METHOD FOR PRODUCING A COMPOSITE COMPONENT
20220203665 · 2022-06-30
Inventors
Cpc classification
B32B37/146
PERFORMING OPERATIONS; TRANSPORTING
B32B2309/72
PERFORMING OPERATIONS; TRANSPORTING
B32B2264/203
PERFORMING OPERATIONS; TRANSPORTING
B32B2305/72
PERFORMING OPERATIONS; TRANSPORTING
B32B37/144
PERFORMING OPERATIONS; TRANSPORTING
B29C44/445
PERFORMING OPERATIONS; TRANSPORTING
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B32B2038/0076
PERFORMING OPERATIONS; TRANSPORTING
B32B2305/30
PERFORMING OPERATIONS; TRANSPORTING
B32B37/02
PERFORMING OPERATIONS; TRANSPORTING
B32B2250/40
PERFORMING OPERATIONS; TRANSPORTING
B32B37/24
PERFORMING OPERATIONS; TRANSPORTING
B32B3/12
PERFORMING OPERATIONS; TRANSPORTING
International classification
B32B37/24
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method for producing a composite component including a bottom layer, cover layer and honeycomb structure, including applying the honeycomb structure to the bottom layer wherein honeycomb chambers are formed. Honeycomb chambers are filled in a reinforcement region with a granular material and granular material is removed from other honeycomb chambers wherein each honeycomb chamber is filled up to a granular-material filling height and honeycomb chambers outside the reinforcement region are free of granular material. The cover layer is applied to the honeycomb structure wherein the honeycomb chambers are closed. The composite component is heated so the granular material in the honeycomb chambers expands to fill it with granular material and the cover layer, the bottom layer, the honeycomb structure and the expanded granular material harden, the density of the expanded granular material in the honeycomb chambers filled with granular material being dependent on the granular-material filling height.
Claims
1. A method for producing a composite component which comprises a base layer, a cover layer and a honeycomb structure disposed between the base layer and the cover layer, the method comprising: applying the honeycomb structure to the base layer such that a multiplicity of honeycomb chambers which are open on a side pointing away from the base layer are formed; filling honeycomb chambers in a reinforcement region with granules during a filling procedure, wherein the granules at a processing temperature at which the filling is carried out do not adhere to the honeycomb structure, the base layer or one another; removing granules to be removed from honeycomb chambers such that, after the filling of honeycomb chambers and the removal of granules to be removed, each honeycomb chamber in the reinforcement region is filled with the granules up to a granule filling level and honeycomb chambers outside the reinforcement region are free of granules; applying the cover layer to the honeycomb structure such that the honeycomb chambers are closed; and heating the composite component to a first process temperature at which the granules filled into the honeycomb chambers expand to fill up the honeycomb chambers filled with granules, and subsequently to a second process temperature at which the cover layer, the base layer, the honeycomb structure as well as the expanded granules cure, wherein a density of the expanded granules in the honeycomb chambers filled with granules depends on the granule filling level.
2. The method of claim 1, wherein granules previously removed from honeycomb chambers are re-used for filling other honeycomb chambers.
3. The method of claim 2, wherein the granules previously removed from honeycomb chambers are cleaned prior to being re-used.
4. The method of claim 1, wherein honeycomb chambers in the reinforcement region during the filling procedure are first completely filled up with the granules, and the granules are subsequently removed from the completely filled-up honeycomb chambers until each honeycomb chamber in the reinforcement region is filled up to the granule filling level with the granules.
5. The method of claim 1, wherein an incorporation of the granules into the honeycomb chambers during the filling procedure is monitored such that the honeycomb chambers in the reinforcement region are filled only up to the granule filling level.
6. The method of claim 5, wherein an actual filling level of each honeycomb chamber is checked and, should the actual filling level in a honeycomb chamber exceed the granule filling level plus a tolerance, granules are removed from the respective honeycomb chamber.
7. The method of claim 1, wherein honeycomb chambers which are to be completely filled up are initially overfilled such that granules protrude from the honeycomb chambers to be completely filled up, and granules protruding from the honeycomb chambers to be completely filled up are subsequently removed by a scraper.
8. The method of claim 7, wherein the granules removed by the scraper are suctioned on the scraper.
9. The method of claim 1, wherein the reinforcement region has a plurality of sub-regions which are not necessarily connected to one another.
10. The method of claim 9, wherein different granule filling levels are provided for different sub-regions of the reinforcement region, wherein sub-regions having different granule filling levels have different densities after the expansion and curing of the granules.
11. The method of claim 1, wherein the base layer having the applied honeycomb structure is set in vibration during the filling procedure to distribute the granules uniformly in the individual honeycomb chambers.
12. The method of claim 1, wherein the honeycomb chambers filled with granules are ventilated when heating the composite component to the first process temperature.
13. The method of claim 12, wherein, for ventilating the honeycomb chambers filled with granules, the cover layer which otherwise is stressed with a tool while heating to the first and the second process temperature is destressed for ventilation intervals such that air displaced from the honeycomb chambers can escape.
