Experimental Examination of Theory of CTE (Coefficient of Thermal Expansion) Control Technology
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概要
- 論文の詳細を見る
A previously proposed lamination tailoring technique for precise control of a coefficient of thermal expansion (CTE) under a wide range of temperature is examined by detailed measurements of a CTE of two types of specimens : rectangular plates and tubes of carbon/epoxy composite. The theoretical basis of the technique consists of two concepts of the thermoelastic invariants and the lamination parameters. Experiments for verification are conducted with a specially designed measurement system. The results of 40% 0°and 60% ±45°plates fall between ±1×10^-7℃^<-1> within the temperature range from -50℃ to 40℃. Quite similar results are obtained for tubular specimens. It is also uncovered that the axial CTE is susceptible to variation of an off-axis angle. Precise control of the angle is a key point of the present technology .
- 一般社団法人日本機械学会の論文
- 1991-04-15
著者
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Hayashi Yoichi
Japan Aerospace Technology Foundation 7-44-1 Jindaiji-higashi Machi Chofu-shi Tokyo 182 Japan
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MATSUSHIMA MASAMICHI
Advanced Composites Evaluation Technology Center, Japan Aerospace Exploration Agency
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ISHIKAWA Takashi
Airframe Division, National Aerospace Laboratory
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HAYASHI Yoichi
Airframe Division, National Aerospace Laboratory
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FUKUNAGA Hisao
Faculty of Engineering, Tohoku University
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MATSUSHIMA Masamichi
Airframe Division, National Aerospace Laboratory
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NOGUCHI Tatsuru
Engineering Division, Japan Aircraft MFG. Co. LTD.(Nippi)
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Fukunaga Hisao
Faculty Of Engineering Tohoku University
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Matsushima Masamichi
Composite Structure Section Airframe Division National Aerospace Laboratory 6-13-1 Ohsawa Mitaka-shi
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Noguchi Tatsuru
Engineering Division Japan Aircraft Mfg. Co. Ltd.(nippi)
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Ishikawa Takashi
Composite Structure Section Airframe Division National Aerospace Laboratory 6-13-1 Ohsawa Mitaka-shi
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