TY - JOUR
T1 - Deformation behaviour of steel/SRPP fibre metal laminate characterised by evolution of surface strains
AU - Nam, J.
AU - Cantwell, Wesley
AU - Das, Raj
AU - Lowe, Adrian
AU - Kalyanasundaram, Shankar
N1 - Publisher Copyright:
© 2016 Techno-Press, Ltd.
PY - 2016/1/1
Y1 - 2016/1/1
N2 - Climate changes brought on by human interventions have proved to be more devastating than predicted during the recent decades. Recognition of seriousness of the situation has led regulatory organisations to impose strict targets on allowable carbon dioxide emissions from automotive vehicles. As a possible solution, it has been proposed that Fibre Metal Laminate (FML) system is used to reduce the weight of future vehicles. To facilitate this investigation, FML based on steel and self-reinforced polypropylene was stamp formed into dome shapes under different blank holder forces (BHFs) at room temperature and its forming behaviour analysed. An open-die configuration was used in a hydraulic press so that a 3D photogrammetric measurement system (ARAMIS) could capture real-time surface strains. This paper presents findings on strain evolutions at different points along and at 45° to fibre directions of circular FML blank, through various stages of forming. It was found initiation and rate of deformation varied with distance from the pole, that the mode of deformations range from biaxial stretching at the pole to drawing towards flange region, at decreasing magnitudes away from the pole in general. More uniform strain distribution was observed for the FML compared to that of plain steel and the most significant effects of BHF were its influence on forming depth and level of strain reached before failure.
AB - Climate changes brought on by human interventions have proved to be more devastating than predicted during the recent decades. Recognition of seriousness of the situation has led regulatory organisations to impose strict targets on allowable carbon dioxide emissions from automotive vehicles. As a possible solution, it has been proposed that Fibre Metal Laminate (FML) system is used to reduce the weight of future vehicles. To facilitate this investigation, FML based on steel and self-reinforced polypropylene was stamp formed into dome shapes under different blank holder forces (BHFs) at room temperature and its forming behaviour analysed. An open-die configuration was used in a hydraulic press so that a 3D photogrammetric measurement system (ARAMIS) could capture real-time surface strains. This paper presents findings on strain evolutions at different points along and at 45° to fibre directions of circular FML blank, through various stages of forming. It was found initiation and rate of deformation varied with distance from the pole, that the mode of deformations range from biaxial stretching at the pole to drawing towards flange region, at decreasing magnitudes away from the pole in general. More uniform strain distribution was observed for the FML compared to that of plain steel and the most significant effects of BHF were its influence on forming depth and level of strain reached before failure.
KW - Fibre metal laminate
KW - Real-time strain measurement system
KW - Self-reinforced polypropylene
KW - Stamp forming
UR - http://www.scopus.com/inward/record.url?scp=85018595331&partnerID=8YFLogxK
U2 - 10.12989/aas.2016.3.1.061
DO - 10.12989/aas.2016.3.1.061
M3 - Article
SN - 2287-528X
VL - 3
SP - 61
EP - 75
JO - Advances in Aircraft and Spacecraft Science
JF - Advances in Aircraft and Spacecraft Science
IS - 1
ER -