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Multi-venturi tube fuel injector for gas turbine combustors

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TLDR
In this paper, the diffusers transition from a circular cross-section at the throat to multiple discrete angularly related side walls at the diffuser exits without substantial gaps there between.
Abstract
A combustor for a gas turbine includes a main fuel injector for receiving compressor discharge air and mixing the air with fuel for flow to a downstream catalytic section. The main fuel injector includes an array of venturis each having an inlet, a throat and a diffuser. A main fuel supply plenum between forward and aft plates supplies fuel to secondary annular plenums having openings for supplying fuel into the inlets of the venturis upstream of the throats. The diffusers transition from a circular cross-section at the throat to multiple discrete angularly related side walls at the diffuser exits without substantial gaps therebetween. With this arrangement, uniform flow distribution of the fuel/air, velocity and temperature is provided at the catalyst inlet.

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Gas turbine combustor

TL;DR: In this article, a gas turbine combustor with a fuel injection nozzle using a fluid other than liquid fuel to atomize the liquid fuel and that can suppress a reduction in power generation efficiency resulting from a heat loss while promoting the atomization of liquid fuel.
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TL;DR: In this paper, a fuel/air mixing disk for use in a fuel and air mixing combustor assembly is provided, which includes a first face, a second face, and at least one fuel plenum disposed there between.
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TL;DR: In this paper, a fuel injection head for a fuel nozzle includes a substantially hollow vesicle body formed with an upstream end face, downstream end face and a peripheral wall extending therebetween, an internal baffle plate extending radially outwardly from a downstream end of the bore, terminating short of the peripheral wall, and a plurality of integral pre-mix tubes extend axially through the upstream and downstream fuel plenums.
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Catalytic combustor with lean direct injection of gas fuel for low emissions combustion and methods of operation

TL;DR: In this article, a post-catalytic combustion zone is proposed for a gas turbine with auto-ignition in the transition between the combustor and turbine. But the combustion reaction temperature is too low to produce thermal NOx.
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Multiple venturi tube gas fuel injector for catalytic combustor

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