Information
-
Patent Grant
-
6443785
-
Patent Number
6,443,785
-
Date Filed
Friday, December 15, 200024 years ago
-
Date Issued
Tuesday, September 3, 200222 years ago
-
Inventors
-
-
Examiners
Agents
- Jenkens & Gilchrist, A Professional Corporation
-
CPC
-
US Classifications
Field of Search
US
- 440 40
- 440 42
- 440 43
- 114 162
- 114 165
-
International Classifications
-
Abstract
A self-deploying rudder assembly for use with a water craft including an exhaust port having a exhaust stream includes a mounting assembly and a pivoting rudder blade assembly. The pivoting rudder blade assembly typically includes a thrust plate attached to one end of a rudder shaft and a rudder blade attached to the other end of the rudder shaft. When the selected thrust level is above the preselected thrust level, the thrust plate is moved out of the exhaust stream and the rudder blade is thereby moved from a deployed, operational position to a stored position.
Description
BACKGROUND OF THE INVENTION
1. Technical Field
This invention relates generally to water craft and rudder/steering devices. More particularly, the invention relates to self-deploying rudder devices which respond to fluid flow pressure, such as that provided by the exhaust from jet-propelled water craft.
2. History of Related Art
Jet-propelled water craft are typically designed to be steered using exhaust fluid flow pressure developed from a movable jet nozzle submerged below the surface of the water. However, as the throttle-controlled thrust is retarded, the ability to steer is substantially reduced. In fact, since most jet-propelled water craft have no rudders, any type of substantial reduction in exhaust pressure, coupled with a steering capability that depends upon a steerable exhaust nozzle, typically makes it impossible to steer such water craft effectively.
Various mechanisms have been developed to provide alternative steering capability for jet-propelled water craft. However, such mechanisms have many shortcomings. For example, some rudder mechanisms require manual operation to deploy into the water, or to be removed from the water. Spring-biased rudder mechanisms, while providing the ability to displace upwardly upon contact with foreign objects, typically remain in the water at all times, producing excessive drag during high-speed operation of the water craft. Finally, some of these mechanisms are designed to deploy automatically, but when stored, trail behind the water craft above the water line. Thus, such devices present a significant safety hazard to anyone falling off of the water craft during use.
Other attempts to deal with the problem of providing slow speed steering control to jet-powered water craft in a safe and efficient manner include the use of a third class lever connected to a rudder, which pivots from the uppermost portion of the lever, where it is attached to the jet nozzle. Thus, the rudder extends behind the craft for some distance while deployed in the steering position, and extends both behind the craft and above the water line while in the stowed, or “running” mode. Such operational characteristics present a significant hazard to any operator, or passenger of the water craft that falls to the rear of the craft during operation. Further, re-boarding of the craft after a fall is quite difficult if the rudder apparatus projects into the path of the boarding operator and/or passenger.
Such devices do not allow for adjustments in the level of thrust required to deploy and/or store the rudder based on the exhaust pressure developed at idle speed, nor do such devices allow for raising the rudder completely out of the way for beaching/launching the water craft. Finally, such devices do not provide any type of stabilizing force for the stored rudder blade during powered operation.
Thus, what is needed is a rudder assembly for use with an exhaust port which operates to automatically deploy the rudder below a selected exhaust thrust level and which operates automatically to store the rudder when the thrust level is above the preselected level. Of course, such a device would be even more useful if it provided the option for manual deployment and storage. Finally, such a device would be most useful if automatic operation could be adjusted to occur at some variable level of thrust, selected by the user.
