GAS TURBINE ENGINE COMPONENTS HAVING SEALED STRESS RELIEF SLOTS AND METHODS FOR THE FABRICATION THEREOF
Embodiments of a gas turbine engine component (60) having sealed stress relief slots are provided, as are embodiments of a gas turbine engine (20) containing such a component. In one embodiment, the gas turbine engine includes a core gas flow path (92), a secondary cooling flow path (94), and a turb...
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Main Authors | , , , , |
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Format | Patent |
Language | English French German |
Published |
28.10.2015
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Subjects | |
Online Access | Get full text |
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