TURBINE ENGINE SHROUD ASSEMBLY
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United States of America Patent
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Issued Date -
Oct 26, 2017
app pub date -
Feb 24, 2017
filing date -
Feb 29, 2016
priority date (Note) -
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Abstract
Disclosed herein is an interlocking shroud assembly for a turbine engine with a plurality of radially extending, circumferentially spaced airfoils terminating in a shroud element and having opposing radial sides with first and second interlock elements. Further provided is a method of forming a shroud about a plurality of rotating blades in a turbine engine.
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