HYDROFOIL FOR SMALL VESSELS

Abstract

The invention relates to a hydrofoil for small vessels (1), comprising a front foil set (3) formed by a wing (32), with marked negative dihedral, which is attached to the vessel (1) by means of two struts (31), of circular or quasi-circular section, and a rear foil set (2) formed by a wing (22) that is flat or with minimal dihedral, attached to the vessel (1) by means of two struts (21); the front (3) and rear (2) foil sets being positioned longitudinally forward and aft, respectively, of the overall centre of gravity of the vessel, including also the pilot and/or crew.

Claims

1. A hydrofoil for small vessels (1), comprising: a front foil set (3) formed by a front wing (32), with marked negative dihedral, the front wing (32) being is attached to the vessel (1) by two front struts (31) of circular or quasi-circular section, such that when the vessel is sailing with slip, hydrodynamic lateral forces produced on the two struts (31) are low; a rear foil set (2) formed by a rear wing (22) that is flat or with minimal dihedral, attached to the vessel (1) by two rear struts (21) having two vertical fins (23) in a form of keels at both tips adapted to provide directional stability of the vehicle; wherein the front foil set (3) and the rear foil set (2) are positioned longitudinally forward and aft, respectively, of the overall centre of gravity of the vessel including a pilot and/or crew.

2. The hydrofoil of claim 1, wherein both the front wing (32) and the rear wing (22) have a chord of 15 to 25 cm, allowing one or both of the front wing (32) and the rear wing (22) to go through a dirty area of water which provides a surface with a greatest stability while sailing.

3. The hydrofoil of claim 1, wherein the two vertical fins (23) positioned at an end of the rear wing (22) of the rear foil set (2) are mounted on horizontal masts (24) attached to the tips of the rear wing (22) and which allow a longitudinal location of the two vertical fins (23) to move to forward or rearward positions with respect to the longitudinal position of the rear wing (22).

4. The hydrofoil of claim 1, wherein the front wing (32) and the rear wing (22) are straight or flared at the tips.

5. The hydrofoil of claim 1, wherein a span of each of the front wing (32) and the rear wing (22) is comprised of at least 4 and 8 characteristic chords, for light sailing vessels.

6. The hydrofoil of claim 1, wherein a location of points for locking the two front struts (31) to the front wing (32) are equidistant with respect to a plane of symmetry of the front wing (32) and have a separation between the two front struts (31) of between 2 and 4 characteristic chords.

7. The hydrofoil of claim 1, wherein the front foil set (3) and the rear foil set (2) are installed with a longitudinal separation of 4 to 8 characteristic chords, such that the centre of gravity of the vehicle is located between both the front foil set (3) and the rear foil set (2).

8. The hydrofoil of claim 1, wherein the two front struts (31) of the front roil set and the two rear struts (21) of the rear foil set (2) each have a length of 2 to 6 characteristic chords.

9. The hydrofoil of claim 1, wherein the two front struts (31) and/or the two rear struts (21) are replaced with one strut.

10. The hydrofoil of claim 1, further comprising a control for regulation of an angle of relative incidence of the front wing (32), to change a height of the vessel above a surface of water.

Description

[0012] As a complement to the description provided herein, and for the purpose of helping to make the features of the invention more readily understandable, the present specification is accompanied by a set of drawings which, by way of illustration and not limitation, represent the following:

[0013] FIG. 1 shows a perspective view of the hydrofoil object of the invention.

[0014] FIG. 2 depicts bottom plan and side elevational views of this device in which dimension marks have been placed, showing the proportions that can be achieved in various dimensions.

[0015] FIGS. 3 and 4 are views of the front and rear foil sets of this hydrofoil, respectively.

[0016] FIG. 5 shows a side view of an alternative embodiment of the rear foil set of a variant of the hydrofoil of the invention.

DETAILED DESCRIPTION OF THE EMBODIMENTS

[0017] Essentially, the invention basically consists of two wings (32, 22) attached to the vessel (1) by means of two struts (31, 21) each. Hereinafter, these wing assemblies with two struts will be referred to as “foil sets”. A front foil set (3) is thereby provided, the longitudinal location of which will be forward with respect to the overall centre of gravity of the vessel, also including the pilot and/or crew. In turn, the rear foil set (2) has a rearward longitudinal location with respect to the overall centre of gravity of the vessel+pilot/crew.

[0018] In the invention, wings with a mean geometric chord media of around 20 cm are used, and this length will be referred to hereinafter as characteristic chord (C). In general, wings with a chord of 15 to 25 cm are used, because in this way, the wing goes through the dirty area of the water while sailing (speaking in hydrodynamic terms), which is the area on surface which gives it the greatest stability. This is where it differs from systems which try to avoid this dirty area, while the present patent seeks this area in order to increase stability.

[0019] With respect to the plan shape of the wings (32, 22), straight wings or wings that flare at the tips are used, unlike the wings used in aeronautics, which are usually flared at the tips. If the flaring parameter (λ) is defined as the ratio between the tip chord (c.sub.t) and the root chord (c.sub.r), wings with a flaring parameter of between 1 (wing straight) and 3 are used.

