COMBUSTION CHAMBER SHINGLE OF A GAS TURBINE
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United States of America Patent
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Issued Date -
Sep 17, 2015
app pub date -
Mar 9, 2015
filing date -
Mar 11, 2014
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Abstract
Combustion chamber shingle of a gas turbine, including a bolt for bearing the combustion chamber shingle at the combustion chamber wall, wherein the combustion chamber shingle is formed substantially in a plate-shaped manner, and has at least one bearing element at one side, at which the bolt that is formed as a separate structural element is anchored in a form-locking manner, wherein the bolt, at its end area, is provided with a baring area that is arranged at a rectangular position to the bolt axis and that is arranged inside a recess of the bearing element, wherein the bolt has a centric passageway recess, and wherein the recess of the bearing element is dimensioned so as to be bigger than the baring area of the bolt, so that a hollow space is created between the surface of the combustion chamber shingle and the baring area of the bolt.
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