发明名称 飛翔体
摘要 <p>PROBLEM TO BE SOLVED: To provide a missile which can inhibit turbulent flow occurring around an antenna.SOLUTION: A shell 100 includes: a metal shell 12; and a bonding layer 30 disposed between the metal shell 12 and an antenna 20. The antenna 20 includes an adhesion layer 23 disposed between an antenna substrate 21 and a protection cover 22. The antenna substrate 21 includes: a substrate body 211 formed by fluororesin; an antenna pattern 212 formed on an outer surface 211S of the substrate body 211; and a metal film 213 formed on an inner surface of the substrate body 211T.</p>
申请公布号 JP2015186079(A) 申请公布日期 2015.10.22
申请号 JP20140061543 申请日期 2014.03.25
申请人 KOMATSU LTD 发明人 BUTSUSHIDA SATORU;MORO KAZUHIKO
分类号 H01Q1/38;B64D47/00;H01Q1/28;H01Q1/40 主分类号 H01Q1/38
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