Low cost chrome and chrome/aluminide process for moderate temperature applications

作者: John F. Ackermann , Andrew J. Skoog , Paul V. Arszman

DOI:

关键词:

摘要: A low cost chromide and chromide/aluminide process for moderate temperature applications. gas turbine engine component is cleaned coated with a layer of metal, generally chromium or aluminum, containing paint. The metal paint heated to first period time in an air environment volatilize the solvents second oxygen-free atmosphere now are third interdiffuse component. diffusion then cooled ambient temperature.

参考文章(15)
William B. Connor, Jon C. Schaeffer, Robert D. Field, Method for forming a thermal barrier coating ,(1997)
Howard John Farr, D. Sangeeta, Method for applying coatings on substrates ,(2000)
Joseph David Rigney, Michael James Weimer, Mark Lloyd Miller, William Evan McCormack, John Lewis Lackman, Jeffrey Allan Pfaendtner, Article protected by a diffusion aluminide coating applied by painting techniques ,(2001)
Frank Boorboor, Richard J. Stueber, Natarajan S. Palanisamy, Method for bonding thermal barrier coatings to superalloy substrates ,(1997)
John G. Smeggil, Norman S. Bornstein, Clyde O. Brown, High temperature coatings by surface melting ,(1982)
Joseph D. Rigney, Michael J. Weimer, Ramgopal Darolia, Protection of internal and external surfaces of gas turbine airfoils ,(1999)
Thomas Alan Taylor, James Kent Knapp, Process for producing an oxide dispersed MCrAlY-based coating ,(1995)