METHOD OF MANUFACTURING A TURBINE COMPONENT
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United States of America Patent
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May 16, 2024
app pub date -
Oct 16, 2023
filing date -
Nov 11, 2022
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Abstract
The present disclose provides a method of manufacturing a turbine component for a gas turbine engine, comprising: forming, by a casting process, a primary component; forming, by an additive manufacturing process, a secondary component, wherein the secondary component comprises a main air passageway extending therethrough; assembling the primary component and the secondary component together to form the turbine component, wherein the main air passageway of the secondary component forms part of an internal air flow path through the turbine component.
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