SYSTEM AND METHOD FOR REDUCING BLADE HOOK STRESS IN A TURBINE BLADE
A turbine assembly includes a rotating blade including a T-root. The T-root defines a first engagement surface that is cylindrical, a rotor including a blade groove arranged to receive the rotating blade, the blade groove including a neck portion that defines a second engagement surface and a neck s...
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Main Authors | , , , |
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Format | Patent |
Language | English |
Published |
21.03.2024
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Subjects | |
Online Access | Get full text |
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