journal article·1998-07

Polymer Foams as Core Materials in Sandwich Laminates (Comparison with Honeycomb)

V. Altstädt, F. Diedrichs, T. Lenz, H. Bardenhagen, D. Jarnot

Polymers and Polymer Composites· Volume 6· Issue 5
Publisher page

Abstract

The mechanical properties of sandwich laminates with two different closed cell polymer foams (PEI and PMI) as core materials were examined compared with sandwich laminates with honeycomb as core material. The applied test methods were compression, tension, four-point bending and instrumented falling weight impact. To examine the influence of the adhesive bonding between the face sheet and the core material, the sandwich laminates were tested with and without adhesive bonding. For comparison purposes the processing procedure for all sandwich laminates was kept constant. Therefore all sandwich laminates were produced at the same time in the same autoclave. In comparison to a honeycomb core, sandwich laminates with foam as core material showed superior surface quality and impact energy absorption. The influence of the adhesive bonding between face sheet and core material was found to be very small under tensile loading conditions. From microscopical investigations of the bond line it was deduced that in the case of direct bonding, sufficient resin was able to flow during processing from the face laminate into the micropores at the foam core surface without adhesive.
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Research context

OpenAlex topics: Cellular and Composite Structures · Polymer Foaming and Composites · Polymer composites and self-healing

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Polymer and Composites Section, Technical University Hamburg-Harburg, Denickestrasse 15, 21073 Hamburg, Germany

Technology/New Programs, Daimler-Benz Aerospace Airbus GmbH, Ottenbecker Damm, 21684 Stade, Germany

References (4)

Show source-provided references
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