Investigation of combustion flame spray as in-situ repair technology for thermal barrier coatings

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Investigation of combustion flame spray as in-situ repair technology for thermal barrier coatings

The continuous increase of Turbine Entry Temperature (TET) in aerospace gas-turbines is the main driver for the research effort in the development of coatings for thermal and oxidation protection: i.e. Thermal Barrier Coatings (TBC). The need for TBC is particularly relevant within the combustor ass...

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Bibliographic Details
Main Author:	Fanicchia, Francesco
Format:	Thesis (University of Nottingham only)
Language:	English
Published:	2018
Subjects:	Flame spraying; Gas-turbines Combustion chambers Maintenance and repair; Thermal barrier coatings
Online Access:	https://eprints.nottingham.ac.uk/51006/

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