NOZZLE ASSEMBLY, COMBUSTOR, AND GAS TURBINE INCLUDING SAME
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United States of America Patent
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Issued Date -
May 30, 2024
app pub date -
Sep 29, 2023
filing date -
Nov 30, 2022
priority date (Note) -
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Abstract
Proposed are a nozzle assembly, a combustor, and a gas turbine. Fuel and compressed air are discharged to a combustion chamber of the combustor of the gas turbine. The nozzle assembly includes a nozzle body, a plurality of injection nozzles provided inside the nozzle body and disposed to be spaced apart from each other, the injection nozzles having inner portions through which the compressed air and the fuel are mixed and moved, and a side wall which is connected to a first side of the nozzle body and through which the injection nozzles passes. A cooling air inlet hole into which cooling air is introduced into a space where the injection nozzles are disposed is formed in the nozzle body, and a cooling air outlet hole through which the cooling air introduced from the cooling air inlet hole is discharged is formed in one region of the side wall.
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