Patent · US Active

Repair or remanufacture of blade platform for a gas turbine engine

US10252380B2 · kind B2 · utility

0Cited by
9References
23Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 10, 2014
Grant dateApr 9, 2019
Priority date
Expiry dateFeb 14, 2037

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2240/80
  • WIPO fieldMachine tools
  • WIPO sectorMechanical engineering

Abstract

A method of remanufacturing a turbine component includes electrical discharge machining a puck via the turbine component to form an electrical discharged machined puck; and brazing the electrical discharged machined puck to the turbine component.

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