Current status and future trends in turbine application of thermal barrier coatingsThis paper provides an overview of the current status and future trends in application of thermal barrier coatings (TBC) to turbine components, and in particular to high turbine airfoils. Included are descriptions of the favorable results achieved to date with bill-of-material applications of plasma deposited TBC, and recent experience with developmental coatings applied by electron beam-physical vapor deposition.
Document ID
19880067128
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sheffler, Keith D. (Pratt and Whitney Aircraft East Hartford, CT, United States)
Gupta, Dinesh K. (Pratt and Whitney East Hartford, CT, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1988
Subject Category
Mechanical Engineering
Report/Patent Number
ASME PAPER 88-GT-286Report Number: ASME PAPER 88-GT-286