The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Feb. 15, 2022

Filed:

Sep. 21, 2018
Applicant:

Safran, Paris, FR;

Inventors:

Amar Saboundji, Moissy-Cramayel, FR;

Virginie Jaquet, Moissy-Cramayel, FR;

Assignee:

SAFRAN, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); C23C 4/08 (2016.01); C23C 14/16 (2006.01); C23C 28/00 (2006.01); C23C 4/073 (2016.01); C22C 19/05 (2006.01); C23C 4/137 (2016.01); C23C 28/02 (2006.01); C22C 19/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/288 (2013.01); C23C 4/073 (2016.01); C23C 4/08 (2013.01); C23C 14/16 (2013.01); C23C 28/321 (2013.01); C23C 28/324 (2013.01); C23C 28/345 (2013.01); C22C 19/007 (2013.01); C22C 19/057 (2013.01); C23C 4/137 (2016.01); C23C 28/027 (2013.01); F05D 2220/32 (2013.01); F05D 2230/31 (2013.01); F05D 2230/311 (2013.01); F05D 2230/313 (2013.01); F05D 2230/90 (2013.01); F05D 2300/132 (2013.01); F05D 2300/143 (2013.01); F05D 2300/1432 (2013.01); F05D 2300/175 (2013.01); F05D 2300/182 (2013.01); F05D 2300/607 (2013.01);
Abstract

A turbine part, such as a turbine blade or a distributor fin, for example, including a substrate made of superalloy based on monocrystalline nickel, including rhenium and/or ruthenium, and having a γ'-NisAI phase that is predominant by volume and a γ-Ni phase, the part also including a sublayer made of metal superalloy based on nickel covering the substrate, wherein the sublayer has a γ′-NisAI phase that is predominant by volume and wherein the sublayer has an average atomic fraction of aluminium of between 0.15 and 0.25, of chromium of between 0.03 and 0.08, of platinum of between 0.01 and 0.05, of hafnium of less than 0.01 and of silicon of less than 0.01. A process for manufacturing a turbine part including a step of vacuum deposition of a sublayer made of a superalloy based on nickel having predominantly by volume a γ′-NisAI phase, on a substrate made of superalloy based on nickel including rhenium and/or ruthenium.


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