PVD thermal barrier coating applications and process development for aircraft engines

Journal of Thermal Spray Technology

Volumn 6, Issue 2, 1997, Pages 167-175

  Rigney, D V ^a   Viguie, R ^b   Wortman, D J ^c   Skelly, D W ^d  

^a Interturbine Coatings Center ^*  (United States)

^b Interturbine Coatings Center   (Netherlands)

^c GE AVIATION   (United States)

^d David W Skelly and Associates   (United States)

Author keywords

Electron beam physical vapor deposition; High pressure turbine airfoils; Process parameters; Thermal barrier coatings; Yttria stabilized zirconia

Indexed keywords

AIRCRAFT ENGINES; AIRFOILS; MICROSTRUCTURE; VAPOR DEPOSITION; ZIRCONIA;

ELECTRON BEAM PHYSICAL VAPOR DEPOSITION; HIGH PRESSURE TURBINE AIRFOILS; THERMAL BARRIER COATINGS; YTTRIA-STABILIZED ZIRCONIA;

PROTECTIVE COATINGS;

EID: 0031166396     PISSN: 10599630     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11666-997-0008-6     Document Type: Article

References (5)

1. S.M. Meier and D.K. Gupta, "The Evolution of Thermal Barrier Coatings in Gas Turbine Engine Applications," 92-GT-203, American Society of Mechanical Engineers, 1992
2. D.W. Wortman, B.A. Nagaraj, and E.C. Duderstadt, Thermal Barrier Coatings for Gas Turbine Use, Mater. Sci. Eng., Vol A 121, 1989, p 433-440
3. B.A. Movchan and A.V. Demchishin, Study of the Structure and Properties of Thick Vacuum Condensates of Nickel, Titanium, Tungsten, Aluminium Oxide and Zirconium Dioxide, Phys. Met. Metallogr. (USSR), Vol 28 (No. 4), 1969, p 83-90
4. J.A. Thornton, J. Vac. Technol., Vol 11, 1974, p 666
5. J.A. Thornton, Ann. Rev. Mater. Sci. Vol 7, 1977, p 239