76results about "Marine propulsion" patented technology

A wing for a traction kite, etc comprises a plurality of cells formed by chordwise-extending ribs (3), valved openings (6) to the cells allowing ram air to inflate the wing. By changing the initial cut-out of the material forming the cells near wing tips (7, 8), compared with that of the cells central to the wing, it is possible to alter the aerodynamic forces at wing tips (7, 8). This allows attachment of flying lines (9, 10) to wing tips (7, 8) only, despite the wing having no framing to maintain its spanwise shape under the loading of flying lines (9, 10). The increased aerodynamic forces at wing tips (7, 8) are achieved by making the aerofoil profiles of the cells progressively more reflexive towards wing tips (7, 8), by giving wing tips (7, 8) a residual twist increasing their angle of incidence, by placing the centres of pressure of the cells near wing tips (7, 8) somewhat forward of the pivot line of the wing, etc.

A kite safety device for a kite having an airfoil with leading and trailing edges, at least two control lines attached to the airfoil and a control flying bar attached to at least two of the control lines. The device features a trim line having a hollow central passageway, sized and shaped to fit slidably through a central opening in the control flying bar. A safety flying line is attached at its first end to a first point adjacent a midpoint along a centerline extending from the leading edge to the trailing edge and attached through said passageway at its second end to a fixture providing a point for attachment of the flying line to a harness. When the control flying bar is released a user may rotate beneath the kite and when the safety flying line is tensioned, the kite will begin to stall and the kite will descend.

A kite safety, control, and depowering device for a kite having an airfoil with leading and trailing edges, at least two control lines attached to the airfoil and a control flying bar attached to at least two of the control lines. The device features a continuous trim and safety flying line disposed at their lower ends over a rapid depowering apparatus. The depowering apparatus includes means for capturing and rapidly releasing an expansion disposed on the trim line, such that when rapid depowering is required, a simply release mechanism may be actuated to change the angle of attack of the airfoil rapidly.

A bladderless inflatable kite usable to propel humans, wherein the kite foregoes some or all conventional bladder structures. A bladderless or partially bladderless inflatable kite reduces the weight, and reduces problems associated with rubbing between the bladders and the outside layer, or the like. A bladderless kite structure is formed of a material that comprises a laminated mix of carbon and polymer filaments into a laminant structure wherein unidirectional prepreg tapes of in-line plasma treated fibers are spread to mono-filament level films and bonded with a UV absorbing titanium resin.

A kite control system having a control bar adapted with an internal sheeting system that provides trim / sheeting control by adjustment of outer steering lines which are attached at or near the rear corners of the kite. A tubular control bar is adapted such that the outer steering lines are routed through the interior of the control bar through openings at each opposing end. The outer steering lines are each joined to a sheeting control line which extends back out one of the opposing ends in either a left hand actuated or right hand actuated embodiment. A fixed pin located approximately mid-length within the control bar provides a fixed structure about which one of the outer lines and / or sheeting control line is routed in U-turn fashion. By pulling the sheeting control line from the end of the control bar, the rider can shorten the effective length of the outer steering lines thereby increasing the angle of attack so as to power up the kite. By releasing the sheeting control line such that it is drawn into the control bar, the ride can allow the outer steering lines to fully deploy thereby reducing the angle of attack so as to depower the kite. The control bar is equipped with means for selectively fixing the sheeting control line so as to achieve a desired angle of attack.

A rope tensioning device configured to prevent unintentional disengagement of the device from the rope. A jam-cleat arrangement coupled with a closed or semi-closed passageway enables the device to function as a tensioning aid while the user may release the device without it falling off the rope.

A kite control system including an aerodynamic wing with a leading edge and first and second opposing wingtips, a control device, a first steering line secured to the first wingtip and the control device, a second steering line secured to the second wingtip and the control device, and a trim line secured to the leading edge substantially between the opposing wingtips, wherein the trim line has a user adjustable length device that allows the user to adjust and mechanically fix the length of the trim line while the aerodynamic wing is in flight.

A buoyancy harness for connecting a rider to a water sport apparatus, including sailboards, boats, and boating accessories, the harness comprised a body portion, a fastener, and a connector. The body portion may take the form of a waist or seat harness that is configured to encircle at least a portion of the lower abdomen of the rider and possibly a portion of the pelvic region. At least a portion of the body portion is comprised of at least one layer of buoyant material. The body portion may also include a water permeable material that permits trapped water to pass through the harness. The fastener is operably connected to the body portion and is configured to secure the body portion to at least a portion of the rider. The connector is also operably connected to the body portion and is configured for operable attachment to the water sport apparatus.

