METHOD FOR MANUFACTURING A LINE COMPONENT
20170014887 · 2017-01-19
Inventors
- Lothar Kroll (Dresden, DE)
- Frank Schubert (Marienberg, DE)
- Stefan Demmig (Chemnitz, DE)
- Sebastian Blümer (Chemnitz, DE)
- Alexander Altmann (Immenstadt, DE)
- Camille Kunzi (Ravensburg, DE)
- David Hölzler (Oberstaufen, DE)
- Gerhard Hummel (Bremen, DE)
Cpc classification
B22F2003/247
PERFORMING OPERATIONS; TRANSPORTING
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B22F10/28
PERFORMING OPERATIONS; TRANSPORTING
F16L41/021
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B22F5/10
PERFORMING OPERATIONS; TRANSPORTING
B22F2003/245
PERFORMING OPERATIONS; TRANSPORTING
B22F3/04
PERFORMING OPERATIONS; TRANSPORTING
B21D26/035
PERFORMING OPERATIONS; TRANSPORTING
B22F10/28
PERFORMING OPERATIONS; TRANSPORTING
B22F2998/10
PERFORMING OPERATIONS; TRANSPORTING
B22F2003/245
PERFORMING OPERATIONS; TRANSPORTING
B22F2998/10
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B22F3/24
PERFORMING OPERATIONS; TRANSPORTING
Y02P10/25
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B22F3/04
PERFORMING OPERATIONS; TRANSPORTING
B22F2005/005
PERFORMING OPERATIONS; TRANSPORTING
International classification
B21D26/035
PERFORMING OPERATIONS; TRANSPORTING
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B22F3/24
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
F16L41/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
According to the manufacturing method of the invention the line component. In particular an additively fabricated line component, comprises a line element for conducting a fluid from a first opening to a second opening, and a line branching connected with the line element for conducting the fluid to a third opening, wherein an outer region of the line component is designed load-compliant by means of a numerical optimization program and thereby includes a multitude of irregular topological structures in its outer region. In the manufacturing method of the line component a notch is incorporated on the inside of the line element, which serves to relieve a tension in a highly loaded state of the line component or the line element, a particle-filled gas stream is guided through the interior of the line component, in order to smooth the inside of the line component and/or the line component is subjected to a pressurization, in order to produce a plastic deformation on an inner surface of the line component.
Claims
1. A method for manufacturing a line component for conducting a fluid, the line component comprising: a line element for conducting a fluid from a first opening to a second opening, and a line branching connected with the line element for conducting the fluid to a third opening, wherein an outer region of the line component is designed load-compliant by means of a numerical optimization program and thereby includes a multitude of irregular topological structures in its outer region, wherein in the manufacturing method: a notch is incorporated on the inside of the line element, which serves to relieve a tension in a highly loaded state of the line component or the line element, a particle-filled gas stream is guided through the interior of the line component, in order to smooth the inside of the line component, and/or the line component is subjected to a pressurization, in order to produce a plastic deformation on an inner surface of the line component wherein the line component is additively fabricated in that in a predetermined region a particle-shaped material is piled up on a base layer of the line component to be fabricated, and the particle-shaped material piled up is heated by means of a heat source such that the particles of the material combine with each other and/or with the base layer within predetermined dimensions.
2. The method according to claim 1, wherein the notch substantially extends along a flow direction of the line element and/or substantially along the longitudinal direction of the line element.
3. The method according to claim 1, wherein the notch is formed to extend substantially linearly.
4. The method according to claim 1, wherein the notch substantially is formed such that it has a shape which corresponds to a part of an outer cylinder surface, preferably a shape which is obtained when pressing a cylinder body into the inside of the line element.
5. The method according to claim 1, wherein the notch partly or entirely is arranged in an inner circumferential region of the line element, in which the line branching from the line element also is located.
6. The method according to claim 1, wherein the notch wholly or partly is arranged in a region adjoining the line branching, which with respect to the geometrical center of gravity of the inner cross-sectional area of the line element includes an angle equal to or less than 75, preferably an angle equal to or less than 45, more preferably an angle equal to or less than 15, with respect to a middle of a line branching opening in the cross-section area.
7. The method according to claim 1, wherein the outer region is an outer circumferential region.
8. The method according to claim 1, wherein the line component comprises a line branching connected with a line element, which branches off from a connecting region of the line element, and the irregular topological structures appear in the outer circumferential region of the line element, which coincides with the connecting region.
