US20030140835A1 - Wind-propelled watercraft - Google Patents

Wind-propelled watercraft Download PDF

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Publication number
US20030140835A1
US20030140835A1 US10/296,649 US29664902A US2003140835A1 US 20030140835 A1 US20030140835 A1 US 20030140835A1 US 29664902 A US29664902 A US 29664902A US 2003140835 A1 US2003140835 A1 US 2003140835A1
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United States
Prior art keywords
watercraft
compressed gas
sheet element
wind
gas containing
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US10/296,649
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English (en)
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Stephan Wrage
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Individual
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Individual
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H9/00—Marine propulsion provided directly by wind power
    • B63H9/04—Marine propulsion provided directly by wind power using sails or like wind-catching surfaces
    • B63H9/06—Types of sail; Constructional features of sails; Arrangements thereof on vessels
    • B63H9/069—Kite-sails for vessels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B35/00—Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for
    • B63B2035/009—Wind propelled vessels comprising arrangements, installations or devices specially adapted therefor, other than wind propulsion arrangements, installations, or devices, such as sails, running rigging, or the like, and other than sailboards or the like or related equipment
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T70/00—Maritime or waterways transport
    • Y02T70/50—Measures to reduce greenhouse gas emissions related to the propulsion system
    • Y02T70/5218—Less carbon-intensive fuels, e.g. natural gas, biofuels
    • Y02T70/5236—Renewable or hybrid-electric solutions

Definitions

  • the invention relates to wind-propelled watercrafts in which at least one sheet element is held with at least one stay rope on a body of the watercraft, in particular a hull.
  • the invention can be employed more particularly with sail ships and other watercrafts as well solely or in combination with additional conventional drives.
  • the watercraft according to the invention uses at least a sheet element which is formed similar to a conventional sail or a sufficiently well-known kite as well to increase the propulsion due to the action of wind force, and to largely reduce the tilting moments already mentioned.
  • a sheet element which should have a small mass, if possible, is held with at least one stay rope in close proximity to the body of the watercraft wherein the stay rope is attached to the sheet element on at least three points spaced apart from each other to allow the sheet element to be deflected and aligned in the vertical and horizontal directions in order to enable an optimum alignment of the sheet element according to the desired direction of motion under consideration of the respective wind direction.
  • Such an element and a plurality of elements as well, wherein a plurality of sheet elements are preferably connected to each other, can be made of a lightweight sheet material.
  • flexible materials may also be employed for such sheet elements which deform themselves due to the wind force then, and equivalently increase the drag factor (EW) such that the component of force usable for the propulsion is also increased.
  • Compressed gas containing chambers can be arranged, formed and also secured, respectively on the one sheet element and a plurality of sheet elements, respectively for increasing the stability as well and lift, as the case may be, for such a sheet element.
  • Such a compressed gas containing chamber which is formed and arranged, respectively in close proximity to the sheet element, and in which compressed gas is contained results in an increase of the stability of such a sheet element.
  • Such compressed gas containing chambers can also achieve a supporting function similar to rigid frame constructions with a smaller mass for sheet elements.
  • the compressed gas containing chambers with gas having a lower density than air such that a lifting force component can be obtained for the sheet elements.
  • Appropriate charging gases for example are helium, but hydrogen as well.
  • the lifting force is at least greater than or equal to the weight of the sheet element.
  • the sheet element is freely floating in the atmospheric air, and it is allowed to be significantly easier manoeuvred and aligned relative to the prevailing wind direction. In addition, thus it is prevented from dropping on the ground and water surface, respectively and then an expense action is required to bring the sheet element into the wind again.
  • the compressed gas containing chamber(s) can also be charged with a gas of lower density, and such a sheet element is allowed to be suspended thereon.
  • a gas of lower density such as a sheet element
  • the compressed gas containing chambers can also be provided with apertures by means of which they can be charged with air due to a dynamic pressure when the sheet element is directed into the wind.
  • each stay rope can be lengthened and also shortened, respectively one by one individually. It is also possible, however, for such two stay ropes each which are arranged on the sheet element in horizontal and vertical planes, respectively, to be lengthened and shortened, respectively with the same length in the opposite direction.
  • the sheet element By simultaneously uniform lengthening or shortening all stay ropes the sheet element can be brought into the wind or can be hauled in.
  • the elements used to vary the length of the stay ropes are allowed to be pulleys, for example, which the respective stay rope can be wound up on and unwound therefrom, respectively.
  • Such pulleys can be constructed such as the elements which in the sailor's language are designated as “winches”.
  • the propulsion can be manually carried out in a controlled manner by means of electric motors and backgeared motors, respectively in which the control of the sheet element, thus shortening and also lengthening the stay ropes can occur under consideration of the measured wind direction, the desired direction of motion and/or else as the case may be under consideration of the tensile forces measured on the individual stay ropes by means of an electronic control.
  • Such a solution can be additionally improved when such a transversal guide is received within two guides aligned in parallel with the longitudinal axis of the body of the watercraft, and is allowed to be displaced by means of such guides along the longitudinal axis of the body of the watercraft.
