Adhesive Joining of Zerodur–CFRP–Zerodur Sandwich Structures for Aerospace Applications. Issue 12 (12th October 2020)

• Record Type: Journal Article
• Authors: la Pierre des Ammbrois, Stefano De; Corazzari, Ingrid; Damiano, Olivier; Cornillon, Laurence; Terenzi, Andrea; Casalegno, Valentina; Ferraris, Monica
• Is Part Of: Macromolecular materials and engineering. Volume 305:Issue 12(2020)
• Page Start: n/a
• Page End: n/a
• Publication Date: 2020-10-12
• Subjects: adhesive joining -- aerospace materials -- CFRPs -- honeycomb structures -- sandwich structures; Plastics -- Periodicals; Polymers -- Periodicals; Polymerization -- Periodicals; 547.705
• DOI: 10.1002/mame.202000464
• Languages: English
• ISSNs: 1438-7492

Abstract

Abstract: 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. Abstract : The design of high performance adhesives is presented for the joining of Zerodur to a carbon fiber reinforced polymer (CFRP) honeycomb in a sandwich structure of carbon fiber reinforced composites for ultra‐stable aerospace applications. A phenolic‐based adhesive appears promising as it shows suitable thermomechanical stability, ease of application on large components and a low curing temperature, compatible with CFRP substrates.