SUMMARY OF THE INVENTION
The self-deploying rudder assembly of the present invention includes a mounting assembly which attaches to an outlet nozzle, or exhaust port, such as those used on jet-propelled water craft. The self-deploying rudder assembly also includes a thrust plate, rudder shaft, and rudder blade, which are typically integrated into a single unit called the rudder blade assembly. The rudder blade attaches to one end of the rudder shaft, and the thrust plate attaches to the other end. The shaft typically operates as a first class lever, having a rudder pivot point, or fulcrum, located between the thrust plate and the rudder blade. A deployment means, such as a spring, is attached to the shaft and the mounting assembly so as to bias the rudder blade in a downward, fully-deployed position, to allow steering the water craft at low levels of thrust. The thrust plate intercepts the exhaust from the exhaust port and operates to urge the rudder blade into a stored position when the thrust level selected by the operator of the water craft is above some preselected thrust level. That is, when the water craft operator increases the amount of throttle to the jet, so the craft moves forward at high speed, the rudder blade will be stored underneath the water craft, typically in a grooved skeg. However, when the throttle is rolled off and the water craft is operated at a low speed, the rudder will be deployed (using the deployment means) into an operative position. The thrust plate may include an adjustable cross-sectional surface area, or an orifice, which allows selection of the low speed threshold for rudder deployment and storage.
An alternative embodiment of the invention divides the rudder shaft into two portions, an upper shaft and a lower shaft. The upper shaft engages the lower shaft in a continuous fashion using a gear attached to each of the shafts, such that the upper shaft and an attached or integral gear is continuously engaged with a lower shaft gear, which is integral with, or attached to, the lower shaft. Alternatively, a pushrod assembly can be attached to the upper and lower shafts so that movement out of the exhaust stream by the upper shaft causes direct movement and storage of the lower shaft and rudder blade. In this case, the rudder shaft no longer operates as a first class lever; however, all of the other advantages of the invention are retained. In addition, at high operating speeds, the rudder blade folds toward the rear of the craft for storage. This allows the fluid forces exerted against the rudder blade during high speed operations to assist retention of the rudder blade when it is stored within the grooved skeg.
As a matter of increased utility, the self-deploying rudder assembly may incorporate a cable or other storage means which allows storage of the rudder unit for beaching and/or launching the water craft. The rudder assembly may also include a rotatable gear engaged to a gear rack which rotates the rudder blade as it moves toward a stored position such that the rudder blade is stored flush, and in the same plane, as the undersurface of the water craft hull.
Dual-shaft, rudder blade combinations can also be used. The use of additional rudder blade area, such as may occur with dual rudders, increases the ability to steer the water craft during conditions of low or no thrust.
BRIEF DESCRIPTION OF THE DRAWINGS
A more complete understanding of the structure and operation of the present invention may be had by reference to the following detailed description when taken in conjunction with the accompanying drawings, wherein:
FIG. 1
is a side view of the self-deploying rudder assembly of the present invention, showing the rudder in a deployed position;
FIG. 2
is a side view of the self-deploying rudder assembly of the present invention, showing the rudder in a stored position;
FIG. 3
is a front view of the self-deploying rudder assembly of the present invention, showing the rudder in a deployed position;
FIG. 4
is a front view of the self-deploying rudder assembly of the present invention, showing the rudder in a stored position;
FIG. 5
is a side view of the self-deploying rudder assembly of the present invention;
FIG. 6
is a side view of the self-deploying rudder assembly of the present invention including a storage means in the form of a cable;
FIGS. 7A
,
7
B, and
7
C are detailed views of the thrust plate, thrust plate adjuster, and the thrust plate joined to the thrust plate adjuster, respectively;
FIG. 8
is an alternative embodiment of the self-deploying rudder assembly of the present invention;
FIG. 9
is a frontal view of an alternative embodiment of the self-deploying rudder assembly of the present invention;
FIG. 10
is a side view of an alternative embodiment of the self-deploying rudder assembly of the present invention;
FIG. 11
is a perspective view of an alternative embodiment of the self-deploying rudder assembly of the present invention;
FIGS. 12A and 12B
are side views of alternative embodiments of the self-deploying rudder assembly of the present invention; and
FIG. 13
illustrates a flow chart of the method of the present invention.
DETAILED DESCRIPTION OF PRESENTLY PREFERRED EXEMPLARY EMBODIMENTS
As mentioned above, jet-propelled water craft generally use a movable nozzle with an exhaust port to provide steering capability. Thus, as shown in
FIG. 1
, the water craft
100
is attached to the nozzle
110
, which can be moved from side to side to direct the exhaust stream
300
and turn the water craft. Since the nozzle
110
is the only mechanism available for steering the water craft
100
, when the thrust of the exhaust stream
300
falls below a preselected level, no steering is available to the operator of the water craft
100
.
