Irradiation in generative fabrication

Patent metadata

Field	Value
Publication number	US-9636769-B2
Application number	US-201414567851-A
Country	US
Kind code	B2
Filing date	Dec 11, 2014
Priority date	Dec 17, 2013
Publication date	May 2, 2017
Grant date	May 2, 2017

Abstract

The present invention relates to a method for the generative production of components, particularly of single-crystalline or directionally-solidified components, particularly for the production of components for turbomachines, in which the component is constructed in layers on a substrate or a previously produced part of the component ( 3 ), wherein a construction in layers takes place by melting of powder material in layers with a high-energy beam ( 14 ) and solidification of the powder melt ( 16 ) takes place, wherein the high-energy beam has a beam cross section ( 19 ) in the area of its impingement on the powder material that is altered in comparison to a circular or other symmetrical cross section and/or the beam energy is distributed non-uniformly, in particular asymmetrically or eccentrically, over the beam section.

First claim

The invention claimed is:

1. A method for the generative production of components for turbomachines, in which the component is constructed in layers on a substrate or a previously produced part of the component ( 3 ), wherein a construction in layers results by melting of powder material in layers with a high-energy beam ( 13 ) and solidification of the powder melt ( 16 ),
wherein
the high-energy beam has a beam cross section ( 19 ) in the area of its impingement on the powder material that is altered in comparison to a circular or other symmetrical cross section and/or the beam energy is distributed, over the beam cross section, in a shape that is selected from the group consisting of non-uniform, asymmetrical and eccentric, and that
the powder material, after melting has occurred, is irradiated a second time, at a time delay to the melting, by a high-energy beam with an energy input into the powder material that is altered in comparison to the melting, and
wherein the solidification of the powder melt occurs epitaxially.

2. The method according to claim 1 ,
wherein
at least two high-energy beams ( 13 ) are irradiated on the powder material in temporal succession at spatially adjacent sites of the component or a part thereof.

3. The method according to claim 1 ,
wherein
the second irradiation or additional irradiations with a high-energy beam ( 13 ) occurs or occur at time points when the melted powder material has not yet fully solidified.

4. The method according to claim 1 , further comprising the step of:
preheating the powder material by radiant heating or induction heating, prior to the melting.

5. The method according to claim 1 ,
wherein
the high-energy beam ( 13 ) is a laser or electron beam.

6. The method according to claim 1 ,
wherein
at least one high-energy beam is directed along movement tracks ( 20 , 20 ′) over the powder material arranged in a powder bed.

7. The method according to claim 6 ,
wherein
the tracks of movement ( 20 , 20 ′) of the high-energy beams with beam cross section ( 19 ) that deviates from circular or otherwise symmetrical cross section and/or non-uniform and/or asymmetrical and/or eccentric energy distribution over the beam cross section, and/or the movement tracks for which the high-energy beam impinges for the first time on the powder material at least partially for melting of the powder material overlap one another.

8. The method according to claim 1 ,
wherein
a computer-assisted simulation of the energy input and the local and/or temporal temperature distribution in the powder material and/or the already produced component ( 3 ) takes place.

9. The method according to claim 1 ,
wherein
a computer-assisted simulation of the phase state of the powder material and/or the direction of solidification and/or the rate of solidification of the melted powder material takes place.

10. The method according to claim 8 ,
wherein
by a computer-assisted simulation, one or more parameters for the irradiation with high-energy beams is or are determined, wherein said parameters are chosen from the group that includes the power of the high-energy beam or beams, the number of high-energy beams, the shape of the beam cross section of the beam or beams, the non-uniform, asymmetric or eccentric energy distribution of the high-energy beam or beams over the beam cross section, the time interval of a second irradiation or of additional irradiations of the powder material, the geometry of the tracks of the high-energy beams, and the track separation of the movement tracks of the high-energy beams.

11. The method according to claim 10 ,
wherein
by a computer-assisted simulation, the parameters for irradiation with high-energy beams are determined so that a desired structure can be created.

12. The method according to claim 1 ,
wherein
the method is used for the production of single-crystalline or directionally solidified components.

13. The method according to claim 9 , wherein
by a computer-assisted simulation, one or more parameters for the irradiation with high-energy beams is or are determined, wherein said parameters are chosen from the group that includes the power of the high-energy beam or beams, the number of high-energy beams, the shape of the beam cross section of the beam or beams, the non-uniform, asymmetric or eccentric energy distribution of the high-energy beam or beams over the beam cross section, the time interval of a second irradiation or of additional irradiations of the powder material, the geometry of the tracks of the high-energy beams, and the track separation of the movement tracks of the high-energy beams.

Assignees

• MTU Aero Engines AG

Inventors

• Goehler Thomas
• Hess Thomas
• Maiwald-Immer Tobias

Classifications

• C30B13/24 Primary

  using electromagnetic waves · CPC title

• B23K15/0006 Primary

  specially adapted for particular articles or work · CPC title

• B22F12/45

  Two or more · CPC title

• B22F12/17

  to heat the build chamber or platform · CPC title

• B22F12/13

  to preheat the material · CPC title