发明名称 Structural component for aircraft shells has reinforcement element, which is partly coated with cladding element, embedded in the carrier element
摘要 <p>The structural component (800) has a reinforcement element (204), partly coated with the cladding element (205), which is embedded in the carrier element (202). The carrier element is made of metallic sheet component (201) with a stringer element or frame. Independent claims are also included for the following: (A) Method for manufacturing structural component; and (B) Use of structural component.</p>
申请公布号 DE102004058014(A1) 申请公布日期 2006.06.08
申请号 DE20041058014 申请日期 2004.12.01
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 VICHNIAKOV, ALEXEI
分类号 B64C1/06 主分类号 B64C1/06
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