Hinged composite sandwich panels

Patent metadata

Field	Value
Publication number	US-10773484-B2
Application number	US-201815887898-A
Country	US
Kind code	B2
Filing date	Feb 2, 2018
Priority date	Feb 2, 2018
Publication date	Sep 15, 2020
Grant date	Sep 15, 2020

Abstract

An apparatus comprises a composite sandwich panel, a seal, and a hinge. The composite sandwich panel has a first edge in a first over-crush edge region, wherein a thickness of the composite sandwich panel decreases within the first over-crush edge region in a direction towards the first edge. The seal is bonded to the first over-crush edge region of the composite sandwich panel and extending past the first edge. The hinge is connected to the composite sandwich panel such that an axis of rotation of the hinge is positioned over the first over-crush edge region of the composite sandwich panel.

First claim

What is claimed is:

1. An apparatus comprising:
a composite sandwich panel having an edge in an over-crush edge region, wherein a thickness of the composite sandwich panel decreases within the over-crush edge region in a direction towards the edge;
a seal bonded to the over-crush edge region of the composite sandwich panel and extending past the edge; and
a continuous hinge connected to the composite sandwich panel such that an axis of rotation of the continuous hinge is positioned over the over-crush edge region of the composite sandwich panel, wherein:
the composite sandwich panel comprises a first face and a second face opposite the first face; and
the second face has a concave surface disposed in the over-crush edge region.

2. The apparatus of claim 1 , wherein the continuous hinge has a length equivalent to a length of the edge.

3. The apparatus of claim 1 , wherein the continuous hinge is a gooseneck hinge.

4. The apparatus of claim 1 , wherein the composite sandwich panel further comprises a decorative laminate covering the first face and the edge.

5. The apparatus of claim 1 , wherein:
the over-crush edge region comprises a first over-crush edge region;
the edge comprises a first edge; and
the composite sandwich panel further comprises:
a second over-crush edge region with a second edge; and
a third over-crush edge region with a third edge.

6. The apparatus of claim 1 , wherein a door assembly comprises the composite sandwich panel, the seal, and the continuous hinge.

7. The apparatus of claim 1 , wherein the continuous hinge is connected to cabinetry in a lavatory of an aircraft.

8. The apparatus of claim 1 , wherein a portion of the seal is sandwiched between the continuous hinge and the composite sandwich panel.

9. The apparatus of claim 1 , wherein the edge in the over-crush edge region has a thickness in a range of 40%-15% of a nominal thickness of the composite sandwich panel.

10. The apparatus of claim 1 , wherein the composite sandwich panel comprises a first composite skin, a second composite skin, and a hollow cell core between the first composite skin and the second composite skin.

11. The apparatus of claim 1 , wherein the edge has a flat appearance without visible core cells.

12. An apparatus that comprises:
a composite sandwich panel having a cut first edge, a cut second edge, and a cut third edge each with a flat appearance without visible core cells;
a seal bonded to the composite sandwich panel adjacent the cut first edge; and
a hinge connected to the composite sandwich panel adjacent the cut first edge, wherein:
a portion of the seal is sandwiched between the hinge and the composite sandwich panel;
the composite sandwich panel comprises a first face opposite a second face; and
the second face has a concave surface disposed in an over-crush edge region, such that:
the cut first edge is within the over-crush edge region of the composite sandwich panel;
the seal is bonded to the over-crush edge region; and
the hinge is connected to the composite sandwich panel such that an axis of rotation of the hinge is positioned over the over-crush edge region.

13. The apparatus of claim 12 , wherein the hinge comprises a continuous hinge that comprises a length equivalent to a length of the cut first edge.

14. An apparatus comprising:
a composite sandwich panel having a first edge in a first over-crush edge region, wherein a thickness of the composite sandwich panel decreases within the first over-crush edge region in a direction towards the first edge;
a seal bonded to the first over-crush edge region of the composite sandwich panel and extending past the first edge; and
a continuous hinge connected to the composite sandwich panel such that an axis of rotation of the continuous hinge is positioned over the first over-crush edge region of the composite sandwich panel, wherein:
the composite sandwich panel has a first face and a second face opposite the first face;
the second face has a concave surface within the first over-crush edge region; and
the composite sandwich panel further comprises a second over-crush edge region with a second edge, and a third over-crush edge region with a third edge.

15. The apparatus of claim 14 , wherein the continuous hinge has a length equivalent to a length of the first edge.

16. The apparatus of claim 14 , wherein the continuous hinge is a gooseneck hinge.

17. The apparatus of claim 14 , wherein the composite sandwich panel further comprises a decorative laminate covering the first face and the first edge.

18. The apparatus of claim 14 , wherein a door assembly comprises the composite sandwich panel, the seal, and the continuous hinge.

19. The apparatus of claim 14 , wherein the continuous hinge is connected to cabinetry in a lavatory of an aircraft.

20. The apparatus of claim 14 , wherein the first edge in the first over-crush edge region has a thickness in a range of about 40%-15% of a nominal thickness of the composite sandwich panel.

Assignees

• Boeing Co

Inventors

• Young Stephen M
• Turner Jason
• Swanson Kevin G
• Egging Duane M

Classifications

• B32B3/12

  characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure · CPC title

• B32B3/06 Primary

  for securing layers together; for attaching the product to another member, e.g. to a support {, or to another product, e.g. groove/tongue, interlocking} · CPC title

• Y02T50/40

  Weight reduction · CPC title

• B64D11/02 Primary

  Toilet fittings · CPC title

• B32B37/16

  with all layers existing as coherent layers before laminating · CPC title