TY - JOUR
T1 - Thermal barrier coatings issues in advanced land-based gas turbines
AU - Parks, W. P.
AU - Hoffman, E. E.
AU - Lee, W. Y.
AU - Wright, I. G.
PY - 1997/6
Y1 - 1997/6
N2 - The Department of Energy's Advanced Turbine Systems (ATS) program is aimed at fostering the development of a new generation of land-based gas turbine systems with overall efficiencies significantly beyond those of current state-of-the-art machines, as well as greatly increased times between inspection and refurbishment, improved environtnental impact, and decreased cost. The proposed duty cycle of ATS machines will emphasize different criteria in the selection of materials for the critical components. In particular, thermal barrier coatings (TBCs) will be an essential feature of the hot gas path components in these machines. The goals of the ATS will require significant improvements in TBC technology, since these turbines will be totally reliant on TBCs, which will be required to function on critical components such as the first-stage vanes and blades for times considerably longer than those experienced in current applications. Important issues include the mechanical and chemical stability of the ceramic layer and the metallic bond coat, the thermal expansion characteristics and compliance of the ceramic layer, and the thermal conductivity across the thickness of the ceramic layer.
AB - The Department of Energy's Advanced Turbine Systems (ATS) program is aimed at fostering the development of a new generation of land-based gas turbine systems with overall efficiencies significantly beyond those of current state-of-the-art machines, as well as greatly increased times between inspection and refurbishment, improved environtnental impact, and decreased cost. The proposed duty cycle of ATS machines will emphasize different criteria in the selection of materials for the critical components. In particular, thermal barrier coatings (TBCs) will be an essential feature of the hot gas path components in these machines. The goals of the ATS will require significant improvements in TBC technology, since these turbines will be totally reliant on TBCs, which will be required to function on critical components such as the first-stage vanes and blades for times considerably longer than those experienced in current applications. Important issues include the mechanical and chemical stability of the ceramic layer and the metallic bond coat, the thermal expansion characteristics and compliance of the ceramic layer, and the thermal conductivity across the thickness of the ceramic layer.
KW - Advanced turbine systems
KW - Bond coatigs
KW - Combustion turbines
KW - Land-based turbines
KW - Thermal barrier coatings
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U2 - 10.1007/s11666-997-0011-y
DO - 10.1007/s11666-997-0011-y
M3 - Article
AN - SCOPUS:0031166424
SN - 1059-9630
VL - 6
SP - 187
EP - 192
JO - Journal of Thermal Spray Technology
JF - Journal of Thermal Spray Technology
IS - 2
ER -