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Prolonging thermal barrier coated specimen life by thermal cycle managementMeasurements were made of the rate of increase in temperature of a ZrO2-8Y2O3 thermal barrier coated (TBC) specimen for various values of fuel/air (F/A) ratios when the specimen is exposed to a 0.3 Mach burner flame. For rod specimens in a carousel, the heating rates increased with (F/A) ratio and were higher at the inward facing surface for a given (F/A). Plate specimens were more sensitive to burner variations. Calculated results are given for the radial stress in the coated rod specimens for variations in (F/A) ratios from 0.04 to 0.065. Over this range, the radial stress varies from 4.3 to 5.3 MPa. The results indicate that controlling the heating rate of a TBC by controlling the (F/A) ratio offers a potential method to prolong TBC cyclic life; uncontrolled (F/A) ratios will produce scatter in experimental results. Geometric arrangement can have an equivalent effect, but is usually fixed by design.
Document ID
19810014884
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hendricks, R. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Mcdonald, G.
(NASA Lewis Research Center Cleveland, OH, United States)
Poolos, N. P.
(Harvard Univ.)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-81742
E-795
Report Number: NASA-TM-81742
Report Number: E-795
Meeting Information
Meeting: Intern. Conf. on Met. Coatings,
Location: San Francisco, CA
Country: United States
Start Date: April 6, 1981
End Date: April 10, 1981
Sponsors: Am. Vacuum Soc.
Accession Number
81N23417
Funding Number(s)
PROJECT: RTOP 506-53-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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