Fuel injecting device

Patent metadata

Field	Value
Publication number	US-11060730-B2
Application number	US-201715435670-A
Country	US
Kind code	B2
Filing date	Feb 17, 2017
Priority date	Aug 18, 2014
Publication date	Jul 13, 2021
Grant date	Jul 13, 2021

Abstract

A fuel injection device for a gas turbine combustor includes a pilot fuel injector disposed on an axis of the fuel injection device; an annular main fuel injector encircling the pilot fuel injector; and a plurality of main fuel injection holes formed in the main fuel injector and spaced circumferentially from each other for injecting fuel axially rearward. The main fuel injector includes an annular fuel passage forming portion, an inner ring portion on an inner peripheral side of the fuel passage forming portion, and an outer ring portion on an outer peripheral side of the fuel passage forming portion. One of a space between the fuel passage forming portion and the inner ring portion and a space between the fuel passage forming portion and the outer ring portion forms a pilot fuel supply passage, and the other one forms a main fuel supply passage.

First claim

What is claimed is:

1. A fuel injection device for a combustor of a gas turbine, the fuel injection device comprising:
a pilot fuel injector disposed on an axis of the fuel injection device;
a main fuel injector having a first annular shape and disposed so as to be concentric with the pilot fuel injector and encircle an outer periphery of the pilot fuel injector;
a plurality of main fuel injection holes that are formed in the main fuel injector so as to be spaced circumferentially from each other and are configured to inject a first fuel axially rearward; and
a main housing including an inner cylindrical portion that covers a radially inner side of the main fuel injector, an outer cylindrical portion that covers a radially outer side of the main fuel injector, a bottom wall portion that covers a front side of the main fuel injector, and a rear wall portion that covers a rear side of the main fuel injector;
the main fuel injector including a fuel passage forming portion of a second annular shape, an inner ring portion located on a radially inner side of the fuel passage forming portion so as to radially confront the fuel passage forming portion, and an outer ring portion located on a radially outer side of the fuel passage forming portion so as to radially confront the fuel passage forming portion,
wherein each of the plurality of main fuel injection holes is formed as a through-hole that opens axially in a rear end portion of the fuel passage forming portion,
wherein one of a first space between the fuel passage forming portion and the inner ring portion and a second space between the fuel passage forming portion and the outer ring portion forms a pilot fuel supply passage of a third annular shape configured to supply a second fuel to the pilot fuel injector,
the other one of the first space and the second space forms a main fuel supply passage of a fourth annular shape configured to supply the first fuel to the plurality of main fuel injection holes of the main fuel injector, and
wherein the main fuel injector is supported by the main housing only at one end portion of the main fuel injector so that a gap is defined between the main housing and the main fuel injector.

2. The fuel injection device as claimed in claim 1 , wherein the pilot fuel supply passage is located on a radially inner side of the main fuel supply passage.

3. The fuel injection device as claimed in claim 1 , further comprising:
a pilot fuel introducing passage provided on a downstream side of the pilot fuel supply passage and configured to introduce the second fuel into the pilot fuel injector; and
a pilot housing covering the pilot fuel introducing passage,

wherein the pilot fuel injector is axially slidably attached to the pilot housing.

4. The fuel injection device as claimed in claim 1 , wherein the main housing covers an entirety of the radially inner side of the main fuel injector.

5. The fuel injection device as claimed in claim 1 , wherein the main housing covers at least a portion of the main fuel injector that confronts the pilot fuel injector.

6. A fuel injection device for a combustor of a gas turbine, the fuel injection device comprising:
a pilot fuel injector disposed on an axis of the fuel injection device;
a main fuel injector having a first annular shape and disposed so as to be concentric with the pilot fuel injector and encircle an outer periphery of the pilot fuel injector;
a plurality of main fuel injection holes that are formed in the main fuel injector so as to be spaced circumferentially from each other and are configured to inject a first fuel axially rearward;
a main housing including an inner cylindrical portion that covers a radially inner side of the main fuel injector, an outer cylindrical portion that covers a radially outer side of the main fuel injector, a bottom wall portion that covers a front side of the main fuel injector, and a rear wall portion that covers a rear side of the main fuel injector; and
a support ring disposed inside the main housing and having a support ring front end portion that is supported by the main housing and a support ring rear end portion that supports the main fuel injector,
the main fuel injector including a fuel passage forming portion of a second annular shape, an inner ring portion located on a radially inner side of the fuel passage forming portion so as to radially confront the fuel passage forming portion, and an outer ring portion located on a radially outer side of the fuel passage forming portion so as to radially confront the fuel passage forming portion,
wherein each of the plurality of main fuel injection holes is formed as a through-hole that opens axially in a rear end portion of the fuel passage forming portion,
wherein one of a first space between the fuel passage forming portion and the inner ring portion and a second space between the fuel passage forming portion and the outer ring portion forms a pilot fuel supply passage of a third annular shape configured to supply a second fuel to the pilot fuel injector,
the other one of the first space and the second space forms a main fuel supply passage of a fourth annular shape configured to supply the first fuel to the plurality of main fuel injection holes of the main fuel injector, and
wherein the main fuel injector is supported by the main housing via the support ring only at one end portion of the main fuel injector so that a gap is defined between the main housing and the main fuel injector.

7. The fuel injection device as claimed in claim 6 , wherein a first radial gap is defined between an inner peripheral surface of the support ring and an outer peripheral surface of the inner cylindrical portion of the main housing,
wherein a second radial gap is defined between an outer peripheral surface of the support ring and an inner peripheral surface of the inner ring portion, and wherein the gap defined between the main housing and the main fuel injector includes the first radial gap and the second radial gap.

Assignees

• Kawasaki Heavy Ind Ltd

Inventors

• Matsuyama Ryusuke
• Nishiura Takeo

Classifications

• F23R3/343 Primary

  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

• F23R3/286

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

• F23R3/283

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

• F02C7/232

  Fuel valves {(control of fuel supply by means of fuel metering valves F02C9/263)}; Draining valves or systems (valves in general F16K) · CPC title

• F23R3/28

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