  • Another alternative to vary the point of application of force of the stay ropes is to provide it excentrically on a rotary table which is rotatable with its centre about a vertically aligned rotational axis such that the point of application of force with respect to the longitudinal axis of the body of the watercraft is allowed to be automatically varied in its position due to the excentric arrangement and the turning moments correspondingly acting.
  • a variation of position can also be implemented in a controlled manner with an equivalent rotary drive for the rotary table.
  • a third alternative of varying the point of application of force for the stay rope(s) is in the use of a lever shaped jib boom which on one side comprises a link by means of which the lever shaped jib boom is attached, e.g., to the longitudinal axis of the body of the watercraft. Then, the stay rope(s) are secured in a distance preferred at the end of this jib boom such that during pivoting the jib boom about the link it can be achieved a variation of the position of the force application point of the stay rope(s) with respect to the longitudinal axis of the body of the watercraft.
  • Ball and socket joints and universal joints are suitable as a link which can also be secured inside a guide which is aligned at right angles to the longitudinal axis.
  • the point of application of force can also be varied with respect to the so-called lateral centre of pressure, and selectively adjusted such as still to be described in the following.
  • the lateral centre of pressure deals with the area related centre of inertia of the projected area on the longitudinal axis of the watercraft. It is allowed to coincide with the mean transversal axis, and the transversal axis can be located close to the lateral centre of pressure, respectively such that this as well can be used as reference for the point of application of force in a simplified manner.
  • the heeling By influencing the position of the point of application of force of the sheet element orthogonally to the longitudinal axis and direction of motion, respectively the heeling can be selectively influenced in a completely compensated manner. Thus, in certain cases even a negative heeling can be met if the point of application of force has been displaced quite far in the direction of the side sheltered from the wind, for example.
  • additional deflection pulleys can be disposed between the point of application of force and the sheet elements.
  • the stay ropes can be deflected through these deflection pulleys which is favourably effecting during the variation of position of the point of application of force, on the one hand.
  • These deflection pulleys can also be displaced, on the other hand, whereby a unique and additional variation of length of a plurality of stay ropes can be achieved in a relatively simple manner and without any required actuating forces.
  • the sheet element For a sufficient manoeuvrability of the sheet element it is advantageous to use at least three stay ropes being variable in its effective length independently from each other, which are attached to the body of the watercraft and to the sheet element then. Mounting on the sheet element is achieved such that the three mounting points of the stay ropes are spanning a triangle, and thus with lengthening and shortening, respectively the effective lengths of the three stay ropes the sheet element can be moved both in horizontal and vertical directions as well by means of the attacking wind force, and in addition the angle of attack is variable with respect to the prevailing wind direction.
  • stay ropes which provide the connection between the sheet element and the body of the watercraft.
  • the four stay ropes are attached to the sheet element such that the mounting points are spanning a square, if possible, wherein each two mounting points are in a common horizontal plane, and the other two mounting points are in a vertical plane.
  • the sheet element For manoeuvring the sheet element at least lengthening and shortening, respectively of a stay rope is required.
  • the stay ropes which mounting points are on the sheet element in a plane can also be lengthened and shortened with the same length if possible in opposite direction each. If this modification will be selected, the actuation power each required can be correspondingly reduced such that manual actuating is readily possible.
  • At least one hydrodynamically effective element which can also be designated with the term “hydrofoil”, on the body of the watercraft.
  • hydroofoil a hydrodynamically effective element
  • such an element is located beneath the floating line on the body of the watercraft and allows stabilizing the watercraft during the progressive movement.
  • such a hydrodynamically effective element can be pivoted about an axis such that a lift force or a depression force can be adjusted for the watercraft.
  • these hydrodynamically effective elements should be arranged such that symmetrical force relations occur with respect to the longitudinal axis of the watercraft.
  • two such elements can be arranged in the same level on the two outer sides of the body of the watercraft.
  • the pivoting angle of the hydrodynamically effective elements can also be adjusted depending on the vehicle speed and/or tensile force of the sheet element. In particular, during immediately occurring gusts of wind, thus it can be ensured that the body of the watercraft will be carried in the water also during extreme situations. With this, the pivoting angle of the hydrodynamically effective elements can be adjusted by a mechanical coupling by means of the tensile force acting on the stay ropes or point of application of force.
  • the aerodynamic properties of the sheet element can be influenced by effecting the three-dimensional form which can be achieved by means of the stay ropes, and if the case may of additional stay ropes.
  • supplementary aerodynamically effective elements can be attached to the sheet element.
  • These aerodynamically effective elements are allowed to be pivotally secured on the sheet element and formed in a flap shape, for example, such that being more or less put upright they cause lift or side forces on the sheet element effected by the correspondingly increased flow resistance against the attacking wind according to the adjusted angle and the corresponding arrangement, and thus allowing for the position of the sheet element to be manipulated with respect to the body of the watercraft and the wind direction.
  • the adjustment of the pivoting angle of these aerodynamically effective elements can be achieved by means of equivalent ropes as well, for example, which are guided toward the body of the watercraft.
  • Another advantageous aspect of the watercraft according to the invention can be equipped with a manipulable leeboard.
