发明名称 |
Component i.e. thermally and/or mechanically attachable shell component for forming carbon fiber reinforced plastic fuselage cell of aircraft, has edge region connectable with another edge region of another component under creation of joint |
摘要 |
<p>The component (1) has an edge region (2) comprising a layer assembly formed with electrically conductive metal layers (5, 11) that are arranged over each other. The metal layers are formed of aluminum alloy, titanium alloy or stainless steel alloy. The edge region is connectable with another edge region of another component (14) including a sandwich structure under creation of an electrically conductive joint. A hybrid region (3) has a layer assembly formed with a composite material layer (6) and the metal layers.</p> |
申请公布号 |
DE102009024397(A1) |
申请公布日期 |
2010.12.16 |
申请号 |
DE20091024397 |
申请日期 |
2009.06.09 |
申请人 |
AIRBUS OPERATIONS GMBH |
发明人 |
GOEHLICH, ROBERT ALEXANDER;SAYILGAN, CIHANGIR |
分类号 |
B64C1/12 |
主分类号 |
B64C1/12 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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