid fuel is directed through the liquid fuel passage and the liquid fuel nozzle to the air/fuel nozzle and mixes with the airflow and wherein air is directed through the gas passage to the air/fuel nozzle to provide distribution and additional cooling of the liquid fuel.

19. The method as claimed in claim 16, wherein the air has a temperature of not more than 600°

C.

20. The method as claimed in claim 18, wherein the liquid fuel is in the form of an emulsion.