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Turbomachine component having an internal cavity reactivity neutralizer and method of forming the same [electronic resource].

Published
Washington, D.C. : United States. Dept. of Energy, 2017.
Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy
Additional Creators
General Electric Company, United States. Department of Energy, and United States. Department of Energy. Office of Scientific and Technical Information
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Summary
A turbomachine component includes a body having an exterior surface and an interior surface, an internal cavity defined by the interior surface, and a reactivity neutralizing member arranged within the internal cavity. The reactivity neutralizing member is configured and disposed to neutralize turbomachine combustion products on the interior surface of the body.
Report Numbers
E 1.99:9,587,492
9,587,492
Subject(s)
Note
Published through SciTech Connect.
03/07/2017.
"9,587,492"
"13/464,134"
Herbert Chidsey Roberts, III; Peter Joel Meschter.
Funding Information
FC26-05NT42643
View MARC record | catkey: 23766352