Abstract: An aerial vehicle is programmed or configured to respond to reports of events or conditions within spaces of a facility. The aerial vehicle travels to a location of a reported event or condition and captures data using onboard sensors. The aerial vehicle independently determines whether the reported event or condition is occurring, or is otherwise properly addressed by resources that are available at the location, using images or other data captured by the onboard sensors. Alternatively, the aerial vehicle transmits a request for additional resources to be provided at the location, where necessary. A map of the location generated based on images or other data captured by the onboard sensors may be utilized for any purpose, such as to make one or more recommendations of products that are appropriate for use at the facility.

Abstract: A grounding skeg for a landing craft configured for stem landing onto, and setting off from, a ground surface, the grounding skeg including: an elongate grounding body having a fore end and an aft end; and a removable pulling propeller functionally connected to the fore end of the body; wherein the pulling propeller is able to drive the landing craft ahead and astern; and the grounding body is locatable on the landing craft such that; the grounding body provides contact with the ground surface during stem landing of the landing craft; the fore end of the grounding body faces a bow end of the landing craft; and the aft end of the grounding body faces a stem end of the landing craft.

Abstract: A watercraft system is provided. The watercraft system includes a lifting body designed to generate dynamic lift during watercraft operation. The lifting body is shaped with a twist from the center to the lateral edges and with a chord and a fore-aft cross-section that both decrease from a center of the lifting body to lateral tips of the lifting body.

Abstract: This relates to the field of aerohydrodynamics and can be used on wings and control surfaces of aircraft, controlled spoilers of sports cars, all-movable masts and sails of sailing yachts and sailboards, as well as on blades and vanes of various bladed machines. An aerohydrodynamic surface includes an array of vortex generators and a main part. The main part comprises two sides mating with each other to form a leading and a trailing edges. The array of vortex generators includes elevations with crescent-shaped working edges located near the leading edge. The elevations and the working edges are configured to generate counter-rotating vortex structures. An array of vortex generators and a method of mounting the same onto the aerohydrodynamic surface are also described. The invention makes it possible to improve the properties of the aerohydrodynamic surfaces at high angles of attack.

Abstract: A multihull watercraft has at least three hulls extending longitudinally along the watercraft. The hulls at least partly define a port side tunnel and a starboard side tunnel therebetween. A port deflection device is configured to engage water in response to the watercraft leaning toward the port side when turning. The port deflection device is laterally aligned with the port side tunnel. A starboard deflection device is configured to engage water in response to the watercraft leaning toward the starboard side when turning. The starboard deflection device is laterally aligned with the starboard side tunnel. Each of the deflection devices includes an angled surface extending downwardly and rearwardly from an upper tunnel surface of a corresponding one of the tunnels. The angled surface is positioned to remain above a water line when the multihull watercraft is at rest on water.

Abstract: A hydrofoil watercraft system comprising: a flotation device; a downward mast extending from a bottom surface of the flotation device; a fuselage, a foil wing extending from one first end of the fuselage; and a plurality of fins independently movable independent of one another, wherein at least two of the movable fins extend in opposite directions from one second end of the fuselage, where the movable fins are used for steering the watercraft. The system further includes a controller for receiving user input, wherein the controller drives the movable fins respectively based on the user input. One of the movable fins is driven by the controller to rotate along a first axis while another of the movable fins is driven by the controller to rotate along a second axis, wherein the first axis and the second axis are substantially symmetrical with respect to the fuselage.

Abstract: A personal watercraft is disclosed including a flotation portion, a strut extending from the flotation portion, and a motor pod is disposed along the strut with an electric motor operably coupled to a driveshaft. A hydrojet unit is removably attached to the motor pod and includes an inlet portion removably attached to the motor pod and a substantially cylindrical housing. The inlet portion includes a substantially conical motor interface with a shaft through-hole for receiving the driveshaft therein, one or more fins extending outwardly from the conical motor interface, and at least one ring encircling the conical motor interface and connecting to each of the one or more fins for inhibiting objects from passing through the inlet region. The housing defines a fluid flow path to an outlet portion. The hydrojet unit includes an impeller coupled to the driveshaft and a stator disposed within the housing.

