GAS TURBINE ENGINE AND FUEL NOZZLE THEREFOR
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United States of America
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Issued Date -
Mar 20, 2025
app pub date -
Sep 18, 2023
filing date -
Sep 18, 2023
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Abstract
A gas turbine engine comprising a combustion section enshrouded by a casing having at least one through passage, the combustion section comprising a dome wall and a liner at least partially defining a combustion chamber; a fuel nozzle connected to the dome wall and having a nozzle tube; and a coupling securing the fuel nozzle with casing and disposed at least partially in the at least one through passage.
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