WATER VEHICLE WITH A HYDROFOIL AND ADDITIONAL SECOND STABILIZER

Abstract

The water vehicle with hydrofoil includes an above-water platform, a supporting mast connecting the above-water platform with a hydrofoil, including a fuselage with a front wing and a first horizontal stabilizer, drive means (6) for creating horizontal thrust and a second horizontal stabilizer located in the vertical direction between the fuselage and the above-water platform, where the second horizontal stabilizer in the longitudinal direction is being located behind the front wing. It is possible that the second horizontal stabilizer is mounted to the above-water platform, the mast, to the additional structurally supporting parts, to the parts that serve to change the angle of attachment of the main horizontal stabilizer, to the fuselage or drive means by means of a support element with the possibility of changing the vertical position.

Claims

1. A water vehicle comprising: an above-water platform, a hydrofoil comprising a fuselage with a front wing and a first horizontal stabilizer, and a supporting mast connecting the above-water platform with the fuselage of the hydrofoil, the water vehicle includes a second horizontal stabilizer located in the vertical direction between the fuselage and the above-water platform, wherein the second horizontal stabilizer, in the longitudinal direction, is located behind the front wing.

2. The water vehicle according to claim 1, the second horizontal stabilizer being mounted to the water vehicle with the possibility of changing of the vertical position.

3. The water vehicle according to claim 1, the second horizontal stabilizer being mounted directly or indirectly to the supporting mast.

4. The water vehicle according to claim 3, the second horizontal stabilizer being mounted to the supporting mast by means of a support element.

5. The water vehicle according to claim 4, the support element of the second horizontal stabilizer being a support beam which is attached to the supporting mast with the possibility of changing its vertical position.

6. The water vehicle according to claim 1, the second horizontal stabilizer being mounted at a distance of at least 10 cm below the above-water platform.

7. The water vehicle according to claim 1, the second horizontal stabilizer being located in the longitudinal direction between the front wing and the first horizontal stabilizer.

8. The water vehicle according to claim 1, further including an underwater drive means for creating of horizontal thrust, and the second horizontal stabilizer being located in the vertical direction between the underwater drive means and the above-water platform.

9. The water vehicle according to claim 8, the drive means including at least one electric motor with a water screw propeller, which electric motor is connected to a source of electricity.

Description

BRIEF DESCRIPTION OF THE FIGURES

[0024] Further in the description of the water vehicle that is the object of the invention, it is explained via a preferred embodiment, given as a non-limiting the scope of the invention example, with a reference to the attached figures, where:

[0025] FIG. 1 is a schematic side view of a water vehicle according to the invention;

[0026] FIG. 2 is a diagram of a force analysis of a hydrofoil according to the invention.

[0027] FIG. 3 is a schematic side view of the vehicle according to another embodiment-windfoil.

EXAMPLES OF EMBODIMENT AND OPERATION OF THE INVENTION

[0028] The terms below, above, in front, front, behind, rear in the present description and in the claims reflect the relative position of the structural elements, as shown in the figures and in the usual operating position of the device.

[0029] The water vehicle according to the invention comprises an above-water platform 1, a hydrofoil and a supporting mast 2 connecting the above-water platform 1 and the hydrofoil (FIG. 1) and supporting the above-water platform 1 during the above-water flight.

[0030] The proposed structural scheme of a hydrofoil, as shown in FIG. 1, complements the standard scheme of a hydrofoil, which includes a fuselage 5, a bearing (front) wing 7 and a rear located first horizontal stabilizer 8, with an additional second horizontal stabilizer 4 located between the above-water platform 1 and the fuselage 5 in height. For the purposes of this description the front part of the fuselage is the part where the bearing (front) wing 7 is located and the rear part of the fuselage is the part where the first horizontal stabilizer 8 is located, so in the fuselage 5 the first horizontal stabilizer 8 is located behind the bearing (front) wing 7 with respect to the movement direction of the vehicle. The hydrofoil may or may not (as shown on the figures) have a vertical stabiliser in the rear part of the fuselage.

[0031] In the preferred embodiment shown in FIGS. 1 and 2, the water vehicle has a drive means 6. Typically, the drive means 6 generates thrust in the direction of movement and includes, for example, at least one electric motor with a water screw propeller, which electric motor is connected to a source of electricity, such as rechargeable batteries. The drive means 6 can be located both on the fuselage (FIG. 1) or be mounted directly to the supporting mast 3 above the fuselage, wherein in the second variant the second horizontal stabilizer 4 is mounted above the drive means 6.

[0032] There are other possible solutions for accomplishing a hydrofoil drive without the use of an electric motor. Such an option is, for example, the windfoil, in which the driving force is generated by the wind caught by a sail 9, attached to an additional beam 10, which is mounted to the above-water platform 1 (FIG. 3). The beam 10 to which the sail 9 is attached has a sufficient degree of freedom so that the surfer can tilt it at a different angle and rotate it 350 degrees in order to catch the headwind to generate the driving force.