Abstract: Various embodiments of a submerged submersible sailing vessel are disclosed. Such a submerged sailing vessel may comprise a submersible hull assembly, a keel coupled to and extending upwards from hull assembly towards a water surface, and a wind-catching assembly coupled to and extending upwards into the air from the keel for propelling the submerged sailing vessel. The hull assembly and the keel are submerged below the water surface as the vessel is propelled by the wind-catching assembly above the water surface.

Abstract: A watercraft including a board having a top surface and a bottom surface and a hydrofoil attached to a strut. The strut attaches at the bottom surface of the board. The watercraft includes a movable portion coupled to the top surface of the board such that the movable portion is configured to move relative to a fixed portion of the board.

Abstract: A system for a transom-mount trim tab with a fluid hinge, including a trim tab having a planar surface, a forward section located under a hull of a watercraft, a rear portion extending aft of a transom, a pair of guiding tabs coupled to the trim tab, and a forward mounting means including fluid hinge brackets, each with a mounting plate, and a containment protrusion. The system further includes a pair of aft mounting brackets configurable for variable mounting, wherein each mounting bracket includes a vertical leg having an upper portion configurable to be angulated relative to a transom of a watercraft and a bottom portion configured in a vertical orientation. The upper portion of the vertical leg and the mounting bracket have a configurable angle there-between.

Abstract: A personal watercraft is disclosed including a flotation portion, a strut extending from the flotation portion, and a motor pod is disposed along the strut with an electric motor operably coupled to a driveshaft. A hydrojet unit is removably attached to the motor pod and includes an inlet portion removably attached to the motor pod and a substantially cylindrical housing. The inlet portion includes a substantially conical motor interface with a shaft through-hole for receiving the driveshaft therein, one or more fins extending outwardly from the conical motor interface, and at least one ring encircling the conical motor interface and connecting to each of the one or more fins for inhibiting objects from passing through the inlet region. The housing defines a fluid flow path to an outlet portion. The hydrojet unit includes an impeller coupled to the driveshaft and a stator disposed within the housing.

Abstract: One embodiment of submerged superventilated blades (101) that provide hydrodynamic force to a vessel or aircraft (117) that can lift it above the surface of the water (106) at high speed by creating thrust with a wetted high pressure surface (111), the low pressure surface (112) being covered with a gas filled void in the liquid, thus preventing sudden loss of lift as speed increases due to cavitation or surface venting. Other embodiments are described and shown.

Abstract: A buoyancy adjusting device for an underwater device is described the device comprising: a tube having first and second ends; a resilient mechanism located at the first end of the tube and extending towards the second end of the tube; an opening near the second end of the tube; a catch at the second end of the tube; 5 and at least one block insertable into from the first end of the tube to adjust the buoyancy.

Abstract: A system of cross-shaped units and nodes used to construct strong, lightweight, inexpensive space frames with alternately rigid and flexible components, in which each cross-shaped unit which fits together with five like units to form a spherical node which can be connected to other nodes to form frames for the production of structures including toys, playground structures, lattices, pergolas, statues, roofs, furniture, fixtures, mattresses, kites, lamps, artistic structures and fixtures, floating platforms, flexible joints for machines or robots, buildings, bridges and space stations.

Abstract: A personal watercraft is disclosed including a flotation portion, a strut extending from the flotation portion, and a motor pod is disposed along the strut with an electric motor operably coupled to a driveshaft. A hydrojet unit is removably attached to the motor pod and includes an inlet portion removably attached to the motor pod and a substantially cylindrical housing. The inlet portion includes a substantially conical motor interface with a shaft through-hole for receiving the driveshaft therein, one or more fins extending outwardly from the conical motor interface, and at least one ring encircling the conical motor interface and connecting to each of the one or more fins for inhibiting objects from passing through the inlet region. The housing defines a fluid flow path to an outlet portion. The hydrojet unit includes an impeller coupled to the driveshaft and a stator disposed within the housing.

