C.T. Sims, Non-Metallic Materials for Gas Turbine Engines—Are They Real?,Adv. Mater. Process.
, Vol 139, 1991, p 32–39Google Scholar
W.N. Harrison, D.G. Moore, and J.C. Richmond, “Review of an Inves- tigation of Ceramic Coatings for Metallic Turbine Parts and Other High Temperature Applications,” NACA TN-1186, National Advisory Com- mittee for Aeronautics, 1947
F.G. Garrett and C.A. Gyorgak, “Adhesive and Protective Charac- teristics of Ceramic Coating A-417 and Its Effects on Engine Life of Forged Refractory-26 (AMS 5760) and Cast Stellite (AMS 5385) Tur- bine Blades,” NACA RM-E52130, 1953
N.I. Cannistraro, Where Do We Stand in Ceramic Coatings?,Met. Prog.
, Vol 74, 1958, p 111–113Google Scholar
N.N. Ault, Characteristics of Refractory Oxide Coatings Produced by Flame Spraying,J. Amer. Ceram. Soc.
, Vol 40, 1957, p 69–74CrossRefGoogle Scholar
W.M. Wheildon, Jr., Oxide Coated Metal Articles with Metal Under- coating, U.S. Patent 3, 006, 782, Oct 1961.
A.V. Levy, Ceramic Coating for Insulation,Met. Prog.
, Vol 75, 1959, p 86–89Google Scholar
L.N. Hjelm and B.R. Bornhorst, “Research-Airplane-Committee Re- port on Conference on the Progress of the X-15 Project,” NASATM X-57072, National Aeronautics and Space Administration, 1961, p 227- 253
H. Davies, The Design and Development of the Thiokol XRL99 Rocket Engine for the X-15 Aircraft,J. R. Aeronaut. Soc.
, Vol 67, 1963, p 79- 91Google Scholar
S.G. Grisaffe, Simplified Guide to Thermal-Spray Coatings,Mach. Des.
, Vol 39, 1967, p 174–181Google Scholar
P.R. Dennis, O.W. Gates, C.R Smith, and J.B. Bond, “Technological Survey—Plasma Jet Technology,” NASA SP-5033, National Aeronau- tics and Space Administration, 1965, p 117–120
H.S. Ingham and A.P. Shepard,Metco Flame Spray Handbook, Vol II,Powder Processes, 2nd ed., Metco Inc., 1964
A.N. Curren, S.G. Grisaffe, and K.C. Wycoff, “Hydrogen Plasma Tests of Some Insulating Coating Systems for the Nuclear Rocket Thrust Chamber,” NASA TM X-2461, National Aeronautics and Space Ad- ministration, 1972
G.W. Goward, Seventeen Years of Thermal Barrier Coatings,Proc. 1987 Coatings for Advanced Heat Engines Workshop, 27–30 July 1987, U.S. Department of Energy, CONF-870762, p III-1 to III-9
K.E. Wilkes and J.F. Lagedrost, “Thermophysical Properties of Plasma Sprayed Coatings,” NASA CR-121144, National Aeronautics and Space Administration, 1973
J. Humink, Jr.,High Temperature Inorganic Coatings, Reinhold, 1963, p 14-15
R. McPherson, The Relationship Between the Mechanism of Forma- tion, Microstructure and Properties of Plasma-Sprayed Coatings,Thin Solid Films
, Vol 83, 1981, p 807–811CrossRefGoogle Scholar
D. Chuanian, R.A. Zatorski, and H. Herman, Oxide Powders for Plasma Spraying—The Relationship Between Powder Characteristics and Coating Properties,Thin Solid Films
, Vol 118, 1984, p 467–475CrossRefGoogle Scholar
V.S. Stubican, Phase Equilibria and Metastabilities in the Systems ZrO2
-CaO, and ZrO2
, Vol 24A, 1984, p71–85Google Scholar
F.C. Toriz, A.B. Thakker, and S.K. Gupta, “Thermal Barrier Coating for Jet Engines,” ASME 88-GT-279, National Aeronautics and Space Ad- ministration, 1988
S.Stecura, “Two-Layer Thermal Barrier Coating for Turbine Airfoils— Furnace and Burner Rig Test Results,” NASA TM X-3425, National Aeronautics and Space Administration, 1976
