发明名称 |
Structural panel component for aircraft fuselage, includes longitudinally extending and crosswise or transverse stiffening elements comprising the skin sheet of the component |
摘要 |
Longitudinally extending and crosswise or transverse stiffening elements (3,4) comprise the skin sheet (2) of the structural panel component (1). The component is formed by performing a material chip removing process on a semi-finished starting material. An independent claim is also included for a method in fabricating a structural panel component.
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申请公布号 |
DE10007995(A1) |
申请公布日期 |
2001.09.06 |
申请号 |
DE20001007995 |
申请日期 |
2000.02.22 |
申请人 |
EADS AIRBUS GMBH |
发明人 |
BRENNEIS, HARTMUT;ZINK, WALTER |
分类号 |
B64C1/12;(IPC1-7):F16S1/10;F16S5/00;B64C1/06 |
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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