Method for manufacturing an ordered network of acoustic channels made of abradable material

Patent metadata

Field	Value
Publication number	US-11478981-B2
Application number	US-201816770323-A
Country	US
Kind code	B2
Filing date	Dec 6, 2018
Priority date	Dec 6, 2017
Publication date	Oct 25, 2022
Grant date	Oct 25, 2022

Abstract

A manufacturing method of an abradable coating consisting of depositing, on a substrate surface a filament of a thermosetting material while providing both a relative displacement between the substrate and the filament along a predetermined deposition path and solidification of the filament in order to create a three-dimensional scaffold of filaments, consisting of superimposed layers of which the filaments of a given layer are not contiguous and can be oriented differently from those of an adjacent layer, so as to confer upon it acoustic wave absorption properties, the thermosetting material being a thixotropic mixture free of solvent and consisting of a polymer base and a cross-linking agent in a weight ratio of a polymer base to a cross-linking agent comprised between 1:1 and 2:1, and of a flowing component, typically a petroleum jelly present between 5 and 15% by weight of the total weight of the thixotropic mixture.

First claim

The invention claimed is:

1. A manufacturing method of an abradable coating comprising:
depositing on a turbomachine wall a filament of a thermosetting material while providing both a relative displacement between said turbomachine wall and said filament along a predetermined deposition path and solidification of said filament in order to create a three-dimensional scaffold of filaments, comprising superimposed layers of which the filaments are not contiguous and can be oriented differently from the filaments of an adjacent layer, so as to confer acoustic wave absorption properties,
wherein said thermosetting material is a thixotropic mixture including a polymer base and a cross-linking agent in a weight ratio of said polymer base to said cross-linking agent comprised between 1:1 and 2:1, and a flowing component present between 5 and 15% by weight of a total weight of said thixotropic mixture.

2. The manufacturing method according to claim 1 , wherein said thixotropic mixture is obtained by co-extrusion of said polymer base and said cross-linking agent in a conical extrusion screw and deposited on said turbomachine wall with an ejection nozzle with calibrated shape and dimensions, an output cross section of which has a major width less than 250 microns.

3. The manufacturing method according to claim 1 , wherein the relative displacement between said turbomachine wall and said filament is provided by a machine with at least three axes or a robot controlled from a computer.

4. The manufacturing method according to claim 1 , wherein the solidification of said filament is provided by a heating element mounted at an output of said calibrated ejection nozzle.

5. The manufacturing method according to claim 1 , wherein said three-dimensional scaffold of filaments comprises superimposed layers of which the filaments of a given layer are oriented alternately at 0° or at 90°, with no offset in the superimposition of filaments of the same direction.

6. The manufacturing method according to claim 1 , wherein said three-dimensional scaffolding of filaments comprises superimposed layers of which the filaments of a given layer are oriented alternately at 0° or at 90° and have an offset in the superimposition of filaments of the same direction.

7. The manufacturing method according to claim 1 , wherein said three-dimensional scaffold of filaments of comprises superimposed layers of filaments having orientation directions of the filaments Di offset by the same angular deviation, comprised between 20° and 40° at each layer i.

8. The manufacturing method according to claim 1 , wherein said three-dimensional scaffold of filaments comprises superimposed layers of filaments having, for each of the layers, both an orientation of filaments at 0° and an orientation of filaments at 90°, so as to form vertical perforations with square cross sections between the filaments.

Assignees

• Safran Aircraft Engines

Inventors

• Mardjono Jacky Novi
• Dubourg Arnaud
• Fotsing Edith-Roland
• Ross Annie

Classifications

• B33Y40/00

  Auxiliary operations or equipment, e.g. for material handling · CPC title

• B33Y80/00

  Products made by additive manufacturing · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• B29K2101/10

  Thermosetting resins · CPC title

• F02C7/24

  Heat or noise insulation (air intakes having provisions for noise suppression F02C7/045; turbine exhaust heads, chambers, or the like F01D25/30; silencing nozzles of jet-propulsion plants F02K1/00) · CPC title