Thermal barrier coating experience in gas turbine engines at Pratt & Whitney

Journal of Thermal Spray Technology

Volumn 6, Issue 1, 1997, Pages 99-104

  Bose, S ^a   DeMasi Marcin, J ^a  

^a PRATT AND WHITNEY   (United States)

Author keywords

EB PVD; Gas turbine engine; Plasma spray; TBC; Thermal barrier

Indexed keywords

CHEMICAL VAPOR DEPOSITION; DURABILITY; ELECTRON BEAMS; FAILURE (MECHANICAL); GAS TURBINES; MECHANICAL PROPERTIES; OXIDATION RESISTANCE; PLASMA SPRAYING; SURFACE PROPERTIES;

AIRFOIL SURFACES; COMPRESSIVE STRESSES; OXIDATION PROTECTION; THERMAL BARRIER COATING; THERMOCYCLIC EXPOSURE;

PROTECTIVE COATINGS;

EID: 0031097294     PISSN: 10599630     EISSN: None     Source Type: Journal    
DOI: 10.1007/BF02646318     Document Type: Article

References (3)

1. S.M. Meier and D.K. Gupta, The Evolution of Thermal Barrier Coatings in Gas Turbine Engine Applications. J. Eng. Gas Turbines Power (Trans. ASME), Vol 116, 1994, p 250-257
2. J.T. DeMasi, M. Ortiz, and K.D. Sheffler, "Thermal Barrier Coating Life Prediction Model Development. Phase I Final Report", NASA Cr-182230, NASA-Lewis Research Center, 1989
3. R.A. Miller and C.E. Lowell, Failure Mechanisms of Thermal Barrier Coatings Exposed to Elevated Temperature, Thin Solid Films. Vol 95, 1982, p 265-273