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A METHOD OF FOLDING AND DEPLOYING THE WINGS OF AN UNMANNED AERIAL VEHICLE WITH TUBE-LAUNCHER TAKE-OFF, AND THE WING OF AN UNMANNED AIRCRAFT WITH TUBE-LAUNCHER TAKE-OFF
A METHOD OF FOLDING AND DEPLOYING THE WINGS OF AN UNMANNED AERIAL VEHICLE WITH TUBE-LAUNCHER TAKE-OFF, AND THE WING OF AN UNMANNED AIRCRAFT WITH TUBE-LAUNCHER TAKE-OFF
A method of folding and deploying the wings of an unmanned aerial vehicle with tube-launcher take-off in which the wings are folded along the fuselage, characterised in that the wings are folded along the fuselage (2), and then a section of the wing is folded along its span. The folded aircraft is inserted into a tube launcher and, after a take-off by launching, the wing deploys in the reverse order. First, the wing profile folds straighten and the profile cross-section assumes its proper shape. Then, the wings deploy out of their orientation along the fuselage (2) into a position transverse to the fuselage (2). The wing of an unmanned aerial vehicle with tube-launcher take-off characterised in that it has at least one fold along its span.
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