Abstract: Disclosed is a method for controlling a hydrofoil board powered by a motor driven propeller. The motor is controlled by a hand controller configured with user selectable operating pre-sets including a first operating pre-set, wherein the board is accelerated to a first speed which is less than that required for the board to hydrofoil, and a second operating pre-set, wherein the board is accelerated to a second speed sufficient for the board to hydrofoil. Alternatively, the operating pre-sets may limit the motor power. A system for operating a hydrofoil board is also disclosed, which includes a propulsion control unit comprising a propulsion source, and a hand controller configured to receive a first user input and a second user input and to transmit the user inputs to the propulsion control unit.

Abstract: A propulsion system for a vessel includes an engine propulsion unit that provides a propulsive force to a hull by using an engine as a power source, an electric propulsion unit that provides a propulsive force to the hull by using an electric motor as a power source, a storing mechanism that is displaced from an actuating position to actuate the electric propulsion unit to a storing position to store the electric propulsion unit and performs a storing operation to store the electric propulsion unit, and an interlock controller that interlocks a storing operation of the storing mechanism with generation of a propulsive force by the engine propulsion unit.

Abstract: A hydrofoil (1) includes a mast (2), with an incoming flow edge (3), a discharge edge (4), lateral surfaces (5) and an upper mast end (6) with a holder (7) to be fastened to a watersports board. A fuselage (8) has front (10) and rear wings (11) are arranged on opposite sides. The mast and the fuselage are configured as separate components and are connected to one another via a screw connection (12). An adapter (13) is connected to the mast and to the fuselage and is arranged in a recess (14) of the fuselage. A positive locking is established between an adapter outer surface (15) and the recess of the fuselage. An adapter mount (16) receives a lower mast end (9). A positive locking is formed between the mast and the adapter such that the lower mast end is arranged within the fuselage.

Abstract: A hull locating arrangement for a vessel is disclosed that has a body at least partially suspended above at least a first hull by at least one support. The hull locating arrangement includes for the first hull a forward locating linkage and a rearward locating linkage, each of the forward locating linkage and the rearward locating linkage being connected between the first hull and the body to together constrain said hull in the lateral, longitudinal, roll and yaw directions relative to the body. The forward locating linkage includes a forward radius arm and a drop link, the drop link being pivotally connected to the radius arm. The rearward locating linkage includes a rearward radius arm connected between the body and the first hull.

Abstract: An inflatable shuttle boat including a seat tube, a pair of exterior buoyancy tubes, and a pair of foot support tubes. The seat tube has an elongate, cylindrical outer surface that is centrally located and extends from a front end to an aft end, the seat tube sized for single-file, straddled seating of a plurality of riders on top of the cylindrical outer surface. The pair of exterior buoyancy tubes have an elongate shape providing exterior sides of the inflatable shuttle boat, each of the pair of exterior buoyancy tubes having a larger diameter and height than the seat tube and extend in a parallel disposition to the seat tube at right and left sides. The pair of foot support tubes have elongate shapes extending adjacent and parallel to the seat tube in coupled engagement between the pair of exterior buoyancy tubes and the seat tube.

Abstract: A vessel having a stern and a bow, a deck having a top surface and a bottom surface; a first outer pontoon, a second outer pontoon, a central pontoon, and the motor pod each disposed below the deck and mounted to the bottom surface of the deck. The central pontoon is disposed between the first outer pontoon and the second outer pontoon, wherein the outer pontoons are spaced apart. The motor pod is disposed behind the central pontoon and between the first outer pontoon and the second outer pontoon. The motor pod defines a running surface, wherein the vessel is capable of planing on the running surface. The motor pod supports a motor at the rear. The vessel provides the ride characteristics and stability of a pontoon-style vessel at rest and at lower speeds while also providing the performance, maneuverability, and turning radius characteristics of a V-hull sport boat.

