SYSTEM FOR THERMALLY SHIELDING A PORTION OF A GAS TURBINE SHROUD ASSEMBLY

In one aspect the present subject matter is directed to a system for thermally shielding a portion of a shroud assembly for a gas turbine 14. The system includes a shroud support 80 having a forward wall 92 that includes a front side 96 that is axially spaced from a back side 98 and a radially inner...

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Bibliographic Details
Main Authors BOGARD, Justin, SHAPIRO, Jason David
Format Patent
LanguageEnglish
French
German
Published 19.06.2019
Subjects
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