  • a leeboard is allowed to be reciprocated in the vertical direction such that the effective area can be adjusted as the occurring heeling on the vehicle according to the invention can be completely, however, at least largely compensated.
  • such a leeboard can also be deflected with respect to the longitudinal axis of the body of the watercraft such that it is allowed to completely take over or support the function of a conventional rudder. In addition, with such a leeboard it is allowed to go higher by the wind (more height running).
  • At least one sensor string can be attached to the sheet element which is guided therefrom to the body of the watercraft.
  • the propulsion of the watercraft can be influenced, and such propulsion can be drastically reduced by the correlative influence of the aerodynamically effective surfaces and shape of the sheet element in a very short time.
  • two sensor strings can be attached to the outer edges of the sheet element.
  • Controlling a watercraft according to the invention can be facilitated by different ways and completely automated with adequate expense as well.
  • measured values detected with various sensors can be processed in control electronics, and at least the position of the sheet element can be influenced with respect to the desired direction of motion and wind direction with this control electronics.
  • controlling a vehicle according to the invention can also be influenced purely mechanically in a relatively simple manner with sling elements for stay ropes which are provided on the body of the watercraft.
  • sling elements for stay ropes which are arranged on the body of the watercraft between the respective mounting point of the corresponding stay rope and the sheet element, influencing the position of the sheet element can be achieved.
  • a sling element for stay ropes is allowed to be a vertically aligned rod attached to the body of the watercraft which the laterally drifting stay rope abuts against during equivalent movement of the sheet body which results in a relatively shortening of the stay rope which prevents a further movement of the sheet element into the direction which is not desired.
  • a sling element for stay ropes can also be designed in the form of a hoop which is attached to the body of the watercraft. The respective stay rope is guided through this hoop such that an abutting limit is provided on both sides in the horizontal direction and upwardly in the vertical direction.
  • the sheet element for a watercraft is allowed to comprise at least one compressed gas containing chamber.
  • the compressed gas containing chamber can be a part of the sheet element or be connected with the sheet element.
  • Such a compressed gas containing chamber should be able to be charged from a gas accumulator tank in which compressed gas being preferably helium is contained via a first conduit which is connected and can be connected to the compressed gas containing chamber, respectively.
  • a defined gas volume is to be filled in into the compressed gas containing chamber which is sufficient to effect a lifting force for the complete sheet element which should be greater than or equal to the component of the gravitational force of the sheet element.
  • connection between the compressed gas accumulator which can be a conventional gas bottle, and the compressed gas containing chamber on the sheet element can be achieved by a valve and can be disconnected therefrom again. Then, the valve can be arranged in close proximity on the outlet of the compressed gas accumulator but also in the first conduit, and can be manually opened and closed in a most simple manner.
  • a valve which automatically closes depending on the internal pressure in the compressed gas containing chamber can also be employed with reaching a predeterminable internal pressure.
  • At least a second conduit should be present which in an alternative is passing in parallel to the first conduit already mentioned, and which can also be connected to the at least one compressed gas containing chamber wherein this second conduit is allowed to lead into a second compressed gas accumulator or into a second port of that one compressed gas accumulator connected to the compressed gas containing chamber as well.
  • the second conduit has not to be absolutely connected in close proximity with a compressed gas containing chamber, but it is also allowed to be connected to the first conduit wherein the port to the first conduit can be achieved through a so-called T-piece.
  • the second conduit can also represent a by-pass around the valve already mentioned to the first conduit, however, wherein in this case the gas recirculated from the compressed gas containing chamber is to be carried into the one compressed gas accumulator.
  • a compressor can be disposed the induction side of which is connected to the portion of the second conduit towards the compressed gas containing chamber, and the delivery side of which is connected to the portion of the second conduit which communicates with the gas accumulator.
  • Compressors in the most different well-known forms are possible, however, wherein on the delivery side a gas pressure should be available by means of which it is ensured that the compressed gas accumulator can be charged again with the recirculated gas.
  • the second gas accumulator into which the gas from the compressed gas containing chamber is again recirculated can be differently dimensioned such that inside thereof a relatively low internal pressure occurs with the recirculated gas wherein the already mentioned compressor can be abandoned as the case may be.
  • the recirculated gas temporarily stored in the second compressed gas accumulator is thus allowed to be recirculated from this second compressed gas accumulator into a first compressed gas accumulator and to be compressed higher at any times by means of an equivalent compressor.
  • the first conduit already mentioned can be temporally connected to the compressed gas containing chamber for charging and recirculating the gas wherein in this case a lockable connecting branch should be provided on such a compressed gas containing chamber.
  • the first conduit should be made of flexible material not only in this case such that handling is facilitated.
  • the first conduit connecting the compressed gas containing chamber and a compressed gas accumulator can also be guided as a by-pass around a compressor wherein the gas stream can be guided through this first conduit or the compressor by means of at least one two-way valve.
  • the second conduit can be formed in this case by the compressor with its two ports. The first conduit can be guided through the compressor housing.
  • the compressed gas accumulator utilized at least for charging the one and also a plurality of compressed gas containing chambers, respectively should have an internal pressure of gas before and during charging which is greater than or equal to the required internal pressure in the pressure chamber and in the pressure chambers, respectively.