S. Stecura and G.H. Liebert, Thermal Barrier Coating System, U.S. Pat- ent 4,055,705, Oct 1977
S. Stecura, “Two Layer Thermal Barrier Coating for High Temperature Components,”Am. Ceram. Soc. Bull.
, Vol 56, 1977, p 1082–1085Google Scholar
C.H. Liebert et al., “Durability of Zirconia Thermal-Barrier Ceramic Coatings on Air-Cooled Turbine Blades in Cyclic Jet Engine Opera-tion,” NASATM X-3410, National Aeronautics and Space Administra- tion, 1976
J.T. DeMasi-Marcin, K.D. Sheffler, and S. Bose, “Mechanisms of Deg- radation and Failure in a Plasma Deposited Thermal Barrier Coating,” ASME 89-GT-132, National Aeronautics and Space Administration, 1989
R.J. Bratton, S.K. Lau, and S.Y. Lee, “Evaluation of Present Thermal Barrier Coatings for Potential Service in Electric Utility Gas Turbines,” NASA CR-165545, National Aeronautics and Space Administration, 1982
S.R. Levine and R.A. Miller, “Thermal Barrier Coatings for Utility Gas Turbines,” NASA TM-85349, National Aeronautics and Space Admini- stration, 1982
R.C. Tucker, T.A. Taylor, and M.H. Weatherly, “Plasma Deposited Ni- CrAlY Airfoil and Zirconia/NiCrAlY Thermal Barrier Coatings,” pre- sented at the Third Conference on Gas Turbine Materials in a Marine Environment Bath University, Bath, England, 20–23 Sept, 1976, ses- sion VII, paper 2Google Scholar
S. Stecura, “Effects of Compositional Changes on the Performance of a Thermal Barrier Coating System,” NASA TM-78976, National Aero-nautics and Space Administration, 1978
P. Boch et al., Plasma-Sprayed Zirconia Coatings,Adv. Ceram.
, Vol 12, 1984, p 488–502Google Scholar
E.C. Duderstadt and P. Agarwal, “Energy Efficient Engine. High Pres- sure Turbine Thermal Barrier Coating Support Technology Report,” NASA CR-168037, National Aeronautics and Space Administration, 1983
I.E. Sumner and D.L. Ruckle, “Development of Improved Durability Plasma Sprayed Ceramic Coatings for Gas Turbine Engines,” AIAA 80-1193, AIAA, 1980
P.A. Siemens and W.B. Hillig, “Thermal-Barrier-Coated Turbine Blade Study,” NASA CR-165351, National Aeronautics and Space Admini-stration, 1981
N.P. Anderson and K.D. Sheffler, “Development of Strain Tolerant Thermal Barrier Coating Systems, Tasks I-III,” NASA CR-168251, Na-tional Aeronautics and Space Administration, 1983
T.A. Taylor, D.L. Appleby, A.E. Weatherill, and J. Griffiths, Plasma- Sprayed Yttria-Stabilized Zirconia Coatings: Structure-Property Rela- tionships,Surf. Coat. Technol.
