Aircraft gas turbine with a seal for sealing an igniter plug on the combustion chamber wall of a gas turbine
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United States of America Patent
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May 29, 2018
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N/A
app pub date -
Jul 28, 2015
filing date -
Jul 28, 2014
priority date (Note) -
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Abstract
A sealing arrangement of an igniter plug of a combustion chamber of a gas turbine, with an igniter plug passing through a recess of a combustion chamber wall, with at least one sealing ring through which the igniter plug projects and which is in sealing contact with an edge area of the recess facing away from the combustion chamber interior, wherein the sealing ring is designed in the form of a flat, annular and flexible disk.
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