发明名称 METAL MATRIX COMPOSITE USED AS HEATING ELEMENT
摘要 PROBLEM TO BE SOLVED: To provide a structural substrate for an aircraft structure, and a method of manufacturing the same.SOLUTION: A structural substrate 300 is made of a multi-layer hybrid composite material, which comprises an outermost layer 302, an intermediate layer 304, and an innermost layer 306. The outermost layer 302 comprises an electrically conductive metal matrix composite 308 that can conduct electricity for heating. The intermediate layer 304 comprises an electrical insulator coupled to the outermost layer to electrically insulate the outermost layer 302 from the innermost layer 306. The innermost layer 306 comprises a composite coupled to the intermediate layer 304.
申请公布号 JP2014195990(A) 申请公布日期 2014.10.16
申请号 JP20140020011 申请日期 2014.02.05
申请人 BOEING CO 发明人 PAUL S NORDMAN;LOFTIS RICHARD J;ANDREW ARMATORIO
分类号 B32B7/02;B32B15/08;B64D15/18;H05B3/10;H05B3/12;H05B3/20 主分类号 B32B7/02
代理机构 代理人
主权项
地址