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Title: Turbine repair process, repaired coating, and repaired turbine component

Abstract

A turbine repair process, a repaired coating, and a repaired turbine component are disclosed. The turbine repair process includes providing a turbine component having a higher-pressure region and a lower-pressure region, introducing particles into the higher-pressure region, and at least partially repairing an opening between the higher-pressure region and the lower-pressure region with at least one of the particles to form a repaired turbine component. The repaired coating includes a silicon material, a ceramic matrix composite material, and a repaired region having the silicon material deposited on and surrounded by the ceramic matrix composite material. The repaired turbine component a ceramic matrix composite layer and a repaired region having silicon material deposited on and surrounded by the ceramic matrix composite material.

Inventors:
; ;
Publication Date:
Research Org.:
General Electric Company, Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1224831
Patent Number(s):
9,175,402
Application Number:
13/561,445
Assignee:
General Electric Company NETL
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 2012 Jul 30
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS; 42 ENGINEERING

Citation Formats

Das, Rupak, Delvaux, John McConnell, and Garcia-Crespo, Andres Jose. Turbine repair process, repaired coating, and repaired turbine component. United States: N. p., 2015. Web.
Das, Rupak, Delvaux, John McConnell, & Garcia-Crespo, Andres Jose. Turbine repair process, repaired coating, and repaired turbine component. United States.
Das, Rupak, Delvaux, John McConnell, and Garcia-Crespo, Andres Jose. Tue . "Turbine repair process, repaired coating, and repaired turbine component". United States. doi:. https://www.osti.gov/servlets/purl/1224831.
@article{osti_1224831,
title = {Turbine repair process, repaired coating, and repaired turbine component},
author = {Das, Rupak and Delvaux, John McConnell and Garcia-Crespo, Andres Jose},
abstractNote = {A turbine repair process, a repaired coating, and a repaired turbine component are disclosed. The turbine repair process includes providing a turbine component having a higher-pressure region and a lower-pressure region, introducing particles into the higher-pressure region, and at least partially repairing an opening between the higher-pressure region and the lower-pressure region with at least one of the particles to form a repaired turbine component. The repaired coating includes a silicon material, a ceramic matrix composite material, and a repaired region having the silicon material deposited on and surrounded by the ceramic matrix composite material. The repaired turbine component a ceramic matrix composite layer and a repaired region having silicon material deposited on and surrounded by the ceramic matrix composite material.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Nov 03 00:00:00 EST 2015},
month = {Tue Nov 03 00:00:00 EST 2015}
}

Patent:

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