  • All the components required for charging and recirculating the gas are allowed to be carried with the wind-propelled watercraft such that replenishing the compressed gas containing chamber is also possible during the further movement.
  • At least one of the compressed gas accumulators should be able for this to be attached to the vehicle wherein the attachment should be formed such that the equivalent compressed gas accumulator can be carried separately of the vehicle to a tank installation for replenishing with gas.
  • FIG. 1 shows an embodiment of a sheet element which can be employed on a watercraft according to the invention
  • FIG. 2 shows another embodiment of a sheet element having a kite shape
  • FIG. 3 illustrates a top view upon a body of the watercraft with an embodiment for a wind propulsion according to the invention
  • FIG. 3 a illustrates an enlarged section X from FIG. 3;
  • FIG. 3 b shows a jib boom which can be employed with the embodiment according to FIG. 3;
  • FIG. 4 illustrates a top view of another embodiment with a body of the watercraft
  • FIG. 4 a shows the enlarged section Y from FIG. 4;
  • FIG. 4 b shows an embodiment of an element suitable for varying the length of stay ropes
  • FIG. 5 shows a top view of another embodiment for carrying out guides on a body of the watercraft
  • FIG. 5 a shows a sectional view along A-A from FIG. 5;
  • FIG. 5 b illustrates the section Z as an enlargement from FIG. 5 a
  • FIG. 6 shows another embodiment of wind propulsion in a top view
  • FIG. 7 shows a top view upon a body of the watercraft having a jib boom for varying the point of application of force
  • FIG. 7 a shows a front view upon an embodiment according to FIG. 7;
  • FIG. 7 b shows the enlargement of the sections W and W′ from FIG. 7 a;
  • FIG. 8 shows a top view upon-another embodiment of a wind propulsion
  • FIG. 8 a shows a side view of FIG. 8
  • FIG. 9 shows a diagrammatic view of an embodiment of a wind propulsion on a sailing boat
  • FIG. 10 shows a top view upon a diagrammatically illustrated body of the watercraft
  • FIG. 11 shows three embodiments of modification for sheet elements and the possible alignment thereof toward the wind
  • FIG. 12 shows three embodiments for adjusted forms of a sheet element under consideration of the wind force
  • FIG. 13 shows a diagrammatic view of a sheet element having aerodynamically effective elements
  • FIG. 14 shows a diagrammatic view of a sling element for stay ropes disposed on a body of the watercraft in three views;
  • FIG. 15 shows diagrammatically a body of the watercraft which is connected to a sheet element by means of a stay rope;
  • FIG. 16 shows an embodiment of a sheet element comprising a compressed gas containing chamber and a connecting branch
  • FIG. 17 shows the structure of an embodiment of a gas supply and recirculation according to the invention in a diagrammatic form
  • FIG. 18 shows a second embodiment of a gas supply and recirculation according to the invention
  • FIG. 19 shows a third embodiment of a gas supply and recirculation to be used according to the invention.
  • FIG. 20 shows an embodiment of a gas supply and recirculation to be used according to the invention with two gas accumulators.
  • FIGS. 1 and 2 are shown two possible embodiments for sheet elements 1 as can be employed in the sail and kite shapes as well, respectively for a wind propulsion according to the invention.
  • the sheet element 1 is attached with four stay ropes 2 to the not illustrated body 3 of the watercraft wherein the length of the four stay ropes 2 can be varied each individually, if possible in order to move the sheet element 1 in the most different directions and align in accordance with the desired direction of motion with a present wind direction.
  • the sheet element 1 is made of a flexible material, for example a film and a textile fabric, respectively which at least are gasproof.
  • the at least two-layered sheet element 1 sealed at the edges defines a compressed gas containing chamber 7 in the complete interior thereof which, e.g., is filled with helium. Charging the compressed gas containing chamber 7 is achieved under consideration of the chamber volume and the masses of the sheet element 1 , the mass thereof and the shared mass of the stay ropes 1 in so far that a lifting force can be generated which is greater than the corresponding gravitational force such that the sheet element 1 will be readily held in the atmosphere as permitted by the respective length of the stay ropes 2 .
  • the sheet element 1 shown herein approximately corresponds to the contour and cross-sectional geometry, respectively of a conventional wing of an aircraft which makes effecting a dynamic lift component caused by flow conditions on the element 1 in addition to the static lift.
  • stay ropes 2 as illustrated herein can also be employed wherein this may be advantageous with large surface dimensioned sheet elements 1 .
  • FIG. 2 The embodiment of a sheet element 1 shown in FIG. 2 is similar to the design of conventional kites, and it is immediately attached to the body 3 of the watercraft also not shown with merely one stay rope 2 .
  • the stay rope 2 runs starting from a hitch 20 in three individual lines which are attached to edge points of the kite-shaped sheet element 1 , wherein the sheet element 1 comprises a frame construction 12 which preferably may be made of a lightweight and solid material. On that occasion, it is allowed to concern with carbon fiber reinforced plastics in tube or rod shapes which adequately stabilize a textile fabric and keep it in form.
