METHOD OF MANUFACTURING A COMPOSITE PART COMPRISING A CORE AND AT LEAST ONE SKIN REGION
20200324493 ยท 2020-10-15
Assignee
Inventors
Cpc classification
B29C70/465
PERFORMING OPERATIONS; TRANSPORTING
B29C43/003
PERFORMING OPERATIONS; TRANSPORTING
B29C43/18
PERFORMING OPERATIONS; TRANSPORTING
B29C70/84
PERFORMING OPERATIONS; TRANSPORTING
B29K2105/251
PERFORMING OPERATIONS; TRANSPORTING
B29C70/12
PERFORMING OPERATIONS; TRANSPORTING
B29K2105/12
PERFORMING OPERATIONS; TRANSPORTING
B29K2823/0683
PERFORMING OPERATIONS; TRANSPORTING
International classification
B29C70/12
PERFORMING OPERATIONS; TRANSPORTING
B29C43/00
PERFORMING OPERATIONS; TRANSPORTING
B29C43/18
PERFORMING OPERATIONS; TRANSPORTING
B29C70/46
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method of manufacturing a composite part comprising, a core (16) and at least one skin region (20, 22) formed of a skin polymer attached thereto, the skin polymer being a low-friction thermoplastic polymer, by: a) providing a mold with a heatable mold cavity; b) loading into the mold cavity a core element having a surface with at least one contacting region provided with a plurality of anchoring sites (10), andpreviously or subsequentlyloading into the mold cavity a layer of the skin polymer in powder form adjacent said contacting region and embedding the anchoring sites; c) applying a heat pressing step melting the skin polymer powder to form a molten skin polymer matrix (20, 22, 32); d) applying a cooling step, solidifying the skin polymer matrix forming a skin region mechanically engaged into anchoring sites of the core element forming the core.
Claims
1. A method of manufacturing a composite part comprising a core (16) and at least one skin region (20, 22) formed of a skin polymer attached thereto, the skin polymer being a low-friction thermoplastic polymer, the method comprising the Mowing steps: a) providing a mold with a heatable mold cavity (4, 14); b) loading into the mold cavity a core element (6) having a surface with at least one contacting region provided with a plurality of anchoring sites (10, 28, 30, 34, 36), andpreviously or subsequentlyloading into the mold cavity a layer (2, 12) of the skin polymer in powder form adjacent said contacting region and embedding the anchoring sites; c) applying a heat pressing step whereby the skin polymer powder is molten to form a molten skin polymer matrix (20, 22, 32); d) applying a cooling step, whereby the skin polymer matrix solidifies to form a skin region mechanically engaged into the anchoring sites of the core element forming the core.
2. The method according to claim 1, wherein the skin polymer is ultra-high molecular weight polyethylene (UHMWPE).
3. The method according to claim 1, wherein the layer of skin polymer powder is applied above and below the core element.
4. The method according to claim 1, wherein the layer of skin polymer powder is applied patchwise.
5. The method according to claim 1, wherein the core element is forted of a thermoplastic fleece (8) with reinforcement fibers (10), wherein the thermoplastic fleece consists of a core thermoplastic polymer, and wherein cavernous surface structures of the thermoplastic fleece and/or surface portions of the reinforcement fibers act as said anchoring sites, the heat pressing step causing melting of the core thermoplastic polymer, whereby the core element is formed to the core.
6. The method according to claim 5, wherein the core thermoplastic polymer is polypropylene.
7. The method according to claim 5, wherein the skin polymer is UHMWPE and the heat pressing step is carried out at a temperature of 190 to 230 C. with a pressure of 20 to 60 bar.
8. The method according to claim 5, wherein the reinforcement fibers (10) are glass fibers.
9. The method according to claim 5, wherein the core element (6) further comprises at least one reinforcement layer (24a, 24b).
10. The method according to claim 9, wherein the reinforcement layer is selected from a fabric, multiaxial stitch or unidirectional reinforcement.
11. The method according to claim 1, wherein the core element (6) is formed as a solid or hollow body (36) and wherein the anchoring sites are configured as surface discontinuities such as recesses (30), rims or under-cuts (34).
12. A composite part comprising a core (16) and at least one skin region (20, 22, 32) formed of a skin polymer attached thereto, the skin polymer being a low-friction thermoplastic polymer, the core element having a surface with at least one contacting region provided with a plurality of anchoring sites (10, 28, 30, 34, 36), and the skin region being mechanically engaged into the anchoring sites of the core element, the skin region having a thickness of 0.5 to 10 mm.
13. The composite pan according to claim 11, wherein the skin polymer is UHMWPE.
14. The composite part according to claim 12, wherein the core comprises a solid matrix (18) of the core thermoplastic and reinforcement fibers (10), which together form anchoring sites embedded by the skin polymer (22).
15. The composite part according to claim 14, wherein the core thermoplastic is polypropylene
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0046] The above mentioned and other features and objects of this invention and the manner of achieving them will become more apparent and this invention itself will be better understood by reference to the following description of various embodiments of this invention taken in conjunction with the accompanying drawings, wherein:
[0047]
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DETAILED DESCRIPTION OF THE INVENTION
[0051] It will be understood that the figures are not necessarily drawn to scale. In some instances, relative dimensions are substantially distorted for ease of visualization. Identical or corresponding features in the various figures will generally be denoted with the same reference numerals.
[0052] In the following examples, UHMWPE was used as skin polymer, polypropylene was used as core thermoplastic polymer, and glass fibers were used as reinforcement fibers. As will be understood from the above, other suitable materials may be chosen. Depending on material choice, the temperature and possibly also the pressure applied in the heat pressing step may have to be adapted. For this purpose it may be appropriate to conduct a small series of test runs systematically changing temperature and pressure.
[0053] In the example of
[0054] The stacked arrangement thus prepared is then subjected to a heat pressing step by driving an upper mold plate 14 against lower mold plate 4 under appropriate heating. During this process, the UHMWPE powder is driven further into the core element and is caused to melt; simultaneously, the PP fibers of the core element are caused to also melt and the lofty fiber arrangement is compressed to some extent. After cooling down, the resulting composite part comprises a central core 16 made up of glass fibers 10 and a solid PP core matrix 18, which is stacked between a lower skin 20 and an upper skin 22 formed of a solid matrix of UWHMPE. As particularly seen from the enlarged section in
[0055] The same principle is applied in the examples of
[0056] In the example of
[0057] Analogously to the first example, the heat pressing step leads to formation of a composite part, wherein the core 16 now contains the reinforcement layers 24a and 24b. Depending on the type of reinforcement element, molten PP is driven into recesses and cavities of the reinforcement element and provides mechanical connection to the core matrix.
[0058] The example of
[0059] A substantially different embodiment is shown in
[0060] As already mentioned, various embodiments of the method and of the composite part are possible.
[0061] The composite part illustrated in