Burner assembly, gas turbine combustor, and gas turbine

Patent metadata

Field	Value
Publication number	US-11859822-B2
Application number	US-202217953578-A
Country	US
Kind code	B2
Filing date	Sep 27, 2022
Priority date	Apr 22, 2020
Publication date	Jan 2, 2024
Grant date	Jan 2, 2024

Abstract

A burner assembly includes a plurality of burners for mixing fuel and air. Each of the plurality of burners includes: a fuel nozzle for injecting the fuel; a mixing passage supplied with the fuel and the air; and a support portion connecting a passage wall of the mixing passage and the fuel nozzle to support the fuel nozzle.

First claim

The invention claimed is:

1. A burner assembly comprising a plurality of burners for mixing fuel and air,
wherein each of the plurality of burners includes:
a fuel nozzle for injecting the fuel;
a mixing passage supplied with the fuel and the air;
a support portion connecting a passage wall of the mixing passage and the fuel nozzle to support the fuel nozzle;
a first passage formed inside the fuel nozzle and extending along an axial direction of the fuel nozzle;
a fuel chamber formed outside of the mixing passage in a radial direction of the fuel nozzle and holding the fuel to be supplied to the fuel nozzle; and
a second fuel passage formed inside the support portion,

wherein one end of the second fuel passage is connected to the first fuel passage, and the other end of the second fuel passage is connected to the fuel chamber.

2. The burner assembly according to claim 1 ,
wherein the fuel nozzle includes a tapered portion whose outer diameter decreases downstream in a flow direction of the air,
wherein the mixing passage includes a contraction portion whose passage width decreases downstream in the flow direction of the air, and
wherein a range where the tapered portion is disposed and a range where the contraction portion is disposed at least partially overlap in an axial direction of the mixing passage.

3. The burner assembly according to claim 1 ,
wherein a fuel passage for supplying the fuel to the fuel nozzle is formed inside the support portion.

4. The burner assembly according to claim 3 ,
wherein the support portion is formed inside the mixing passage.

5. The burner assembly according to claim 3 ,
wherein the support portion is disposed upstream of the mixing passage in a flow direction of the air.

6. The burner assembly according to claim 5 ,
wherein an upstream end portion of the fuel nozzle in the flow direction of the air is located outside the mixing passage, and
wherein the support portion extends away from a fuel injection hole of the fuel nozzle in an axial direction of the mixing passage as the support portion comes close to the fuel nozzle.

7. The burner assembly according to claim 1 ,
wherein an upstream surface of the support portion in a flow direction of the air includes a convex curved surface.

8. The burner assembly according to claim 1 ,
wherein a downstream surface of the support portion in a flow direction of the air includes a stepped surface.

9. The burner assembly according to claim 1 ,
wherein each of the burners includes a plurality of the support portions, and
wherein the plurality of support portions are arranged around the fuel nozzle at intervals.

10. The burner assembly according to claim 9 ,
wherein each of the plurality of support portions is a swirl vane configured to form an air flow in a common swirling direction.

11. A gas turbine combustor, comprising:
the burner assembly according to claim 1 ; and
a combustion liner forming a space in which a flame is formed downstream of the burner assembly.

12. A gas turbine, comprising:
a compressor;
a gas turbine combustor configured to be supplied with air compressed by the compressor and fuel, and produce a combustion gas by combusting the fuel; and
a turbine driven by the combustion gas produced by the gas turbine combustor,
wherein the gas turbine combustor is the gas turbine combustor according to claim 11 .

13. The burner assembly according to claim 1 ,
wherein the burner assembly comprises a partition wall separating two adjacent mixing passages of the plurality of burners,
wherein the fuel chamber is formed inside the partition wall.

Assignees

• Mitsubishi Heavy Ind Ltd

Inventors

• Fukuba Shinichi
• Takiguchi Satoshi
• Miura Keisuke
• Asai Tomohiro
• Miyamoto Kenji
• Kawakami Tomo

Classifications

• F23R3/286 Primary

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

• F23R3/14

  by using swirl vanes · CPC title

• F23D14/04 Primary

  induction type, e.g. Bunsen burner · CPC title

• F23R3/28 Primary

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

• F23D11/102

  in an internal mixing chamber · CPC title