Attachment of ceramic matrix composite panel to liner
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United States of America Patent
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Feb 13, 2018
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N/A
app pub date -
Jan 2, 2015
filing date -
Jan 10, 2014
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Abstract
A combined liner and panel for use in a gas turbine engine comprise a ceramic matrix composite panel having a plurality of extending members extending away from a face of ceramic matrix composite panel which will face hot products of combustion. A liner includes a plurality of spring members that apply a bias force biasing the extending members. The spring members bias the extending members on the panel in a direction away from the face of the panel which will face the hot products of combustion. A gas turbine engine, and a method of attaching a ceramic matrix composite panel to a liner are also disclosed.
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