Inventor
GREGG JASON RAY
US4 patents
Patents
4 patentsUS10655489B2May 19, 2020
Systems and methods for assembling flow path components
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Two portion cooling passage for airfoil
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System and method for shroud cooling in a gas turbine engine
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US10933481B2Mar 2, 2021
Method of forming cooling passage for turbine component with cap element
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