发明名称 |
Welded aluminum structural component for aircraft comprises a skin field and a reinforcing element on which a connecting element made from an aluminum cast material is arranged |
摘要 |
Welded aluminum structural component (1) comprises a skin field (2) and a reinforcing element (3) on which a connecting element (4) made from an aluminum cast material is arranged. An independent claim is also included for a aircraft fuselage partially made from the welded aluminum structural component. |
申请公布号 |
DE10332003(B3) |
申请公布日期 |
2004.12.16 |
申请号 |
DE2003132003 |
申请日期 |
2003.07.14 |
申请人 |
EADS DEUTSCHLAND GMBH |
发明人 |
PALM, FRANK |
分类号 |
B23K26/14;B23K26/20;B23K26/24;B23K26/32;B64C1/12 |
主分类号 |
B23K26/14 |
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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