[0033] It is possible to combine the water vehicle in a known way with a windfoil as a means of propulsion.

[0034] The additional second horizontal stabilizer 4 in the longitudinal direction is located behind the front wing 7 with respect to the movement direction of the vehicle. By longitudinal direction is meant a direction parallel to the longitudinal axis of the fuselage 5. In the embodiment shown in FIGS. 1 and 2 the second horizontal stabilizer 4 in the longitudinal direction is between the front wing 7 and the first horizontal stabilizer 8. This arrangement allows the overall design of the water vehicle to be more compact. In addition, the optimum action of the second horizontal stabilizer and the best stabilization effect are achieved.

[0035] Variants are also possible in which the second horizontal stabilizer 4 is located immediately above or behind the first horizontal stabilizer 8.

[0036] It will be apparent to those skilled in the art that the location, configuration, dimensions and fastening of the front wing 7 and the first horizontal stabilizer 8 to the fuselage 5 may be different as long as the above condition is met that the second horizontal stabilizer 4 is located longitudinally behind the front wing 7. For example, the front wing 7 and the first horizontal stabilizer 8 may be located in one plane or the first horizontal stabilizer 8 may be located lower than the front wing 7.

[0037] The second horizontal stabilizer 4 may have the shape and dimensions of the first horizontal stabilizer 8, but may have another shape that must meet the following criteria: [0038] to have a streamlined profile, which can be dense (solid) or hollow, and waterproof; [0039] have a hydrodynamic shape with low hydrodynamic resistance; [0040] to generate a downward force that creates a stabilizing moment.

[0041] The elements of the hydrofoil are made of the usual, known from the prior art, suitable materials. The second horizontal stabilizer 4, as well as the front wing 7 and the first horizontal stabilizer 8, for example, may be made of expanded polystyrene (EPS), expanded polypropylene (EPP), impregnated plywood and the like. The listed materials may also be in combination with a carbon coating applied via a known method.

[0042] Preferably, the second horizontal stabilizer 4 is mounted at a distance l.sub.3 below the above-water platform 1 not less than 10 cm (FIG. 1). It is also recommended that the second horizontal stabilizer 4 is not mounted directly above the fuselage 5.

[0043] In a preferred embodiment, the second horizontal stabilizer 4 is mounted directly or indirectly to the supporting mast 2.

[0044] As shown in FIGS. 1 and 2, the second horizontal stabilizer 4 may be located on a supporting element 3. For example, the second horizontal stabilizer 4 may be attached to the rear of a support beam, which with its front part is mounted with fastening means to the supporting mast 2 with the possibility of vertical relocation and fastening in a different vertical position. This can be done, for example, by providing mounting holes in the supporting mast 2 at different heights, in which the fastening means of the supporting beam, such as a screw, a bolt with a nut or other suitable known detachable fastening means, are arranged. The detachable fastening of the support element 3 to the supporting mast 2 can also be achieved in other ways known to those skilled in the art. The beam can be mounted perpendicular to the supporting mast 2 or at another angle from 1 to 179. The support element may consist of two arms located at different angles to each other. It is also possible for the support means to be telescopic, for example a telescopic extension beam.

[0045] Attaching the supporting beam with the additional second horizontal stabilizer 4 allows to change the position of the whole unit along the height of the supporting mast 2. This allows the second horizontal stabilizer 4 to be at a variable distance from the fuselage 5 and to have a different effect on the longitudinal stability of the entire hydrofoil, resulting in a greater or lesser pitching moment, which raises or lowers the nose of the hydrofoil.

[0046] In addition, it is possible that the second horizontal stabilizer 4 is mounted to the above-water platform 1, to the additional structurally supporting details, to the details that serve to change the angle of attachment of the main horizontal stabilizer, to the fuselage 5 or to the drive means 6 by means of a support element 3 with a possibility to change the vertical position.

[0047] There are additional details that constructively support the attaching of the supporting mast to the above-water platform (such as mounting plates or those that change the profile at one end of the mounting between the supporting mast and the above-water platform), as well as such additional details that allow changing the angle on the mounting of the front wing or the first (main) horizontal stabilizer (such are the so-called shims).

[0048] FIG. 4 shows schematically the following alternatives for attaching the second horizontal stabilizer 4 to the water vehicle: [0049] mounting by means of a support element 3 to the above-water platform 1, the support element being a beam or other suitable mechanical part which descends vertically to the fuselage 5 at an angle of 90 degrees to the above-water platform or at another angle (or a combination of vertical arm and arm at an angle of 1 to 89 degrees); [0050] mounting by means of a supporting element or directly to the additional structurally supporting details (at an angle), located between the above-water platform 1 and the supporting mast 2; [0051] mounting by means of a support element or directly to the additional details, which usually serve to change the angle of the first horizontal stabilizer 8; in such an installation of the second horizontal stabilizer, the supporting element, for example a beam, may be located both parallel to the supporting mast and at an angle to the supporting mast or to the longitudinal axis of the fuselage; [0052] mounting by a support element to the fuselage 5 of the hydrofoil, wherein the support element, for example a beam, may be attached vertically or at an acute angle to the longitudinal axis of the fuselage 5; [0053] mounting by means of a support element to the housing of the drive means 6, the support element, for example a beam, being able to be located vertically or at an acute angle to the longitudinal axis of the drive means 6.

