A wingsail comprising: a first aerofoil having a leading edge at a front of the wingsail and a trailing edge behind the front edge; and a second aerofoil having a leading edge and a trailing edge, the leading edge of the second aerofoil being closer than the trailing edge of the second aerofoil to a point of maximum cross-sectional width of the second aerofoil; wherein the wingsail is configured such that the leading edge of the second aerofoil can be positioned behind the trailing edge of the first aerofoil; wherein the first aerofoil comprises: an air inlet; an air outlet; a channel inside the first aerofoil connecting the air inlet and the air outlet; wherein air flow from the air inlet is directed by the channel to the air outlet.

A wind propulsion unit including a dual wingsail mounted on a structure that is angularly controlled about a generally vertical axis depending on the conditions, the dual wingsail including a front flap, a rear flap and a supporting structure that allows the front flap and the rear flap to pivot about two axes that are generally parallel and spaced apart from one another, the unit also including a device for controlling the orientation of the rear flap according to the direction of incidence of the wind during propulsion. The device for controlling the orientation of the rear flap is also configured to bring the rear flap, when the wind propulsion unit is in an inactive position, into a folded orientation wherein a substantial portion of its cross-sectional extent is positioned along a substantial portion of the cross-sectional extent of the front flap.

A ship comprises at least one sail propulsion unit (100) extending in a generally vertical direction in a position of use and comprising one or more propulsion elements (111, 112) and a mast (121). According to the invention, the structure of the ship intrinsically comprises transverse structural elements (T; 300) defining at least in part at least one respective cavity, while the ship comprises at least one sail propulsion unit (100) situated generally above a cavity. The ship additionally comprises a support (210) for the sail propulsion unit, the support being movable in a generally vertical direction within the cavity (CA), and drive means for selectively moving the support between a raised position of use and a retracted position of stowage.

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.

A frame device (200) for a profiled sail device, the frame device (200) having at least one adjustable frame element (202), the at least one adjustable frame element (202) having longitudinal struts which are spaced apart from one another and are assigned to sail surfaces which are spaced apart from one another, and transverse struts which extend between the longitudinal struts, characterized in that the longitudinal struts and the transverse struts delimit quadrangles which each have two diagonals with varying lengths depending on the adjustment, and the diagonals each have a predetermined maximum length, and a profiled sail device having sail surfaces which are spaced apart from one another and against which the flow can impinge and which form profiled surfaces, a sail front edge and an adjustable skeleton device arranged between the sail surfaces. The skeleton device has at least one frame device (200) of this type.

The present invention relates broadly to a rigid wing (10) which in its preferred embodiment is a rigid wing sail fitted to a water-borne vessel. The rigid wing sail (10) comprises a pair of elongate rigid panels (12A) and (12B), and a hinge element designated generally as (14) coupled to the panels (12/B) to permit pivotal movement of the panels (12A/B) relative to one another. Each of the pair of panels such as (12A) includes an adjoining edge (16A) and an opposing lateral edge (18A). The hinge element (14) is coupled to the panels (12A/B) at the respective adjoining edges (16A/B) to form either: 1) a closed configuration of the wing (10) with lateral edges (18A/B) of respective panels (12A/B) positioned adjacent one another wherein the rigid wing sail (10) is closed; or 2) an open configuration of the wing (10) with the lateral edges (18A/B) of the respective panels (12A/B) separated from one another wherein the rigid wing sail (10) is set at a variable camber.

Provided is a radar and communications enhanced sail for a sailboat, sail ship, or sail drone. The sail includes a first sail section comprising an active communication system, a second sail section comprising a passive communication system, or a combination thereof. The active communication system includes an antenna array (transceiver) and a software-defined radio (SDR), while the passive communication system comprises a reflective panel or sections and/or array of reflector panels or sections. The active system utilizes its SDR and transceiver to communicate back and forth with an onshore SDR and transceiver to provide information as necessary. The passive system receives a radar signal via the reflective material on the sail and reflects the signal back at the radar, which produces a radar cross section indicating that there is an object (in this case the sailboat) in the ocean.

A wingsail for a powered watercraft comprising a first aerofoil element, a second aerofoil element, and a third aerofoil element, wherein each of the aerofoil elements is rotatable about an axis and has an aerofoil section with a centre of area which is closer to its leading edge than its trailing edge, and the aerofoil elements are movable to a configuration in which flow from the trailing edge of one of the first or third element is directed toward the leading edge of the second element, and flow from the trailing edge of the second element is directed toward the leading edge of the other of the first or third element.

A vessel is provided with a mast, sail, and halyard for hoisting the sail. The sail includes dollies configured to be movable along the mast. The mast includes a guide member, the guide dollies configured to cooperate with said guide member, wherein: the sail includes rigid panels, articulated two by two; the mast is equipped with a transit part positioned at the end of the guide member, which has a flared lower portion and is open at its opposite ends, wherein during hoisting of the sail, each dolly is received in the transit part and is guided along to leave it through its upper opening and cooperate with the guide member, while during its lowering, each dolly is disengaged from the guide member, is received in the transit part, moves along it, and escapes from it by following the movement of the portion of the sail with which it is integral.

A self-trimming wingsail system, comprising a wingsail body mounted on a mast and configured to rotate freely around the mast, an adjustable tail connected to the wingsail body, and a tail control mechanism configured to adjust an angle of the adjustable tail. The tail control mechanism comprising a motor, and a slidable collar connected to the motor via a collar cable and connected to the adjustable tail via a tail cable. Movement of the slidable collar transmits a linear force via the tail cable to the adjustable tail to adjust the angle of the adjustable tail.