Patent · US Active

Method for repairing a turbine nozzle segment

US8296945B2 · kind B2 · utility

4Cited by
4References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 29, 2007
Grant dateOct 30, 2012
Priority date
Expiry dateJul 30, 2031

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/4973
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A method for repairing a turbine nozzle segment includes providing a turbine nozzle segment having an enclosure with an integral discourager, removing the enclosure and/or the discourager from the turbine nozzle segment and attaching a new enclosure ad/or discourager to the turbine nozzle segment.

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