The self-deploying rudder assembly
50
of the present invention provides steering control for the water craft
100
by deploying a rudder blade
160
into an operational position when the thrust level of the exhaust stream
300
falls below a preselected thrust level. However, as can be seen in
FIG. 2
, when the thrust level of the exhaust stream
310
rises above the preselected thrust level, the rudder blade
160
is moved to a stored position. At these higher thrust levels, the rudder blade
160
is no longer needed for steering control, since the control provided by the movable nozzle
110
is sufficient. The thrust level of the exhaust stream
300
is typically selected by operating a throttle control on the water craft.
The rudder assembly
50
includes a mounting assembly
120
for attaching the self-deploying rudder assembly
50
to the exhaust port or nozzle
110
. The mounting assembly
120
may include a mounting ring
140
as a means of circular, removable attachment to the nozzle
110
. Of course, the mounting assembly
120
may also be formed integrally with the nozzle
110
for non-removable attachment of the self-deploying rudder assembly
50
to the nozzle
110
. Thus, the self-deploying rudder assembly
50
can be manufactured as an attachment to the nozzle
110
of the water craft
100
, or as an integral portion of the nozzle
110
, and sold as a part of the water craft
100
. The rudder assembly
50
also includes a thrust plate
180
which is attached to the first end of a rudder shaft
170
; the rudder blade
160
is attached to the second end of the rudder shaft
170
. There is a fulcrum, or rudder pivot
200
, which is attached to the mounting assembly
120
and pivotally attached to the rudder shaft
170
between the first end of the rudder shaft
170
and the second end of the rudder shaft
170
(i.e. between the point where the thrust plate
180
is attached, and the point where the rudder blade
160
is attached). The combination of the thrust plate
180
, the rudder shaft
170
, and the rudder blade
160
make up the pivoting rudder blade assembly
130
.
A deployment means
210
, such as a spring, has a first end attached to the mounting assembly
120
, and a second end attached to the rudder shaft
170
. Any number of elastic devices, acting under tension, may be used for the deployment means to
210
, including rubber bands, elastic cord, or other natural and/or synthetic elastic materials. The deployment means serves to pull the thrust plate
180
into position in line with the exhaust stream
300
during those times when the thrust level of the exhaust stream
300
is below the preselected thrust level. Alternatively, a deployment means
210
′ operating under compression, such as a spring, a shock absorbing piston, or some other device which operates to urge the rudder blade
160
into the deployed position during low thrust conditions may be used in place of the deployment means
210
.
As seen in
FIG. 2
, the mounting assembly
120
includes the mounting ring
140
and the storage skeg
150
. Thus, the self-deploying rudder assembly
50
can be said to include the mounting assembly
120
pivotally attached to the pivoting rudder blade assembly
130
. This combination is realized when the mounting assembly
120
is manufactured as an integral unit, typically molded from high impact plastic, including the mounting ring
140
and the storage skeg
150
. Similarly, the pivoting rudder blade assembly
130
can be constructed as a single unit including the thrust plate
180
, the rudder shaft
170
, and the rudder blade
160
. The pivoting rudder blade assembly
130
can also be molded from high-impact plastic. Of course, any other suitable materials, such as metals, including aluminum, plastics, including polymers, ceramics, or even wood can be used to fabricate the mounting assembly
120
, the pivoting rudder blade assembly
130
, and their component elements. The rudder blade assembly
130
can be mounted to the mounting assembly
120
using a separately-manufactured rudder pivot
200
, or may include the pivot/fulcrum function in the form of a snap together assembly, wherein holes are formed in either the mounting assembly
120
or the pivoting rudder blade assembly
130
, and mated to complementary snap-in shafts or “ears” formed in the pivoting rudder blade assembly
130
, and the mounting assembly
120
, respectively.
As shown in
FIG. 1
, when the thrust level of the exhaust stream
300
is below the preselected thrust level, the deployment means
210
operates to pull the rudder blade assembly
130
into an upright position, which places the thrust plate
180
into the exhaust stream
300
, in line with the nozzle
110
. At this time, the rudder blade
160
is in a deployed position, upright in the water
400
, and provides operational steering for the water craft
100
as the nozzle
110
is moved side to side by the water craft
100
operator.
