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Title:
レニウムおよび/またはルテニウムを含む超合金で作られたタービン部品および関連する製造方法
Document Type and Number:
Japanese Patent JP7222984
Kind Code:
B2
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.

Inventors:
The Boonge, Amar
Jacke, Birginie
Application Number:
JP2020516683A
Publication Date:
February 15, 2023
Filing Date:
September 21, 2018
Export Citation:
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Assignee:
saffron
International Classes:
F01D25/00; C23C14/14; C23C14/34
Domestic Patent References:
JP2015059235A
JP2007092168A
JP2008095191A
Foreign References:
US20090185944
Attorney, Agent or Firm:
Kawaguchi International Patent Office