TURBINE BLADE SHROUD FOR GAS TURBINE ENGINE WITH POWER TURBINE AND METHOD OF MANUFACTURING SAME

A blade (50) for a gas turbine engine (20) includes an airfoil (58) that includes an internal passage (70). A shroud (52) is arranged at an end of the airfoil (58) and has a shroud perimeter (64). Axially spaced knife edges (54) extend radially from the shroud (52). An area is provided between the k...

Full description

Saved in:
Bibliographic Details
Main Authors STONER, Alan W, BERGMAN, Russell J
Format Patent
LanguageEnglish
French
German
Published 17.02.2021
Subjects
Online AccessGet full text

Cover

Loading…