METHOD FOR THE ADDITIVE MANUFACTURE OF METALLIC COMPONENTS
20180178325 ยท 2018-06-28
Inventors
Cpc classification
B22F10/32
PERFORMING OPERATIONS; TRANSPORTING
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B23K15/0086
PERFORMING OPERATIONS; TRANSPORTING
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
B22F10/32
PERFORMING OPERATIONS; TRANSPORTING
B23K26/34
PERFORMING OPERATIONS; TRANSPORTING
B23K26/0861
PERFORMING OPERATIONS; TRANSPORTING
B22F10/25
PERFORMING OPERATIONS; TRANSPORTING
B22F10/25
PERFORMING OPERATIONS; TRANSPORTING
B23K15/002
PERFORMING OPERATIONS; TRANSPORTING
B33Y40/00
PERFORMING OPERATIONS; TRANSPORTING
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
B23K26/34
PERFORMING OPERATIONS; TRANSPORTING
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y40/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The invention relates to a method for the additive manufacture of three-dimensional metallic components (12), said components (12) being built layer-by-layer or section-by-section under vacuum conditions by fusing a metallic material with the component (12) at a machining point by means of a radiation source with a high energy density. In order to keep the energy applied to the machining point by the radiation itself relatively low, the metallic material is supplied in the form of a wire (28) which is preheated under vacuum conditions before reaching the machining point.
Claims
1. A method for the additive manufacture of three-dimensional metallic components (12), wherein the components (12) are built up in layers or sections under vacuum conditions by fusion of a metallic material with the component (12) at a processing location by means of a radiation source with high energy density, characterized in that the metallic material is supplied as a wire (28), wherein the wire is preheated under vacuum conditions before reaching the processing location.
2. The method as claimed in claim 1, characterized in that the wire is directly electrically preheated (resistance heating).
3. The method as claimed in claim 2, characterized in that the current for heating the wire (28) is conducted via the wire (28) and the workpiece.
4. The method as claimed in claim 3, characterized in that the wire is heated using direct current, wherein a negative polarity is applied to the wire (28) and a positive polarity is applied to the workpiece.
5. The method as claimed in claim 1, characterized in that the wire (28) is inductively preheated.
6. The method as claimed in claim 1, characterized in that the wire (28) is supplied through a vacuum leadthrough (32) into a vacuum chamber (14) in which the component (12) is additively manufactured.
7. The method as claimed in claim 6, characterized in that the wire (28) is supplied preheated into the vacuum chamber (14).
8. The method as claimed in claim 1, characterized in that the fusion energy is imparted by means of a laser beam (2).
9. The method as claimed in claim 8, characterized in that the laser beam (22) is introduced through a window (24) into the vacuum chamber (14).
10. The method as claimed in claim 9, characterized in that the window is purged with a gas.
11. The method as claimed in claim 1, characterized in that the workpiece is moved relative to the processing location, which is configured so as to be static.
12. The method as claimed in claim 1, characterized in that the wire (28) is heated to a temperature which lies between a temperature slightly below or slightly above the solidus temperature of the metallic material.
Description
[0021] Two exemplary embodiments of the invention will be discussed in more detail below on the basis of the appended drawings. In the drawings:
[0022]
[0023]
[0024]
[0025] A vacuum pump 18 evacuates the interior of the vacuum chamber 14 to the pressure values that are conventional in the field of thermal processing methods in a vacuum.
[0026] The introduction of energy required for the fusion of supplied metallic material in the applied material layer 16 is provided by means of a laser 20 which is arranged outside the vacuum chamber 14. The laser beam 22 is conducted through an entrance window 24 in the wall of the vacuum chamber 14 to a processing location on the component 12, at which a melt bath 26 forms owing to the high light power of the laser 20. Aeration (not illustrated in any more detail) of the inner side of the entrance window 24 prevents metal vapors from being able to precipitate there as condensate.
[0027] The metallic material is supplied as a wire 28, by means of a wire supply 30 which is illustrated in highly simplified form, to the processing location at the melt bath 26. Here, the wire 28 is supplied through a vacuum leadthrough 32 in the wall of the vacuum chamber 14 into the interior of the vacuum chamber, and is advanced for example by means of driven friction rollers.
[0028] In the exemplary embodiment shown, the wire 28, which may possibly have already been pre-heated outside the vacuum chamber 14, is heated further by means of a resistance heater, such that, already before it reaches the processing location, said wire reaches a temperature in the region of the solidus point of the metallic material. In the exemplary embodiment shown in
[0029] As a result of the additional heating of the wire 28 before it reaches the melt bath 26, the light power of the laser 20 can be set to be considerably lower than would be necessary without electric preheating of the wire 28. This has the advantage that the melt bar 26 extends to a lesser depth into the workpiece, such that previously applied layers on the workpiece 12 are impaired to a lesser extent by the application of the further layer. Aside from the advantage of more precise execution of the method, the laser 20 can also be dimensioned to be smaller, which has a positive effect on the overall costs of the device 10.
[0030] As the wire is being supplied, under the action of the electric heating and the laser beam, the wire is fused in the melt bath 26 and is applied as a material layer 16 to the workpiece 12. During the process, the component 12 is moved in a processing direction, such that a line-by-line construction is realized. It is basically also possible for movements to be performed simultaneously in multiple corner directions, but in general, a line-by-line construction of the material will be desired. If a discontinuous form of the material layer is desired at a particular location, because it is sought for no material to be present there on the finished component owing to the construction, the supply of the wire is interrupted, the laser beam is deactivated, and/or the movement speed of the component 12 is briefly greatly increased in said regions.
[0031]