  • FIG. 3 being a top view upon a diagrammatically illustrated body 3 of the watercraft shows a possibility with four stay ropes 2 in all which each can be individually varied with elements 5 in its effective length between the body 3 of the watercraft and the sheet element 1 not shown.
  • the elements 5 which are commonly formed as pulleys which the respective stay ropes 2 can be wound up on and unwound therefrom, respectively are allowed to be anchored on the body 3 of the watercraft. From these pulleys 5 the four stay ropes 2 are guided over a deflection pulley 6 ′ which herein is modified as a so-called four-pulley block or with two double blocks, over further four deflection pulleys 6 toward a deflection element which represents the actual point 4 of application of force of the stay ropes 2 on the body 3 of the watercraft, and therefrom to the sheet element 1 not shown.
  • a deflection pulley 6 ′ which herein is modified as a so-called four-pulley block or with two double blocks, over further four deflection pulleys 6 toward a deflection element which represents the actual point 4 of application of force of the stay ropes 2 on the body 3 of the watercraft, and therefrom to the sheet element 1 not shown.
  • the force application point 4 and the sheet element 1 are selectively drifting caused either by lengthening and shortening, respectively the individual stay ropes 1 due to winding up and unwinding, respectively on the pulleys 5 . It is also allowed to drift in that the double block 6 ′ as deflection pulleys for the stay ropes 2 will be varied its position.
  • the double block 6 ′ as deflection pulleys for the stay ropes 2 will be varied its position.
  • FIGS. 3 a and 3 b it shall be still referred back to possibilities, for example, on how this can be achieved.
  • FIG. 3 a the detail X from FIG. 3 is shown as an enlargement.
  • a lever arm and jib boom 10 respectively secured to a joint 16 on the body 3 of the watercraft which the deflection system 6 ′ is attached to as two double blocks.
  • the jib boom 10 can be automatically adequately pivoted, selectively manually but also mechanically at the upper end due to the deflection of the sheet element 1 such that the deflection point for the stay ropes 2 , which is predetermined by the deflection system 6 ′, is drifting therewith according to the movement of the jib boom 10 .
  • FIG. 3 a on the bottom of the body 3 of the watercraft anchored eyes can be seen which the four another deflection pulleys 6 are attached to, which one stay rope 2 each is further deflected on.
  • FIGS. 4, 4 a and 4 b for the wind propulsion according to the invention four stay ropes 2 have been used again which are guided on a sheet element 1 and attached thereto which can be formed such as according to FIG. 1.
  • Each individual stay rope 2 is guided through a separate deflection pulley 6 toward an element 5 by means of which the respective length of the stay rope 2 can be varied.
  • Such an element 5 can be formed as indicated with FIG. 4 b , for example, as a conventional winch as it is used on sailing boats and sail ships, respectively, and is allowed to comprise a free-wheel and brake.
  • a crank can be joined by means of which the respective stay rope can be wound up and unwound.
  • the force application point 4 for the four stay ropes on the body 3 of the watercraft can be varied by means of a deflection system, for example a pulley system which in the sailor's language is designated as a four-pulley block, and the position thereof by varying the length of the four stay ropes 2 under consideration of the desired direction of motion and the present wind direction.
  • a deflection system for example a pulley system which in the sailor's language is designated as a four-pulley block
  • guides 8 and 9 are employed to vary the position of the force application point 4 with respect to the longitudinal and transversal axes of the body 3 of the watercraft.
  • two longitudinal guides 9 which are aligned in parallel to the longitudinal axis of the body 3 of the watercraft are disposed at the edges of the body 3 of the watercraft.
  • a transversal guide 8 is held and guided such that it can be displaced over the total length of the body 3 of the watercraft, as required.
  • the guide element 14 can be reciprocated along the transversal guide 8 which it is guided on in a form-fit manner and held as indicated with double arrow such that the force application point 4 can be varied orthogonally to the longitudinal axis of the body 3 of the watercraft by means of shifting the guide element 14 . If the transversal guide 8 now is displaced along the longitudinal guides 9 a further variation of the position of the force application point 4 can be obtained.
  • a double lever 5 has been used which ends each a stay rope 2 is attached to. Then, the double lever arm 5 can be distorted about an axis 15 of rotation such that according to the distortion angle of the double lever 5 about the rotational axis the right and the left stay ropes 2 , respectively either can be lengthened or shortened.
  • the stay ropes are guided to the sheet element 1 around one deflection pulley 6 each which can be formed here as a double block. On that occasion, this deflection pulley system 6 is allowed to represent the force application point 4 .
  • a jib boom 10 which is attached to the body 3 of the watercraft with a joint 16 , is used for varying the position of the force application point 4 for the stay ropes.
  • the joint 16 is preferably a ball and socket joint and a universal joint, respectively by means of which the jib boom 10 can be pivoted into the most different directions.
  • the jib boom 10 can be held and aligned with at least one and preferably two (in opposition to the illustration) rope systems in the form of sheets as such elements are commonly designated in the sailor's language.
  • FIG. 7 b sections W and W from FIG. 7 a are shown to indicate the configuration of the joint 16 with its fixation on the body 3 of the watercraft and slinging the stay ropes 2 on the jib boom 10 .
