Thermal degradation behaviour of resins in aluminium composite under isothermal condition

Guoliang Zhu; Wei Wang; Rui Wang; Yanping Xiao; Yongxiang Yang; Anping Dong; Donghong Wang; Da Shu; Jun Wang; Baode Sun; Rob Boom

doi:10.1016/j.polymertesting.2017.05.038

Thermal degradation behaviour of resins in aluminium composite under isothermal condition

Guoliang Zhu, Wei Wang, Rui Wang, Yanping Xiao, Yongxiang Yang, Anping Dong^*, Donghong Wang, Da Shu, Jun Wang, Baode Sun, Rob Boom

^*Corresponding author for this work

Materials Science and Engineering

Research output: Contribution to journal › Article › Scientific › peer-review

3 Citations (Scopus)

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.

Original language	English
Pages (from-to)	448-454
Journal	Polymer Testing
Volume	61
DOIs	https://doi.org/10.1016/j.polymertesting.2017.05.038
Publication status	Published - 2017

Keywords

Delamination
GLARE
Isothermal kinetics
TGA
Thermal degradation

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10.1016/j.polymertesting.2017.05.038

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title = "Thermal degradation behaviour of resins in aluminium composite under isothermal condition",

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.",

keywords = "Delamination, GLARE, Isothermal kinetics, TGA, Thermal degradation",

author = "Guoliang Zhu and Wei Wang and Rui Wang and Yanping Xiao and Yongxiang Yang and Anping Dong and Donghong Wang and Da Shu and Jun Wang and Baode Sun and Rob Boom",

year = "2017",

doi = "10.1016/j.polymertesting.2017.05.038",

language = "English",

volume = "61",

pages = "448--454",

journal = "Polymer Testing",

issn = "0142-9418",

publisher = "Elsevier",

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TY - JOUR

T1 - Thermal degradation behaviour of resins in aluminium composite under isothermal condition

AU - Zhu, Guoliang

AU - Wang, Wei

AU - Wang, Rui

AU - Xiao, Yanping

AU - Yang, Yongxiang

AU - Dong, Anping

AU - Wang, Donghong

AU - Shu, Da

AU - Wang, Jun

AU - Sun, Baode

AU - Boom, Rob

PY - 2017

Y1 - 2017

N2 - 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.

AB - 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.

KW - Delamination

KW - GLARE

KW - Isothermal kinetics

KW - TGA

KW - Thermal degradation

UR - http://www.scopus.com/inward/record.url?scp=85020917217&partnerID=8YFLogxK

U2 - 10.1016/j.polymertesting.2017.05.038

DO - 10.1016/j.polymertesting.2017.05.038

M3 - Article

AN - SCOPUS:85020917217

SN - 0142-9418

VL - 61

SP - 448

EP - 454

JO - Polymer Testing

JF - Polymer Testing

ER -

Thermal degradation behaviour of resins in aluminium composite under isothermal condition

Abstract

Keywords

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