Thermal degradation behaviour of resins in aluminium composite under isothermal condition
G Zhu (TU Delft - Materials Science and Engineering, Shanghai Key Laboratory of Advanced High-temperature Materials and Precision Forming)
Wei Wang (Shanghai Key Laboratory of Advanced High-temperature Materials and Precision Forming)
Rui Wang (Shanghai Key Laboratory of Advanced High-temperature Materials and Precision Forming)
Y. Xiao (Anhui University of Technology, (OLD) MSE-3)
Y. Yang (Anhui University of Technology, TU Delft - Materials Science and Engineering, (OLD) MSE-3)
Anping Dong (Shanghai Key Laboratory of Advanced High-temperature Materials and Precision Forming)
Donghong Wang (Northeastern University China)
Da Shu (Shanghai Key Laboratory of Advanced High-temperature Materials and Precision Forming)
Jun Wang (Shanghai Jiao Tong University, Shanghai Key Laboratory of Advanced High-temperature Materials and Precision Forming)
Baode Sun (Shanghai Key Laboratory of Advanced High-temperature Materials and Precision Forming, Shanghai Jiao Tong University)
R Boom ((OLD) MSE-1)
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Abstract
As a member of the aluminium composite, GLARE (GLAss fibre/epoxy REinforced aluminium laminates) was used in the upper fuselage of Airbus A380 because of its superior mechanical properties over monolithic aluminium alloys. Thermal processing is a potential method for materials recycling and reuse from GLARE scrap with the aim of environmental protection and economic benefits. Thermal delamination is a crucial pre-treatment step for GLARE recycling. Differential scanning calorimetry (DSC) and Thermogravimetric analysis (TGA) tests have been used to identify the decomposition temperature range of epoxy resins under non-isothermal condition in our previous work [1]. To obtain an appropriate solution for GLARE thermal delamination, the thermal degradation behaviour of epoxy resins in GLARE under isothermal conditions were investigated and isothermal decomposition kinetic models were built up based on DSC and thermogravimetric analysis TGA. The thermal delamination process of GLARE is determined based on thermal analysis results and experimental optimization.
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