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Title: Turbine component having surface cooling channels and method of forming same

A component for a turbine engine includes a substrate that includes a first surface, and an insert coupled to the substrate proximate the substrate first surface. The component also includes a channel. The channel is defined by a first channel wall formed in the substrate and a second channel wall formed by at least one coating disposed on the substrate first surface. The component further includes an inlet opening defined in flow communication with the channel. The inlet opening is defined by a first inlet wall formed in the substrate and a second inlet wall defined by the insert.
Inventors:
; ;
Issue Date:
OSTI Identifier:
1379210
Assignee:
General Electric Company NETL
Patent Number(s):
9,752,440
Application Number:
14/725,695
Contract Number:
FC26-05NT42643
Resource Relation:
Patent File Date: 2015 May 29
Research Org:
General Electric Company, Schenectady, NY (United States)
Sponsoring Org:
USDOE
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING

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