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논문 기본 정보

자료유형
학술저널
저자정보
Tetsuo Yasuoka (Tokyo Institute of Technology) Yoshinobu Shimamura (Shizuoka University) Akira Todoroki (Tokyo Institute of Technology)
저널정보
한국항공우주학회 International Journal of Aeronautical and Space Sciences International Journal of Aeronautical and Space Sciences Volume.14 Number.2
발행연도
2013.6
수록면
146 - 151 (6page)

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초록· 키워드

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Carbon nanofibers (CNFs) are electrically conductive. When CNFs are used as fillers in resin, this electrical conductivity can be yielded without adversely affecting the mechanical properties of the resin. When an elastomer is adopted as the resin, a conductive elastomer can then be produced. Due to its flexibility and conductive properties, a large strain sensor based on changes in resistivity may be produced, for strain sensing in flexible structures. In this study, a patch-type large strain sensor using resistivity change in a CNF/elastomer composite was proposed. The measurement limits of the sensor were investigated experimentally, and the limit was found to be 40%, which greatly exceeded the limits of conventional metal-foiled strain gages. Also, the proposed CNF/elastomer large strain sensor can be used to measure flexible materials, while conventional strain gages cannot be used to measure such strains.

목차

Abstract
1. Introduction
2. Large strain sensor using CNF/elastomer composite
3. Conclusions
References

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UCI(KEPA) : I410-ECN-0101-2014-550-002959737