| 摘要 |
<p>Unmanned air vehicle (UAV) having wings 104, 106 and tailerons 108, 110 hinged (fig 6) to a fuselage (102, fig 1) to move between deployed and stowed positions, preferably with a combination of translation and rotation. The wings and tailerons may be magnetically 402, 404, (3020, 3022, 1142, 1140, fig 30) coupled to the fuselage. The power supply may be load bearing. The propeller 116 may also be hinged. The fuselage may comprise a plurality of bonded layers or additive layers formed by a printing process. Packaging for storing the vehicle is also disclosed (figs 22-24).</p> |
