| 摘要 |
A wing (12) for a projectile is described, which has a strut arrangement (14, 16, 18) which can be folded out and consists of a leading-edge spar (14), a rear spar (18) and a root spar (16), and has a covering which covers the strut arrangement when the wing (12) is in the folded-out position. In order to restretch the covering when the strut arrangement (14, 16, 18) is in the folded-out position, a lever element (40) is provided between two spars (14, 16 and 14, 18 respectively) which are connected to one another in a hinged manner, which lever element (40) is connected in a hinged manner by means of its one end section (42) to one of the spars which are connected in a hinged manner, and which, by means of its second end section (44), can be displaced along a link (46) which is provided on the other of these spars. A restretching device (52), which is effectively connected to the lever element (40) via a cable run (38, 58), is provided for restretching the covering of the folded-out wing (12). <IMAGE>
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