Cutouts in gas turbine structures for deflection control

A mid-turbine frame is provided. The mid-turbine frame may comprise an inner case having an annular surface with an interface section disposed on the annular surface. The interface section may include an interface feature. A balancing section may be disposed on the annular surface defining an openin...

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Bibliographic Details
Main Authors Devaney Patrick M, Sedor Joseph J, Collier Michael D, Nadeau Patrick M, Broulidakis Alexander, Treat Christopher
Format Patent
LanguageEnglish
Published 26.09.2017
Subjects
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