Gas turbine combustion chamber having a flow sleeve with a plurality of integrated segments
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United States of America Patent
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Mar 20, 2018
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app pub date -
Nov 14, 2013
filing date -
Nov 30, 2012
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Abstract
A gas turbine combustion chamber is provided, including a flow sleeve structure with an improved anti-vibration performance. A gas turbine combustion chamber of the present invention includes a liner, a transition piece, and a flow sleeve including a plurality of segments and integrated by welding a tie piece along joint portions of the segments. The tie piece includes a first member and a second member, the first member continuously extending along a longitudinal direction of the joint portions of the segments and being arranged to cover the joint portions, and the second member being formed at an end portion of the first member, having a width wider than the first member, and including a recess.
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