Abstract: One embodiment of submerged blades (101) that provide hydrodynamic force to a vessel or aircraft (117) that can lift it above the surface of the water (106) at high speed by creating thrust with a single wetted high pressure surface (111), the low pressure surface (112) being covered with a gas filled void in the liquid, thus preventing sudden loss of lift as speed increases due to cavitation or surface venting. Other embodiments are described and shown.

Abstract: A boat maneuvering control method for a boat provided with a propulsion device includes acquiring a target orientation, acquiring an actual orientation of the boat, setting a target yaw rate value based on orientation information of at least one of the target orientation and the actual orientation, detecting an actual yaw rate value of the boat, and controlling a direction of a thrust force of the propulsion device based on the target yaw rate value and the actual yaw rate value.

Abstract: A catamaran hull of hybrid structure includes a first lateral float, a second lateral float and a central float connecting the first lateral float to the second lateral float; the hull further including a first beam having a first bulkhead and a second beam having a second bulkhead, each bulkhead lying in a plane substantially perpendicular to the bow-stern line and including: a central part including a lower element intended to collaborate with a lower part of the central float; a first lateral part including a lower element intended to collaborate with a lower part of the first lateral float; a second lateral part including a lower element intended to collaborate with a lower part of the second lateral float; the hull part arranged between the first bulkhead and the second bulkhead defining a monobloc hull portion.

Abstract: A motion control system for a ship has one or more sensors generating sea condition data and at least one ship control system. Analyzer software receives the sea condition data and predicts a sea condition event. Calculator software calculates one or more commands in preparation for the sea condition event. Interface software communicates the one or more commands to the at least one ship control system and the at least one ship control system implements a command in advance of the event. The at least one ship control system may comprise a ride control system having one or more motion control devices. The at least one ship control system may also comprise an auto pilot system.

Abstract: A system of cross-shaped units and nodes used to construct strong, lightweight, inexpensive space frames with alternately rigid and flexible components, in which each cross-shaped unit which fits together with five like units to form a spherical node which can be connected to other nodes to form frames for the production of structures including toys, playground structures, lattices, pergolas, statues, roofs, furniture, fixtures, mattresses, kites, lamps, artistic structures and fixtures, floating platforms, flexible joints for machines or robots, buildings, bridges and space stations.

Abstract: A propulsion system for a vessel includes an engine propulsion unit that provides a propulsive force to a hull by using an engine as a power source, an electric propulsion unit that provides a propulsive force to the hull by using an electric motor as a power source, a storing mechanism that is displaced from an actuating position to actuate the electric propulsion unit to a storing position to store the electric propulsion unit and performs a storing operation to store the electric propulsion unit, and an interlock controller that interlocks a storing operation of the storing mechanism with generation of a propulsive force by the engine propulsion unit.

Abstract: An aircraft of flying wing or blended wing body type comprising, for access to a pressurized housing, a non-pressurized door in the trailing edge of the aircraft and a pressurized door on the pressurized housing. The distance between the center of the pressurized door and a plane of symmetry of the aircraft is less than or equal to the distance between the center of the non-pressurized door and the plane of symmetry, and the pressurized door is located on a wall other than a rear wall of the pressurized housing or upstream of a rear extremum point of the housing in the absence of any such rear wall.

Abstract: A suspension system for a multi-hulled vessel including: a chassis and at least one left hull and at least one right hull; a front left, a back left, a front right and a back right support arrangements with respective rams; a first adjustment accumulator having a fluid chamber and a gas chamber; and a first actuator to transfer or effectively transfer fluid between the fluid chamber of the first adjustment accumulator and at least one compression chamber of a respective ram of a first support arrangement comprising one or more of the front left, front right, back left or back right support arrangements. A static pressure in the gas chamber of the first adjustment accumulator being within 25% of a static operating pressure in the at least one compression chamber of the at least one ram of the first support arrangement.

