Sandwich panel with recessed channel network

Patent metadata

Field	Value
Publication number	US-10723098-B2
Application number	US-201815865357-A
Country	US
Kind code	B2
Filing date	Jan 9, 2018
Priority date	Jan 10, 2017
Publication date	Jul 28, 2020
Grant date	Jul 28, 2020

Abstract

A composite sandwich panel comprises a top layer, a bottom layer, and a honeycomb core layer sandwiched between the top layer and the bottom layer. The honeycomb core layer includes an array of hollow cells formed between vertical walls. This array of hollow cells is recessed in the form of a channel network running from a first side face of the sandwich panel through the honeycomb core layer to a second side face, opposite to the first side face of the sandwich panel.

First claim

The invention claimed is:

1. A composite sandwich panel, comprising:
a top layer;
a bottom layer; and
a honeycomb core layer sandwiched between the top layer and the bottom layer, the honeycomb core layer including an array of hollow cells formed between vertical walls, the array of hollow cells being recessed in the form of a channel network running from a first side face of the sandwich panel through the honeycomb core layer to a second side face of the sandwich panel, the second side face being located on the opposite side of the first side face of the sandwich panel,
wherein the recessed channel network of the honeycomb core layer of the sandwich panel has at least a portion of a planar core panel embedded therein, the planar core panel having a space frame structure of load bearing space frame rods,
wherein the space frame structure of load bearing space frame rods are interconnected within the honeycomb core layer.

2. The sandwich panel according to claim 1 , wherein the top layer comprises one of glass-fiber fabric, carbon-fiber fabric and aramid-fiber fabric.

3. The sandwich panel according to claim 1 , wherein the bottom layer comprises one of glass-fiber fabric, carbon-fiber fabric and aramid-fiber fabric.

4. The sandwich panel according to claim 1 , wherein the honeycomb core layer is glued to the bottom layer.

5. The sandwich panel according to claim 1 , wherein the honeycomb core layer is glued to the top layer.

6. The sandwich panel according to claim 1 , further comprising:
a honeycomb core infill panel having the inverse shape of the recessed channel network, the honeycomb core infill panel being sandwiched between the honeycomb core layer and the top layer.

7. The sandwich panel according to claim 1 , wherein the honeycomb core layer comprises one of fiberglass, carbon-fiber reinforced plastics, aramid-paper reinforced plastics and metallic materials.

8. The sandwich panel according to claim 1 , wherein the recessed channel network is machined into the honeycomb core layer.

Assignees

• Airbus Operations Gmbh

Inventors

• Martial Somda Nabankele
• Sanders Inge
• Schaefer Bastian

Classifications

• B64C1/06

  Frames; Stringers; Longerons {; Fuselage sections} · CPC title

• B32B2262/101

  Glass fibres · CPC title

• B32B7/12

  using interposed adhesives or interposed materials with bonding properties · CPC title

• B32B2250/03

  3 layers · CPC title

• B32B37/12

  characterised by using adhesives · CPC title