Gas turbine engine with dovetail connection having contoured root
A gas turbine engine includes a turbine having turbine blades and a shroud having a blade track for positioning radially outside of the blades. At least one of the blades and the blade track are secured in place using a dovetail connection between a dovetail receiver and a dovetail assembly formed t...
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Main Authors | , , , , |
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Format | Patent |
Language | English |
Published |
03.03.2020
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Subjects | |
Online Access | Get full text |
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Summary: | A gas turbine engine includes a turbine having turbine blades and a shroud having a blade track for positioning radially outside of the blades. At least one of the blades and the blade track are secured in place using a dovetail connection between a dovetail receiver and a dovetail assembly formed to include a contoured root. |
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Bibliography: | Application Number: US201615365498 |