  • each of the two stay ropes 2 herein are wound up on a pulley 5 as a “winch” and guided through a deflection pulley system herein comprising four, however at least two deflection pulleys 6 .
  • At least two of the deflection pulleys 6 can be translationally displaced forth and back.
  • FIG. 9 In FIG. 9 is shown a sailing boat with a hull as a body 3 of the watercraft having a leeboard 21 and a conventional rudder 22 .
  • Four stay ropes 2 are slung on the body 3 of the watercraft and at the other ends attached to a sheet element 1 in the form of a textile sail.
  • a sheet element 1 At the edge of this sail-shaped sheet element 1 an encircling compressed gas containing chamber 7 is formed which can also comprise a plurality of separated individual chambers in which compressed gas is contained.
  • a frame and stabilization function for a flexible sheet element 1 is achieved.
  • the stability can be further increased as indicated with additional rod-shaped elements and also by means of an adequate chamber design, respectively.
  • the length of the four stay ropes can be varied in a most different form for example with one of the already previously described systems.
  • FIG. 10 is diagrammatically shown a top view upon a body 3 of the watercraft for an embodiment of the watercraft according to the invention.
  • the hatched area which can extend over the total width of the body 3 of the watercraft and also beyond as the case may be, and which is arranged in the area of the drawn transversal axis of the body 3 of the watercraft herein represents the surface in which the point of application of force can be positioned by means of guides 8 and 9 as shown in FIGS. 5 a and 5 b in order to minimize the heeling and to be able to achieve an optimum driving speed.
  • This area is allowed to be circular when a rotary table or a jib boom 10 are used.
  • FIG. 11 three embodiments relating to the forms of modification of the sheet elements are illustrated wherein the individual cross-sections are discernible herein.
  • the construction of the sheet elements 1 is based on the shapes known from wings of aircrafts, and sheet elements 1 thus formed are allowed to be aligned with respect to the wind as shown in FIG. 11 such that on these sheet elements 1 a lifting component is generated with the wind which can be used for the propulsion of the watercraft through the stay ropes 2 not shown herein.
  • different propulsion forces acting as a tensile force on the point of application of force can be implemented by the correspondingly varied flow relations.
  • the shape of the sheet elements 1 can also be influenced by varying the internal pressure within the compressed gas containing chambers 7 .
  • FIG. 12 there are shown three further embodiments for adjusted shapes of a sheet element 1 which can be adjusted by varying the length of individual stay ropes 2 and by means of which differently great wind forces can be taken into account.
  • the shape shown above can be met with small up to mean wind forces to keep to aerodynamic relations by means of this shape, which a maximum propulsion can be achieved with.
  • the propulsion force can be reduced at greater wind forces, and with quite high wind forces such as occurring with gusts of wind, a variation of the shape of the sheet element 1 as shown in the bottom illustration of FIG. 12 results in that the propulsion force is reduced toward 0, and accordingly a very low tensile force occurs on the point of application of force.
  • Such a modification can also be adjusted in other situations of danger such as by means of the at least one sensor string already mentioned in the general part of the description.
  • FIG. 13 shows in a diagrammatic form a sheet element 1 having four aerodynamically effective pivotable elements 32 in all which can be pivoted individually or together such that they are allowed to act similar to flaps and horizontal stabilizers known from aircrafts in order to be able to be used for a selective motion of the sheet element 1 in the vertical and horizontal direction when a determined pivoting angle is adjusted with respect to the surface of the sheet element 1 .
  • these elements 32 for example, adequate ropes can be attached by means of which the angle of attack can be adjusted. In the cases in which these elements 32 engage the remaining part of the sheet element 1 in a two-dimensional manner they are ineffective.
  • the Ca/Cd ratio can be influenced as well to manipulate the propulsion in the each desired form.
  • FIG. 14 the effect and function of sling elements 35 for stay ropes shall be explained in a diagrammatic form. On that occasion, merely one such element 35 which is present in a rod-shaped manner on the body 3 of the watercraft is shown with its effect and function for only one stay rope 2 .
  • a stay rope 2 is illustrated with the solid lines when the sheet element 1 is positioned into the wind such that the watercraft is on the desired course that means it is moved in the desired direction of motion.
  • sling elements 35 for stay ropes can be present in the form not shown. These are also allowed to be employed in pairs for one stay rope 2 each to limit the drifting motion of the sheet element 1 in two directions.
  • sling elements 35 for stay ropes are also allowed to be formed in a bundle shaped manner as already mentioned in the general part of the description.
  • FIG. 15 a wind-propelled vehicle 3 is shown in a very simplified manner which is connected to a sheet element 1 being similar to a kite through at least one stay rope 100 such that the wind forces attacking the sheet element 1 can be used for the propulsion of the body 3 of the watercraft.
  • a sheet element 1 is shown with a compressed gas containing chamber 7 which comprises a connecting branch 108 .
  • the connecting branch 108 can be connected to a conduit 111 which the compressed gas containing chamber 7 can be charged through with a gas which is preferably helium such that by means of the charged compressed gas containing chamber 7 a lift component can be achieved which is sufficient to balance the gravitational force acting upon the sheet element 1 .