A leading edge inflatable traction kite wherein the leading edge structure includes a plurality of spaced segments that are fabricated from a material with a higher elasticity, thus allowing for a greater amount of twisting and bending. The inflatable leading edge includes a series of elastically deformable segments disposed throughout the length thereof to facilitate selective torsional deformation of the leading edge and resulting overall angle of attack of the kite. These elastically deformable segments are preferably integrally formed as part of the leading edge support and are comprised of a material with a high elasticity, namely a higher elasticicity than the remaining leading edge segments. Providing elastically deformable segments of high elasticitity dispersed along the leading edge combined with regions of lower elasticity maximizes responsiveness and control by allowing leading edge deformation in response to user applied force, while the providing sufficient support to maintain kite stability.

An aerodynamic wing with a leading edge inflatable strut and at least one inflatable rib strut, wherein the struts are provided with a connection air pathway that allows the leading edge strut to act as a manifold for the inflation of the connected rib struts. Preferably, the connection air pathway is provided with a valve mechanism for selectively isolating the connected rib strut from the leading edge strut.

An improvement to kite control systems for power kites, comprising at least one proportional redirection mechanism, which balances the forces of the main lifting force of the kite and the control handlebar, thus assisting with steering the kite and significantly reducing the effort needed to hold or pull the control handlebar, without taking away the flexibility to instantly depower the kite. A compound pulley system can be used as a proportional redirection device as described in one embodiment, or levers can used as shown in an alternative embodiment.

An aerodynamic wing formed by a flexible canopy with an internally routed canopy line for controlling the canopy profile. Preferably, the canopy line is routed through a gatherable tube secured to the trailing edge of the canopy. Tensioning the canopy line alters the canopy profile to facilitate launching the kite.

A control device for use with an aerodynamic wing including a bar having a safety system that restrains one of the flying lines by routing an attachment through an aperture on the bar. Preferably, the system includes a stopper housing that engages an increased diameter element of the flying line. During normal operation, the increased diameter element is secured by the stopper housing, preventing the flying line from being pulled beyond the stopper housing. When the safety system is deployed, the increased diameter element is pulled from the stopper housing and slack is developed along the remaining flying lines to depower the kite.

The present invention is a safety system for use in conjunction with a control bar for a kite wherein the two front lines are secured by a front line swivel positioned between the bar and the kite. One front line terminates at the swivel and one extension of the other front line, the center line, travels through a central aperture in the swivel. The center line is then routed through an aperture on the control bar and terminated with an end that can be secured to the user either manually or by a leash arrangement. The swivel allows any twists that may form in the front lines to unwind. An increased diameter element located proximally of the swivel is configured to engage the center swivel, but is configured to pass through the aperture on the control bar. When the bar is released, sufficient slack is imparted into the remaining flying lines to effectively depower the kite while retaining attachment to the kite through the restrained front line.

A device for managing lines of a kite has a means for securing the device to a control bar of a kite and a line attachment portion of the device, the line attachment portion having a plurality of means for detachably retaining lines of a kite. The means for securing is formed to have an internally cylindrical sleeve having a longitudinal opening. Opposing portions of the sleeve adjacent the longitudinal opening are biased towards each other, and are elastically flexible to allow insertion of the control bar while frictionally retaining the control bar once inserted. The means for detachably retaining lines is formed as a slit in a circumferential direction with respect to the sleeve, which slit is formed to frictionally and removably retain a line inserted therein. In one embodiment, a stem portion extends radially from the means for securing, the line attachment portion residing at the distal end of said stem, the line attachment portion being formed as a longitudinal member perpendicular to the stem. In an alternate embodiment, the means for retaining the lines is formed adjacent an outer surface of the sleeve.

A kite control system having a control bar adapted with an internal sheeting system that provides trim / sheeting control by adjustment of outer steering lines which are attached at or near the rear corners of the kite. A tubular control bar is adapted such that the outer steering lines are routed through the interior of the control bar through openings at each opposing end. The outer steering lines are each joined to a sheeting control line which extends back out one of the opposing ends in either a left hand actuated or right hand actuated embodiment. A fixed pin located approximately mid-length within the control bar provides a fixed structure about which one of the outer lines and / or sheeting control line is routed in U-turn fashion. By pulling the sheeting control line from the end of the control bar, the rider can shorten the effective length of the outer steering lines thereby increasing the angle of attack so as to power up the kite. By releasing the sheeting control line such that it is drawn into the control bar, the ride can allow the outer steering lines to fully deploy thereby reducing the angle of attack so as to depower the kite. The control bar is equipped with means for selectively fixing the sheeting control line so as to achieve a desired angle of attack.

A control device for use with an aerodynamic wing including a bar having a safety system that restrains one of the flying lines by routing an attachment through an aperture on the bar. Preferably, the system includes a stopper housing that engages an increased diameter element of the flying line. During normal operation, the increased diameter element is secured by the stopper housing, preventing the flying line from being pulled beyond the stopper housing. When the safety system is deployed, the increased diameter element is pulled from the stopper housing and slack is developed along the remaining flying lines to depower the kite.