Composite panel edge treatments and joints and cargo body having same

Patent metadata

Field	Value
Publication number	US-11428556-B2
Application number	US-202117155340-A
Country	US
Kind code	B2
Filing date	Jan 22, 2021
Priority date	Jun 4, 2014
Publication date	Aug 30, 2022
Grant date	Aug 30, 2022

Abstract

A cargo body panel includes a composite construction including an interior skin, an exterior skin, and a core positioned between the interior and exterior skins. The panel has parallel first and second edges spaced in a first direction. A pocket is formed by the interior skin at a location spaced away from the first and second edges, the pocket extending parallel to the first and second edges to define a length. The pocket is wide enough to accommodate a logistics profile insert having a width that exceeds a depth of the pocket, the depth measured into the panel, perpendicular to both the first direction and the length.

First claim

What is claimed is:

1. A cargo body panel comprising:
a composite construction including an interior skin, an exterior skin, and a core positioned between the interior and exterior skins;
a first edge;
a second edge parallel to the first edge and spaced apart from the first edge in a first direction; and
a pocket formed by the interior skin at a location spaced away from the first and second edges, the pocket extending parallel to the first and second edges to define a length, wherein the pocket is wide enough to accommodate a logistics profile insert having a width that exceeds a depth of the pocket, the depth measured into the panel, perpendicular to both the first direction and the length, and
wherein the core is absent at the pocket such that the pocket divides the core into separate sections.

2. The cargo body panel of claim 1 , wherein the interior skin is pressed to the exterior skin at the pocket.

3. The cargo body panel of claim 1 , wherein the interior skin is bent into a shape defining the pocket such that a portion of the interior skin lies against the exterior skin.

4. The cargo body panel of claim 1 , wherein the exterior skin is flat to define a single plane across the pocket and on both sides of the pocket where the exterior skin overlies the core.

5. The cargo body panel of claim 1 , wherein one or both of the interior and exterior skins continuously spans across the pocket in the first direction, including adjacent portions overlying the core.

6. The cargo body panel of claim 1 , wherein the pocket is one of a plurality of pockets formed in the panel.

7. The cargo body panel of claim 1 , wherein the pocket is centered between the first and second edges.

8. The cargo body panel of claim 1 , wherein the core is a sheet of anticlastic form having an array of interspersed peaks and valleys.

9. The cargo body panel of claim 8 , wherein a maximum thickness of the core between the first and second skins is more than 10 times the material thickness of the sheet.

10. The cargo body panel of claim 8 , wherein the maximum thickness of the core between the first and second skins is more than 20 times the material thickness of the sheet.

11. The cargo body panel of claim 8 , wherein the sheet is a metal sheet manufactured by embossing from a flat starting sheet.

12. A cargo body panel comprising:
a composite construction including an interior skin, an exterior skin, and a profiled metal sheet core positioned between the interior and exterior skins;
a first edge;
a second edge parallel to the first edge and spaced apart from the first edge in a first direction; and
a pocket formed by the interior skin at a location spaced away from the first and second edges, the pocket extending parallel to the first and second edges to define a length, wherein the pocket is wide enough to accommodate a logistics profile insert having a width that exceeds a depth of the pocket, the depth measured into the panel, perpendicular to both the first direction and the length,
wherein a flat, unprofiled strip of the core extends across the pocket between the interior and exterior skins.

13. The cargo body panel of claim 12 , wherein the interior skin is pressed to the flat, unprofiled strip of the core at the pocket.

14. The cargo body panel of claim 12 , wherein the flat, unprofiled strip of the core is pressed between the interior skin and the exterior skin.

15. The cargo body panel of claim 12 , wherein the exterior skin is flat to define a single plane across the pocket and on both sides of the pocket where the exterior skin overlies the core.

16. The cargo body panel of claim 12 , wherein one or both of the interior and exterior skins continuously spans across the pocket in the first direction, including adjacent portions overlying the core.

17. The cargo body panel of claim 12 , wherein the pocket is one of a plurality of pockets formed in the panel.

18. The cargo body panel of claim 12 , wherein the pocket is centered between the first and second edges.

19. The cargo body panel of claim 12 , wherein the core is a sheet of anticlastic form having an array of interspersed peaks and valleys.

20. The cargo body panel of claim 19 , wherein a maximum thickness of the core between the first and second skins is more than 10 times the material thickness of the metal sheet.

21. The cargo body panel of claim 19 , wherein the maximum thickness of the core between the first and second skins is more than 20 times the material thickness of the metal sheet.

22. The cargo body panel of claim 19 , wherein the sheet is a metal sheet manufactured by embossing from a flat starting sheet.

Assignees

• Sti Holdings Inc

Inventors

• Fenton Gary L

Classifications

• G01F25/10

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