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Title: Development of improved corrosion- and erosion-resistance coatings for gas-turbine airfoils

Technical Report ·
DOI:https://doi.org/10.2172/6426373· OSTI ID:6426373

The main objective of this program is to obtain a ceramic coating with sufficient density to prevent hot-corrosion element diffusion while accommodating the thermal induced stresses and strain encountered in the gas turbine airfoil application. A secondary objective is to include ceramic coatings for outer air seals and combustor components such as falseheads, crossover tubes, and igniters. In addition, these coatings may directly, or with minor modification, be of major interest for insulating diesel engine combustion zones. The application objective is to significantly enhance diesel and gas turbine engine durability when operating with minimally processed alternative fuels. Both steel tabs and IN-738 pins were used as substrate to be coated with Yttria-stabilized Zirconia using EB-PVD technique. Various bond layers including CoCrAlY, NiCrAlY and NiCoCrAlY were also deposited by PVD in a 100 kW coater followed by glass bead peening and vacuum heat-treatment at 1975/sup 0/F for four (4) hours. ZrO/sub 2/(Y/sub 2/O/sub 3/) top layers were deposited in a 200 kW coater with a pressure barrier system to enable oxygen gas being introduced during the coating process. Results are presented and discussed. (WHK)

Research Organization:
Airco Temescal Div., Berkeley, CA (USA)
DOE Contract Number:
AC03-78ET12292
OSTI ID:
6426373
Report Number(s):
DOE/ET/12292-T1
Country of Publication:
United States
Language:
English