Referring now to
FIG. 2
, wherein the exhaust stream
310
of the nozzle
110
has risen above the preselected thrust level, and provides sufficient force to overcome the tension of the deployment means
210
, the rudder blade
160
moves into a stored position within the storage skeg
150
. In the stored position, the rudder blade
160
is typically shielded or protected by a groove
155
(see
FIG. 4
) formed into the skeg
150
.
In the deployed position (FIG.
1
), the rudder blade
160
provides operational steering control to the operator of the water craft
100
. In the stored position (FIG.
2
), the rudder blade
160
is stored within the skeg
150
and does not impede the exhaust stream
310
flow from the nozzle
110
. Operation of the self-deploying rudder assembly
50
is thus automatic, and depends only on the level of thrust selected by the operator for the exhaust stream
300
,
310
. Thus, the safety feature of low speed operational steering control is provided without the need for any conscious action on the part of the water craft operator. This feature should serve to reduce the danger of incidents which required immediate reduction in throttle application, combined with the need for steering control of the water craft
100
.
Turning now to
FIGS. 3 and 4
, frontal views of the rudder blade in a deployed position, and a stored position, respectively, can be seen. In the deployed position (FIG.
3
), the thrust plate (and optional thrust plate adjuster
190
) can be seen as ready to intercept the exhaust stream which propagates through the mounting ring
140
. In the stored position, the thrust plate
180
is moved out of the way of the exhaust stream which propagates through the mounting ring
140
. Also shown in these views is a rudder blade plate
230
which can be molded into the rudder blade
160
, or manufactured as a separate component. The rudder blade plate
230
provides added upward force to the rudder blade
160
when in the stored position, which tends to stabilize the rudder blade
160
as it rests within the groove
155
of the skeg
150
. The added upward force provided by the rudder blade plate
230
is most useful during high speed runs and abrupt course change operations that are a normal part of water craft
100
operations. The rudder blade plate
230
can be seen more clearly from the side in FIG.
5
.
Also apparent in
FIG. 5
is the optionally-provided thrust plate adjuster
190
, which is typically mounted to the thrust plate
180
using a thrust plate pivot
220
. The thrust plate pivot
220
can be molded so as to form an integral part of the thrust plate
180
, or the thrust plate adjuster
190
, and attached to the mating component using a “snap-fit” through a hole in the mating component, as is well known to those skilled in the art.
Turning now to
FIG. 6
, the storage means
260
, which typically takes the form of a cable, can be seen. The storage means
260
is normally attached to the pivoting rudder blade assembly
130
, at some point along the rudder shaft
170
, or the rudder blade
160
. Of course, the storage means
260
may also be attached to the thrust plate
180
, depending on the particular implementation of the design. If the storage means
260
is a cable, then a rudder cable mount
270
will usually be used to guide the storage means
260
along the path from the area of the self-deploying rudder assembly
50
to the operator. As shown, the storage means
260
is in the second operating position (which results in allowing the rudder blade to deploy).
The storage means
260
allows the water craft operator to raise and stow the rudder blade
160
during beaching, launching, or transportation of the water craft
100
. The end of the storage means
260
which is not attached to the rudder blade
160
is typically guided through the rudder cable mount
270
up to the operator of the water craft, where it terminates in a “turn and lock” handle device (not shown) on the control panel of the water craft
100
. When the operator pulls the handle (i.e. places the storage means
260
in a first operating position), the rudder blade
160
is manually rotated into the stored position. An electrically or hydraulically powered raising device can be used to place the rudder blade
160
into the stored position by operator command, as is well known to those skilled in the art.
