Patent · US Active

Gas turbine component and process for producing gas turbine component

US9719420B2 · kind B2 · utility

5Cited by
4References
42Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 2, 2014
Grant dateAug 1, 2017
Priority date
Expiry dateJul 16, 2034

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T428/24355
  • WIPO fieldMaterials, metallurgy
  • WIPO sectorChemistry

Abstract

A process of producing a ceramic matrix composite gas turbine component and a ceramic matrix composite gas turbine component are provided. The process includes modifying a surface of the ceramic matrix composite gas turbine component to produce a modified surface with a surface roughness of less than 6 micrometers. The modifying is selected from the group of techniques consisting of applying unreinforced matrix plies to the surface, vapor depositing silicon on the surface, honing the surface, applying braze paste to the surface, and combinations thereof. The component includes a modified surface including a surface roughness of less than 6 micrometers. The modified surface being selected from the group consisting of unreinforced matrix plies applied to a surface of the ceramic matrix composite gas turbine component, silicon vapor deposited on the surface, a honed surface, a braze paste applied to the surface, and combinations thereof.

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