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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Main Authors | , , , |
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Format | Patent |
Language | English |
Published |
30.04.2020
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Subjects | |
Online Access | Get full text |
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Summary: | 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 extend from an aft surface of the rotor; and a retaining ring that engages each aft tab of the plurality of turbine blades and each of the plurality of tabs that extend from the aft surface of the rotor. |
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Bibliography: | Application Number: US201816177331 |