Dip process thermal barrier coatings for gas turbines

  • David J. Rowcliffe
  • , Ibrahim M. Allam

Research output: Contribution to journalArticlepeer-review

1 Scopus citations

Abstract

A new concept to apply zirconia-based thermal barrier coatings on cobalt base alloys has been developed. Contrary to plasma spraying or electron beam vaporization, the new process produces a dense and highly adherent zirconia coating that resists thermal cycling and penetration by corrosive molten salts. The new method is based on thermally growing a ZrO2-based layer from a Zr-rich alloy, predeposited on a Y-rich substrate by hot dipping. The coating consists of an outer ZrO2/Y2O3 layer and an inner oxide-metal composite layer next to the substrate surface. The outer oxide layer acts as a thermal barrier, while the inner layer acts as a graded seal that improves the adhesion of the coating to the substrate. Thermal cycling experiments showed that the coating has a good resistance to spallation between room temperature and 1100 C.

Original languageEnglish
Pages (from-to)2652-2655
Number of pages4
JournalJournal of Vacuum Science and Technology A: Vacuum, Surfaces and Films
Volume4
Issue number6
DOIs
StatePublished - Nov 1986

ASJC Scopus subject areas

  • Condensed Matter Physics
  • Surfaces and Interfaces
  • Surfaces, Coatings and Films

Fingerprint

Dive into the research topics of 'Dip process thermal barrier coatings for gas turbines'. Together they form a unique fingerprint.

Cite this