Core assemblies and gas turbine engine components formed therefrom
AssigneeUnited Technologies Corporation
InventorChristopher King
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AssigneeUnited Technologies Corporation
InventorChristopher King
Estimating the term…
Core assemblies and methods for manufacturing components of gas turbine engines include a first core body having a first trunk configured to attach to a first location of a cavity core structure, a first branch extending from the first trunk and configured to form a first portion of a first cooling circuit, the first branch having a first joining surface, and a second core body having a second trunk configured to attach to a second location of a cavity core structure, a first branch of the second core body extending from the second trunk and configured to form a first portion of a second cooling circuit in the component. The first branches of the core bodies joined to form a junction. The junction defines a merger of the first cooling circuit and the second cooling circuit proximate to an exit of the first and second cooling circuits.
A core assembly for manufacturing a component of a gas turbine engine, the core assembly comprising:
A component for a gas turbine engine comprising:
A method of forming a core for a component of a gas turbine engine, the method comprising:
Dependencies are inferred from the claim text.