TY - GEN
T1 - Shape recovery mechanics of fiber-reinforced shape-memory polymer composite
AU - Lan, Xin
AU - Liu, Yanju
AU - Leng, Jinsong
PY - 2010
Y1 - 2010
N2 - A fiber reinforced thermosetting styrene-based shape-memory polymer composite (SMPC) is developed, and the main objective is to investigate the deployment performances for SMPC. Firstly, the fundamental material properties, such as mechanical properties and shape recovery properties, are evaluated. It indicates that the SMPC shows nonlinear viscoelasticity at a temperature range between Tg-20°C and Tg +20°C. At/above T g, the shape recovery ratio of SMPC upon bending is above 90%. The shape recovery properties of SMPC become relatively stable after some packaging/deployment cycles. Then, the micro-deformation mechanism is characterized by optical microscopy and SEM. The fiber microbuckling is the primary deformation mechanism in bending of SMPC, and it ensures that the SMPC can achieve high packaging strain and avoid fiber failure. With the microbuckling, SMPC materials are suitable to be used in deployable structure components because of their high strain-to-failure capability. For the analytical research, the relationship between deployment moment and angle is derived by using dynamic theory. It shows that the SMPC shell shows a linear bending stiffness when recovering, and meanwhile performs a self-locking function at the final state because of sharply increase in moment. It implies that SMPC is a good candidate material for deployable structures.
AB - A fiber reinforced thermosetting styrene-based shape-memory polymer composite (SMPC) is developed, and the main objective is to investigate the deployment performances for SMPC. Firstly, the fundamental material properties, such as mechanical properties and shape recovery properties, are evaluated. It indicates that the SMPC shows nonlinear viscoelasticity at a temperature range between Tg-20°C and Tg +20°C. At/above T g, the shape recovery ratio of SMPC upon bending is above 90%. The shape recovery properties of SMPC become relatively stable after some packaging/deployment cycles. Then, the micro-deformation mechanism is characterized by optical microscopy and SEM. The fiber microbuckling is the primary deformation mechanism in bending of SMPC, and it ensures that the SMPC can achieve high packaging strain and avoid fiber failure. With the microbuckling, SMPC materials are suitable to be used in deployable structure components because of their high strain-to-failure capability. For the analytical research, the relationship between deployment moment and angle is derived by using dynamic theory. It shows that the SMPC shell shows a linear bending stiffness when recovering, and meanwhile performs a self-locking function at the final state because of sharply increase in moment. It implies that SMPC is a good candidate material for deployable structures.
KW - Shape memory polymer composite
KW - Shape recovery mechanics
UR - https://www.scopus.com/pages/publications/77953249699
U2 - 10.1117/12.847810
DO - 10.1117/12.847810
M3 - 会议稿件
AN - SCOPUS:77953249699
SN - 9780819480606
T3 - Proceedings of SPIE - The International Society for Optical Engineering
BT - Industrial and Commercial Applications of Smart Structures Technologies 2010
T2 - Industrial and Commercial Applications of Smart Structures Technologies 2010
Y2 - 8 March 2010 through 9 March 2010
ER -