Chemical Removal of Ceramic Thermal Barrier and Metallic Bond Coats from Gas Turbine Combustion Components

Format:

Conference/Event

Author/Creator:

Bleeks, Thomas W., author.

Conference Name:

International Pacific Air & Space Technolgy Conference (1994-02-14 : Singapore, Singapore)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1994

Summary:

This paper describes a chemical immersion process capable of removing ceramic thermal barrier coatings, high temperature oxidation resistant coatings, and, nickel-aluminide bond coat materials from gas turbine engine components typically found in commercial and military jet engines. This process was originally developed to remove thermal barrier coatings from JT-8D combustion chambers for commercial aircraft. Since then, the process has been utilized to remove a variety of MCrAlY coatings from commercial and military aircraft engines

Notes:

Vendor supplied data

Publisher Number:

940053

Access Restriction:

Restricted for use by site license