A sandwich panel for an aircraft includes a lower top layer, an upper top layer and a core layer, wherein the core layer in turn includes pins. The pins extend from a lower top layer in the direction of the upper top layer, and the pins are interconnected by rods. In addition, the rods run inside the core layer, and the pins and rods form a one-piece network.
SANDWICH PANEL FOR AN AIRCRAFT
2016-10-13
Patent
Electronic Resource
English
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