发明名称 COMPOSITE MATERIAL HULL STRUCTURE
摘要 PURPOSE:To reduce the weight of wires, to decrease the electric resistance loss, to make it unnecessary to design and manufacture the installing metal and exclusive jig and tool for wiring, and to eliminate a complicated wiring work, by burying and incorporating wires in the layer of a laminated composite material. CONSTITUTION:When an outer hull for an aircraft body is formed, glass cloths 4 impregnated with resin are labeled sheet by sheet on a wooden pattern over which a pattern removing agent is spread. When the laminating work is completed partially, wire collections 2 are arranged at specific positions, over which resin-impregnated glass cloths are labeled again to complete the remaining lamination. After that, the composition is dried, and removed from the wooden pattern to form a hull 1 in which wires 3 have been buried.
申请公布号 JPS63285808(A) 申请公布日期 1988.11.22
申请号 JP19870118985 申请日期 1987.05.18
申请人 MITSUBISHI HEAVY IND LTD 发明人 SUMIYAMA AKIRA
分类号 B64D47/00;B64C1/00;H01B7/00 主分类号 B64D47/00
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