发明名称 RADOME FOR AVIATION BODY AND MANUFACTURING METHOD OF THE SAME
摘要 PROBLEM TO BE SOLVED: To provide a radome for an aviation body, light weight, having a sandwich structure of a three-dimensional shape, excellent in electromagnetic wave transmissivity and a manufacturing method of the same.SOLUTION: The radome for an aviation body has a shape of covering an electromagnetic wave instrument installed on an aviation body, and is formed with a sandwich panel structure in which a core material (30), compounded by foaming insulting reinforced fiber (31) and a heat-resistant resin (32), is held between skin materials (20), composed of a fiber-reinforced material formed by compounding a quartz cloth (21) and a heat-resistant resin (22).SELECTED DRAWING: Figure 1
申请公布号 JP2016149756(A) 申请公布日期 2016.08.18
申请号 JP20160000388 申请日期 2016.01.05
申请人 MITSUBISHI ELECTRIC CORP 发明人 KUME MASASANE;KOBAYASHI HIROKI
分类号 H01Q1/42;B32B5/24;B32B27/34;B64C1/36;H01Q1/28 主分类号 H01Q1/42
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