HEAT SHIELD PANELS WITH OVERLAP JOINTS FOR A TURBINE ENGINE COMBUSTOR

A combustor wall is provided for a turbine engine. The combustor wall includes a combustor shell and a combustor heat shield that is attached to the shell. The heat shield includes a first panel and a second panel that sealingly engages the first panel in an overlap joint. A cooling cavity extends b...

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Bibliographic Details
Main Authors CUNHA, Frank J, KOSTKA, Stanislav
Format Patent
LanguageEnglish
French
German
Published 15.05.2019
Subjects
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Summary:A combustor wall is provided for a turbine engine. The combustor wall includes a combustor shell and a combustor heat shield that is attached to the shell. The heat shield includes a first panel and a second panel that sealingly engages the first panel in an overlap joint. A cooling cavity extends between the shell and the heat shield and fluidly couples a plurality of apertures in the shell with a plurality of apertures in the heat shield.
Bibliography:Application Number: EP20140851011