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Adhesive Joining of Zerodur–CFRP–Zerodur Sandwich Structures for Aerospace Applications
Author(s) -
Pierre des Ammbrois Stefano De,
Corazzari Ingrid,
Damiano Olivier,
Cornillon Laurence,
Terenzi Andrea,
Casalegno Valentina,
Ferraris Monica
Publication year - 2020
Publication title -
macromolecular materials and engineering
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.913
H-Index - 96
eISSN - 1439-2054
pISSN - 1438-7492
DOI - 10.1002/mame.202000464
Subject(s) - materials science , adhesive , composite material , cyanate ester , curing (chemistry) , ultimate tensile strength , carbon fiber reinforced polymer , epoxy , layer (electronics) , composite number
A high performance adhesive is used to join Zerodur to a carbon fiber reinforced polymers (CFRPs) honeycomb (HC) in a sandwich structure for aerospace applications. The main problem of finding an adhesive with suitable thermomechanical stability and ease of application for use in large components, together with a lower curing temperature than 160 °C, in order to avoid detrimental effects on the CFRPs is resolved. Two phenolic‐based and one cyanate ester‐based adhesives are considered. One phenolic‐based adhesive that is already proven effective in the joining of carbon/carbon composites (C/C) is used to join CFRP slabs and Zerodur–CFRP–Zerodur in a sandwich structure. Thermal analysis is conducted to characterize and compare the phenolic adhesive, cured at 150 °C and at 260 °C, with a cyanate ester‐based adhesive and a commercial phenolic‐based one. The phenolic adhesive cured at 150 °C results to be the most suitable joining material; the lap shear strength of the CFRP slabs joined at room temperature is measured after thermal cycling. Zerodur–CFRP–Zerodur sandwich structures, joined by the phenolic adhesive cured at 150 °C, are tested in tensile and lap shear modes.