14. The method of claim 1, wherein granules to be removed are suctioned.
15. A composite component produced by the method of claim 1.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0031] The disclosure herein will be explained in more detail hereunder with reference to the drawing in which:
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[0047] An example embodiment of a method according to the disclosure herein for producing a composite component according to the disclosure herein will be explained hereunder. A flow chart having steps 1, 3, 5, 7, 9, 11 of the example embodiment of a method according to the disclosure herein is shown in
[0048] As is illustrated in
[0049] Prior to carrying out the second method step 3, the workpiece 23 is disposed in a metering system 25 which comprises a table 27 and a metering device 29 which is able to travel across the table 27, the table 27 and the metering device 29 being illustrated in more detail in
[0050] The metering device 29, which in various embodiments will be described in more detail hereunder with reference to
[0051] Examples of metering devices 29, which can in each case be used as part of the metering system 25 from
[0052] The granules from the hopper 33 are incorporated into the honeycomb chambers 19 by way of a respective metering head 35 which either bears directly on the honeycomb structure 17 (
[0053] Illustrated in
[0054] A second embodiment in which the grains of the granules 41 drop freely from the metering head 35 is shown in
[0055] Finally shown in
[0056] As has already been explained above, in the second method step 3 those honeycomb chambers 19 of the workpiece 23 that lie within the reinforcement region 31 are filled with the granules 41. It is the objective of the filling procedure to fill the honeycomb chambers 19 up to a predetermined granule filling level, wherein the granule filling level may be uniform for the entire reinforcement region 31, or else the granule filling levels are independently established for each sub-region 31a, 31b, 31c, 31d, 31e, 31f, 31g, 31h, 31k, 31m, 31n. Because the size of the sub-regions toward the bottom is only restricted by the size of the honeycomb chambers 19, an individual granule filling level which is between 100% (completely filled) and a minimum filling level can be fundamentally established for each honeycomb chamber 19. A granule filling level of 0% is not provided within the reinforcement region because the latter comprises only honeycomb chambers 19 filled with granules, and empty honeycomb chambers 19 lie outside the reinforcement region 31. The minimum filling level is preferably chosen such that the honeycomb chamber 19 after the complete expansion of the granules 41 is completely filled up and the lowest possible density of the expanded granules 41 is achieved.
[0057] The granule filling level can be achieved in two different ways. The honeycomb chambers 19 are either filled directly only up to the envisaged granule filling level including a tolerance range. To this end, the metering heads 35 shown in
[0058] Suitable to this end are in particular the metering heads 35 which are shown in
[0059] In the example embodiments shown in
[0060] A similar arrangement is provided in the embodiment shown in
[0061] In the third method step 5, however, excess granules 41 are not only removed from honeycomb chambers 41 which form part of the reinforcement region in order for the envisaged granule filling level to be achieved. Rather, granules 41 are additionally also suctioned from the honeycomb chambers 19 that lie outside the reinforcement region 31 and are therefore not to be reinforced. It is thus preferably avoided that the weight of the composite component 15 is unnecessarily increased.
[0062] The suctioned granules 41 can be advantageously re-used, as is schematically illustrated in
[0063] Once all of the excess granules have been removed from the honeycomb chambers 19 so that all of the honeycomb chambers 19 within the reinforcement region 31 have been filled within a tolerance up to the respective granule filling level with granules 41 and have been completely removed, i.e. preferably as far as technically expedient, from all honeycomb chambers outside the reinforcement region 31, the cover layer 65 is applied to the workpiece 23 in the fourth method step 7, the cover layer 65 being illustrated in
[0064] In the fifth method step 9, the composite component 15 is finally heated to a first process temperature at which the granules 41 in the honeycomb chambers 19 expand and fill up the latter. To this end, the workpiece 25 is firmly held between an upper tool 67 and a lower tool 69 such that the workpiece 25 cannot be deformed. However, in order for the granules 41 to be able to expand without impediment, the upper tool 67 is lifted for ventilation intervals so that air which conjointly with the granules 41 is situated in the honeycomb chambers 19 can escape beforehand.
[0065] Finally, the workpiece 25 in a final sixth method step 11 is cured so as to form the composite component 15. To this end, the process temperature here is kept constant because the first process temperature at which the granules 41 expand or foam, respectively, and the second process temperature at which the expanded granules 41, the base layer 13, the honeycomb structure 17 and the cover layer 65 cure and connect to one another, are identical. The workpiece 25 is held between the upper and the lower tool 67, 69 also during the sixth method step 11.
[0066] A composite component 15 which has been locally reinforced in that granules 41 are incorporated in a targeted manner into honeycomb chambers 19 in the reinforcement region 31 and expanded therein has thus been produced by the example method. Because the filling level in the individual honeycomb chambers 19 can be set, it is moreover possible for the density of the expanded honeycomb chambers 19 to be adapted in a targeted manner to the arising loads and thus for an ideally positive balance between a sufficiently high load-bearing capability and a low weight of the composite component 15 to be achieved, this being particularly advantageous in the aerospace industry in which already minor reductions in weight are associated with significant savings in terms of fuel consumption. Moreover, the proportion of the granules 41 actually used in the composite component 15 can be significantly increased in comparison to conventional methods, because excess granules 41 can be suctioned, treated and further processed.
[0067] While at least one example 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 example 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.