PRODUCTION METHOD FOR A SHAPING TOOL COMPONENT OF A PRESS HARDENING TOOL
20180354036 ยท 2018-12-13
Assignee
Inventors
Cpc classification
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B22D27/04
PERFORMING OPERATIONS; TRANSPORTING
B22F5/10
PERFORMING OPERATIONS; TRANSPORTING
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
B22D19/06
PERFORMING OPERATIONS; TRANSPORTING
B22F5/10
PERFORMING OPERATIONS; TRANSPORTING
B22F10/28
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
B22D25/02
PERFORMING OPERATIONS; TRANSPORTING
B22F2005/002
PERFORMING OPERATIONS; TRANSPORTING
B22F3/24
PERFORMING OPERATIONS; TRANSPORTING
B22F10/47
PERFORMING OPERATIONS; TRANSPORTING
International classification
B22F5/00
PERFORMING OPERATIONS; TRANSPORTING
B22D27/04
PERFORMING OPERATIONS; TRANSPORTING
B22D25/02
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The present disclosure provides a production method for a shaping tool component of a press hardening tool that includes producing a preform by an additive production method from metal material. The preform having an outer wall, which at least partially corresponds to a shaping operating face of the tool component. The preform further includes at least one channel wall of a cooling channel adjacent to the outer wall and at least one recess which is at least for the most part further away from the outer wall than the channel wall. After the preform is produced, the at least one recess is filled with liquid metal, which subsequently hardens and forms a portion of the tool component.
Claims
1. A production method for a shaping tool component of a press hardening tool, the production method comprising: producing a preform from metal material by an additive production method, the preform comprising: an outer wall at least partially corresponding to a shaping operating face of the tool component; at least one channel wall of a cooling channel adjacent to the outer wall; and at least one recess, wherein at least half of the recess is located further away from the outer wall than the at least one channel wall; and filling the at least one recess with liquid metal, wherein the liquid metal subsequently hardens and forms a portion of the tool component.
2. The production method as claimed in claim 1, wherein the additive production method is selective laser melting.
3. The production method as claimed in claim 1, wherein the at least one recess includes an opening at a side remote from the operating face, wherein the liquid metal is poured in through the opening.
4. The production method as claimed in claim 1, wherein a surface of the outer wall is reprocessed by erosive processing after the surface has been produced.
5. The production method as claimed in claim 4, wherein the reprocessing operation is carried out after filling the at least one recess with liquid metal and hardening the liquid metal.
6. The production method as claimed in claim 1 further comprising producing support structures configured to connect a base portion of the press hardening tool to the tool component.
7. The production method as claimed in claim 6, wherein the support structures are produced by the additive production method.
8. The production method as claimed in claim 1, wherein the additive production method is electron beam melting or selective laser sintering.
9. A production method for a shaping tool component of a press hardening tool, the production method comprising: producing a preform made of a metal material by an additive production method, the preform comprising: an outer wall corresponding to an operating face of the tool component; a plurality of channel walls, each channel wall defining a cooling channel that merges into the outer wall; and at least one recess partially enclosed by the outer wall and defining an opening; producing at least one support structure within the at least one recess of the preform by the additive production method; and pouring liquid metal through the opening defined by the recess to fill at least a portion of the recess with liquid metal, wherein the liquid metal subsequently hardens and forms a portion of the tool component.
10. The production method as claimed in claim 9 further comprising removing the at least one support structure before pouring the liquid metal into the recess of the preform.
11. The production method as claimed in claim 9, wherein the additive production method is selective laser melting.
12. The production method as claimed in claim 9, wherein the additive production method is electron beam melting or selective laser sintering.
13. The production method as claimed in claim 9, wherein a surface of the outer wall is reprocessed by an erosive process after the surface has been produced.
14. The production method as claimed in claim 13, wherein the reprocessing is carried out after filling the at least one recess with liquid metal and hardening the liquid metal.
15. The production method as claimed in claim 9 further comprising placing the preform in a container containing a temperature-resistant material before pouring the liquid metal into the recess of the preform.
16. The production method as claimed in claim 15, wherein the preform is placed in the container upside down and embedded into the temperature-resistant material.
17. The production method as claimed in claim 15, wherein the temperature-resistant material is sand.
18. The production method as claimed in claim 15 further comprising removing the preform from the container after the liquid metal hardens and cools.
19. The production method as claimed in claim 9, wherein the preform further comprises at least one continuation, the continuation defining a through-opening.
20. The production method as claimed in claim 9, wherein the outer wall and the channel wall defines the cooling channel.
Description
DRAWINGS
[0030] In order that the disclosure may be well understood, there will now be described various forms thereof, given by way of example, reference being made to the accompanying drawings, in which:
[0031]
[0032]
[0033]
[0034]
[0035]
[0036]
[0037] The drawings described herein are for illustration purposes only and are not intended to limit the scope of the present disclosure in any way.
DETAILED DESCRIPTION
[0038] The following description is merely exemplary in nature and is not intended to limit the present disclosure, application, or uses. It should be understood that throughout the drawings, corresponding reference numerals indicate like or corresponding parts and features.
[0039]
[0040] In order to produce the tool component 1, a preform 6 is first produced within a production installation 20 which is illustrated in
[0041] When the application device 23 has applied a layer of metal powder 28, using a laser beam 26, a portion of the powder 28 is selectively melted, whereby a layer of the preform 6 which is intended to be produced is produced. The laser beam 26 is produced by a laser 25 and directed by a pivotable mirror 27 onto a provided coordinate location within the surface of the metal powder 28. The activation of the laser 25 and the control of the mirror 27 are carried out in this instance in a computer-controlled manner in accordance with predetermined CAM data of the preform 6. The base plate 21 is in the present example operated in an intermittent manner, that is to say, it is stopped whilst a powder layer is applied and partially melted and subsequently moved downward by a distance which corresponds to the provided layer thickness.
[0042] The preform 6 produced has an outer wall 7 which substantially corresponds to the path of the operating face 2 and the path of the side walls 3. Furthermore, in a state adjacent to the outer wall 7 there are produced a series of channel walls 8 which in this instance merge into the outer wall 7. Each channel wall 8 defines (together with the outer wall 7) a cooling channel 9. As can be clearly seen in
[0043] As a result of the action of the laser beam 26, the preform 6 produced is heated powerfully, although the molten powder 28 hardens again when the action of the laser beam 26 is ended. An effective heat discharge is not possible either to the surrounding powder 28 or to the surrounding atmosphere (which may, for example, comprise inert gas). Therefore, in order to inhibit thermally related deformations of the preform 6, it is advantageous to support the heat discharge to the base plate 21 by support structures 10 which are connected to the base plate 21 being produced. These support structures 10 on the one hand stabilize the preform 6, but above all they are used for better heat discharge into the base plate 21. The support structures 10 may further serve to space apart the usable portion of the preform 6 from the base plate 21 so that, after the production is complete, the preform 6 can be separated without the usable portion being damaged. Furthermore, it may be advantageous to use the support structures 10 at locations or surfaces which have an angle of less than approximately 45 with respect to the base plate 21. In
[0044]
[0045] The material thickness which is thus lacking in the preform 6 is, as shown in
[0046] Optionally, as illustrated in
[0047]
[0048] The description of the disclosure is merely exemplary in nature and, thus, variations that do not depart from the substance of the disclosure are intended to be within the scope of the disclosure. Such variations are not to be regarded as a departure from the spirit and scope of the disclosure.