FIBER-COMPOSITE SANDWICH MATERIAL CONTAINING SHAPE-MEMORY ALLOYS
20190210320 ยท 2019-07-11
Inventors
Cpc classification
B29C70/46
PERFORMING OPERATIONS; TRANSPORTING
B32B27/42
PERFORMING OPERATIONS; TRANSPORTING
B32B15/04
PERFORMING OPERATIONS; TRANSPORTING
B32B27/12
PERFORMING OPERATIONS; TRANSPORTING
B64C3/20
PERFORMING OPERATIONS; TRANSPORTING
B29C43/18
PERFORMING OPERATIONS; TRANSPORTING
B32B15/098
PERFORMING OPERATIONS; TRANSPORTING
B32B5/18
PERFORMING OPERATIONS; TRANSPORTING
B32B25/16
PERFORMING OPERATIONS; TRANSPORTING
B29C70/885
PERFORMING OPERATIONS; TRANSPORTING
B29C43/20
PERFORMING OPERATIONS; TRANSPORTING
B32B27/30
PERFORMING OPERATIONS; TRANSPORTING
B64C9/00
PERFORMING OPERATIONS; TRANSPORTING
B29D99/0021
PERFORMING OPERATIONS; TRANSPORTING
B32B15/082
PERFORMING OPERATIONS; TRANSPORTING
Y10S428/913
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
B32B15/02
PERFORMING OPERATIONS; TRANSPORTING
Y02T50/40
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
B29K2305/00
PERFORMING OPERATIONS; TRANSPORTING
B64D11/06
PERFORMING OPERATIONS; TRANSPORTING
B32B2250/40
PERFORMING OPERATIONS; TRANSPORTING
B32B25/10
PERFORMING OPERATIONS; TRANSPORTING
B29C70/12
PERFORMING OPERATIONS; TRANSPORTING
International classification
B32B5/02
PERFORMING OPERATIONS; TRANSPORTING
B29C70/34
PERFORMING OPERATIONS; TRANSPORTING
B32B27/12
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A sandwich component including at least two cover layers and one core layer containing wires including shape-memory metal. A process for producing the sandwich component is also disclosed.
Claims
1. A sandwich component comprising at least two cover layers and one core layer containing wires comprising shape-memory metal.
2. The sandwich component according to claim 1, wherein the wires comprising shape-memory metal in the core layer are arranged substantially in parallel to one another.
3. The sandwich component according to claim 1, wherein the wires comprising shape-memory metal in the core layer are arranged in relation to one another substantially in a form of a woven fabric.
4. The sandwich component according to claim 1, wherein the wires comprising shape-memory metal in the core layer are heatable.
5. The sandwich component according to claim 1, wherein the cover layers comprises epoxy, vinyl ester, phenol or unsaturated polyester resin.
6. The sandwich component according to claim 1, comprising an intermediate layer comprising an elastomer.
7. The sandwich component according to claim 6, wherein the intermediate layer comprises EPDM, BR or EVA.
8. The sandwich component according to claim 6, wherein the intermediate layer comprises EPDM, BR and EVA.
9. The sandwich component according to claim 6, wherein the intermediate layer comprises elastomer in a form of calendered films.
10. The sandwich component according to claim 6, wherein the intermediate layer comprises elastomer in a form of a plurality of calendered films, between which the wires comprising shape-memory metal are disposed.
11. The sandwich component according to claim 1, wherein the wires comprising shape-memory metal are electrically heatable.
12. The sandwich component according to claim 1, wherein the wires comprising shape-memory metal are electrically heatable by application of an electric voltage to the wires themselves.
13. The sandwich component according to claim 1, wherein the wires comprising shape-memory metal are heatable by induction.
14. The sandwich component according to claim 1, wherein the wires comprising shape-memory metal are temperature-adjustable by a cooling device.
