TY - GEN
T1 - Ultra-thin, ultra-lightweight, and multifunctional skin for highly deformable structures
AU - Yao, Yao
AU - Taylor, Jacob
AU - Cirullo, Luke
AU - Leguarda, Rainmar
AU - Sheeran, Brett
AU - Ning, Xin
N1 - Funding Information:
This research was supported by the start-up fund from the Department of Aerospace and College of Engineering at the Pennsylvania State University.
Publisher Copyright:
© 2019 by Xin Ning. Published by the American Institute of Aeronautics and Astronautics, Inc.
PY - 2019
Y1 - 2019
N2 - One of the challenges that space exploration encounters is creating deployable structures that are lightweight and that can survive, monitor, and mitigate the harsh and extreme environments in space. It is also evident that future space structures will require flexible and multifunctional electronics embedded onto its skin to carry out the desired multiple functions of the structures in low launch weight and volume. This paper presents an architecture and fabrication method for a multifunctional skin with integrated electronic components that can be embedded onto highly deformable structures. This multifunctional structural skin is ultra-thin and ultra-lightweight. The skin includes multiple passive and active components, including strain sensors, temperature sensors, and micro-heater. The fabrication method combines advanced micro/nano-fabrication technologies, which are well established in semiconductor industry, with novel transfer printing techniques. The fabrication method developed in this paper exploits the high-performance electronic materials and enables the flexibility of devices. Experiments have shown that the structural skin can be embedded on highly deformable structures. Initial efforts on creating lightweight origami multifunctional structures have been demonstrated as well.
AB - One of the challenges that space exploration encounters is creating deployable structures that are lightweight and that can survive, monitor, and mitigate the harsh and extreme environments in space. It is also evident that future space structures will require flexible and multifunctional electronics embedded onto its skin to carry out the desired multiple functions of the structures in low launch weight and volume. This paper presents an architecture and fabrication method for a multifunctional skin with integrated electronic components that can be embedded onto highly deformable structures. This multifunctional structural skin is ultra-thin and ultra-lightweight. The skin includes multiple passive and active components, including strain sensors, temperature sensors, and micro-heater. The fabrication method combines advanced micro/nano-fabrication technologies, which are well established in semiconductor industry, with novel transfer printing techniques. The fabrication method developed in this paper exploits the high-performance electronic materials and enables the flexibility of devices. Experiments have shown that the structural skin can be embedded on highly deformable structures. Initial efforts on creating lightweight origami multifunctional structures have been demonstrated as well.
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U2 - 10.2514/6.2019-2028
DO - 10.2514/6.2019-2028
M3 - Conference contribution
AN - SCOPUS:85083943211
SN - 9781624105784
T3 - AIAA Scitech 2019 Forum
BT - AIAA Scitech 2019 Forum
PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)
T2 - AIAA Scitech Forum, 2019
Y2 - 7 January 2019 through 11 January 2019
ER -