Method for manufacturing a line component
10441989 · 2019-10-15
Assignee
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
B24B1/00
PERFORMING OPERATIONS; TRANSPORTING
B22F5/10
PERFORMING OPERATIONS; TRANSPORTING
F16L41/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B21D26/035
PERFORMING OPERATIONS; TRANSPORTING
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
B22F3/24
PERFORMING OPERATIONS; TRANSPORTING
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 method comprising: additively fabricating a line component that includes a line element and a line branching by: piling, in a predetermined region, a particle-shaped material on a base layer of the line component to be fabricated; and heating up the piled particle-shaped material by means of a heat source such that particles of the particle-shaped material combine with each other and/or with the base layer within predetermined dimensions; incorporating a notch on an inside of the line element, the notch serving to relieve a tension in a loaded state of the line component or the line element; guiding a particle-filled gas stream through an interior of the line component in order to smooth an inside of the line component; and/or pressurizing the line component to produce a plastic deformation on an inner surface of the line component, wherein the line element is configured to conduct a fluid from a first opening to a second opening, wherein the line branching connected with the line element is configured to conduct the fluid to a third opening, and wherein an outer region of the line component is designed load-compliant by a numerical optimization program to include a multitude of irregular topological structures in the outer region.
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.
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 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 branching is connected with the line element, and wherein the line branching 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 the numerical optimization program so as to include a multitude of irregular topological structures in the 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, wherein the line branching is connected with the line element, wherein the line branching 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, further comprising supplying the particle-filled gas stream in a region of a lowest flow velocity of the line component.
14. The method according to claim 1, further comprising changing the flow direction of the particle-filled 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, further comprising performing the pressurization by introducing a medium into the line component.
17. The method according to claim 4, wherein the notch substantially is formed such that it has a shape obtained by pressing a cylinder body into the inside of the line element.
18. 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 45 with respect to a middle of a line branching opening in the cross-section area.
19. 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 15 with respect to a middle of a line branching opening in the cross-section area.
20. The method according to claim 1, further comprising changing the introduction direction of the gas stream into the output direction of the gas stream.
Description
(1) Further particulars and details of the invention will be described with reference to the drawings, in which:
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(15) 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 cp. As an alternative reference point instead of the middle of the notch, there can also be used the deepest point of the notch 3 in the cross-sectional views. This angle 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.
(16) 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.
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(18) 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.
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(20) The left representation shows the conventionally formed lined component comprising the line element 1 and the line branching 2. The right presentation of
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(22) 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 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 of 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.
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(24) 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.
(25) 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.
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(28) The broken line 50 indicates the original course of the inner region of the line component 10. Reference numeral 51 designates the inner region after application of the method step described above. Preferably, the pressurization of the fluid-carrying line component 10 is effected by means of a medium such that the material load on the surface of the component facing the pressure lies above the yield point of the material. Furthermore preferably, the pressure range is to be chosen such that the surface of the component facing away from the pressure side is deformed largely linear-elastically. Residual compressive stresses thereby can be generated particularly effectively in additively fabricated line components.
(29) 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.