Turning now to
FIGS. 7A
,
7
B and
7
C, the details of the thrust plate
180
, and thrust plate adjuster
190
, can be seen. In the simplest implementation, the thrust plate
180
can be used alone as an element of the pivoting rudder blade assembly
130
, as shown in
FIGS. 2 and 4
. In this case, the thrust plate
180
includes one or more thrust plate holes
185
to allow the passage of some selected amount of the exhaust stream
300
, which prevents storage of the pivoting rudder blade assembly
130
until the selected thrust level of the exhaust stream
300
is above a preselected thrust level. The level of thrust required to rotate the pivoting rudder blade assembly
130
into the stored position thus depends upon the size of the thrust plate holes
185
in relation to the surface area of the thrust plate
180
, along with the level of thrust present in the exhaust stream
300
. In more complex implementations of the self-deploying rudder assembly
50
of the present invention, a thrust plate adjuster
190
, having adjuster holes
195
, can also be mounted in line with the exhaust stream
300
and the thrust plate
180
, as shown in FIG.
7
C. Using the thrust plate pivot
220
, the thrust plate adjuster
190
can be rotated in the “A” direction to provide an orifice having a variable surface area (i.e. the “orifice” may include the combined surface area of the thrust plate holes
185
, minus the area closed off by the thrust plate adjuster
190
). Thus, by rotating the thrust plate adjuster
190
in the (A) direction, the thrust plate holes
185
can be completely open, or completely obscured, as desired by the operator. Thus, the thrust plate
180
can include at least one orifice having a variable surface area, in this fashion. As shown in the exemplary
FIGS. 7A-7C
, four orifices (or any desired number) having a variable surface area can be realized. Of course, as is well known to those skilled in the art, other methods of providing a variable orifice can be effected.
In relation to the maximum thrust level developed by the exhaust port (i.e., the selected thrust lever has a maximum thrust level) the user may select a thrust level for storage of the rudder of about 5% to 50% of the maximum level. However, it is preferred to select a thrust level between about 10% to 40% of the maximum thrust level, with an optimum selected thrust level for storage of about 20% of the maximum level. Similarly, the thrust plate may include an adjustable orifice, having a variable surface area, such that the rudder moves to a deployed position at some thrust level selected by the user. Thus, when the thrust level is below the pre-selected thrust level, the rudder deploys. The selected thrust level is typically between about 5% and 50% of the maximum thrust level, but may also be selected to be between about 10% to 20% of the maximum thrust level, and most preferably, to be about 20% of the maximum thrust level.
Turning now to
FIG. 8
, a pivoting rudder blade assembly
130
, providing increased safety to operators and passengers, is shown. In this implementation of the pivoting rudder blade assembly
130
, a flexible portion
175
of the rudder shaft
170
is used to protect the rudder blade
160
upon encountering some hard or immovable object. The rudder blade
160
in this case is allowed to move out of the way of such objects due to the flexible portion
175
action, which prevents breakage of the rudder blade
160
upon encountering underwater obstacles.
To provide increased design flexibility and safety, the embodiment of the self-deploying rudder assembly
50
shown in
FIG. 9
can be used. In this instance, the entire rudder blade assembly
130
is designed to rotate 90° about the longitudinal axis
172
of the rudder shaft
170
at the same time the rudder blade
160
moves upward into the stored position when the thrust level selected by the operator is above the preselected thrust level set using the thrust blade adjuster
190
.
FIGS. 9 and 10
illustrate rotation of the rudder blade assembly
130
about the longitudinal axis
172
of the shaft
170
as a rudder shaft gear
240
attached to the rudder shaft
170
engages with the main body rudder gear rack
250
. The rotational movement about the longitudinal axis
172
of the rudder shaft
170
allows the rudder blade
160
to be stowed in a flat, horizontal position against the skeg
150
of the water craft
100
. In this stored position, the rudder blade
160
offers less resistance to the water during high speed operation of the water craft
100
, and is better protected against shear forces. To secure the rudder blade assembly
130
for geared rotation, bushings
320
, mounted to a rotational mounting plate
330
, can be used. Of course, as is well known to those skilled in the art, other implementations for rotating the rudder blade assembly
130
are possible. If a rudder blade plate
230
(not shown) is mounted to the rudder blade
160
for this implementation of the invention, it must be repositioned to the side of the rudder blade
160
(i.e., parallel to the rudder blade
160
, instead of perpendicular to the rudder blade
160
) for effective use.
