journal article·2014-01

Acceleration of the curing process of a paste adhesive for aerospace applications considering cure dependent void formations

A. Sánchez Cebrián, R. Basler, F. Klunker, M. Zogg

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Abstract

In this publication, the acceleration of the curing process of a paste adhesive used for bonding aerospace components is investigated. Previous investigations have proven that the use of high temperatures not only reduces the curing time but also increases the void formation. This phenomenon takes place due to evaporation of volatiles at high temperatures and affects the mechanical performance of the bonded joint. In this study a dual step cure process is investigated, where the curing temperature is increased depending on the degree of cure of the paste adhesive. In this context, the impact of increasing the temperature at different stages of the curing reaction is analyzed, determining a strategy to accelerate the curing reaction without major void formation. By this approach, the curing time of the paste adhesive used for this investigation could be reduced from 4 h to 30 min without decreasing the mechanical performance of the bonded joint.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Epoxy Resin Curing Processes · Synthesis and properties of polymers · Mechanical Behavior of Composites

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

References (24)

Show source-provided references
1. Department of Defense. Adhesive bonding (structural) for aerospace and other systems, requirements for. Department of Defense. Handbook, MIL-HDBK-8337; 1997.
2. Methodology for optimization of the curing cycle of paste adhesives10.1016/j.ijadhadh.2012.09.002 ↗
3. Modelling anomalous moisture uptake, swelling and thermal characteristics of a rubber toughened epoxy adhesive10.1016/j.ijadhadh.2004.02.002 ↗
4. The effect of composite prebond moisture on adhesive-bonded CFRP-CFRP joints10.1016/0010-4361(83)90008-3 ↗
5. Blackwell · 2000
6. Davis M. Aircraft airworthiness and Sustainment Conference. Brisbane, AUS; 2011.
7. Curing effects on viscosity and mechanical properties of a commercial epoxy resin adhesive10.1016/S0143-7496(02)00013-1 ↗
8. Modeling of induction heating devices in examples of induction heating platens of vulcanization presses
9. Numerical modelling on induction heating of long workpieces10.1109/20.334291 ↗
10. Computational modeling of induction heating process10.2528/PIERL09071509 ↗
11. Induction heated joining of aluminum and carbon fiber reinforced nylon 6610.1177/0892705709105969 ↗
12. Accelerated curing of adhesives in bonded joints by induction heating10.1177/002199839903301704 ↗
13. Induction heating of continuous carbon-fibre-reinforced thermoplastics10.1016/S1359-835X(00)00094-4 ↗
14. A study on the induction heating of conductive fiber reinforced composites10.1177/0021998302036004171 ↗
15. Epoxy resins (DGEBA): the curing and physical aging process10.1002/polb.1990.090280401 ↗
16. Viscoelastic properties of an epoxy resin during cure10.1177/002199801772662442 ↗
17. Simulation of the cure of paste adhesive by induction heating
18. Verclos O, Scobbie K, Tsotra P, Wilbers H. Toughened Epoxy paste adhesives for aerospace applications. In: Proceedings of the 17th international conference on composite materials. Edimburg, UK; July 2009. p. 27–31
19. A variable reaction order model for prediction of curing kinetics of thermosetting polymers10.1016/j.polymer.2007.07.067 ↗
20. Kinetics and rheology characterization during curing of dicyanates10.1002/(SICI)1097-4628(19961017)62:3<567::AID-APP14>3.0.CO;2-W ↗
21. Glass transition of polymers: atomistic simulation versus experiments
22. Glass transition temperatures versus conversion relationships for thermosetting polymers10.1002/polb.1990.090280107 ↗
23. Isothermal rheokinetic study of a precured resol resin beyond gelation by torsion
24. Sánchez Cebrián A, Zogg M, Ermanni P. ECCM 15. In:Proceedings of the 15th European conference on composite materials. Venice, IT; 2012.