Keywords
deposition, roughness, turbines
Abstract
Turbine blade coupons with three different surface treatments were exposed to deposition conditions in an accelerated deposition facility. The facility simulates the flow conditions at the inlet to a first stage high-pressure turbine (T=1150 C, M=0.31). The combustor exit flow is seeded with dust particulate that would typically be ingested by a large utility power plant. The three coupon surface treatments included: (1) bare polished metal; (2) polished thermal barrier coating with bondcoat; and (3) unpolished oxidation resistant bondcoat. Each coupon was subjected to four successive 2 h deposition tests. The particulate loading was scaled to simulate 0.02 parts per million weight (ppmw) of particulate over 3 months of continuous gas turbine operation for each 2 h laboratory simulation (for a cumulative 1 year of operation). Three-dimensional maps of the depositroughened surfaces were created between each test, representing a total of four measurements evenly spaced through the lifecycle of a turbine blade surface. From these measurements the surface topology and roughness statistics were determined. Despite the different surface treatments, all three surfaces exhibited similar nonmonotonic changes in roughness with repeated exposure. In each case, an initial buildup of isolated roughness peaks was followed by a period when valleys between peaks were filled with subsequent deposition. This trend is well documented using the average forward facing roughness angle in combination with the average roughness height as characteristic roughness metrics. Deposition-related mechanisms leading to spallation of the thermal barrier coated coupons are identified and documented.
Original Publication Citation
Wammack, J. E., J. Crosby, D. Fletcher, J. P. Bons, T. H. Fletcher, “Evolution of Surface Deposits on a High Pressure Turbine Blade, Part I: Physical Characteristics,” ASME Journal of Turbomachinery, 130, 021020-1 thru 8 (2008).
BYU ScholarsArchive Citation
Wammack, James Edward; Crosby, Jared M.; Fletcher, Daniel; Bons, Jeffrey P.; and Fletcher, Thomas H., "Evolution of Surface Deposits on a High-Pressure Turbine Blade—Part I: Physical Characteristics" (2008). Faculty Publications. 7026.
https://scholarsarchive.byu.edu/facpub/7026
Document Type
Peer-Reviewed Article
Publication Date
2008
Publisher
ASME
Language
English
College
Ira A. Fulton College of Engineering
Department
Chemical Engineering
Copyright Status
Copyright © 2008 by ASME
Copyright Use Information
https://lib.byu.edu/about/copyright/