, Vol 43/44, 1990, p 470–480CrossRefGoogle Scholar
D.S. Duvall, Processing Technology for Advanced Metallic and Ce- ramic Turbine Airfoil Coatings,Proc. 2nd Conf. Advanced Materials for Alternative-Fuel-Capable Heat Engines, 24–28 Aug 1981, EPRI RD-2369-SR, Electric Power Research Institute, p 6-102 to 6-117
S.M. Meier, D.M. Nissley, and K.D. Sheffler, Status of Ceramic Ther- mal Barrier Coatings—Gas Turbine Applications and Life Prediction,Proc. 1990 Coatings for Advanced Heat Engines Workshop, 6–9 Aug 1990, U.S. Department of Energy, CONF-9008151, p 11–57 to II–65
T.E. Strangman, Development and Performance of Physical Vapor Deposition Thermal Barrier Coating Systems,Proc. 1987 Coatings for Advanced Heat Engines Workshop, 27–30 July 1987, U.S. Depart- ment of Energy, CONF-870762, p III-63 to III-71
R.E. Demaray, W.K. Halnan, and S. Shen, Development of Electron Beam Physical Vapor Deposition of Ceramic Coatings,Proc. 2nd Conf. Advanced Materials for Alternative-Fuel-Capable Heat En- gines, 24–28 Aug 1981, EPRI RD-2369-SR, Electric Power Research Institute, p6-151 to 6-184
R. Shankar, Electron-Beam Physical Vapor Deposition Development of Zirconia Coatings (abstract only),Proc. 1987 Coatings for Advanced Heat Engines Workshop, 27–30 July 1987, U.S. Department of En- ergy, CONF-870762, p III-43
H. Lammermann and G. Kienel, PVD Coatings for Aircraft Turbine Blades,Adv. Mater. Process
, Vol 140 (No. 6), 1991, p 18–23Google Scholar
S.M. Meier, D.M. Nissely, and K.D. Sheffler, “Thermal Barrier Coating Life Prediction Model Development, Phase II—Final Report,” NASA CR-189111, National Aeronautics and Space Administration, 1991
R.A. Miller and C.E. Lowell, Failure Mechanisms of Thermal Barrier Coatings Exposed to Elevated Temperatures,Thin Solid Films
, Vol 95, 1982, p 265–273CrossRefGoogle Scholar
R.A. Miller, Oxidation-Based Model for Thermal Barrier Coating Life,J. Am. Ceram. Soc.
, Vol 67, 1984, p 517–521CrossRefGoogle Scholar
R.A. Miller, Life Modeling of Thermal Barrier Coatings for Aircraft Gas Turbine Engines,J. Eng. Gas Turbines Power (Trans. ASME)
, Vol 3, 1989, p 301–305Google Scholar
G.C. Chang, W. Phucharoen, and R.A. Miller, Behavior of Thermal Barrier Coatings for Advanced Gas Turbine Blades,Surf. Coat. Tech- nol.
, Vol 30, 1987), p 13–28CrossRefGoogle Scholar
J.T. Demasi, K.D. Sheffler, and M. Ortiz, “Thermal Barrier Coating Life Prediction Model Development, Phase I—Final Report,” NASA CR-182230, National Aeronautics and Space Administration, 1989
T.A. Cruse, S.E. Stewart, and M. Ortiz, Thermal Barrier Coating Life Prediction Model Development,J. Eng. Gas Turbines Power
, Vol 110, 1988, p 610–616CrossRefGoogle Scholar
R.V. Hillery, B.H. Pilsner, R.L. McKnight, T.S. Cook, and M.S. Hartle, “Thermal Barrier Coating life Prediction Model Development, Final Report,” NASA CR-180807, National Aeronautics and Space Admini- stration, 1988
T.E. Strangman, J. Neumann, and A. Liu, “Thermal Barrier Coating Life-Prediction Model Development,” NASA CR-179648, National Aeronautics and Space Administration, 1987
C.H. Liebert and F.S. Stepka, “Potential Use of Ceramic Coating as a Thermal Insulation on Cooled Turbine Hardware,” NASA TM X-3352, National Aeronautics and Space Administration, 1976
D.E. Andress, “An Analytical Study of Thermal Barrier Coated First- Stage Blades in an F100 Engine,” NASA CR-135359, National Aero-nautics and Space Administration, 1978
P.L. Meitner, “Analysis of Metal Temperature and Coolant Flow with a Thermal Barrier Coating on a Full-Coverage-Film-Cooled Turbine Vane,” NASA TP-1310, National Aeronautics and Space Administra- tion, 1978
H.J. Gladden and C.H. Liebert, “Effects of a Ceramic Coating on a Met- al Temperatures of an Air-Cooled Turbine Vane,” NASA TP-1598, Na- tional Aeronautics and Space Administration, 1980
R.A. Miller,R.G. Garlick, and J.L. Smialek, Phase Stability in Plasma-Sprayed Zirconia-Yttria,Am. Ceram. Soc. Bull.
