×

Thermal barrier coating material method of production thereof, gas turbine member using the thermal barrier coating material, and gas turbine

  • US 20040156724A1
  • Filed: 12/08/2003
  • Published: 08/12/2004
  • Est. Priority Date: 06/15/2001
  • Status: Active Grant
First Claim
Patent Images

1. A thermal barrier coating material, comprising a metal binding layer laminated on a base material and a ceramic layer laminated on the metal binding layer, the ceramic layer comprising partially stabilized ZrO2 which is porous and has microcracks that extend in a thickness direction of the ceramic layer.

View all claims
  • 1 Assignment
Timeline View
Assignment View
    ×
    ×