Abstract: The present invention relates to a charging station for electric vehicles comprising a containment body that houses a plurality of electric charging systems, each of which is independent and provided with a battery charger operatively connected to the electric power supply, a charging cable operatively connected to the battery charger, a management device of the charging cable; wherein each of the electric charging systems comprises an activation button and wherein the containment body comprises a plurality of inner carters able to define separate housing portions for the charging cables and an initialization button of the charging station, wherein the computerized control means are able to allow the activation of the battery charger by simultaneously pressing said initialization button and the activation button, and are able to allow the movement of the pulley for the winding of the charging cable following a winding command from the user or after a predetermined deactivation time of the battery charger, whe

Abstract: The present invention relates to an aircraft (100) comprising: a fuselage (101) comprising a plurality of panels (105) adapted to define an aerodynamic shape for a cockpit or a cargo hold of the aircraft (100); at least one wing (103) structurally connected to the fuselage (101) and adapted to allow flying of said aircraft (100), the wing (103) comprising a plurality of wing surfaces and at least a frame configured to support the wing surfaces; a propulsion system for the aircraft (100), comprising at least one electric motor, and batteries adapted to store electrical energy to supply the electric motor. The batteries comprise first structural batteries which constitute at least one surface (104a, 104b) of the wing surfaces, and further second structural batteries which constitute at least one panel (105) of the panels of the fuselage.

Abstract: An arm made of composite material, and relative production method, consisting of a plurality of articulated segments with a longitudinal main axis (x), pivoted to each other, each of the articulated segments comprising a box-like structure and at least a joint element attached thereto by means of gluing, the box-like structure having an end cooperating with an end of the joint element on the inside of the surface of the joint element. The ends define a substantially conical reciprocally overlapping area and have profiles concordantly inclined by an angle (?) with respect to the longitudinal axis (x).

Abstract: An arm made of composite material, and relative production method, consisting of a plurality of articulated segments with a longitudinal main axis (x), pivoted to each other, each of the articulated segments comprising a box-like structure and at least a joint element attached thereto by means of gluing, the box-like structure having an end cooperating with an end of the joint element on the inside of the surface of the joint element. The ends define a substantially conical reciprocally overlapping area and have profiles concordantly inclined by an angle (?) with respect to the longitudinal axis (x).