9. The method according to claim 1, wherein an inner region of the line component is designed load-compliant by means of a numerical optimization program and thereby includes a multitude of irregular topological structures in its inner region.
10. The method according to claim 9, wherein the inner region is an inner circumferential region.
11. The method according to claim 10, furthermore comprising a line branching connected with a line element, which branches off from a connecting region of the line element, wherein the irregular topological structures appear in the inner circumferential region of the line element, which coincides with the outer connecting region of line branching and line element.
12. The method according to claim 1, wherein the particles of the gas stream have an abrasive and/or compacting effect.
13. The method according to claim 1, wherein the particle-filled gas stream is supplied in a region of the lowest flow velocity of the line component.
14. The method according to claim 1, wherein the flow direction of the particle-filled gas stream is changed, preferably the introduction direction of the gas stream is changed into the output direction of the gas stream.
15. The method according to claim 1, wherein on an inner surface of the line component the pressurization lies above the yield point of the material of the line component.
16. The method according to claim 15, wherein the pressurization is effected by introducing a medium into the line component.
Description
[0037] Further particulars and details of the invention will be described with reference to the drawings, in which:
[0038]
[0039]
[0040]
[0041]
[0042] of irregular topological structures in its outer region,
[0043]
[0044]
[0045]
[0046]
[0047]
[0048] not required that the notch 3 has the shape of a cylinder divided along its axis rotation. This is merely one of several possible variants.
[0049]
[0050]
[0051] For definition of a reference straight line 33, two points are fixed in the cross-sectional view. The one is the geometrical center of gravity 31 of the inner cross-sectional area of the line element 1 without taking account of the opening for the line branching. The other one is a center 32 between the two edge regions of the line element 1 as shown in the cross-sectional view, which define the region of transition to the line branching. In the Figure, the reference straight line 33 accordingly extends proceeding from the middle 31 of the circular inner cross-section of the line element 1 in direction of the line branching 2, so that the opening area of the line element is divided approximately centrally for the branching. Proceeding from the geometrical center of gravity 31 of the inner cross-sectional area, a connecting straight line 34, which extends from the middle of the notch 3 to the geometrical center of gravity 31, includes an angle . As an alternative reference point instead of the middle of the notch, there can also the deepest point of the notch 3 in the cross-sectional view. This angle is advantageously should be 75, preferably 45, and more preferably 15. The closer the notch 3 is positioned with respect to the line branching 2, the better can occurring forces be reduced in the case of a pressure load of the line component 10.
[0052] The middle of the cross-sectional area of the line element in the case of an irregular shape here is understood to be the geometrical center of gravity of the cross-sectional area. In the illustrated example of a substantially circular cross-sectional area of the line element 1 this is the circle center which lies in the axis of rotation of a basic cylindrical construction.
[0053]
[0054] It can be seen in the Figure that the topological structures 4 of the line element 1 are present only in an outer circumferential region which coincides with the connecting region with the line branching 2. This means that the topological structures 4 in particular are arranged in the vicinity of a branching area from the line element 1. The external shape of the line component 10 thereby can be designed load-compliant. This procedure in particular is advantageous when the inner structures are subject to strong geometrical limitations and allow only minor topological modifications.
[0055]
[0056] The left representation shows the conventionally forme line component comprising the line element 1 and the line branching 2. The rig representation of
[0057]
[0058] It is advantageous when the flow direction of the particle-filled gas stream 6 can be varied. This means that the direction of introduction of the gas stream 6 is changed, so that the opening into which the particle-filled gas stream is introduced now is the opening in which the particle-filled gas stream is blown out. As the particles 61 chiefly collide with other areas of the inner region depending on the direction introduction into the line component 10, this results in a better smoothing of the inner region and an even better continuous-use property of the line component 10.
[0059]
[0060] What is advantageous is the introduction of the particle-filled gas stream 6 into the line component in a region of the lowest flow velocity. In the Figure, the gas stream 6 hence preferably is introduced through one of the two openings of the line element 1, as the cross-sectional area of the line element 1 in this region is greater than in the region of the opening of the line branching 2.
[0061] A further method step, which serves to improve the continuous-use property of the line component, is the introduction of residual compressive stresses into the additively fabricated line component 10.
[0062]
[0063]
[0064] All embodiments described with reference to the Figures can be combined with each other with their respective features or with a selection of their respective features.