  • the connecting branch 108 is allowed to be desiged in the form of a conventional quick acting closure, for example, which should be able to be locked after charging the compressed gas containing chamber 7 such that the first conduit 111 (not shown herein) can be released again from the connecting branch 108 after charging the compressed gas containing chamber 7 , and the connection will be provided again only if the gas is to be recirculated again from the compressed gas containing chamber 7 .
  • FIG. 17 an embodiment is shown in a diagrammatic form how compressed gas can be directed from a compressed gas accumulator 104 into the compressed gas containing chamber 7 of the sheet element 1 after opening the valve 102 which is disposed in a first conduit 111 .
  • the valve 105 disposed in the second conduit 103 which is put around the valve 102 in the form of a by-pass, is closed.
  • valve 102 For recirculating the gas from the compressed gas containing chamber 7 into the compressed gas accumulator 104 the valve 102 will be closed, and the valve 105 in the second conduit 103 will be opened wherein preferably a force of expansion can be exerted upon the compressed gas containing chamber 7 at least to assist the recirculation of the gas from the compressed gas containing chamber 7 into the compressed gas accumulator 104 .
  • FIG. 18 is shown another embodiment of gas supply and recirculation from a compressed gas accumulator 104 into a compressed gas containing chamber 107 and vice versa.
  • two conduits 111 and 103 are connected in parallel to each other to the compressed gas accumulator 104 and the compressed gas containing chamber 7 .
  • the gas contained in a compressed form within the compressed gas accumulator 104 is allowed to pass into the compressed gas containing chamber 7 after opening the valve 102 , and can be temporarily stored there and used for the lift of the sheet element 1 .
  • FIG. 19 is modified with respect to the embodiment according to FIG. 18 in that the conduit 103 is formed as a by-pass around the valve 102 .
  • the valve 102 and compressor 107 as well as the conduits 111 and 103 can be exchanged.
  • FIG. 19 is also indicated that at least one area 111 ′ of the first conduit 111 can be formed in a flexible manner.
  • FIG. 20 is shown an embodiment of a gas supply and recirculation device having two compressed gas accumulators 104 and 114 .
  • the gas which is adequately compressed in the compressed gas containing chamber 7 is allowed to be recirculated into the second compressed gas accumulator 114 and temporarily stored there with relatively low pressure, wherein the internal volume of the compressed gas accumulator 114 is preferably allowed to be relatively great with respect to that of the compressed gas accumulator 104 .
  • the temporarily stored gas from the low pressure gas accumulator 114 into the compressed gas accumulator 104 can be subsequently compressed and replenished, at a suitable time after switching oh the compressor 107 which is connected with its induction side to the compressed gas accumulator 104 and with its delivery side to the compressed gas accumulator 104 .

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Ocean & Marine Engineering (AREA)
  • Wind Motors (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Addition Polymer Or Copolymer, Post-Treatments, Or Chemical Modifications (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
US10/296,649 2000-05-31 2001-05-31 Wind-propelled watercraft Abandoned US20030140835A1 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DE10027691 2000-05-31
DE10027691.1 2000-05-31
DE10065630.7 2000-12-21
DE10065630 2000-12-21

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US20030140835A1 true US20030140835A1 (en) 2003-07-31

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US10/296,649 Abandoned US20030140835A1 (en) 2000-05-31 2001-05-31 Wind-propelled watercraft

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US (1) US20030140835A1 (ja)
EP (1) EP1409339B8 (ja)
JP (1) JP2003534982A (ja)
KR (1) KR100833146B1 (ja)
CN (1) CN1431963A (ja)
AT (1) ATE399709T1 (ja)
AU (1) AU2001267326A1 (ja)
DE (2) DE50114078D1 (ja)
DK (1) DK1409339T3 (ja)
NO (1) NO335589B1 (ja)
PL (1) PL200417B1 (ja)
WO (1) WO2001092102A1 (ja)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040035345A1 (en) * 2000-08-31 2004-02-26 Edwin Lundgren Control device for steering kite on a boat
US20050127240A1 (en) * 2003-12-16 2005-06-16 Culp David A. Apparatus and method for aerodynamic wing
US20070157868A1 (en) * 2004-04-19 2007-07-12 Stephan Wrage Placement system for a flying kite-type wind-attacked element in a wind-powered watercraft
