Method for in situ additive manufacturing of a coating on a turbomachine casing

Patent metadata

Field	Value
Publication number	US-11554534-B2
Application number	US-201816770364-A
Country	US
Kind code	B2
Filing date	Dec 6, 2018
Priority date	Dec 6, 2017
Publication date	Jan 17, 2023
Grant date	Jan 17, 2023

Abstract

A method of a coating by additive manufacturing on a turbomachine casing includes depositing on an internal surface of the turbomachine casing a filament of an abradable material to create a three-dimensional scaffold of filaments. A filamentary material deposition system is positioned from the internal surface of the casing; a first layer of the coating is deposited over 360′; a rotation of the filamentary material deposition system is carried out by a first predetermined angle and the filamentary material deposition system is positioned from the deposited layer; a second layer of coating is deposited on the first coating layer, on a sector of the casing; a displacement is carried out corresponding to the first sector already covered, then for the following sectors until 360° is covered; and after having carried out a rotation of the filamentary material deposition system.

First claim

The invention claimed is:

1. An in situ deposition method of a coating by additive manufacturing on a turbomachine casing, the method comprising:
depositing on an internal surface of said turbomachine casing a filament of a size of at most 250 microns of diameter of an abradable material in a predefined deposition path in order to create a three-dimensional scaffold of filaments having a coating thickness and forming between the filaments an ordered array of channels by
positioning a filamentary material deposition system along a longitudinal axis of said casing at a predetermined position and distance relative to said internal surface of said casing, the filamentary material deposition system including an ejection nozzle fed by a conical extrusion screw which mixes components of the coating of the abradable material to obtain a thixotropic fluid,
depositing a first layer of said coating by depositing the thixotropic fluid using the ejection nozzle of the filamentary material deposition system on 360° of the circumference of said casing by a circumferential displacement between said casing and said filamentary material deposition system,
carrying out a rotation of said filamentary material deposition system by a first predetermined angle and positioning said filamentary material deposition system along said longitudinal axis of said casing at a predetermined position and distance relative to said first layer of said coating,
depositing, on a first sector of said casing by an axial displacement between said casing and said filamentary material deposition system, a second layer of said coating on said first layer of said coating by the depositing the thixotropic fluid using the ejection nozzle of the filamentary material deposition system,
carrying out a circumferential displacement between said casing and said filamentary material deposition system by a predetermined angular deviation corresponding to the first sector already covered during the deposition of said second layer of said coating,
repeating the step of depositing on said first sector of said casing by the depositing the thixotropic fluid using the ejection nozzle of the filamentary material deposition system and the step of carrying out the circumferential displacement by said predetermined angular deviation for the following sectors until 360° of the circumference of said casing are covered, and
after having carried out a rotation of said filamentary material deposition system by a second predetermined angle, repeating the preceding steps of depositing by the depositing the thixotropic fluid using the ejection nozzle of the filamentary material deposition system and carrying out the circumferential displacement for further layers of said coating until the coating thickness is obtained.

2. The in situ deposition method of a coating by additive manufacturing according to claim 1 , wherein, prior to the deposition of said first layer of said coating, a layer of a material is deposited on said turbomachine casing having a non-axisymmetric geometry to obtain a deposition surface with an axisymmetric geometry.

3. The in situ deposition method of a coating by additive manufacturing according to claim 1 , wherein said step of rotation of said filamentary deposition system is carried out twice by successive 90° rotations, the first predetermined angle being equal to 90°.

4. The in situ deposition method of a coating by additive manufacturing according to claim 1 , wherein said step of rotation of said filamentary deposition system is carried out as many times as there exists different predetermined orientation directions of the filaments.

5. The in situ deposition method of a coating by additive manufacturing according to claim 4 , wherein said step of rotation of said filamentary deposition system is carried out six times by successive 30° rotation, the first predetermined angle being equal to 30°.

6. The in situ deposition method of a coating by additive manufacturing according to claim 1 , wherein additional layers of said coating are added locally to overcome a non-axisymmetric geometry of said turbomachine casing.

7. The in situ deposition method of a coating by additive manufacturing according to claim 1 , wherein the deposition of filamentary material is carried out by a plurality of ejection nozzles wherein a vertical positioning of each of said ejection nozzles is independently adjustable.

8. The in situ deposition method of a coating by additive manufacturing according to claim 1 , wherein said turbomachine casing is a fan casing of woven composite material.

9. A filamentary material deposition system for the implementation of the in situ deposition method of a coating by additive manufacturing according to claim 1 .

10. An abradable turbomachine wall coating obtained from the in situ deposition method of a coating by additive manufacturing according to claim 1 .

11. The in situ deposition method of a coating by additive manufacturing according to claim 1 , wherein a distance sensor is provided to measure distances between the ejection nozzle and the casing or the abradable material.

12. The in situ deposition method of a coating by additive manufacturing according to claim 1 , wherein a heating lamp is mounted in proximity to the ejection module and stabilizes the deposited thixotropic fluid.

Assignees

• Safran Aircraft Engines

Inventors

• Jodet Norman Bruno Andre
• Gonzalez Jeremy Paul Francisco
• Mardjono Jacky Novi
• Dubourg Arnaud
• Fotsing Edith-Roland
• Ross Annie
• Therriault Daniel

Classifications

• F05D2260/96

  Preventing, counteracting or reducing vibration or noise · CPC title

• B33Y30/00

  Apparatus for additive manufacturing; Details thereof or accessories therefor · CPC title

• F05D2230/30

  with deposition of material · CPC title

• F01D11/122

  with erodable or abradable material (blades having cutting or grinding tips F01D5/20) · CPC title

• B29C70/326

  by rotating the mould around its axis of symmetry · CPC title