GAS TURBINE COMBUSTION CHAMBER WITH MODIFIED WALL THICKNESS
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United States of America Patent
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Issued Date -
Jun 23, 2016
app pub date -
Dec 17, 2015
filing date -
Dec 19, 2014
priority date (Note) -
Abandoned
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Abstract
A gas turbine combustion chamber, including at least one combustion chamber wall in which mixed air holes are formed in a predefined area that extends around the combustion chamber in a ring-shaped manner with respect to the central axis of the combustion chamber in a central area of the same, characterized in that the combustion chamber wall has a greater thickness in the ring-shaped area of the mixed air holes than in the areas that are not provided with mixed air holes.
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