NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Investigation into Spectroscopic Techniques for Thermal Barrier Coating Spall DetectionSpectroscopic methods are proposed for detection of thermal barrier coating (TBC) spallation from engine hot zone components. These methods include absorption and emission of airborne marker species originally embedded in the TBC bond coat. In this study, candidate marker materials for this application were evaluated. Thermochemical analysis of candidate marker materials combined with additional constraints such as toxicity and uniqueness to engine environment, provided a short list of four potential species: platinum, copper oxide, zinc oxide. and indium. The melting point of indium was considered to be too low for serious consideration. The other three candidate marker materials, platinum, copper oxide, and zinc oxide were placed in a high temperature furnace and emission and absorption properties were measured over a temperature range from 800-1400 C and a spectral range from 250 to 18000 nm. Platinum did not provide the desired response, likely due to the low vapor Pressure of the metallic species and the low absorption of the oxide species. It was also found, however. that platinum caused a broadening of the carbon dioxide absorption at 4300 nm. The nature of this effect is not known. Absorption and emission caused by sodium and potassium impurities in the platinum were found in the platinum tests. Zinc oxide did not provide the desired response, again, most likely due to the low vapor pressure of the metallic species and the low absorption of the oxide species. Copper oxide generated two strongly temperature dependent absorption peaks at 324.8 and 327.4 nm. The melting point of copper oxide was determined to be too low for serious consideration as marker material.
Document ID
20010050139
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
deGroot, Wim
(DYNACS Engineering Co., Inc. Brook Park, OH United States)
Opila, Beth
(Cleveland State Univ. Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/CR-2001-210468
NAS 1.26:210468
E-12465
Report Number: NASA/CR-2001-210468
Report Number: NAS 1.26:210468
Report Number: E-12465
Funding Number(s)
PROJECT: RTOP 274-00-00
CONTRACT_GRANT: NAS3-98008
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available