Patent · US Active

Method for producing a turbine engine part, and resulting mould and intermediate blank

US9969035B2 · kind B2 · utility

0Cited by

0References

14Claims

0Family size

Assignee

SNECMA · FR

Inventors

Patrick Emilien Paul Emile Huchin · Les Mureaux, FR
Karine Deschandol · Moissy-Cramayel, FR
Sebastien Digard Brou De Cuissart · Ardee, IE
Serge Fargeas · Paris, FR
Marc Soisson · Moissy-Cramayel, FR
Anthony Texier · Moissy-Cramayel, FR
Valéry Piaton · Moissy-Cramayel, FR

Key dates

Filing date	Dec 9, 2014
Grant date	May 15, 2018
Priority date	—
Expiry date	Dec 9, 2034

Classification

Technology area (CPC F)Mechanical Engineering; Lighting; Heating
CPC primaryF05D2300/608
WIPO fieldMaterials, metallurgy
WIPO sectorChemistry

Abstract

The invention relates to a method for producing multiple metal turbine engine parts, comprising steps consisting in:

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