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Fabrication of strain-isolated ceramic coated combustor componentsThe use of strain-isolated ceramic coated material to produce an AGT1500 combustor scroll-shaped transition duct which requires no air for film cooling is investigated. The scroll receives the exhaust of the can-style combustor liner and turns it into the annular inlet of the high pressure gas producer turbine nozzle. Strain-isolation of plasma sprayed thermal barrier coating is achieved by placing a compliant pad between the structural base metal and the ceramic coating. The compliant pad is brazed to the metal structure. In order to achieve a good braze bond, the strain-isolating compliant pad and base metal must be closely matched in shape and tightly fixtured for joining. The complex geometry of the AGT1500 scroll makes it impractical to attack pads to the supporting structure in its finished shape. Instead the pads are brazed to flat stock and post-formed into scroll sections. While test samples were successfully post-formed, plasma sprayed, and subjected to cyclic heating, the forming of full scale parts by normal methods resulted in tearing of the Hastelloy-X base metal because of embrittlement by the braze material. Several solutions were explored which finally resulted in the successful forming of full scale scroll parts.
Document ID
19890004292
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rutter, S.
(Avco Lycoming Div. Stratford, CT, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Publication Information
Publication: NASA, Lewis Research Center, Thermal Barrier Coatings. Abstracts and Figures
Subject Category
Nonmetallic Materials
Accession Number
89N13663
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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