The development of the hydrofoil lifting device has the potential to greatly advance the performance of watercraft. Both powered and sail craft may benefit from the application of the hydrofoil device. These performance enhancements have been limited by difficulties associated with the hydrofoil control mechanisms. Previous applications of hydrofoils to sailcraft have also been limited in that the designs were effective only in high wind conditions.
For large powered watercraft, fully electronic control mechanisms have been developed to optimize performance and stability under varying weather and sea conditions. For smaller powered vessels, or for sail boats in particular, the power consumption, weight, and complexity of fully electronic control systems is not as practical. The present invention offers many of the advantages of an electronic control system with a much simpler design, suitable for use even in small power or sailboats.
Previous designs for hydrofoil craft have not fully addressed all the requirements for a control system that accommodates varying weather, sea, and load conditions. One such design (U.S. Pat. No. 6,578,507 to Bergmark) employs hydrofoil devices intended to counteract the heeling force of the wind against the sail. The design does not address altitude stabilization or automatically adjust for changing wind conditions or sail trim (“the wings may be actuated by means of control means that are accessible from the cockpit)”.
In a similar U.S. patent (Baulard-Caugan U.S. Pat. No. 4,385,579) hydrofoil-like devices are linked to the mast to provide some means of compensating for wind variations. This design improves roll stabilization but does not exploit the lifting potential of the hydrofoils to reduce hull drag, nor does it attempt to control the altitude of the craft.
U.S. Pat. No. 3,762,353 (Shutt) is also designed primarily to counteract the heeling force exerted by the sail/mast. The hydrofoil's angle of attacked is controlled by a small float assembly linked to the main hull. This design does not exploit the lifting potential of the hr drofoil, and is also very susceptible to localized variations in wave height that could adversely affect stability.
The catamaran stabilization structure of U.S. Pat. No. 4,561,371 (Kelley et al) employs passive wing structures whose angle of attack is fixed and therefore do not adjust to accommodate changing conditions.
In U.S. Pat. No. 5,168,824 (Ketterman) the hydrofoil control mechanism also makes use of a small “canard” on the water surface near the foil. To reduce susceptibility to localized wave action, a flexible linkage absorbs higher-frequency variations in canard height. The rudder foil does not employ the canard control mechanism, and is therefore less effective in counteracting any pitching motion that may be induced by wind/wave interaction. The canard mechanisms on the lateral foils may also be susceptible to swamping by large waves which could destabilize the craft.
The present invention uses a foil control mechanism which addresses many of the problems of prior designs, while adding additional benefits. Rather than using localized float sensing mechanisms, the new design controls the foils based on the buoyancy along the entire length of two or more hulls. This method minimizes any disturbance from localized wave action and automatically compensates against heeling, pitch, and roll. The buoyancy provided by the hulls combines with the hydrodynamic force from the foils, so that performance is improved even for a sailcraft in low wind conditions.
In a catamaran configuration, the preferred embodiment of the invention uses two hydrofoils per hull, located on vertical struts near the forward and aft ends of the hull. The struts are rigidly fixed to a deck structure that supports the two hulls.
The key to the design is the mechanical decoupling of the hulls from the deck structure. The hulls are allowed a small range of vertical motion relative to the struts and the deck structure. This motion is constrained by springs, pads, or other compressible elements. The vertical motions of the hulls (relative to the rest of the boat) are then linked to the foils to vary the hydrodynamic lift and thereby stabilize the craft under a wide range of wind and ocean conditions. The adjustment of a foil's hydrodynamic lift is typically accomplished by varying the foil's angle of attack, although other methods may be used to accomplish the same result.
At rest, the weight of the boat is supported entirely by the buoyancy of the hulls. The control mechanism in this state places the foils at angle of attack such that lifting forces will be generated as soon as the boat gains forward motion.
As the boat picks up speed, the lifting force contributed by the foils will increase, causing the boat to move higher in altitude with respect to the ocean surface. At the same time, the lifting force contributed by the hulls will decrease as they are raised higher out of the water. The control mechanism will sense this shift in load on the hulls, and begin to decrease the angle of attack on the foils. At a point where the hulls are almost clear of the water the control system will achieve equilibrium, and the boat will continue to move forward with greatly reduced hull drag.
A conventional catamaran design is subject to capsize under certain extreme conditions. High winds can generate heeling (tipping) forces strong enough to lift one hull of a multi-hull sailboat completely out of the water. In a powered catamaran, this risk occurs during highspeed turns in a tight radius. If not controlled, these forces can cause a capsize.
The current design minimizes the risk of capsize in both powered and sail craft. If a hull is lifted past the control mechanism's equilibrium point, the angle of attack on the foils will be reversed to provide negative lift to counteract the heeling force. This allows safe operation at higher speeds than would be possible in a conventional multihull craft.
The catamaran configuration may alternately use one controlled foil at the bow of each hull, and a fixed (non-adjustable) hydrofoil at the stern. This does not provide all the benefits of using two controlled foils per hull, but the cost and complexity of the craft is reduced.
A trimaran embodiment is similar to the z-hull discussed above, with the addition of a center hull. The control mechanisms in the outside hulls' hydrofoil assemblies regulate the boat's altitude and reduce risk of capsize in the same manner as the catamaran configuration.
