COMBUSTOR OF GAS TURBINE
Number of patents in Portfolio can not be more than 2000
United States of America
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Issued Date -
Feb 20, 2025
app pub date -
Dec 23, 2022
filing date -
Dec 23, 2022
priority date (Note) -
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status (Latency Note)
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Abstract
A combustor of a gas turbine according to one aspect of the present disclosure includes: an outer wall surrounding a combustion chamber; a liner located inside the outer wall and facing the combustion chamber; and a fixture that attaches the liner to the outer wall in a state where there is a gap between the outer wall and the liner. The fixture includes: a shaft portion penetrating the outer wall; a head supporting the liner; and a head groove that is located on an outer peripheral surface of the head and includes a first end portion connected to the gap and a second end portion connected to the combustion chamber.
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