Combustor nozzle, combustor, and gas turbine including same
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United States of America Patent
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Aug 6, 2024
Grant Date -
Aug 31, 2023
app pub date -
Nov 21, 2022
filing date -
Jan 28, 2022
priority date (Note) -
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Abstract
A combustor nozzle including nozzle modules, a combustor, and a gas turbine including the same are proposed. The nozzle module includes a fuel supply pipe having an internal fuel flow path, manifolds communicating with the fuel supply pipe and arranged in a row in a radial direction, and fuel mixers disposed along a circumferential direction at the rear side of the manifold to receive the fuel from the manifold and inject the fuel, each of the plurality of fuel mixers including a mixer body having one end communicating with the manifold, the other end that is opened, and an mixing flow path through which air and the fuel flow, an air inlet port formed on a lateral side of the mixer body, a fuel port formed inside the mixer body and discharging the fuel supplied from the manifold to the mixing flow path, and an extension located at the other end of the mixer body.
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