发明名称 THERMAL CONDUCTIVITY CONTROL METHOD FOR FAIRING HIGH- SPEED FLYING BODY
摘要 PROBLEM TO BE SOLVED: To provide a thermal conductivity control method for a fairing of high-speed flying body, the method being capable of adjusting to optimum heat resistance performance depending on a heating rate. SOLUTION: This fairing of high-speed flying body which flies at high speed while mounting a mounted object inside the fairing and is heated at high heating rate by aerodynamic heating in high-speed flight, comprises: a heating layer integrated by impregnating a matrix resin to heat resistance reinforced fiber; and a heat dispersion layer stacked to an inside facing the mounted object of the heating layer and comprised of a material having thermal conductivity and heat capacity larger than those of the heating layer. The reinforced fiber of the heating layer is formed into a strip shape, and the orientation of the reinforced fiber is changed depending on the heating rate so as to be made perpendicular to a heating surface as the heating rate becomes large, and made parallel to the heating surface as the heating rate becomes small.
申请公布号 JP2003112699(A) 申请公布日期 2003.04.15
申请号 JP20010306857 申请日期 2001.10.02
申请人 KAWASAKI HEAVY IND LTD 发明人 OKUYAMA KEIICHI
分类号 F42B15/34;B64C1/38;B64G1/58;(IPC1-7):B64G1/58 主分类号 F42B15/34
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