COMPONENT FOR A GAS TURBINE ENGINE
A component for a gas turbine engine includes a first surface and a second surface. The component additionally includes one or more layers of ceramic matrix composite material extending between the first and second surfaces. A thermal void extends between a first end and a second end. The second end...
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Main Authors | , , |
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Format | Patent |
Language | English |
Published |
28.09.2023
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Subjects | |
Online Access | Get full text |
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Summary: | A component for a gas turbine engine includes a first surface and a second surface. The component additionally includes one or more layers of ceramic matrix composite material extending between the first and second surfaces. A thermal void extends between a first end and a second end. The second end of the thermal void is a terminal end embedded in the component between the first and second surfaces. |
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Bibliography: | Application Number: US202318093044 |