US7287481B1 (en) * 2006-08-15 2007-10-30 Skysails Gmbh & Co. Kg Launch and retrieval arrangement for an aerodynamic profile element and an aerodynamic profile element
US20090266283A1 (en) * 2004-04-19 2009-10-29 Stephan Wrage Placement system for a flying kite-type wind-attacked element in a wind-powered watercraft
US20100133385A1 (en) * 2008-12-03 2010-06-03 Olson Gaylord G Launch and recovery system for tethered airborne elements
US20130285377A1 (en) * 2010-08-05 2013-10-31 Michael Andrew Tattersfield Method And System For Harnessing Wind Energy Using A Tethered Airfoil
US20160108888A1 (en) * 2013-06-12 2016-04-21 Kite Gen Research S.R.L. Kite wind energy collector

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AU2003233775A1 (en) 2002-05-16 2003-12-02 Stephan Wrage Wind-propelled watercraft
DE202004013841U1 (de) 2004-09-06 2006-01-19 Skysails Gmbh & Co. Kg Wasserfahrzeug mit einem drachenartigen Element
DE102004018837A1 (de) 2004-04-19 2005-11-03 Skysails Gmbh Wasserfahrzeug mit einem frei ausfliegenden drachenartigen Windangriffselement als Windantrieb
DE102004018838A1 (de) 2004-04-19 2005-11-03 Skysails Gmbh Positionierungsvorrichtung für ein frei ausfliegendes drachenartiges Windangriffselement bei einem Wasserfahrzeug mit Windantrieb
DE202004013840U1 (de) 2004-09-06 2006-01-19 Skysails Gmbh & Co. Kg Wasserfahrzeug mit einem drachenartigen Element
EP2066554B1 (en) 2006-09-14 2011-12-07 Skysails GmbH Steering unit for free flying, confined wing element
EP2844552B1 (en) 2012-05-03 2017-03-08 Skysails GmbH Aerodynamic wind energy conversion device and method for controlling such a device
DE102015111224A1 (de) 2015-07-10 2017-01-12 Skysails Gmbh Start- und Bergevorrichtung für ein gefesseltes Windkraftelement

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US3839978A (en) * 1973-07-12 1974-10-08 W Hendrickson Yacht kit
US4296704A (en) * 1979-05-07 1981-10-27 Bridge John G Anti-gravity spinnaker
US4497272A (en) * 1982-06-01 1985-02-05 Veazey Sidney E Mastless sails
US4671201A (en) * 1985-06-26 1987-06-09 K.K. Yokoyama Zosen Sekkei Jimusho Method and apparatus of automatically controlling sailboat
US5095837A (en) * 1990-09-28 1992-03-17 Baird Lincoln F Ram-air inflatable beam for use with a spinnaker
US5642683A (en) * 1996-04-26 1997-07-01 Bedford; Norman Parachute-type sail for boats

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040035345A1 (en) * 2000-08-31 2004-02-26 Edwin Lundgren Control device for steering kite on a boat
US6910434B2 (en) * 2000-08-31 2005-06-28 Edwin Lundgren Control device for steering kite on a boat
US20050127240A1 (en) * 2003-12-16 2005-06-16 Culp David A. Apparatus and method for aerodynamic wing
US7093803B2 (en) 2003-12-16 2006-08-22 Culp David A Apparatus and method for aerodynamic wing
US20090266283A1 (en) * 2004-04-19 2009-10-29 Stephan Wrage Placement system for a flying kite-type wind-attacked element in a wind-powered watercraft
US20070157868A1 (en) * 2004-04-19 2007-07-12 Stephan Wrage Placement system for a flying kite-type wind-attacked element in a wind-powered watercraft
AU2005232890B2 (en) * 2004-04-19 2010-11-11 Skysails Gmbh & Co. Kg Placement system for a flying kite-type wind-attacked element in a wind-powered watercraft
US7866271B2 (en) 2004-04-19 2011-01-11 Skysails Gmbh & Co. Kg Placement system for a flying kite-type wind-attacked element in a wind-powered watercraft
US7287481B1 (en) * 2006-08-15 2007-10-30 Skysails Gmbh & Co. Kg Launch and retrieval arrangement for an aerodynamic profile element and an aerodynamic profile element
US20100133385A1 (en) * 2008-12-03 2010-06-03 Olson Gaylord G Launch and recovery system for tethered airborne elements
US7775483B2 (en) 2008-12-03 2010-08-17 Gaylord G Olson Launch and recovery system for tethered airborne elements
US20130285377A1 (en) * 2010-08-05 2013-10-31 Michael Andrew Tattersfield Method And System For Harnessing Wind Energy Using A Tethered Airfoil
US9046072B2 (en) * 2010-08-05 2015-06-02 Crosswind Power Systems Inc. Method and system for harnessing wind energy using a tethered airfoil
US20160108888A1 (en) * 2013-06-12 2016-04-21 Kite Gen Research S.R.L. Kite wind energy collector

Also Published As

Publication number Publication date
NO335589B1 (no) 2015-01-05
PL200417B1 (pl) 2009-01-30
DK1409339T3 (da) 2008-10-27
PL358964A1 (en) 2004-08-23
EP1409339A1 (de) 2004-04-21
EP1409339B8 (de) 2008-08-27
NO20025746D0 (no) 2002-11-29
KR100833146B1 (ko) 2008-05-28
EP1409339B1 (de) 2008-07-02
CN1431963A (zh) 2003-07-23
JP2003534982A (ja) 2003-11-25
KR20030025232A (ko) 2003-03-28
ATE399709T1 (de) 2008-07-15
DE10192193D2 (de) 2003-04-24
NO20025746L (no) 2003-01-29
WO2001092102A1 (de) 2001-12-06
DE50114078D1 (de) 2008-08-14
AU2001267326A1 (en) 2001-12-11

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