Gas turbine combustor injector assembly comprising an air supply unit having an inclined surface relative to an inclined injection pipe
Number of patents in Portfolio can not be more than 2000
United States of America
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Nov 12, 2024
Grant Date -
Jun 6, 2024
app pub date -
Sep 24, 2023
filing date -
Sep 24, 2023
priority date (Note) -
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status (Latency Note)
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Abstract
Proposed is a combustor that includes a liner provided with a combustion chamber at an inner side of which a mixture of fuel and compressed air is combusted, a transition piece connected to an end of the liner, a fluid-flowing sleeve disposed at an outer side of the liner and the transition piece, and at least one injector configured to inject the mixture of fuel and air by being disposed on the liner or the transition piece, wherein the injector includes an injection pipe connected to the liner or the transition piece, a fuel supply unit configured to supply the fuel from a center part of a rear end of the injection pipe, and an air supply unit configured to supply the air from an inner circumferential part of the rear end of the injection pipe.
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