Abstract: The invention relates to systems and methods for charging a vehicle. A vehicle and charging station can be designed such that an electric or hybrid vehicle can operate in a fashion similar to a conventional vehicle by being opportunity charged throughout a known route.

Abstract: A blade for a wind turbine defines an airfoil with a leading edge section and a trailing edge section, notably a flat-back trailing edge. A rounded connecting section interconnects a pressure side section of the airfoil and the trailing edge section. The rounded connecting section attaches to the pressure side section at a transition point, in which the pressure side section's tangent does not coincide with the rounded connecting section's tangent, so that the outer surface of the airfoil has a sharp corner at said transition point. The truncated radius, i.e. geometrical discontinuity, thus formed at the transition between the pressure side section and the trailing edge section increases the aerodynamically effective surface of the pressure side and enables forced and hence controlled flow separation without compromising ease of manufacture and structural stability of a fiber-reinforced structure making up a shell of the blade.

Abstract: An aircraft assembly is disclosed and includes a fuselage including a turbine engine mounted within the aft fuselage. A burst zone is defined about the turbine engine and a tail is disposed at least partially with the burst zone. The tail includes primary control surfaces and sacrificial control surfaces. The sacrificial control surfaces can break away in a defined manner to maintain integrity of the primary control surfaces outside of the burst zone.

Abstract: A ship hull comprises a main hull portion having a bottom extending along a centerline from a leading edge, having first and second sides and having a top surface and an inclined leading surface. The ship hull further comprises first and second side skegs extending along the first and second sides of the main hull portion from the leading edge thereof, each of the first and second side skegs having outside and inside surfaces and extending to a bottom surface below the leading surface. A foil located between the first and second side skegs extends between first and second ends at a position below the leading surface. The leading surface of the main hull portion joins with the bottom surface of the first and second side skegs at a transition location forming a single continuous bottom surface aft thereof.

Abstract: A rotor blade of an axial compressor includes: a blade root; and a blade leaf. The blade leaf has: a flow inlet edge, a flow outlet edge, a pressure side extending between the flow inlet edge and the flow outlet edge and a suction side extending between the flow inlet edge and the flow outlet edge, which together define a blade profile of the blade leaf in Cartesian coordinate values x, y and z such that first and second profile coordinates, or the coordinates x and y when joining via continuous arcs, each describe a smooth profile section on a radial section height along a third profile coordinate, or the coordinate value z, and the joining of the radial profile sections with a smoothing function describe the blade profile of the blade leaf.

Abstract: In an apparatus for controlling posture of a small boat having a hull and an even number of outboard motors mounted side by side on a stern of the hull, each equipped with a propeller driven by an engine and a throttle actuator adjusting a throttle valve opening of the engine, an inclinometer is installed in one of the outboard motors that produces an output indicating inclination of the hull relative to a vertical axis around a roll axis. It is determined whether the hull inclines to port or starboard from the output of the inclinometer and when it does, operation of the throttle actuators of the outboard motors are controlled on a side determined to incline downward to increase engine speed, while controlling operation of the throttle actuator of the outboard motor on a side determined to incline upward to decrease the engine speed.

Abstract: A novel hull form is described consisting of a base hull that incorporates flared sides along a bow, middle, and stern sections with raked bow and stern stem lines. The bow and stern sections have lateral oriented shapes, either as an attachment or integral to the hull, spanning the hull beam. The cross sections of these shapes have a novel and specific geometric relationship in conjunction with the base hull to provide a constant cross sectional area between the forward and aft perpendiculars. The shape improves the powering and seakeeping of the vessel hull in the marine environment.

Abstract: The aerodynamic element has a cross section in an airflow direction with a trailing edge (10c). The aerodynamic element (10) further includes a non-symmetrical swallow tail shaped cavity body (1, 2) attached to the trailing edge (10c) of the aerodynamic element (10). The aerodynamic element (10) is e.g. applied in a rotor blade for a wind turbine.

