Combustor and gas turbine

Patent metadata

Field	Value
Publication number	US-9926845-B2
Application number	US-201213687587-A
Country	US
Kind code	B2
Filing date	Nov 28, 2012
Priority date	Feb 28, 2012
Publication date	Mar 27, 2018
Grant date	Mar 27, 2018

Abstract

A combustor according to the invention includes a combustor basket to which air A is supplied from the outside, a plurality of first nozzles that are annularly provided along the inner periphery of the combustor basket and that supply premixed gas M of the air and fuel to the inside of the combustor basket, and a transition piece in which the combustor basket is connected to a base end thereof and which burns the premixed gas supplied from the first nozzles, thereby forming a flame front spread to the outer periphery side toward the leading end in an axial direction, wherein each first nozzle supplies the premixed gas with fuel concentration changed around the center axis of the first nozzle such that the flame front has a uniform temperature in the axial direction.

First claim

The invention claimed is:

1. A combustor, comprising:
a combustor basket which is configured to receive air from the an outside of the combustor;
a plurality of first nozzles that are provided along an inner periphery of the combustor basket and that extend in an axial direction of the combustor basket;
a second nozzle that is arranged at a center of the combustor basket and that extends in an axial direction of the combustor basket; and
a transition piece that is connected to the combustor basket and that is configured to allow high-temperature combustion gas to flow inside of the transition piece, wherein
each of the first nozzles has fuel discharge holes and is surrounded by a first nozzle pipe which is configured to mix the air and fuel discharged from the fuel discharge holes forming a premixed gas,
the second nozzle has fuel discharge holes and is surrounded by a second nozzle pipe, a gap is provided between the first nozzle pipe and the second nozzle pipe, which is configured to provide cooling air into combustion zone,
cooling air is configured to flow around the first nozzles, the second nozzle, combustor basket and the transition piece,
an area located near the outlet of the first nozzles, which is positioned inside the combustor basket, includes a first area near a radially outer periphery of the first nozzles receiving the cooling air and a second area near a radially inner periphery of the first nozzles located radially inward with respect to the first area, and which receives the cooling air from the gap, radially being defined relative to a combustor axis, and
wherein a flow amount of the cooling air in the second area is larger than a flow amount of the cooling air in the first area, the first nozzles are configured such that, in the first nozzle pipes at their outlets, a fuel concentration of the premixed gas in the second area is relatively higher than that in the first area, and mixing of the cooling air with the premixed gas in the first area and second area promoting relatively uniform flame temperature.

2. The combustor according to claim 1 , wherein said first nozzle pipe includes a main nozzle cylinder and an extension pipe connected to the main nozzle cylinder.

3. The combustor according to claim 1 , wherein said second nozzle pipe includes a pilot nozzle cylinder and a pilot cone connected to the pilot nozzle cylinder.

4. The combustor according to claim 1 , wherein:
each of the first nozzles includes a first swirler blade extending radially on a periphery of the first nozzle, and each of the first swirler blades includes a fuel discharge hole formed on a radially inward side of the first swirler blade and a fuel discharge hole formed on a radially outward side of the first swirler blade; and
each of the first nozzles supplies a premixed gas with fuel concentration adjusted around a center axis of the first nozzle such that a flame front has uniformity in temperature in an axial direction based on: a discharge quantity of the fuel being adjusted by opening areas of the fuel discharge holes formed on the radially inward side and the fuel discharged holes formed on the radially outward side differing from each other.

5. A combustor, comprising:
a combustor basket which is configured to receive air from an outside of the combustor;
a plurality of first nozzles that are provided along an inner periphery of the combustor basket and that extend in an axial direction of the combustor basket; and
a transition piece that is connected to the combustor basket and that is configured to allow high-temperature combustion gas to flow inside of the transition piece, wherein
each of the first nozzles has fuel discharge holes and is surrounded by a first nozzle pipe which is configured to mix the air and fuel discharged from the fuel discharge holes forming a premixed gas,
a gap is provided between the transition piece and the combustor basket, which is configured to provide cooling air into combustion zone,
cooling air is configured to flow around the first nozzles, combustor basket, and the transition piece,
an area located near the outlet of the first nozzles, which is positioned inside the combustor basket, includes a first area near a radially outer periphery of the first nozzles receiving the cooling air and a second area near a radially inner periphery of the first nozzles located radially inward with respect to the first area and which also receives the cooling air, radially being defined relative to a combustor axis, and
wherein a flow amount of the cooling air in the second area is larger than a flow amount of the cooling air in the first area, the first nozzles are configured such that, in the first nozzle pipes at their outlets, a fuel concentration of the premixed gas in the second area is relatively higher than that in the first area, and mixing of the cooling air with the premixed gas in the first area and second area promoting relatively uniform flame temperature.

6. The combustor according to claim 5 , wherein
another gap is provided between an outer surface of the first nozzle pipe and an inner surface of the combustor basket, which is configured to provide the cooling air into the combustion zone.

7. The combustor according to claim 5 , wherein
the transition piece includes a penetrating hole on its wall, which are configured to provide the air into the combustion zone.

8. The combustor according to claim 7 , wherein
the penetrating hole is located upstream of a flame front.

9. The combustor according to claim 5 , wherein:
each of the first nozzles includes a first swirler blade extending radially on a periphery of the first nozzle, and each of the first swirler blades includes a fuel discharge hole formed on a radially inward side of the first swirler blade and a fuel discharge hole formed on a radially outward side of the first swirler blade; and
each of the first nozzles supplies a premixed gas with fuel concentration adjusted around a center axis of the first nozzle such that a flame front has uniformity in temperature in an axial direction based on: a discharge quantity of the fuel being adjusted by opening areas of the fuel discharge holes formed on the radially inward side and the fuel discharged holes formed on the radially outward side differing from each other.

Assignees

• Mitsubishi Heavy Ind Ltd
• Mitsubishi Hitachi Power Sys

Inventors

• Nakamura Sosuke
• Matsumura Yoshikazu
• KATANO Hikaru
• Taniguchi Kenta
• Yamasaki Hiroyuki

Classifications

• F02C7/22 Primary

  Fuel supply systems · CPC title

• F23R3/00

  Continuous combustion chambers using liquid or gaseous fuel · CPC title

• F23D2900/00018

  Means for protecting parts of the burner, e.g. ceramic lining outside of the flame tube · CPC title

• F23D11/24

  by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space · CPC title

• F23D11/38

  Nozzles; Cleaning devices therefor · CPC title