Patent · US Active

Method for producing a metal reinforcement for a turbine engine blade

US9199345B2 · kind B2 · utility

6Cited by
7References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 22, 2010
Grant dateDec 1, 2015
Priority date
Expiry dateJun 28, 2032

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/4998
  • WIPO fieldOther special machines
  • WIPO sectorMechanical engineering

Abstract

A method for creating a metal reinforcement for a leading or trailing edge of a turbine engine blade including a reinforcement foot and head, the method including: creating a plurality of V-shaped tapered elements that form different parts of the metal reinforcement so that the metal reinforcement is divided into a plurality of parts distributed between the foot and the head; positioning the parts on equipment that is shaped like the leading or trailing edge of the turbine engine blade; and rigidly connecting the different parts so as to form the complete profile of the one-piece metal reinforcement the by recombining the different parts.

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