[00001]$\lambda =\frac{c_t}{c_r}=\left[1,3\right]$

[0020] For constructive simplicity, straight wings are used, although tip flaring is used when lateral stability of the vehicle is intended to be increased.

[0021] With respect to the span of the wings (32, 22), spans of between 4 and 8 characteristic chords (80-160 cm) are generally used, while larger spans are used in the embodiment corresponding to light sailing vessels, as will be described in detail in the corresponding section.

[0022] With respect to the deflection of the wings (32, 22), wings without any deflection are normally used, although the use of wings with moderate deflection is contemplated for aesthetic purposes in order to delay the effects of cavitation in high-speed vehicles, or to avoid entanglement and entrainment of debris that may be found in the aquatic environment.

[0023] With respect to the location of the points for locking the struts to the wings, these are equidistant with respect to the plane of symmetry of the wing and have a separation between one another of between 2 and 4 characteristic chords (40-80 cm). See FIG. 2.

[0024] As for the particular features of the front foil set (3), it should be mentioned that the wing (32) has a marked negative dihedral (>10 degrees).

[0025] The struts (31) of the front foil set (3) are of circular or quasi-circular section, such that when the vehicle is sailing with slip, the hydrodynamic lateral forces produced on said struts (31) are very low; therefore, they will never be flat so that they do not exert lift.

[0026] In turn, the rear foil set (2) has a wing (22) that is normally flat, although it may exhibit a certain dihedral.

[0027] The struts (21) of the rear foil set (2) are either flat or have a symmetrical hydrodynamic profile. In both cases, it is intended that, when the vehicle is sailing with slip, significant lateral forces are produced which enhance the directional stability of the vehicle when said struts (21) are submerged or partially submerged. That is, when the vehicle is floating, taking off, or in flight at a low speed. The embodiment of the struts (21) in a symmetrical aerodynamic profile is only contemplated to reduce the drag caused by said struts.

[0028] Vertical fins (23) in the form of keels are installed at the tips of wing of the rear wing (22) which are responsible for the directional stability of the vehicle. Said fins (23) are installed directly at the tips of the rear wing (22). In an alternative embodiment, said rear wings (22) are mounted on horizontal masts (24) which are attached to the tips of the wing (22) and allow the longitudinal location of said fins (23) in more forward or rearward positions with respect to the longitudinal position of the tips of the wing. The longitudinal location of these fins largely determines the behaviour of the vehicle in lateral manoeuvres, so being able to modify their longitudinal installation position is extremely important in order to configure how the vehicle is driven.

[0029] As for the longitudinal location of the front (3) and rear (2) foil sets, it should be pointed out that they are installed with a longitudinal separation of between 4 and 8 chords (80-160 cm) between one another, and such that the centre of gravity of the vehicle is located between both.

[0030] The struts (31, 21) of the front (3) and rear (2) foil sets have a length of between 2 and 6 characteristic chords (40-120 cm). It should be noted that the two struts can be replaced with one strut, but when there are two, each of them withstands less stress, and when they are detachable, it is easier to put them in place as they would require a less robust fixing mechanism as they withstand less stress than if there were only one strut.

[0031] The preferred embodiment of the invention is a hydrofoil jet ski. Said embodiment is the result of the installation of the above description on a small hull measuring 200-300 cm in length 80-120 cm in width, provided with a drive system based on a spark-ignition engine or an electric engine with propeller or water jet drive.

[0032] There is arranged on said hull a seat which allows the pilot to straddle the hull, and a handlebar the turning of which allows directional control of the vehicle by means of lateral deflection of the thrust produced by the propeller or water jet, or else by means of the deflection of one or two rear vertical fins in the form of a rudder.

[0033] The propeller or water jet outlet nozzle is installed in a centred and rearward position with respect to the rear foil set and at a height coinciding with the height of the rear wing, within a range of +/−1 characteristic chord.

[0034] Gas or power control is actuated by means of a trigger or grip installed on one of the handlebars.

[0035] In this embodiment of the invention, there is a control for regulating the height of the vehicle above the surface of the water. Said control is performed by means of regulating the angle of relative incidence of the front wing (32). The implementation of this regulation of the angle is contemplated in three different ways: [0036] By means of the actuation of ailerons on the trailing edge of the wing. [0037] By means of the turning of the entire wing (32) with respect to its anchoring (33, 34) to the struts. [0038] By means of the turning of the entire front foil set (3) with respect to the hull of the vessel (1).

[0039] Four different ways of actuating this control are contemplated: [0040] By means of the grip installed on one side of the handlebars. [0041] By means of hand lever (type of brake) installed on one side of the handlebars. [0042] By means of a pedal operated by one of the feet of the pilot. [0043] By means of the longitudinal displacement of the handlebar.

[0044] Actuation of this control results in an increase in the incidence of the front wing (32), which causes the vehicle to accommodate a greater angle of attack and a greater height above the water.

[0045] Having sufficiently described the nature of the invention, in addition to a preferred exemplary embodiment, it is hereby stated for the relevant purposes that the materials, shape, size and layout of the described elements may be modified, provided that it does not imply altering the essential features of the invention claimed below.