Burner, gas turbine combustor, burner cooling method, and burner modifying method

Abstract

In a burner for injecting mixed gas fuel containing at least one of hydrogen and carbon monoxide into a combustion chamber of a gas turbine combustor, the burner includes a fuel nozzle for startup from which liquid fuel is injected into the combustion chamber, and a mixed fuel nozzle disposed around the fuel nozzle for injecting the mixed gas fuel. An air swirler is disposed at a downstream end of the mixed fuel nozzle and has a plurality of flow passages from which compressed air is injected into the combustion chamber, and the mixed fuel nozzle has injection ports disposed in the inner peripheral side of the flow passages of the air swirler. Cooling holes formed in the nozzle surface and positioned to face the combustion chamber introduce a part of the mixed gas fuel injected from the mixed fuel nozzle into the combustion chamber.

Description

BACKGROUND OF THE INVENTION [0001] 1. Field of the Invention [0002] The present invention relates to a burner using mixed fuel containing at least one of hydrogen and carbon monoxide, and also relates to a gas turbine combustor, a burner cooling method, and a burner modifying method. [0003] 2. Description of the technology [0004] Recently, the varieties of fuel for use in gas turbines have been increased. The use of multi-component mixed gas fuel containing hydrogen, carbon monoxide, etc. (hereinafter referred to simply as “mixed fuel”) has been proposed in addition to conventional primary fuel for gas turbines, such as LNG (liquefied natural gas), light oil, and A-heavy oil. Such mixed fuel has a higher flame temperature than LNG. In particular, hydrogen has a wider flammable range and a faster burning velocity and is easy to burn. [0005] LNG is burned primarily by employing a premixed combustion system. However, when the mixed fuel is burned by employing the premixed combustion sy...

AI Technical Summary

Benefits of technology

[0007] An object of the present invention is to provide a burner, a gas turbine combustor, a burner cooling method, and a burner modifying method, which can hold metal temperature at a nozzle surface within a proper range and can increase reliability even when mixed fuel containing at least one of hydrogen and carbon monoxide is used as fuel.

[0008] (1) To achieve the above object, the present invention provides a burner for injecting mixed fuel containing at least one of hydrogen and carbon monoxide into a combustion chamber of a gas turbine combustor, wherein the burner comprises a fuel nozzle for startup from which fuel for startup is injected into the combustion chamber; a mixed fuel nozzle disposed around the fuel nozzle for startup and injecting the mixed fuel; an air swirler disposed at a downstream end of the mixed fuel nozzle positioned in the combustion chamber and having a plurality of flow passages through which a part of compressed air from a compressor is injected into the combustion chamber to hold a flame, the mixed fuel nozzle having injection ports disposed in the inner peripheral side of the flow passages of the air swirler; and cooling holes formed in a nozzle surface positioned to face the combustion chamber and introducing a part of the mixed fuel injected from the mixed fuel nozzle into the combustion chamber, to thereby reduce flame temperature near the nozzle surface.

[0013] (6) Also, to achieve the above object, the present invention provides a gas turbine combustor for burning mixed fuel containing at least one of hydrogen and carbon monoxide, wherein the combustor comprises an outer casing serving as a pressure vessel; a combustion liner disposed inside the outer casing and forming a combustion chamber therein; a burner for forming a flame in the combustion chamber within the combustion liner; and a transition piece for introducing, to a burner, the burned gas generated with the formation of the flame by the burner, the burner comprising a fuel nozzle for startup from which fuel for startup is injected into the combustion chamber; a mixed fuel nozzle disposed around the fuel nozzle for startup and injecting the mixed fuel; an air swirler disposed at a downstream end of the mixed fuel nozzle positioned in the combustion chamber and having a plurality of flow passages through which a part of compressed air from a compressor is injected into the combustion chamber to hold a flame, the mixed fuel nozzle having injection ports disposed in the inner peripheral side of the flow passages of the air swirler; and cooling holes formed in a nozzle surface positioned to face the combustion chamber and introducing a part of the mixed fuel injected from the mixed fuel nozzle into the combustion chamber, to thereby reduce flame temperature near the nozzle surface.

[0014] (7) Further, to achieve the above object, the present invention provides a method of cooling a burner employing a diffusive combustion system and injecting mixed fuel containing at least one of hydrogen and carbon monoxide into a combustion chamber of a gas turbine combustor, wherein the method comprises the steps of forming cooling holes in a nozzle surface positioned to face the combustion chamber such that a part of the mixed fuel is injected through the cooling holes; and injecting the part of the mixed fuel into the combustion chamber through the cooling holes, to thereby reduce flame temperature near the nozzle surface and suppress a rise of metal temperature at the nozzle surface.

[0017] (10) Still further, to achieve the above object, the present invention provides a method of cooling a burner employing a diffusive combustion system and injecting mixed fuel containing at least one of hydrogen and carbon monoxide into a combustion chamber of a gas turbine combustor, wherein the method comprises the steps of providing a mixed fuel nozzle for injecting the mixed fuel to be disposed around a fuel nozzle for startup from which fuel for startup is injected into the combustion chamber; and supplying inert gas from an inert gas supply system to the fuel nozzle for startup such that the inert gas is injected to the vicinity of a nozzle surface from the fuel nozzle for startup during a gas combustion mode using only the mixed fuel, thereby reducing flame temperature near the nozzle surface and suppressing a rise of metal temperature at the nozzle surface.

[0022] According to the present invention, even when the mixed fuel containing at least one of hydrogen and carbon monoxide is used as fuel, the flame temperature can be reduced by increasing a fuel concentration near the nozzle surface, whereby the metal temperature at the nozzle surface can be held within a proper range and reliability can be increased. In addition, the metal temperature at the nozzle surface can also be held within the proper range by supplying inert gas to the vicinity of the nozzle surface.

Problems solved by technology

However, after the shift to the gas combustion mode using only the mixed fuel, there is a fear that a flame may become apt to come close to a nozzle surface and metal temperature at the nozzle surface may rise excessively because the mixed fuel has a higher flame temperature and a faster burning velocity.

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