IP Library › Granted Patent US 10,723,098
Granted Patent B2
US 10,723,098 · App. 15/865,357 · Granted Jul 28, 2020

Sandwich panel with recessed channel network

Inventors: Nabankele Martial Somda (Hamburg, DE); Inge Sanders (Hamburg, DE); Bastian Schaefer (Hamburg, DE)
Assignee: AIRBUS OPERATIONS GMBH
B32B3/12B32B3/18B32B3/266B32B5/024B32B5/26B32B7/12B32B15/14B32B37/12B32B38/0012B64C1/06B32B2250/03B32B2260/023B32B2262/0269B32B2262/101B32B2262/106B32B2307/546B32B2419/00B32B2605/18B32B2607/00B33Y80/00
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Quick Facts
Patent No.
US 10,723,098
App. No.
15/865,357
Granted
Jul 28, 2020
Kind
B2
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.

Claims (14)

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.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 10, 2018
From: SCHAEFER, BASTIAN; SANDERS, INGE; MARTIAL SOMDA, NABANKELE
To: AIRBUS OPERATIONS GMBH
Reel/Frame 045773/0485 →
Priority Claims (1)
EP 17150762 · Jan 10, 2017 · regional
Continuity (1)
Related Publication 20180194096A1 · Jul 12, 2018