Method for manufacturing a composite turbomachine bladed disk (BLISK) with ceramic reinforcement

Patent metadata

Field	Value
Publication number	US-12428714-B2
Application number	US-202017785329-A
Country	US
Kind code	B2
Filing date	Dec 10, 2020
Priority date	Dec 20, 2019
Publication date	Sep 30, 2025
Grant date	Sep 30, 2025

Abstract

A method for manufacturing a metal bladed wheel of a turbomachine reinforced by an insert made of metal matrix composite material, includes winding the ceramic fibers around a mandrel in order to form the insert, the ceramic fibers being surrounded by a material constituting the matrix; and spark plasma sintering the insert with a powder of metal constituting the bladed wheel to be manufactured.

First claim

The invention claimed is:

1. A method for manufacturing a metal bladed wheel of a turbomachine reinforced by an insert made of metal matrix composite material, said method comprising:
winding the ceramic fibers around a mandrel in order to form the insert, the ceramic fibers being surrounded by a material constituting the matrix;
performing a consolidation on the mandrel of the insert by spark plasma sintering with a first powder of metal constituting the bladed wheel to be manufactured;
placing the consolidated insert in a mold comprising a second powder of metal constituting the bladed wheel to be manufactured, and
densifying the insert by spark plasma sintering with the second metal powder in the mold.

2. The method according to claim 1 , wherein the insert reaches a compaction rate comprised between 60% and 80% at the end of the consolidation step.

3. The method according to claim 1 , wherein the first metal powder and the second metal powder are different.

4. The method according to claim 1 , wherein the first metal powder and the second metal powder are identical.

5. The method according to claim 1 , wherein the ceramic fibers are coated with a layer made of material constituting the matrix.

6. The method according to claim 1 , wherein yarns made of material constituting the matrix are stranded around the ceramic fibers.

7. The method according to claim 1 , wherein the bladed wheel is made of nickel-based alloy, the ceramic fibers comprise carbon and are coated with a diffusion protection layer.

8. The method according to claim 1 , wherein the bladed wheel is made of titanium-based alloy.

9. The method according to claim 1 , wherein the ceramic fibers are made of silicon carbide.

10. The method according to claim 1 , wherein the bladed wheel is a one-piece bladed ring.

Assignees

• Safran

Inventors

• Sallot Pierre Jean
• Franchet Jean-Michel Patrick Maurice

Classifications

• F01D5/34

  Rotor-blade aggregates of unitary construction {, e.g. formed of sheet laminae; (discs formed of sheet laminae F01D5/028; ceramic materials F01D5/284, composite materials F01D5/282)} · CPC title

• C22C47/14

  by powder metallurgy, i.e. by processing mixtures of metal powder and fibres or filaments · CPC title

• B23P15/006

  turbine wheels · CPC title

• F01D5/282

  Selecting composite materials, e.g. blades with reinforcing filaments · CPC title

• F05D2300/6032

  Metal matrix composites [MMC] · CPC title