This invention relates to a steering mechanism for jet-propelled watercraft. More particularly, it relates to a steering mechanism for jet-propelled watercraft that is engaged at varying speeds.
Steering devices for watercraft are well-known. The art abounds, in particular, with references to improved rudders for such craft: U.S. Patent No. 6,428,372, for example, makes claim to a pivotally-mounted rudder for a jet-propulsion unit, while U.S. Patent No. 5,167,547 discloses a pivotally-mounted rudder that is movable into a steering position.
One example of the major disadvantages associated with the current art is that the watercraft cannot be steered, or cannot be steered satisfactorily if they are not accelerating, as there is insufficient water passing through the engine to provide the jet thrust that is required to steer and turn the craft. When faced with obstacles or other dangerous circumstances in the water, therefore, an operator of watercraft would necessarily be obliged to accelerate in order to provide sufficient power to manoeuvre the craft away from the danger. Such acceleration may often only serve to add to the danger of the situation, particularly for inexperienced operators, and in circumstances in which there is insufficient time to accelerate in order to avoid the danger.
Certain inventions have been directed at the partial alleviation of these disadvantages. In particular, U.S. Patent No. 5,167,547 claims a steering rudder that is selectively operable at the operator's option, while U.S. Patent No. 4,949,662 is directed at an auxiliary steering means to create a steering effect in a jet propulsion boat at low speeds. Other patents concentrate more generally on the coupling of an actuator onto a rudder (cf: U.S. Patent No. 6,428,372).
While this last-mentioned patent discloses an invention that certainly aids the steering of watercraft, it does little to alleviate the second disadvantage, namely engaging an improved steering mechanism within the critical time available to avoid danger when travelling at low speeds.
It is accordingly an object of the present invention to provide an improved steering mechanism for watercraft that engages automatically at off-throttle conditions, and which, at least partially, overcomes the disadvantages outlined above.
According to the invention there is provided a steering mechanism for jet-propelled watercraft comprising
According to the invention there is provided a steering mechanism for jet-propelled watercraft comprising:
The securing mechanism is preferably affixed to the outlet nozzle of the watercraft.
The securing means may incorporate nut-and-bolt fixtures for affixing the steering mechanism to the body of the watercraft.
The rudder may incorporate a plate member located in a substantially ventral position.
The biasing means may incorporate a spring-loaded engaging member that is configured to engage the plate member of the rudder at high speeds or high nozzle velocities, and to disengage from the plate member at low speeds or low nozzle velocities.
In an alternative embodiment of the invention, the biasing means may incorporate a piston-and-lug arrangement that biases the rudder towards the non-steering position, preferably wherein the lugs are coupled to the actuating means.
The actuating means may be coupled to the speedometer, alternatively revolution-counter of the engine, of the watercraft and may incorporate speed-sensitive apparatus which, on the speed, alternatively engine-revolutions of the watercraft dropping below a predetermined level, overcomes the biasing means to reverse the direction of its bias, allowing the rudder to move towards the steering position.
In an alternative embodiment of the invention, the biasing means may be caused to reverse the direction of its bias via the activation of a source of pressure.
In such an embodiment, the source of pressure may be a pneumatic cylinder.
The source of pressure may be activated by a solenoid.
In a further alternative embodiment of the invention, the actuating means may be coupled to the outflow nozzle of the watercraft, and may incorporate pressure-sensitive apparatus, such as a feedback control device and/or venturi. On the pressure dropping below a predetermined level, the control device compels the biasing means to overcome the bias, allowing the rudder to move towards the steering position.
According to a second aspect of the invention, there is provided a method for the automatic deployment of a steering mechanism in a watercraft, comprising the step of actuating the rudder into the steering position as defined in any of the above consistories.
In order to illustrate the invention an embodiment thereof is described hereunder purely as an example, without limiting the scope of the invention, wherein:
a is a profile view showing the engagement of the rudder and the plate member when in the non-steering position (position I) at high speeds;
b is a profile view showing the engagement of the rudder and the plate member when in the steering position (position II) at low speeds;
Referring to the drawings, a steering mechanism in accordance with the invention is provided, referred to generally by numeral 10, incorporates a rudder 20 that is coupled to the steering column (not shown) of the watercraft 30. The steering mechanism 10 is secured to the outlet nozzle 60 of the watercraft 30 by means of a steel nut-and-bolt arrangement 70.
a & 3b depict a biasing means according to a preferred embodiment of the invention, wherein the biasing means comprises a plate member 140 and a rudder 20. The rudder 20 is attached to the steering outlet nozzle 60 of the watercraft 30 at it's upper end. The rudder 20 has a hook-like catch member 150 at its upper attached end that is biased to move in a downwards position by a spring 170 which is attached at one end to the rudder 20 and at the other end to the watercraft nozzle 60 in an offset fashion. The plate member is pivotable about a pivot 160. At low speeds, the free end of the rudder 20 drops under gravity and spring tension, and its hook-like formation 150 disengages from the subjacent plate member 140, thereby causing the rudder 20 to move into the steering position as the direction of bias changes.
Conversely, at high speeds, the higher water pressure acting against the forward surface of the rudder 20 compels the rudder 20 to pivot upwardly in the direction of the water's surface, in which case the hook-like formation 150 engages with the plate member 140.
When, after the speed of the watercraft 30 falls below the predetermined level, the watercraft is caused to accelerate, the increase in water pressure will again cause the rudder 20 to pivot in the direction of the water's surface, and the hook-like formation 150 to engage with the plate member 140 as the rudder becomes biased in the non-steering position. This process of engaging and disengaging the rudder into the steering and non-steering positions respectively may be repeated ad infinitum. The rudder 20 is disposed of a further plate member 180, in a substantially ventral position (i.e., facing the outlet nozzle 60); the further plate member 180 aiding the hydrodynamics of the rudder 20 through water, and thus facilitating the engaging/disengaging process described above.
In an alternative embodiment of the invention, as depicted in
A further component of the actuating means 90 in this embodiment of the invention is the revolution counter of the engine 100, which is coupled to an electrical solenoid 120 via a switch 110 that is built into the revolution counter 100, and which is activated on the watercraft speed falling below a predetermined level. The solenoid 120, when so activated, permits the opening of a valve 130 on a source of pressure—in this instance, being the pneumatic cylinder 80—which allows for the release of pressure from the pneumatic cylinder 80, causing the displacement of a pneumatic piston 40. This displacement of the pistons 40, in turn, results in a reversal of the direction of the bias of the rudder 20, as it is moved into the steering position.
While the embodiments described above show what is envisaged as the more practical embodiments of the invention, it is understood that the concept of actuating a rudder 20 against a bias in an automatic response to the speed of a watercraft could also be used in alternative embodiments, in particular the biasing of the rudder to a steering position, and the automatic actuation of the movement of the rudder towards a non-steering position, on the speed of the watercraft dropping below a predetermined level.
It will further be appreciated that numerous embodiments of the invention may be performed without departing from the scope of the invention as defined in the consistory statements above.
Number | Date | Country | Kind |
---|---|---|---|
2003/2710 | Apr 2003 | ZA | national |