An autonomous sailing vessel may include a hull, a mast, a sail, and a rudder. The mast may be mechanically coupled to the hull. The sail may be mechanically coupled to the mast. The rudder may be mechanically coupled to the hull. A heading of the autonomous sailing vessel may be regulated by actively controlling the rudder without actively controlling the sail. Alternatively or additionally, the autonomous sailing vessel may include an anticapsize stabilizer tank, a lidar system, and/or marine mammal monitoring and identification.

A system for autonomous ocean data collection includes at least one sensor capable of collecting sensor data, at least one transmission device, and at least one computing device comprising one or more hardware processors and memory coupled to the one or more hardware processors, the memory storing one or more instructions which, when executed by the one or more hardware processors, cause the at least one computing device to generate data for transmission based on the sensor data collected by the at least one sensor, and cause the at least one transmission device to transmit the data.

The systems and associated methods are for autonomously launching and recovering payload objects such as vessels, equipment and people by partially submerging a multi-mode unmanned vehicle in a controlled manner. Mechanical, power, signal and logical system components operate in a coordinated manner to repeatedly and reliably perform unmanned launch and recovery of payloads in a variety of conditions and sea states from a catamaran style hull with multi-mode, high-performance characteristics.

A sail includes at least three sides, namely two longitudinal sides respectively called luff and leach, as well as a lower transverse side called foot consisting of an assembly of panels having transverse edges parallel to the foot and longitudinal edges parallel to the luff and the leach, each panel being hinged to the adjoining panel around an axis parallel to the foot. Each of the panels includes reinforcing elements distributed into the two following groups: (a) a first group in which they extend parallel and in proximity to said transverse edges, and (b) a second group in which they extend parallel and in proximity to the longitudinal edges of the panel. They are connected two by two by connection parts in the continuation of the reinforcing elements of the second group, so that the forces assumed by the reinforcing elements are transmitted longitudinally from one panel to another.

A submersible vessel having wing and keel assemblies that are extendable for wind-powered surface operation and retractable to reduce drag for submerged operation or to place the vessel in a more compact configuration. A deployment mechanism including an actuator and linkage pivots the wing and keel assemblies-simultaneously between the deployed and retracted configuration. The vessel may have first and second pressure hulls flanking the wing and keel assemblies. A drive mechanism including a motor and a gear train employing pulley-and-cable assemblies rotates either the wing and flap together such that the flap angle relative to the wing is constant, or to change the flap angle relative to the wing with the wing angle of incidence held constant. The invention also provides a retractable wind-powered propulsion apparatus that is mountable to the hull assembly of a submersible or non-submersible vessel.

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.

The invention relates to an at least partially wind-propelled ship, comprising a double airfoil mounted on a structure controlled angularly around a generally vertical axis depending on conditions, where the double airfoil comprises a fore flap and an aft flap at least one of which has a fore-to-aft asymmetry and separated by a slit, where each flap comprises a series of shape members distributed in height, wherein said structure comprises a fore mast and an aft mast connected by a boom member and by a gaff member.

The shape members of the fore flap are traversed by the fore mast while being able to turn around an axis defined thereby, while the shape members of the aft flap are traversed by the aft mast while being able to turn around an axis defined thereby.

The invention relates to a wing type rigid sail fragmented into independent segments, where general principle involves diving the rigid sail into different segments that can position themselves independently from neighboring segments, depending on the wind received, with the profile of the sail controlled following two independent but complementary methods, where the segments at the front of the sail are linked together by their front flap, through a process that allows adjusting their relative freedom, playing on the angle that each segment can take compared to neighboring segments, and on the back of the sail sheet, the rope allowing sail adjustment links each segment by its back flap, top to bottom, allowing for adjustment of the opening up of the sail while keeping the desired flexibility of the sail.

In order to be able to determine with precision the location of the stagnation point at different zones along the leading edge of an aerodynamic profile, a system comprises rows of pressure sensors distributed on either side of the leading edge and forming, virtually, patterns that are spaced apart from one another in the form of simple polygonal lines, and a computer connected to the pressure sensors. The computer determines, along each of the patterns, a respective stagnation point position that is defined by a curved abscissa for which a pressure interpolated on the basis of pressure measurements provided by the pressure sensors of the corresponding row is at a maximum, and by an altitude evaluated on the basis of respective altitude data from the pressure sensors of the corresponding row.

This relates to a propulsion device for a vessel, including at least one hollow wing which includes: an envelope which delimits an internal volume and which includes a rear part including two perforated zones; a suction device, to generate a flow of sucked air which is intended to pass through the perforated zones; and a shutter, adapted to alternately close one of the two perforated zones. The shutter includes: at least one shutter member which consists of a flexible flap, and an operator structured to operate the flexible shutter within the frame.