Patent · US Active

Abrasive coated preform for a turbine blade tip

US8616847B2 · kind B2 · utility

14Cited by
10References
18Claims
0Family size

Assignee

Inventor

Key dates

Filing dateAug 30, 2010
Grant dateDec 31, 2013
Priority date
Expiry dateJul 16, 2032

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49336
  • WIPO fieldSurface technology, coating
  • WIPO sectorChemistry

Abstract

A squealer tip preform having a coating including an abrasive is disclosed. The squealer tip may be separately formed from a generally elongated blade to which the squealer tip preform is configured to be attached. The squealer tip may be configured such that an outer surface of the squealer tip preform is generally aligned with an outer side surface of the turbine blade defining a cross-sectional profile of the turbine blade. Forming the squealer tip preform with an abrasive coating separate from the turbine blade greatly reduces costs and improves efficiency as compared with conventional systems.

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