Burners having fuel plenums

Patent metadata

Field	Value
Publication number	US-9982891-B2
Application number	US-201414563532-A
Country	US
Kind code	B2
Filing date	Dec 8, 2014
Priority date	Aug 17, 2012
Publication date	May 29, 2018
Grant date	May 29, 2018

Abstract

Burners having a fuel plenum in a base are disclosed. One disclosed example apparatus includes a base of a burner, the base comprising a fuel plenum and coupled to fuel nozzles, where at least one of the fuel nozzles is in fluid communication with the fuel plenum. The disclosed example apparatus also includes a burner head of the burner comprising nozzle passages in fluid communication with an airflow path, where the burner head defines a pilot combustion space that opens towards a flame tube of the burner, and is in fluid communication with the airflow path, and where each nozzle passage is to receive a fuel nozzle to provide fuel to entrain with air from the airflow path.

First claim

What is claimed is:

1. A burner to produce heated gas, comprising:
a flame tube located in an air guiding device that encloses the flame tube and defines an airflow path; and
a burner head coupled to a base, the burner head comprising a burner-head body, the burner-head body having a plurality of nozzle passages that fluidly communicate with the airflow path,
wherein a fuel nozzle of a plurality of fuel nozzles projects into each nozzle passage to provide fuel mixed with air from the airflow path into the flame tube,
wherein each fuel nozzle is fastened to the base and fluidly coupled to a fuel plenum formed in the base,
wherein the burner-head body encloses a pilot combustion space that is open towards the flame tube and is in fluid communication with the air guiding device, the burner-head body has a substantially cup-shaped design with a bottom wall and a pilot combustion-space wall to enclose the pilot combustion space,
wherein the bottom wall has a bottom-side opening for a pilot fuel nozzle that projects into the burner-head body a plurality of air guiding passages which extend into the bottom wall, open into and has the bottom-side opening and are in fluid communication with the air guiding device, and
wherein the pilot combustion-space wall has a wall surface delimiting the pilot combustion space, and wherein the nozzle passages that communicate with the airflow path in the air guiding device are formed in the pilot combustion-space wall.

2. The burner as defined in claim 1 , wherein the pilot combustion space is formed in an insert, the insert fastened on the base, the insert including a wall which projects into the burner-head body and is cooled with air that flows through at least one fluid passage that is in fluid communication with the airflow path and located between the insert and the burner head.

3. The burner as defined in claim 1 , wherein the fuel plenum is an annular passage of the base.

4. The burner as defined in claim 1 , wherein the fuel nozzles are fastened to a mounting device that covers the fuel plenum.

5. The burner as claimed in claim 4 , wherein the fuel nozzles are welded or screwed onto the mounting device.

6. The burner as defined in claim 1 , wherein the fuel nozzles are produced from temperature-resistant bar stock provided with a core bore.

7. The burner as defined in claim 1 , wherein the base is shaped as a flanged part to fasten the burner in a pressure casing.

8. The burner as defined in claim 1 , wherein airflow is guided along at least a portion of the burner head on a burner-head outer surface to cool the burner-head body.

9. The burner as defined in claim 1 , wherein the pilot combustion space is provided with fuel via a pilot fuel nozzle.

10. The burner as defined in claim 1 , wherein the wall surface for the pilot combustion space is coated with a thermal protective coating.

11. The burner as defined in claim 1 , wherein the air guiding device comprises an air guiding tube supported by a spring-elastic bearing of the base and is movable relative to the base to compensate for thermal expansion.

12. The burner as defined in claim 11 , wherein the spring-elastic bearing has a spring seated on the base and is supported by a spring strut fastened to the air guiding tube.

13. A gas turbine plant including the burner as defined in claim 1 .

14. A burner to produce heated gas, comprising:
a flame tube located in an air guiding device that encloses the flame tube and defines an airflow path; and
a burner head coupled to a base and comprising a burner-head body, the burner-head body having a plurality of nozzle passages that fluidly communicate with the airflow path, wherein a fuel nozzle of a plurality of fuel nozzles projects into each nozzle passage to provide fuel mixed with air from the airflow path into the flame tube, wherein each fuel nozzle is fastened to the base and fluidly coupled to a fuel plenum formed in the base, wherein the burner-head body encloses a pilot combustion space that is open towards the flame tube and is in fluid communication with the air guiding device, wherein the air guiding device comprises an air guiding tube supported by a spring-elastic bearing of the base and is movable relative to the base to compensate for thermal expansion, wherein the spring-elastic bearing has a spring seated on the base and is supported by a spring strut fastened to the air guiding tube, wherein the air guiding tube is movable relative to a baffle plate by a radially extending flange of the spring strut that is coupled to the air guiding tube, wherein the baffle plate is cup-shaped and fits over the air guiding tube, wherein the baffle plate fastened to the base, and wherein the baffle plate deflects the air from the air guiding tube into the nozzle passages.

15. The burner as defined in claim 14 , further comprising an insulation shield between the baffle plate and the base to thermally decouple the baffle plate, the air guiding device and the flame tube from the base.

16. A burner comprising:
a flame tube defining a combustion chamber and having a longitudinal axis;
a substantially flat base that is arranged at an end of the flame tube; the base including an insulation shield;
a plurality of fuel nozzles and a pilot fuel nozzle, wherein the plurality of fuel nozzles and the pilot fuel nozzle extend from the base; and
a burner-head axially offset from the base and extending from the base to fit within the flame tube, wherein the burner-head comprises an annular wall which radially encloses a pilot combustion space and a lower wall that is proximate the base, wherein the burner-head is proximate the annular wall and forms an axial boundary of the pilot combustion space, the annular wall including axially arranged nozzle passages that extend substantially parallel to the longitudinal axis, wherein each one of the nozzle passages receives a respective fuel nozzle of the plurality of fuel nozzles, the lower wall including air passages that are radially oriented, and include air inlets at a radially outer surface of the lower wall and air outlets that supply air to a mixing chamber formed in the lower wall, the pilot nozzle extending into the mixing chamber,
wherein each one of the nozzle passages is sized so that air flows through nozzle passage inlets and around the respective fuel nozzle to mix with fuel from the nozzle and create an air fuel mixture, the fuel nozzle passages configured to provide the air fuel mixture downstream of the pilot combustion space and into the flame tube.

17. The burner as defined in claim 16 , further including a fuel plenum that is an annular passage of the base.

18. The burner as defined in claim 16 , wherein the pilot combustion space is formed in an insert, the insert fastened on the base, the insert including a wall which projects into the burner-head and is cooled with air that flows through at least one fluid passage that is in fluid communication with an airflow path and located between the insert and the burner head.

19. The burner as defined in claim 18 , wherein the fuel nozzles are each fastened to a mounting device that covers the fuel plenum.

20. The burner as claimed in claim 17 wherein the fuel nozzles are welded or screwed onto the mounting device.

21. The burner as defined in claim 16 , wherein the fuel nozzles are produced from temperature-resistant bar stock provided with a core bore.

22. The burner as defined in claim 16 , wherein the base is shaped as a flanged part to fasten t

Assignees

• Duerr Systems Ag
• Deutsch Zentr Luft & Raumfahrt

Inventors

• Widenhorn Axel
• Stoll Roland
• Lebküchner Dominik
• Kissel Thilo
• Zanger Jan
• Zornek Timo
• Monz Thomas

Classifications

• F23R3/54

  Reverse-flow combustion chambers · CPC title

• F23R3/286 Primary

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

• F23R3/283 Primary

  Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances · CPC title

• 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

• F23R2900/03282

  High speed injection of air and/or fuel inducing internal recirculation · CPC title