Abstract: The invention relates to a vessel for operating on a body of water comprising: a non-planing hull having a waterline and a longitudinal direction with a forward portion, an aft portion, and a central portion, the hull being configured to have the aft portion with a smaller water displacement relative to a water displacement at the central portion; and an aft foil affixed to the aft hull portion with one or more connecting members, and below the surface of the water, and spaced from the hull, the aft foil having a span, a chord, and a leading edge and a trailing edge relative to a forward direction, wherein the leading edge of the aft foil is tilted at a downward angle relative to the horizontal, wherein the aft foil has a chord and profile in longitudinal cross section, with a configuration to provide a lifting force, the tilt angle of the chord of the aft foil being measured with respect to the horizontal, and wherein the aft foil is oriented to provide a continuous, upward, forwardly directed component of t

Abstract: A system (16) for providing an air lubricating layer between a substantially flat bottom (6) of the hull (4) of a vessel (1) and water flowing under the bottom as the vessel is moving through the water. The system has a cavity (33) with a deflector. The deflector has an elongate part (29,34,34?) extending in the length direction of the cavity over at least at least 5%, preferably at least 10% of the cavity length L, wherein a projected area of the at least one deflector member (24,24?-26,26?) on the interface plane (30) covers at least 25%, preferably at least 50%, most preferably at least 75% of the surface area of the interface plane.

Abstract: A hull mounted, steerable marine drive system having trim actuation is both steerable through 360 degrees and is trimmable. The marine drive system includes a watertight enclosure assembly for sealing the hull, which is adapted for keeping much of the marine drive system from being exposed to water. The enclosure includes a gasket flange plate, a retention plate and a folded gasket. The gasket flange plate closely follows the contour of the hull and enhances the hydrodynamic and wake performance of the present marine drive system. Further, marine drive system includes a forward-neutral-reverse (FNR) transmission assembly, a drive unit assembly having a trimmable upper unit and a steerable lower unit, a steering actuator assembly, a trim actuator assembly, and, preferably, trim foils for providing enhanced negative and positive trim and for providing enhanced positive and negative lift.

Abstract: Disclosed is an apparatus, optionally mounted on a stand up paddle board, or surfboard, to lift the board above the water surface and support the board in a stable position above the water surface while a rider standing on the board and maintaining a speed in the water via paddling. In one embodiment, the apparatus includes a strut; a fuselage connected to said strut; a back foil portion connected to an aft end of said fuselage wherein the back foil portion includes two back wings extending outwardly from said aft end of said fuselage; and a forward foil portion connected to a fore end of said fuselage wherein the forward foil portion includes two front wings extending outwardly from said fore end of said fuselage and wherein the forward foil portion has a maximum thickness located at first distance from the fore edge of the forward foil portion.

Abstract: A hydrofoil having an integrated yoke-bridge to preclude expansion of the channel defined by the yoke when the hydrofoil is secured to the cavitation plate. The single piece hydrofoil is secured to the cavitation by lateral screws passing through the hydrofoil and engaging the side of the cavitation plate. Additionally, one or two holes are optionally drilled through the single piece hydrofoil and through the cavitation plate followed by insertion of bolts passing through the hydrofoil and the cavitation plate.

Abstract: An aeroplane includes a fuselage having a pair of hydrofoils providing hydrodynamic lift and stabilization arranged in the form of an inverted V. The junction between each hydrofoil and fuselage is situated forward the center of gravity of the aeroplane. The distance separating the junction between each hydrofoil and the fuselage, with respect to the center of gravity of the aeroplane is comprised between 0 and 170% of the mean aerodynamic chord of the main wing of the aeroplane, preferably between 20% and 135%. Each hydrofoil is inclined downwards, from its leading edge in the direction of its trailing edge. The straight line connecting these two edges form, a nominal pitch angle comprised between 2 and 12°, preferably between 6 and 8°. A part of the hydrofoil is located beneath a horizontal tangential plane of the aeroplane; each hydrofoil has a flexible intermediate section allowing the hydrofoil to flex upwards.

