Fuel injector with multi tube gas distribution

Patent metadata

Field	Value
Publication number	US-10082082-B2
Application number	US-201614988588-A
Country	US
Kind code	B2
Filing date	Jan 5, 2016
Priority date	Jan 5, 2016
Publication date	Sep 25, 2018
Grant date	Sep 25, 2018

Abstract

A fuel injector for a gas turbine engine is disclosed. The fuel injector includes a flange assembly with a distribution block, three main gas tubes, and an injector head. The distribution block evenly distributes a main gas fuel to the three main gas tubes. The injector head includes an injector body with a primary gas gallery including an annular shape. The three main gas tubes are connected in a parallel configuration between the distribution block and the primary gas gallery. The three main gas tubes are all in flow communication with the primary gas gallery and provide the main gas fuel from the same main gas fuel source.

First claim

What is claimed is:

1. A fuel injector for a gas turbine engine, comprising:
a first primary tube;
a second primary tube;
a secondary tube;
a flange;
a distribution block for distributing a main gas fuel to the first primary tube, the second primary tube and the secondary tube, the distribution block extending from the flange, the distribution block defining
a first primary passage in flow communication with the first primary tube,
a second primary passage in flow communication with the second primary tube, the second primary passage and the second primary tube being in a first parallel configuration with the first primary passage and the first primary tube, and
a secondary passage in flow communication with the secondary tube, the secondary passage and the secondary tube being in a second parallel configuration with the first primary passage and the first primary tube, and in a third parallel configuration with the second primary passage and the second primary tube;
a gas inlet passage extending into the distribution block to the first primary passage, the second primary passage and the secondary passage, the gas inlet passage in flow communication with the first primary passage, the second primary passage, and the secondary passage;

a primary gas fitting for supplying the main gas fuel to the distribution block, the primary gas fitting in flow communication with the gas inlet passage;
an injector body defining a primary gas gallery having an annular shape;
a first primary fuel transfer fitting in flow communication with the primary gas gallery and connected to the first primary tube for directing the main gas fuel from the first primary tube into the primary gas gallery;
a second primary fuel transfer fitting in flow communication with the primary gas gallery and connected to the second primary tube for directing the main gas fuel from the second primary tube into the primary gas gallery;
a secondary fuel transfer fitting in flow communication with the primary gas gallery and connected to the secondary tube for directing the main gas fuel from the secondary tube into the primary gas gallery;
wherein the first primary passage, the second primary passage and the secondary passage all intersect at the gas inlet passage; and
wherein the first primary passage, the second primary passage, and the secondary passage are cross-drilled into the distribution block, and wherein the distribution block includes a first plug at a first end of the first primary passage, a second plug at a second end of the second primary passage, and a third plug at a third end of the secondary passage.

2. The fuel injector of claim 1 , wherein the distribution block is integral to the flange and extends axially from the flange relative to an assembly axis of the fuel injector.

3. The fuel injector of claim 1 , wherein the gas inlet passage is further defined by the flange, and wherein the gas inlet passage extends through the flange and into the distribution block, and the primary gas fitting is affixed to the flange.

4. The fuel injector of claim 1 , wherein the secondary tube extends from the distribution block to the injector body to support the injector body and prevent deflection of the injector body.

5. The fuel injector of claim 1 , further comprising a tube stem extending through the flange to the injector body, the tube stem defining a pilot gas passage for providing a pilot gas fuel to the injector head.

6. A fuel injector for a gas turbine engine, comprising:
a flange;
a distribution block extending from the flange;
a primary gas fitting for supplying a main gas fuel to the distribution block;
a gas inlet passage formed in the distribution block and extending into the distribution block from the primary gas fitting, the gas inlet passage being in flow communication with the primary gas fitting;
a first primary passage formed in the distribution block and in flow communication with the gas inlet passage;
a second primary passage formed in the distribution block and in flow communication with the gas inlet passage and in a first parallel configuration with the first primary passage;
a secondary passage formed in the distribution block and in flow communication with the gas inlet passage and in a second parallel configuration with the first primary passage and in a third parallel configuration with the second primary passage;
an injector head including an injector body;
a primary gas gallery formed in the injector body, the primary gas gallery having an annular shape;
a first primary tube extending from the distribution block to the injector head, the first primary tube being in flow communication with the first primary passage and the primary gas gallery;
a second primary tube extending from the distribution block to the injector head, the second primary tube being in flow communication with the second primary passage and the primary gas gallery;
a secondary tube extending from the distribution block to the injector head to support the injector head and prevent deflection of the injector head, the secondary tube being in flow communication with the secondary passage and the primary gas gallery; wherein the distribution block is configured to distribute the main gas fuel to the primary gas gallery through the first primary tube, the second primary tube, and the secondary tube;
wherein the first primary passage, the second primary passage and the secondary passage all intersect at the gas inlet passage; and
wherein the first primary passage, the second primary passage, and the secondary passage are cross-drilled into the distribution block, and wherein the distribution block includes a first plug at a first end of the first primary passage, a second plug at a second end of the second primary passage, and a third plug at a third end of the secondary passage.

7. The fuel injector of claim 6 , wherein the distribution block is integral to the flange and extends axially from the flange relative to an assembly axis of the fuel injector.

8. The fuel injector of claim 6 , wherein the gas inlet passage extends through the flange and the primary gas fitting is affixed to the flange.

9. The fuel injector of claim 6 , further comprising a tube stem extending through the flange to the injector head, the tube stem defining a pilot gas passage for providing a pilot gas fuel to the injector head.

10. The fuel injector of claim 6 , further comprising:
a first primary tube port formed in the distribution block and fluidly connecting the first primary passage to the first primary tube;
a second primary tube port formed in the distribution block and fluidly connecting the second primary passage to the second primary tube; and
a secondary tube port formed in the distribution block and fluidly connecting the secondary passage to the secondary tube.

11. A fuel injector for a gas turbine engine, comprising:
a flange assembly including
a flange, and
a distribution block extending from the flange;

an injector head including
an injector body,
an inner premix tube joined to the injector body, the inner premix tube including a premix tube inner surface, and
an outer premix barrel joined to the injector body, the outer premix barrel including
a plurality of vanes, and
a premix tube outer surface located outward from the premix tube inner surface, the premix tube outer surface and the premix tube inner surface forming a premix passage that directs a mixture of a main gas fuel and air into a combustion chamber of the gas turbine engine; and

a single main gas fuel circuit for providing the main gas fuel to the premix passage, the single main gas fuel circuit including
a primary gas fitting for

Assignees

• Solar Turbines Inc

Inventors

• Spivey Sean Kelly
• Cramb Donald James
• Piper James Scott
• Ramotowski Michael John

Classifications

• F23R3/36

  Supply of different fuels · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F23R2900/00004

  Preventing formation of deposits on surfaces of gas turbine components, e.g. coke deposits · CPC title

• F23R3/34

  Feeding into different combustion zones · CPC title

• F02C7/222 Primary

  Fuel flow conduits, e.g. manifolds · CPC title