Composite panel edge treatments and joints and cargo body having same
A cargo body includes a floor configured to support a cargo load and a roof positioned above the floor. The roof includes a roof panel having a composite construction including a first skin, a second skin, and a core positioned between the first and second skins. The cargo body includes first and second lateral sidewalls, each having an upper rail extending along an upper edge thereof. An edge portion of the roof panel is joined to one of the first and second upper rails.
1. A cargo body comprising:
a panel assembly having first and second edges spaced apart from each other along a first direction, the panel assembly including
an interior skin facing an interior of the cargo body,
an exterior skin facing an exterior of the cargo body,
a core positioned between the interior and exterior skins,
a pocket formed by the interior skin at a location spaced away from the first and second edges, the pocket being open toward the interior of the cargo body, and
a logistics profile insert positioned in the pocket,
wherein the core is absent at the pocket such that the pocket divides the core into separate sections.
2. The cargo body of claim 1 , wherein the interior skin is pressed to the exterior skin at the pocket.
3. The cargo body 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 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 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 of claim 1 , wherein the pocket is one of a plurality of pockets formed in the panel assembly.
7. The cargo body of claim 1 , wherein the pocket is centered between the first and second edges.
8. The cargo body of claim 1 , wherein the core is a metal sheet of anticlastic form having an array of interspersed peaks and valleys.
9. The cargo body of claim 8 , wherein a maximum thickness of the core between the first and second skins is more than 20 times the material thickness of the metal sheet.
10. The cargo body of claim 1 , wherein the logistics profile insert is secured in the pocket with one or both of mechanical fasteners and adhesive.
11. The cargo body of claim 1 , further comprising:
a floor spanning a length and a width of the cargo body; and
a roof spanning the length and the width of the cargo body,
wherein the panel assembly is a sidewall panel assembly.
12. A cargo body panel assembly comprising:
a panel having a composite construction including an interior skin, an exterior skin, and a core positioned between the interior and exterior skins, wherein the panel has first and second edges spaced apart from each other in a first direction; and
a logistics profile insert;
wherein a pocket is formed by the interior skin at a location spaced away from the first and second edges, and the logistics profile insert is positioned in the pocket, and
wherein the core is absent at the pocket such that the pocket divides the core into separate sections.
13. The cargo body panel assembly of claim 12 , wherein the interior skin is pressed to the exterior skin at the pocket.
14. The cargo body panel assembly of claim 12 , 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.
15. The cargo body panel assembly 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 assembly 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 assembly of claim 12 , wherein the pocket is one of a plurality of pockets formed in the panel.
18. The cargo body panel assembly of claim 12 , wherein the pocket is centered between the first and second edges.
19. The cargo body panel assembly of claim 12 , wherein the core is a metal sheet of anticlastic form having an array of interspersed peaks and valleys.
20. The cargo body panel assembly of claim 19 , wherein a maximum thickness of the core between the first and second skins is more than 20 times the material thickness of the metal sheet.
21. The cargo body panel assembly of claim 12 , wherein the logistics profile insert is secured in the pocket with one or both of mechanical fasteners and adhesive.
22. The cargo body panel assembly of claim 12 , wherein the pocket extends parallel to the first and second edges.
23. The cargo body panel assembly of claim 12 , wherein the pocket extends perpendicular to the first and second edges.
24. A cargo body panel assembly comprising:
a panel having a composite construction including an interior skin, an exterior skin, and a profiled metal sheet core positioned between the interior and exterior skins, wherein the panel has first and second edges spaced apart from each other in a first direction; and
a logistics profile insert;
wherein a pocket is formed by the interior skin at a location spaced away from the first and second edges, and the logistics profile insert is positioned in the pocket, and
wherein a flat, unprofiled strip of the core extends across the pocket between the interior and exterior skins.