Additive manufacturing of a component made from a metal matrix composite

Patent metadata

Field	Value
Publication number	US-10286476-B2
Application number	US-201615239489-A
Country	US
Kind code	B2
Filing date	Aug 17, 2016
Priority date	Aug 18, 2015
Publication date	May 14, 2019
Grant date	May 14, 2019

Abstract

The embodiments relate to a method for additive manufacturing of a component made from a metal matrix composite for a vehicle. In a step of the method, a plurality of elongated filaments is provided. In another step, metallic powder is provided. In a further step, the metal matrix composite component is additively manufactured by melting the metallic powder.

First claim

What is claimed is:

1. A method for additively manufacturing of a component made from a metal matrix composite for a vehicle, the method comprising the steps of:
providing metal powder as a powder bed in a manufacturing apparatus;
disposing a plurality of elongated filaments on the powder bed, such that the elongated filaments are elongated along a moving direction; and
melting the metal powder, with a laser beam that scans the metal powder in a scanning direction, while moving the elongated filaments along the moving direction, wherein the moving direction is transverse to the scanning direction, to form the metal matrix component.

2. The method of claim 1 , wherein at least one of the elongated filaments is a metal filament, a metal-coated non-metallic filament, a semi-metallic filament or a polymer fiber.

3. The method of claim 1 ,
wherein the metal powder is scanned by the laser beam in the scanning direction to achieve melting and to fuse at least a part of said elongated filaments with each other and thereby to selectively melt the metal powder into a desired shape.

4. The method of claim 3 ,
wherein the powder bed is disposed within a manufacturing device;
wherein the manufacturing device comprises at least one opening suitable for receiving the elongated filaments; and
wherein the elongated filaments are moved along the moving direction transverse to the scanning direction, whereby a desired length of the component is formed.

5. The method of claim 4 , wherein a chemically inert atmosphere is provided within the manufacturing device.

6. The method of claim 1 , wherein the elongated filaments have a round or polygonal cross-section.

7. A manufacturing apparatus for additive manufacturing of components made from a metal matrix composite with elongated filaments, comprising:
a powder bed comprising a metallic powder;
a feed to dispose a plurality of elongated filaments on the powder bed, such that the elongated filaments are elongated along a moving direction; and
a heat source comprising a movable laser beam having a scanning direction;
wherein the heat source is configured to melt the metal powder with the laser beam by scanning the metallic powder in the scanning direction while the elongated filaments are moved along the moving direction, wherein the moving direction is transverse to the scanning direction, to selectively fuse the metallic powder with the elongated filaments into a desired shape.

8. The manufacturing apparatus according to claim 7 , wherein the manufacturing apparatus comprises at least one opening which is suitable for receiving the elongated filaments.

9. The manufacturing apparatus according to claim 7 , further comprising:
a manufacturing chamber, in which the metallic powder is melted and in which there is a chemically inert atmosphere.

Assignees

• Airbus Operations Gmbh

Inventors

• Wendt Christiane
• Wienberg Thorsten Michael

Classifications

• B22F12/47

  parallel to the deposition plane · CPC title

• B22F10/32

  of the atmosphere, e.g. composition or pressure in a building chamber · CPC title

• B22F10/28

  Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title

• Y02P10/295

  Cross-Sectional Technologies · mapped topic

• B22F3/1055

  Operations & Transport · mapped topic