Nickel Oxide, Ceramic Insulated, High Temperature Coating.

Abstract

A three layer composite coating for gas turbine engine materials and other materials exposed to high temperatures, thermal cycling, and corrosive environments. The base layer is Aluminide or an MCrAlY composite, where M is a metal selected from the group consisting of nickel or cobalt, alone or in combination, The middle layer is a ceramic composite. The outer layer is composed of nickel oxide.

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Document Details

Document Type
Technical Report
Publication Date
Jan 27, 1987
Accession Number
ADD014239

Entities

People

  • Louis F. Aprigliano

Organizations

  • United States Department of the Navy

Tags

DTIC Thesaurus Topics

  • Alloys
  • Ceramic Materials
  • Ceramic Matrix Composites
  • Chemical Composition
  • Coatings
  • Composite Materials
  • Elements
  • Gas Turbine Blades
  • Gas Turbines
  • High Temperature
  • Materials
  • Patents
  • Protective Coatings
  • Silicon Carbide
  • Substrates
  • Turbine Blades
  • Turbines

Fields of Study

  • Materials science

Readers

  • Surface Engineering/Surface Coating Technology.

Technology Areas

  • Microelectronics
  • Microelectronics - Graphene