发明名称 Wing for aircraft has first end sector of wing spar welded to wing under-plating and/or second end sector welded to top plating
摘要 <p>The aircraft wing (200) has under-plating (202), top plating (201) and a wing spar (203), which may be of double-T or C-shaped cross section. The first end sector of the spar is welded to the under-plating by laser, friction contact or electron beam welding, and/or the second sector welded to the top plating in one of these ways.</p>
申请公布号 DE102004058910(A1) 申请公布日期 2006.06.08
申请号 DE20041058910 申请日期 2004.12.07
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 SCHMIDT, HANS-JUERGEN;TELGKAMP, JENS
分类号 B64C3/00 主分类号 B64C3/00
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