发明名称 |
CORROSION-RESISTANT CONNECTION BETWEEN A FIRST COMPONENT AND A SECOND COMPONENT |
摘要 |
<p>The invention relates to a connection 1 between a first component and a second component, the first component being formed from an aluminium alloy in particular and the second component being formed from a carbon-fibre-reinforced plastics material in particular. The first component is a rib 6 in particular and the second component is preferably an angle bracket 7, with which the rib 6 is connected to an aircraft fuselage skin 2 within a fuselage reinforcement structure. The connection 1 between the components comprises, according to the invention, a ceramic coating 16 which is applied for protection against corrosion at least in the region of a contact area 9 between the components, the components being riveted and/or adhesively bonded. The ceramic coating 16 is less than 0.1 mm thick and may be formed from a mixture of aluminium oxide (AI2O3) and TiO2 for example.</p> |
申请公布号 |
WO2009000863(A1) |
申请公布日期 |
2008.12.31 |
申请号 |
WO2008EP58097 |
申请日期 |
2008.06.25 |
申请人 |
AIRBUS DEUTSCHLAND GMBH;KIRSTEIN, HAUKE;ROMING, THORSTEN;SCHROEER, THORSTEN |
发明人 |
ROMING, THORSTEN;SCHROEER, THORSTEN |
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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