, Vol 62, 1983, p 1355–1358Google Scholar
R.A. Miller and W.J. Brindley, “Thermal Properties of Thermal Barrier Coatings,” NASA TM-105923, National Aeronautics and Space Ad-ministration, 1991
C.C. Berndt et al., Current Problems in Plasma Spray Processing,J. Therm. Spray Technol
, Vol 1, 1992, p 341–356Google Scholar
R.A. Miller and J. Doychak, Plasma Sprayed Ceramic Thermal Barrier Coatings for Smooth Intermetallic Alloys,J. Therm. Spray Technol.
, Vol 1, 1992, p 211–213Google Scholar
K.N. Lee, R.A. Miller, and N.S. Jacobson, Development of Thermal Shock Resistant Mullite Coating on Silicon Carbide,Ceramic Trans- actions: Advances in Ceramic Matrix Composites, N.P. Bansal, Ed., American Ceramic Society, 1994, p 565–575
K.N. Lee, N.S. Jacobson, and R.A. Miller, Refractory Oxide Coatings on Silicon-Based Ceramics,MRS Bull.
, Vol XIX, 1994, p 35–38Google Scholar
S. Stecura, “Advanced Thermal Barrier System Bond Coatings for Use on Ni-, Co-, and Fe-Base Alloy Substrates,” NASA TM-87062, Na-tional Aeronautics and Space Administration, 1985
W.J. Brindley and R.A. Miller, Thermal Barrier Coating Life and Iso- thermal Oxidation of Low-Pressure Plasma-Sprayed Bond Coat Al- loys,Surf. Coat. Technol.
, Vol 43/44, 1990, p 446–457CrossRefGoogle Scholar
C.E. Lowell, R.G. Garlick, and B. Henry, Thermal Expansion in the Ni- Cr-Al and Co-Cr-Al Systems to 1200 °C Determined by High-Tem- perature X-Ray Diffraction,Metall. Trans.
, Vol 7A, 1976, p 655–660Google Scholar
W.J. Brindley and J.D. Whittenberger, Stress Relaxation of Low Pres- sure Plasma-Sprayed NiCrAlY Alloys.Mater. Sci. Eng.
, Vol A163, 1993, p 33–41Google Scholar
D.J. Wortman, E.C. Duderstadt, and W.A. Nelson, “Bond Coat Devel- opment for Thermal Barrier Coatings,” ASME 89-GT-134, American Society of Mechanical Engineers, 1989
S. Stecura, New ZrO2
Plasma-Sprayed Coatings for Thermal Barrier Applications,Thin Solid Films
, Vol 150, 1987, p 15–40CrossRefGoogle Scholar
V.S. Stubican, G.S. Corman, J.R. Hellmann, and G. Senft, Phase Rela- tionships in Some ZrO2 Systems,Adv. Ceram.
, Vol 12, 1984, p96–106Google Scholar
R.A. Miller, W.J. Brindley, J.G. Goedjen, R. Tiwari, and D. Mess, The Effect of Silica on the Cyclic Life of a Zirconia-Yttria Thermal Barrier Coating,Thermal Spray Industrial Applications, C.C. Berndt and S. Sampath, Ed., ASM International, 1994, p 49–54
R.A. Miller and G.W. Leissler, “Characterization and Durability Test- ing of Plasma-Sprayed Zirconia-Yttria and Hafnia- Yttria Thermal Bar-rier Coatings, Part II. Effect of Spray Parameters on the Performance of Several Hafnia-Yttria and Zirconia-Yttria Coatings,” NASA TP-3296, National Aeronautics and Space Administration, 1993
R.A. Miller, W.J. Brindley, C.J. Rouge, and G.W. Leissler, “Metal/Ce- ramic Bond Coatings for High Temperatures,” NASA Tech Brief 12, National Aeronautics and Space Administration, 1988, p 51