Advanced coating systems in conjunction with novel internal airfoil cooling configurations continue to be a critical research focus to provide enhanced oxidation protection and cooling of commercial metal alloys as future land-based gas turbines are being designed for inlet gas temperature operations of >1300–1400°C. With the application of densified oxide dispersion strengthened (ODS) coatings on cast near surface embedded micro-channel (NSEMC) airfoil surfaces, improvements of >50–70% in heat removal capabilities are projected over that of conventional, smooth-channeled, internally-cooled, airfoil configurations. For turbine inlet and airfoil surface design temperatures exceeding 1400–1600°C, oxide-coated, silicon carbide-based ceramic matric composites (CMCs) have been developed. In this paper we will review our recent advancements that have been made with respect to ODS coating development and the oxidation stability of CMCs during bench-scale laboratory testing.
Skip Nav Destination
ASME Turbo Expo 2015: Turbine Technical Conference and Exposition
June 15–19, 2015
Montreal, Quebec, Canada
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5675-8
PROCEEDINGS PAPER
Development of Advanced Material Systems for Future Gas Turbine Applications
M. A. Alvin,
M. A. Alvin
U.S. DOE National Energy Technology Laboratory, Pittsburgh, PA
Search for other works by this author on:
R. Bhatt,
R. Bhatt
NASA Glenn Research Center, Cleveland, OH
Search for other works by this author on:
J. Grady,
J. Grady
NASA Glenn Research Center, Cleveland, OH
Search for other works by this author on:
B. McMordie,
B. McMordie
Coatings for Industry Inc., Souderton, PA
Search for other works by this author on:
B. Warnes
B. Warnes
Corrosion Control Consultants, Inc., Beaver, PA
Search for other works by this author on:
M. A. Alvin
U.S. DOE National Energy Technology Laboratory, Pittsburgh, PA
I. Anderson
Iowa State University, Ames, IA
A. Heidloff
Iowa State University, Ames, IA
E. White
Iowa State University, Ames, IA
R. Bhatt
NASA Glenn Research Center, Cleveland, OH
J. Grady
NASA Glenn Research Center, Cleveland, OH
B. McMordie
Coatings for Industry Inc., Souderton, PA
B. Warnes
Corrosion Control Consultants, Inc., Beaver, PA
Paper No:
GT2015-43456, V006T21A010; 8 pages
Published Online:
August 12, 2015
Citation
Alvin, MA, Anderson, I, Heidloff, A, White, E, Bhatt, R, Grady, J, McMordie, B, & Warnes, B. "Development of Advanced Material Systems for Future Gas Turbine Applications." Proceedings of the ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. Volume 6: Ceramics; Controls, Diagnostics and Instrumentation; Education; Manufacturing Materials and Metallurgy; Honors and Awards. Montreal, Quebec, Canada. June 15–19, 2015. V006T21A010. ASME. https://doi.org/10.1115/GT2015-43456
Download citation file:
61
Views
Related Proceedings Papers
Related Articles
Improved Performance Rhenium Containing Single Crystal Alloy Turbine Blades Utilizing PPM Levels of the Highly Reactive Elements Lanthanum and Yttrium
J. Eng. Gas Turbines Power (January,1999)
Experimental Assessment of Fiber-Reinforced Ceramics for Combustor Walls
J. Eng. Gas Turbines Power (April,2001)
Development and Turbine Engine Performance of Three Advanced Rhenium Containing Superalloys for Single Crystal and Directionally Solidified Blades and Vanes
J. Eng. Gas Turbines Power (July,1998)
Related Chapters
Part 2, Section II—Materials and Specifications
Companion Guide to the ASME Boiler and Pressure Vessel Code, Volume 1, Third Edition
Part 2, Section II—Materials and Specifications
Companion Guide to the ASME Boiler & Pressure Vessel Code, Volume 1, Second Edition
Surface Analysis and Tools
Tribology of Mechanical Systems: A Guide to Present and Future Technologies