Alternative embodiments of the invention include employing dual rudder blades
280
, as shown in FIG.
11
. In this implementation, a first and second rudder shaft
170
,
170
′ can be attached to the first and second rudder blades
160
,
160
′, respectively. The thrust plate
180
and pivoting action of the rudder blade assemblies
130
operate in the same manner as described above. Dual grooves
155
in the storage skeg
150
accommodate the rotor blades
160
,
160
′ when the rudder blade assemblies
130
move into the stored position. The use of dual rudders
280
increases the effective rudder surface area and provides more efficient steering characteristics for the water craft
100
.
The invention may include a water craft
100
attached to the self-deploying rudder assembly
50
as a complete apparatus for recreational operation on the water, or the invention may be considered as the self-deploying rudder assembly
50
alone. The assembly
50
is a simple, yet effective, auxiliary rudder device for water craft and other vehicles which make use of an exhaust port which includes an exhaust stream operating at various selected thrust levels. The design, using a tension spring or rubber band deployment means
210
maintains the rudder blade
160
in a deployed, functional position when the water craft is idling, or during low speed operations. This is especially useful in emergency situations, wherein throttle operation is typically reduced in an immediate fashion, and the need for steering in an effective manner remains. The natural tendency of the water craft operator to release the throttle lever and steer to avoid obstacles in emergency situations, such as impending collisions, is thereby augmented using the self-deploying rudder assembly
50
. Further safety advantages include the use of rudder blades
160
which operate substantially directly below the nozzle
110
of the water craft
100
when deployed, and which remain in a storage skeg
150
when stored. Thus, the rudders are not available to injure swimmers which may come in to close proximity of the water craft
100
during high speed operations. Passengers and/or operators falling off of the water craft
100
during high speed operations are likewise relatively safe from contact with the rudder blades
160
. The first class lever or rudder shaft
170
, used by the present invention is in direct contrast to other designs which make use of third class levers, and which are relatively unsafe.
Another possible implementation of the invention can be seen in
FIGS. 12A and 12B
. Here, the rudder shaft
170
is divided into two parts: an upper shaft
171
, and a lower shaft
172
. The shaft
170
, thus divided, is operated as an integral unit by means of a pair of interlocking gears (see FIG.
12
A), the plate gear
206
, and the rudder gear
207
. Alternatively, the shaft
170
can be divided as shown in
FIG. 12B
, wherein the upper shaft
171
and the lower shaft
172
are attached or connected to a pushrod
173
using pivot points
174
, such as rivets, screws, shafts and bushings, etc. While the rudder blade
160
continues to pivot about the rudder pivot
200
, the upper shaft
171
now pivots about the plate pivot
205
. Thus, when the exhaust stream thrust level is below the preselected thrust level designated by the operator of the water craft, the self-deploying rudder assembly
50
of the present invention maintains the configuration shown in
FIGS. 12A and 12B
. However, as the selected thrust level increases above the preselected thrust level, the rudder blade
160
will move in the “B” direction. The upper shaft
171
, along with the thrust plate
180
and thrust plate adjuster
190
, will move in the “A” direction out of the exhaust stream. In this stored position, the rudder blade will lie substantially beneath the thrust plate
180
, which positioning serves a dual purpose. First, the rudder blade
160
will normally be urged into the storage groove
155
by increasing water flow pressure as the water craft operates at higher speeds. Second, the rudder blade
160
will typically not extend beyond the end of the thrust plate
180
, so that no additional hazard is presented toward operators and passengers of the water craft.
The method of deploying a pivoting rudder blade assembly is shown in FIG.
13
. It is assumed that the rudder blade assembly includes a rudder shaft with a first end attached to a thrust plate, and a second end attached to a rudder blade using an exhaust port including an exhaust stream exiting the exhaust port at a selected thrust level, the method begins at step
500
and includes the steps of pivotally attaching the rudder shaft to the exhaust port
510
, retaining the thrust plate within the exhaust stream so that the rudder blade is in a deployed position so long as the selected thrust level is below a preselected thrust level
520
, and moving the thrust plate out of the exhaust stream so that the rudder moves to a stored position when the selected thrust level is above the preselected thrust level
530
, typically the rudder blade lies substantially beneath the exhaust port when in the stored position. Throughout the method the rudder blade assembly typically operates as a first class lever, as described above, and repeats steps
520
and
530
. However, as illustrated in
FIG. 12
, the rudder blade assembly is not necessarily operated as a first class lever in every case.
