TURBINE BLADE ASSEMBLY

A turbine blade assembly for a gas turbine engine is provided. The turbine blade assembly having: a rotor; a plurality of turbine blades mounted to the rotor, each of the plurality of turbine blades having a forward tab that contacts a front face of the rotor and an aft tab; a plurality of tabs that...

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Bibliographic Details
Main Authors Bergman, Russell J, Caprario, Joseph T, Virkler, Scott D, Eastwood, Jonathan Jeffery
Format Patent
LanguageEnglish
Published 30.04.2020
Subjects
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