熱膨張率を制御した積層複合材の設計法

抄録

A lamination tailoring technique is proposed in order to control a coefficient of thermal expansion (CTE) of carbon/epoxy composites in a principal direction. This technique consists of two concepts of the thermoelastic invariants and the lamination parameters. The expansion free condition yields to a parabola in the feasible region of the lamination parameters. The calculated curves for a wide range of temperature intersect almost at a point. A laminate with the construction corresponding to this point exhibits a null CTE in one direction in that temperature range. Some experimental results indicate that the present procedure is possible and promising. Controlling to a small negative CTE to cancel an extension of metal part is also feasible.