Although the invention has been described with reference to specific embodiments, this description is not meant to be construed in a limited sense. The various modifications of the disclosed embodiments, as well as alternative embodiments of the invention, will become apparent to persons skilled in the art upon reference to the description of the invention. It is, therefore, contemplated that the appended claims will cover such modifications that fall within the scope of the invention, or their equivalents.
Claims
- 1. A self-deploying rudder assembly for use with an exhaust port including an exhaust stream exiting the exhaust port at a selected thrust level, said self-deploying rudder assembly comprising:a mounting assembly for attaching the self-deploying rudder assembly to the exhaust port; a rudder blade assembly pivotally attached to said mounting assembly; a thrust plate constructed and arranged to intercept the exhaust stream, said thrust plate including at least one orifice having a variable surface area; a rudder shaft having a first end connected to said rudder blade assembly and a second end connected to said thrust plate assembly; whereby said rudder blade assembly is caused to pivotally move under the exhaust port to a stored position when the thrust level on said thrust plate is above a pre-selected level.
- 2. The self-deploying rudder assembly of claim 1 further including:a skeg attached to said mounting assembly.
- 3. The self-deploying rudder assembly of claim 2, wherein said skeg includes a groove constructed and arranged to receive said rudder blade in its stored position.
- 4. The self-deploying rudder assembly of claim 1 wherein said rudder shaft is divided into an upper shaft and a lower shaft connected by a pair of interlocking gears.
- 5. The self-deploying rudder assembly of claim 4 wherein:a rudder shaft gear is attached to said upper shaft; and a gear rack is rotatably engaged with said rudder shaft gear.
- 6. The self-deploying rudder assembly of claim 1 wherein said rudder shaft is divided into an upper shaft and a lower shaft connected by a pushrod.
- 7. The self-deploying rudder assembly of claim 1 wherein said stored position of said rudder blade is substantially beneath said thrust plate.
- 8. The self-deploying rudder assembly as defined in claim 1 further including deployment means to move said rudder blade assembly out of said stored position when the thrust level on said thrust plate is below a preselected level.
- 9. The self-deploying rudder assembly of claim 8 wherein said deployment means is a spring.
- 10. An apparatus for recreational operation in water comprising:a water craft having an exhaust port including an exhaust stream exiting the exhaust port at a preselected thrust level; a self-deploying rudder assembly attached to said water craft, said self-deploying rudder assembly including: a mounting assembly for attaching said self-deploying rudder assembly to said exhaust port; a rudder blade assembly pivotally attached to said mounting assembly; a thrust plate constructed and arranged to intercept said exhaust stream, said thrust plate including at least one orifice having a variable surface area; a rudder shaft having a first end connected to said rudder blade assembly and a second end connected to said thrust plate assembly; whereby said rudder blade assembly is caused pivotally to move under the exhaust port to a stored position when said thrust level on said thrust plate is above a pre-selected level.
- 11. The apparatus of claim 10 wherein said stored position of said rudder blade is substantially beneath said thrust plate.
- 12. The self-deploying rudder assembly as defined in claim 10 further including deployment means to move said rudder blade assembly out of said stored position when the thrust level on said thrust plate is below a preselected level.
- 13. The apparatus of claim 11 wherein said rudder shaft is divided into an upper shaft and a lower shaft connected by a pair of interlocking gears.
- 14. The apparatus of claim 13 wherein:rudder shaft gear is attached to said upper shaft; and a gear rack is rotatably engaged with said rudder shaft gear.
- 15. The apparatus of claim 10 wherein said rudder shaft is divided into an upper shaft and a lower shaft connected by a pushrod.
US Referenced Citations (6)
Foreign Referenced Citations (2)
Number |
Date |
Country |
5-162689 |
Jun 1993 |
JP |
283593 |
Nov 1999 |
JP |