Combustion chamber with a wall section and a brim element
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United States of America Patent
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Apr 19, 2016
Grant Date -
Jan 23, 2014
app pub date -
Feb 1, 2012
filing date -
Feb 18, 2011
priority date (Note) -
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Abstract
A combustion chamber for a gas turbine is proposed. The combustion chamber has a wall section and a brim element. The wall section has an inlet aperture for injecting a cooling medium into the combustion chamber. The brim element is mounted to an inner face of the wall section. The brim element is formed in such a way that a projected area of the brim element onto the inner face along a direction of a normal of the inner face at least partially covers the inlet channel.
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