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Title: Turbomachine component having an internal cavity reactivity neutralizer and method of forming the same

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.
Inventors:
;
Issue Date:
OSTI Identifier:
1346056
Assignee:
GENERAL ELECTRIC COMPANY NETL
Patent Number(s):
9,587,492
Application Number:
13/464,134
Contract Number:
FC26-05NT42643
Resource Relation:
Patent File Date: 2012 May 04
Research Org:
GENERAL ELECTRIC COMPANY, Schenectady, NY (United States)
Sponsoring Org:
USDOE
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING

Other works cited in this record:

Sacrificial anode
patent, November 1976

Ceramic coated strip anode for cathodic protection
patent, August 1990

Ceramic turbine airfoils with cooled trailing edge blocks
patent, December 2001

Hollow fan blade for gas turbine engine
patent, May 2006

Composite sacrificial anodes
patent, May 2008

System for protecting turbine engine surfaces from corrosion
patent, September 2012

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