Patent · US Active

Method for manufacturing a turbine engine part and the thereby produced part

US11346250B2 · kind B2 · utility

1Cited by
10References
15Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 19, 2017
Grant dateMay 31, 2022
Priority date
Expiry dateApr 9, 2038

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A method for manufacturing a turbine engine part in which a first rough casting element includes a first face and a second face opposite to each other is assembled by the second face on an orifice which has a second element of the part. The method includes machining a through-cavity in the first element which opens at the first face and from the second face of the first element and machining the first face of the first element so as to form an area suitable for ensuring the attachment of a conduit on the first element. The machining of the cavity and of the first face is achieved by using a machining reference frame based on the second element.

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