Device for shaping a workpiece
09987770 ยท 2018-06-05
Assignee
Inventors
Cpc classification
B29K2105/0854
PERFORMING OPERATIONS; TRANSPORTING
B29C33/00
PERFORMING OPERATIONS; TRANSPORTING
B29C2033/385
PERFORMING OPERATIONS; TRANSPORTING
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B32B7/02
PERFORMING OPERATIONS; TRANSPORTING
B29C33/38
PERFORMING OPERATIONS; TRANSPORTING
B32B2262/106
PERFORMING OPERATIONS; TRANSPORTING
B29C33/3842
PERFORMING OPERATIONS; TRANSPORTING
B32B5/12
PERFORMING OPERATIONS; TRANSPORTING
B29K2105/06
PERFORMING OPERATIONS; TRANSPORTING
B29C43/10
PERFORMING OPERATIONS; TRANSPORTING
International classification
B29C33/38
PERFORMING OPERATIONS; TRANSPORTING
B29C43/10
PERFORMING OPERATIONS; TRANSPORTING
B29C43/02
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A device for shaping a workpiece is provided. The device includes at least one first and one second component between which the workpiece to be shaped can be molded under the effect of heat. The design and/or the material properties of the first and/or the second component are selected such that the component's thermal expansion is different in different directions.
Claims
1. A device for shaping a workpiece, the device comprising: a first component; and a second component, wherein, the first and second components of the device are arranged concentrically to each other, wherein between the first and second component the workpiece is arranged for molding while heated, and wherein a configuration and material properties of the first or second components is selected such that thermal expansion of the first or second component is different in different directions, wherein the first or second component, which has a different thermal expansion in different directions, comprises at least one layer of carbon fiber reinforced plastic arranged on top of at least one layer of glass fiber reinforced plastic, wherein fibers of the at least one layer of carbon fiber reinforced plastic and fibers of the at least one layer of glass fiber reinforced plastic are not oriented parallel to each other, wherein the layer of carbon reinforced plastic and the layer of glass fiber reinforced plastic are arranged in such a manner relative to each other that the thermal expansion takes place in the circumferential direction and does not take place in the axial direction of the first component, and wherein the first or second component has a sandwich structure in which two layers of glass fiber reinforced plastic are arranged between two layers of carbon reinforced plastic.
2. The device according to claim 1, wherein the fibers of the at least one layer of carbon fiber reinforced plastic and the fibers of the at least one layer of glass fiber reinforced plastic are oriented to each other at an angle of approximately 90.
3. The device according to claim 1, wherein the first or second component, which has the different thermal expansion in different directions, comprises a second layer of carbon fiber reinforced plastic and a second layer of glass fiber reinforced plastic, wherein the at least one layer and the second layer of glass fiber are arranged adjacent to each other and between the at least one layer and the second layer of carbon fiber reinforced plastic, and wherein all layers are connected to each other in a firm bonding or form-locking manner.
4. The device according to claim 1, wherein the workpiece to be shaped is arranged between an outer circumferential surface of the first component and an inner circumferential surface of the second component, and wherein the configuration and the material properties of the first component are selected such that the thermal expansion of the first component is different in different directions and the second component has an identical thermal expansion in the different directions.
5. The device according to claim 4, wherein the first and second components are cylindrical.
6. The device according to claim 4, wherein, when heated, the first component has a thermal expansion in a circumferential direction.
7. The device according to claim 4, wherein, when heated, the first component has no thermal expansion in an axial direction.
8. The device according to claim 4, wherein the second component is a homogenous material or material composite.
9. The device according to claim 8, wherein, when heated, the second component has an approximately identical thermal expansion in a circumferential direction and an axial direction.
Description
BRIEF DESCRIPTION OF THE DRAWING FIGURES
(1) The invention is explained in more detail hereinafter by means of an exemplary embodiment. In the figures:
(2)
(3)
DETAILED DESCRIPTION
(4)
(5) At least one of the two components 11, 12 of a device according to the invention is configured such that due to the design and/or the material properties, the device has, in different directions, a different thermal expansion. In the exemplary embodiment described here, the first component 11 is configured such that, when heated, it has a thermal expansion in the circumferential direction 50, but no thermal expansion in the axial direction 51 (i.e. into the sheet plane).
(6) This property of the first component 11 is achieved in that the latter is formed from a plurality of layers 30, 31, 32, 33 from different composites, in particular fiber composites, with different thermal expansion coefficients. Here, the layers 30, 31, 32, 33 are arranged in such a manner relative to each other and/or connected to each other that the thermal expansion takes place in the desired circumferential direction 50 and does not take place in the undesired axial direction 51. Through the selection of the material, the arrangement of the layers relative to each other, and the type of connection of the layers, it is also possible, when heated, to determine the extent of the thermal expansion of the first component 11 in the circumferential direction.
(7) In one exemplary embodiment, the layer structure of the first component 11 is schematically illustrated in
(8) The layer structure for the first component 11 shown in
(9) Due to the suitable material selection and/or the design of the first component 11, under the influence of temperature, the result for the component is a thermal expansion in the circumferential direction 50. However, a temperature expansion in the axial direction 51 by the first component does not take place. Due to the fact that when heated, the second component 12 has an identical heat expansion in the circumferential and axial directions 50, 51, the workpiece 20 is molded between the first and the second component 11, 12, wherein a movement in the axial direction does not take place. Accordingly, the quality of the workpiece 20 with regard to its fiber orientation and dimensional stability can be improved over conventional devices.
(10) By using a device with directed heat expansion, it is possible during manufacturing to mold workpieces made from fiber reinforced composites in a certain direction. Thus, forces or relative displacements in another undesired direction can be avoided, which otherwise would cause an impairment of the workpiece to be manufactured, e.g. by fiber warpage. Moreover, a device according the invention has the advantage that manufacturing and demolding of certain geometries is possible which is not possible with conventional devices, the components of which have an identical thermal expansion in all directions.
(11) The device 10 according to the invention illustrated in
(12) Also, the sequence of layers of a plurality of layers from different fiber reinforced composites shown in
(13) The 90 orientation of the fibers of the layers consisting of carbon reinforced plastics shown in
(14) The foregoing disclosure has been set forth merely to illustrate the invention and is not intended to be limiting. Since modifications of the disclosed embodiments incorporating the spirit and substance of the invention may occur to persons skilled in the art, the invention should be construed to include everything within the scope of the appended claims and equivalents thereof.
REFERENCE LIST
(15) 10 Device 11 First component 12 Second component 13 Outer circumferential surface of the first component 14 Inner circumferential surface of the second component 20 Workpiece 30 Layer of a fiber reinforced composite 31 Layer of a fiber reinforced composite 32 Layer of a fiber reinforced composite 33 Layer of a fiber reinforced composite 34 Fibers of the layer 30 35 Fibers of the layer 31 36 Fibers of the layer 32 37 Fibers of the layer 33 50 Circumferential direction 51 Axial direction