Thermal barrier coatings for aircraft engines: history and directions |
| |
Authors: | R A Miller |
| |
Affiliation: | (1) NASA Lewis Research Center, 44135 Cleveland, OH, USA |
| |
Abstract: | Thin thermal barrier coatings (TBCs) for protecting aircraft turbine section airfoils are examined. The discussion focuses
on those advances that led first to TBC use for component life extension and more re-cently as an integral part of airfoil
design. Development has been driven by laboratory rig and furnace testing, corroborated by engine testing and engine field
experience. The technology has also been sup-ported by performance modeling to demonstrate benefits and life modeling for
mission analysis. Factors that have led to the selection of current state-of-the-art plasma-sprayed and physical-vapor-deposited
zirconia-yttria/MCrAlX TBCs are emphasized, as are observations fundamentally related to their behav-ior. Current directions
in research into TBCs and recent progress at NASA are also noted. |
| |
Keywords: | historical review thermal barrier coatings zirconia |
本文献已被 SpringerLink 等数据库收录! |