Abstract: An assembly (300), including a hydrofoil (302), is provided for mounting on the anti-ventilation plate (14) of a sterndrive or outboard motor (16) without the need to modify the plate or motor. The hydrofoil (302) of the assembly (300) has a series of holes (308) spaced along its width to receive a series of mounting disk assemblies (304) having a stepped disk (310). A carriage bolt (314) forming a part of each mounting disk assembly (304) is placed in the hole (308) closest the edge (36, 38) of the plate (14), a stepped disk (310) is placed over the end of the bolt (314) and the hydrofoil (302) is clamped on the plate (14) by tightening nuts (316) to clamp the plate (14) between the hydrofoil (302) and step (362) of the disk (310). Friction material (312) on the mounting disk assemblies provides firm engagement with the plate (14). A catch (206) can be mounted between the hydrofoil (302) and the trim tab or anode recess (76) in the plate (14).

Abstract: A watercraft including a side-hull extending downwardly from each side of a hull of the watercraft. A foil extends downwardly and inwardly from each side-hull.

Abstract: A watercraft, including; a mid section (2) and two side sections (3,4), whereby the mid section (2) has a seat (5) for a passenger and whereby the watercraft (1) has a steering mechanism. The watercraft (1) includes a front part (2) and a rear part, relative to a direction of travel of the watercraft (7), that are coupled together by means of a hinged coupling (8). The front part (2) of the watercraft (1) includes the mid section (2) of the watercraft (1), and the rear part (7) of the watercraft (1) includes the two side sections (3,4). The hinged coupling (8) forms part of the steering mechanism, such that as a result of a rotation of the front part (2) with respect to the rear part (7) of the watercraft (1) around the hinged coupling (8), the direction of travel of the watercraft (1) is changed.

Abstract: A hydrofoil having an integrated yoke-bridge to preclude expansion of the channel defined by the yoke when the hydrofoil is secured to the cavitation plate. The single piece hydrofoil is secured to the cavitation by lateral screws passing through the hydrofoil and engaging the side of the cavitation plate. Additionally, one or two holes are optionally drilled through the single piece hydrofoil and through the cavitation plate followed by insertion of bolts passing through the hydrofoil and the cavitation plate.

Abstract: A board including a contact section, and a first step section which is at a different height from the contact section so that it does not make contact with a substantially level water surface when the board is at rest on the top of the substantially level water surface. The board further including a first hydrofoil fixed to the first step section. The first hydrofoil includes a keel and the first hydrofoil is fixed the first step section so that the keel is substantially perpendicular to the board. The first hydrofoil includes a wing which is fixed to and substantially perpendicular to the keel of the first hydrofoil. The wing is angled relative to the first step section from zero degrees to ninety degrees. The board may include a second step section and a second hydrofoil, which may be fixed to the second step section.

Abstract: An improved elongated board for a flying ski designed to be towed behind a conventional powered watercraft utilizing a standard ski tow rope or similar device. The elongated board comprises a front end and a back end. The front end extending from a front edge to about one-half of the length of the elongated board, the back end extending from a back edge to about one-half of the length of the elongated board, and the back end has a greater mass than the front end.

Abstract: A foil structure for providing buoyancy and lift to a floating device is provided. The foil structure comprises an elongated left hand side floating device section and an elongated right hand side floating device section. The left hand side floating device section and the right hand side floating device section are placed at a predetermined distance to a longitudinal axis of the floating device and oriented substantially parallel thereto. A left hand side foil and a right hand side foil protrudes from the left hand side floating device section and the right hand side floating device section, respectively, towards a vertical plane through the longitudinal axis and is oriented at an acute angle to a horizontal plane. A leading edge of each foil intersects the respective floating device section in proximity to a bow portion thereof. Each foil extends along the respective floating device section and terminates in proximity to a stern portion thereof.