发明名称 HEAT RESISTANCE RESTRAINING STRUCTURE FOR FAIRING HIGH- SPEED FLYING BODY
摘要 PROBLEM TO BE SOLVED: To provide a heat resistance restraining structure of a fairing outer wall used in a high-speed flying body, the structure being capable of implementing optimum heat resistance restraining performance depending on an aerodynamic heating rate. SOLUTION: In this heat resistance restraining structure for the fairing outer wall used in the 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, a thermal conduction excellent material in which a metal particulate is mixed to a heat resistance fluid body is interposed between 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, so as to maintain to be equal to or less than a wear temperature by heat of a surface facing outside of the heating layer.
申请公布号 JP2003112698(A) 申请公布日期 2003.04.15
申请号 JP20010306856 申请日期 2001.10.02
申请人 KAWASAKI HEAVY IND LTD 发明人 OKUYAMA KEIICHI
分类号 F42B15/34;B32B5/00;B32B7/02;B64C1/38;B64G1/00;B64G1/58;(IPC1-7):B64G1/58 主分类号 F42B15/34
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