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 代理人
主权项
地址