15. A wing tip of an aircraft that comprises a sandwich component according to claim 1.
16. An aileron, elevator or rudder of an aircraft that comprises a sandwich component according to claim 1.
17. An air channel for an aircraft that comprises a sandwich component according to claim 1.
18. A seat, recliner or bed for an aircraft that comprises a sandwich component according to claim 1.
19. A wing of an aircraft that comprises a sandwich component according to claim 1.
20. An air flap or ventilation nozzle of an aircraft that comprises a sandwich component according to claim 1.
21. A horizontal stabilizer or vertical stabilizer of an aircraft that comprises a sandwich component according to claim 1.
22. A sandwich component comprising at least two cover layers and one core layer containing wires comprising shape-memory metal, obtainable by a process comprising: providing a press device having a first mold part and a second mold part which can be moved relative to one another between a closed position, in which they enclose a cavity, and an open position, in which the cavity is open to an environment, wherein the first mold part and/or the second mold part are heatable; providing a semi-finished sandwich product having a first cover-layer semi-finished ply comprising a long-fiber-reinforced press compound with thermoset matrix, a second cover-layer semi-finished ply comprising a long-fiber-reinforced press compound with thermoset matrix, and, between them, a core-layer semi-finished ply; in the open position of the press device, inserting the semi-finished sandwich product into the cavity; moving the first and the second mold part relative to one another into the closed position; and pressing together the first and the second mold part, wherein the semi-finished sandwich product experiences a certain press pressure, and heating the first and/or the second mold part, wherein the semi-finished sandwich product experiences a certain processing temperature, wherein the press device comprises a spacer, which, in the closed position, defines a minimum distance between the first and the second mold part and thus sets the minimum dimensions of the cavity, and wherein the spacer is adjusted such that the press pressure in the closed position is between a minimum processing pressure of the first and/or the second cover-layer semi-finished ply and a maximum permissible pressure limit for the core-layer semi-finished ply.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0018]
[0019]
DETAILED DESCRIPTION
[0020]
[0021] As shown in
[0022] Thereafter, as shown in
[0023] As depicted in
[0024] In order not to destroy the foam of the core-layer semi-finished ply 7 owing to the press pressure, the press device 11 comprises a spacer 21 which, in the closed position 17, defines the minimum distance between the first and the second mold part 13, 15 and thus sets the minimum dimensions of the cavity 9 and therefore the maximum press pressure. The spacer 21 is, depending on the geometry of the cavity 9 and on the materials of the cover-layer semi-finished plies 3, 5 and of the core-layer semi-finished ply 7, adjusted such that the press pressure in the closed position 17, when the spacer 21 limits the distance between the first and the second mold part 13, 15 to the minimum distance, is between a minimum processing pressure of the first and the second cover-layer semi-finished ply 3, 5 and a maximum permissible pressure limit for the core-layer semi-finished ply 7. In the present embodiment, the spacer 21 is designed as a stop element 22, which is provided on the second mold part 15 to the side of the cavity 9 and stops on the first mold part 13 upon a movement into the closed position 17 in order to thus set the minimum distance between the first and the second mold part 13, 15. Further provided is a control device 23 which controls the movement of the second mold part 15 onto the first mold part 13 into the closed position 17 or the force with which the second mold part 15 presses onto the first mold part 13 such that the pressure of the first and the second mold part 13, 15 on the semi-finished sandwich product 1 is only very slowly increased before the stopping of the stop element 22 and achievement of the press pressure.
[0025] As shown in
[0026]
[0027] While the disclosure herein has been illustrated and described in detail in the drawings and the preceding description, the intention is that such illustrations and descriptions are merely of an illustrative or exemplary nature and not of a limiting nature, and so the disclosure herein is not limited by the disclosed embodiments. Just the fact that certain features are mentioned in various dependent claims does not limit the subject matter of the disclosure herein. Combinations of the features can be advantageously used, too. The reference signs in the claims are not intended to limit the scope of the claims.
[0028] While at least one exemplary embodiment of the present invention(s) is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. This disclosure is intended to cover any adaptations or variations of the exemplary embodiment(s). In addition, in this disclosure, the terms comprise or comprising do not exclude other elements or steps, the terms a, an or one do not exclude a plural number, and the term or means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority.