Abstract: A rigid propulsion wing for a moving vehicle, including at least one first section and one second section, a first end and a second end each including attachment means for reversibly connecting to said moving vehicle, said first section and said second section being movable with respect to each other by means of articulating means such that said propulsion wing assumes, and moves from, at least a first deployed position to a second deployed position, and vice versa, in which deployed positions said first and second sections are arranged, substantially vertically, in the extension of each other, and in which said first end, or respectively said second end, are reversibly connected to said moving vehicle by means of the attachment means thereof.

Abstract: A wing for the propulsion of a craft includes an external envelope and at least one profile structure surrounded by the external envelope. The profile structure has an articulated internal structure and an assembly of controllers to control a deformation of the external envelope. Each controller is rotatably mounted with respect to the internal structure. Each controller is also rotatably mounted with respect to the external envelope through at least one rotating link, and includes at least one curved surface configured to orient a curvature of the external envelope locally between a controller and an adjacent control controller.