| 摘要 |
The invention relates to a device for in-flight adjustment of the incidence of a lifting wing such as a parachute for example. The control of the shrouds a, b, c, d gathered into a bundle is done by means of a right-hand lever 10D and of a left-hand lever 10G by virtue of anchoring means configured in such a way that a controlled curvature of each of the two half-wings, controlled by each of the levers, is obtained symmetrically or asymmetrically. The invention applies especially to lifting wings. <IMAGE>
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