[0054] Mounting of a second horizontal stabilizer 4 to the hydrofoil of the water vehicle is intended to provide variable behaviour of the hydrofoil during above-water flight, which is expressed in a continuous (cyclic) transition from floating at a certain height to subsequent diving to prevent uncontrolled emerging out of the water of the underwater part, leading to loss of control and falling of the surfer. In other words, a system is created to support stabilization along a longitudinal angle of inclination.

[0055] The principle of operation of the additional second horizontal stabilizer 4 is as follows: during the initial acceleration of the hydrofoil, the second horizontal stabilizer 4 is under water together with the other structural elements of the underwater part. Thus, it acts as the rear first horizontal stabilizer 8, generating a downward force, which in turn creates a stabilizing moment, assisting the first horizontal stabilizer 8 in balancing the hydrofoil system. When take-off speed is reached (separation of the above-water platform from the water surface), the hydrofoil begins to rise, which continues until the second horizontal stabilizer 4 rises above the water. At this point, it loses its lift power, and the stabilizing moment created by it disappears. Thus, the total moment balancing the hydrofoil system is reduced and a tendency is created to reduce the angle of attack of the wing 7, provided that the surfer's position is maintained invariably relative to the longitudinal axis of the hydrofoil. Reducing the angle of attack of the wing leads to a subsequent dive down and re-entry of the second horizontal stabilizer 4 in the water, which in turn leads to a tendency to increase the angle of attack. This is followed by a new rise above the water of the second horizontal stabilizer 4 and so diving and rising are repeated cyclically in order to maintain a certain altitude above the water (flight is maintaining a certain distance between the water surface and the above-water platform), without significant intervention of the surfer. The immersion depth of the underwater part of the hydrofoil can be adjusted by changing the vertical position of the second horizontal stabilizer 4 on the supporting mast 2, for example by changing the place of attachment of the supporting beam in the vertical direction. The closer the support beam and the second horizontal stabilizer 4 are to the fuselage 5, the higher will be the surfacing of the above-water platform 1 and vice versathe farther the second horizontal stabilizer 4 is from the fuselage 5, the lower will be the surfacing of the above-water platform 1.

[0056] In the embodiment in which the second horizontal stabilizer 4 in the longitudinal direction is located between the front wing 7 and the first horizontal stabilizer 8, optimal stabilization is achieved, wherein the distance of the above-water platform to the water surface varies within small limitswith minimal oscillations of movement as to facilitate the management of the surfboard along the longitudinal axis.

[0057] The proposed design with two horizontal stabilizers achieves, with appropriate adjustment, stable maintenance of a certain flight height of the above-water platform above the water.

[0058] The force analysis shown in FIG. 2 of a hydrofoil with an additional horizontal stabilizer shows the main forces acting on the underwater elements of the hydrofoil.

DESCRIPTION OF REFERENCE POSITIONS

[0059] Mpitching moment of the wing; [0060] Gtotal weight of the hydrofoil; [0061] L.sub.1lifting force of the first horizontal stabilizer; [0062] L.sub.2lifting force of the second horizontal stabilizer; [0063] .sub.1arm of the first horizontal stabilizer; [0064] .sub.2arm of the second horizontal stabilizer; [0065] .sub.Garm of the total weight;

[00001]$\begin{array}{cc}\mathrm{Equation}\left(1\right)& \\ M+G.Math.l_G-L_1.Math.l_1-L_2{l}_2=0& \left(1\right)\end{array}$

represents the moment equation about the 25% point of the mean aerodynamic chord of the wing, i.e. the application point of the lifting force of the wing. It describes the balance in the longitudinal direction and helps to understand the principle of operation of the second horizontal stabilizer 4

[0066] When all the elements of the hydrofoil, including the second horizontal stabilizer 4, are under water, the complete scheme of FIG. 2 is valid and the equilibrium is determined by equation (1). When the take-off speed is reached, a process of emerging up at an angle of attack of the wing set by the position of the surfer is performed, as the surfer is the largest single mass in the system. In the case when the second horizontal stabilizer 4 emerges above water, and the force L2 becomes zero, then the system tends to dive into the water, reducing its angle of attack. This behaviour is best described by inequality (2):

[00002]$\begin{array}{cc}{L}_1.Math.l_1+L_2{l}_2>L_1.Math.l_1& \left(2\right)\end{array}$

[0067] The reference numbers of the technical features are included in the claims only for the purpose of increasing the comprehensibility of the claims and, therefore, these reference numbers have no restrictive effect on the interpretation of the elements indicated by these reference numbers.