Combustor with radially varying leading end portion of basket and gas turbine
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United States of America Patent
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Aug 10, 2021
Grant Date -
Sep 26, 2019
app pub date -
May 23, 2017
filing date -
May 23, 2016
priority date (Note) -
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Abstract
A combustor includes: a fuel nozzle extending along an axis; a tubular combustor basket configured to cover the fuel nozzle; and a tubular transition piece configured to define a cooling air passage through which air from outside is introduced between the tubular transition piece and an outer circumferential surface of a leading end portion of the tubular combustor basket. The tubular transition piece extends toward a leading end side of the tubular combustor basket.
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