Patent · US Expired

Product, especially a gas turbine component, with a ceramic heat insulating layer

US6764771B1 · kind B1 · utility

25Cited by
17References
9Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 22, 2000
Grant dateJul 20, 2004
Priority date
Expiry dateDec 22, 2020

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldSurface technology, coating
  • WIPO sectorChemistry

Abstract

The invention relates to a product (1), particularly a gas turbine blade that can be exposed to a hot aggressive gas (7). The product (1) has a metallic basic body (2), which is provided with a thermal barrier coating (4) having a spinel of the composition AB2O4.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.