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> |