Is it clear that the principles and benefits of the present invention may be applied as well to vessels with more than three hulls.
To accommodate varying sea states the control system includes adjustable dampers that control the response time to changes in hull buoyancy. Thus the system can be tuned to provide the most comfortable and safe ride for the passengers.
The upper end of the control rod is attached to the hull 4. The hydrofoil element 6 is supported by a vertical strut 7 affixed rigidly to the deck structure 5. The strut is mounted through a hollow sleeve 18 embedded in the hull. The sleeve allows the hull to move up and down relative to the deck structure 5, strut 7, and hydrofoil 6. The upward motion of the hull is constrained by a spring 14. The downward hull motion is constrained by a limiter 11.
At rest in the water, the hull 4 provides an upward buoyant force to support the weight of the boat. This force compresses the spring 14 causing the hull to move upward towards the deck structure 5 until the buoyant force of the hull matches the compression force of the spring. The upward movement of the hull also causes the hydrofoil 6 to swing upward by way of control rod 12 to a positive angle of attack.
In an ocean breeze the boat will begin to move forward as the sails are raised and trimmed. As the forward momentum increases, hydrofoil 6 will begin to generate lift, causing the boat to gain altitude above the ocean surface. As the hydrodynamic force contributed by the foil continues to increase, the hull contributes a correspondingly smaller portion of the total lifting force, therefore the hull 4 will start to slide downward on the strut 7. The farther the boat lifts out of the water, the lower the resulting hull position on the strut. As the hull drops, the hydrofoil angle of attack is automatically decreased via control rod 12. Eventually, as the lifting force contributed by the hull approaches zero, the hydrofoil angle of attack will decrease to the point that the boat altitude stabilizes.
If the wind on the sails is strong enough, the windward hull of a conventional catamaran will tend to lift out of the water completely, which could lead to a dangerous capsize. With the present invention, this heeling (tipping) force will be counteracted automatically by the control mechanism. The length of the control rod is set so that if the hull slides too far down the strut, the hydrofoil angle of attack will change to negative, causing a negative lifting force to counteract the heeling moment caused by the sails. The hull will be in minimal contact with the surface but the control mechanism will not allow the hull to “fly” or leave the surface completely, thereby avoiding the risk of capsize.
In a powered watercraft the heeling force is not generated by a sail, but rather by forces encountered when executing tight-radius turns at high speed. The control mechanism of the present mechanism serves to counteract this heeling moment in the same manner as described for the sail-powered craft; the hull always stays in minimal contact with the surface. This characteristic is one of the most valuable advantages of the present invention, as it improves both performance and safety for sail or power boats alike.
A shock absorbing device 15 is employed at the end of each hull to dampen the control mechanism for smooth operation. The preferred embodiment will use a gas or liquid filled linear damper (readily available from industrial suppliers) as the shock absorbing device. The linear damper typically provides an adjustable damping coefficient, which can be used to trim the response to accommodate various sea states.
In a sea condition of short choppy waves, a high degree of damping will prevent the chop from causing vibration or oscillations as the mechanism adjusts. In a sea state with long, high swell, a lower amount of damping will allow the boat to follow the altitude contour of the swell. This reduces wave collisions which drastically impede the forward motion of the boat.
There are numerous well-known mechanisms for adjusting the lift generated by a hydrofoil. Changing the foil's angle of attack as discussed above is the simplest mechanism. An alternate approach utilizes adjustable flaps on the trailing edge of the foil, similar to those used on airliners.
The invention discloses a multihull watercraft with automatic control of altitude, pitch and roll, which is able to accommodate varying weather and sea conditions while providing a smooth ride for passengers. These benefits are obtained without the cost, complexity, and reliability issues of an electronic control system.
Variations to the embodiments shown may be implemented that are functionally equivalent to the invention disclosed here. The hydrofoil lift may alternately be adjusted using equivalent methods, such as changing the camber (shape) of a flexible hydrofoil. Any of the well-known motion damping devices may be substituted for the shock absorber 15, including linear dampers filled with a gas or liquid. The function of the control rod 12 to link the hull movement to the foil adjustment may be provided by many other well-known linkage means, including flexible cables, hydraulic lines, or servo-electric devices. Many well-known mechanisms including roller bearings, ball bearings, or swing arms may be used in place of the sleeve 18 to allow vertical motion of the hulls relative to the deck structure.
Thus the scope of the invention is defined not by the embodiments presented but by the attached claims.
This application claims priority to provisional case 60/857,720 filed Nov. 8, 2006
Number | Name | Date | Kind |
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2387907 | Hook | Oct 1945 | A |
2709979 | Bush et al. | Jun 1955 | A |
3092062 | Savitsky | Jun 1963 | A |
3149602 | Vogt | Sep 1964 | A |
3762353 | Shutt | Oct 1973 | A |
3812806 | Korotkov et al. | May 1974 | A |
4711195 | Shutt | Dec 1987 | A |
5168824 | Ketterman | Dec 1992 | A |
Number | Date | Country | |
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60857720 | Nov 2006 | US |