Cargo management system for a vehicle and including a pair of opposing cargo trim panels, each of which is made by a composite, compression molding process and has a wood grain finish
US-9346375-B2 · May 24, 2016 · US
US11059259B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11059259-B2 |
| Application number | US-201715818033-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 20, 2017 |
| Priority date | Nov 21, 2016 |
| Publication date | Jul 13, 2021 |
| Grant date | Jul 13, 2021 |
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Some embodiments provide a core member for a composite panel that includes a hollow cell network structure, such as a honeycomb arrangement for example, and reinforced plastic strips positioned on a portion of the continuous honeycomb structure. The honeycomb structure and the solid plastic strips may be fastened together using heat and/or pressure applications. Additionally, the method for the production of the core member is provided.
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I claim: 1. A composite panel, comprising: an inner sheet and an outer sheet disposed opposite of the inner sheet, and a core member positioned between the inner and outer sheets, the core member comprising a continuous material including a) a partially hollow structure and b) a gap section, the gap section extending between a first end and a second end of the partially hollow structure and having a shorter height than the partially hollow structure to create a gap, wherein the partially hollow structure has a lower volumetric mass density than the gap section as a result of the gap section being formed by an interruption during a vacuum forming process of the core member or compressing a portion of the partially hollow structure. 2. The composite panel of claim 1 further including a reinforced material, wherein the reinforced material is designed to be inserted into the gap and coupled to the partially hollow structure. 3. The composite panel of claim 2 , wherein the reinforced material is coupled to the partially hollow structure adjacent the first end thereof. 4. The composite panel of claim 3 , the reinforced material is coupled to the partially hollow structure adjacent the second end thereof. 5. The composite panel of claim 2 , wherein the partially hollow structure is at least 80% of a volume of the core member. 6. The composite panel of claim 5 , wherein the partially hollow structure is at least 95% of the volume of the core member. 7. The composite panel of claim 2 , wherein the reinforced material is selected from the group consisting of high density polyethylene, high density polypropylene, low density polyethylene, polyethylene terephthalate, polypropylene, and combinations thereof. 8. The composite panel of claim 2 , wherein the composite panel has a length dimension ranging between about 2.5 meters to about 3.5 meters. 9. The composite panel of claim 8 , wherein the composite panel has a width dimension ranging between about 1 meter to about 2 meters. 10. The composite panel of claim 2 , wherein the partially hollow structure is provided as a network of hexagonal cells. 11. The composite panel of claim 2 , wherein the reinforced material is designed to be welded to the partially hollow structure. 12. The composite panel of claim 2 , wherein the partially hollow structure has a lower volumetric mass density than the reinforced material. 13. The composite panel of claim 1 , wherein the partially hollow structure is interrupted by a plurality of gap sections. 14. The composite panel of claim 1 , wherein the gap section is created by interrupting the vacuum forming process. 15. The composite panel of claim 2 , wherein the reinforced material is a solid material that fills the gap.
the structure having joined ribs, e.g. honeycomb · CPC title
Producing honeycomb structures (consisting of porous ceramic ware C04B38/0006) · CPC title
using only vacuum · CPC title
honeycomb structures · CPC title
Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore {(B29C48/001 takes precedence)} · CPC title
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