发明名称 |
Structural component for aircraft |
摘要 |
<p>The component forms a flexible beam, particularly a supporting one in an aircraft. It can comprise top and bottom shells one above the other in the vertical direction (6,7) and respectively of metal and composite fibre. Together these can form an aircraft wing (2) or an aileron. Aluminium, titanium- or steel-alloy can be used as the metal, and carbon-fibre-reinforced plastic as the composite material. Alternatively, boron-, glass- or synthetic fibre can be used as the reinforcement.</p> |
申请公布号 |
EP0732262(B1) |
申请公布日期 |
2004.11.17 |
申请号 |
EP19960101397 |
申请日期 |
1996.02.01 |
申请人 |
AIRBUS DEUTSCHLAND GMBH |
发明人 |
GILLANDT, SIEGFRIED, DIPL.-ING.;KROEBER, INGO, DIPL.-ING. |
分类号 |
B64C1/00;B64C3/20;(IPC1-7):B64C1/00 |
主分类号 |
B64C1/00 |
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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