U.S. patent number 3,776,173 [Application Number 05/193,761] was granted by the patent office on 1973-12-04 for propulsion system for a boat.
Invention is credited to Robert P. Horwitz.
United States Patent |
3,776,173 |
Horwitz |
December 4, 1973 |
PROPULSION SYSTEM FOR A BOAT
Abstract
The present invention relates to a propulsion system for a boat;
and more particularly discloses a propulsion system that not only
provides forward movement and directional control, but also
provides means for controlling the attitude of the boat. The
disclosed system accomplishes this dual result by the use of a
novel jet nozzle mounting structure that permits the nozzle to
pivot in a horizontal direction and/or in a vertical direction.
Pivoting in either direction is independent of the other, but may
still be combined with the other one when so desired, so that any
combination of boat heading and attitude may be provided.
Inventors: |
Horwitz; Robert P. (Newport
Beach, CA) |
Family
ID: |
22714896 |
Appl.
No.: |
05/193,761 |
Filed: |
October 29, 1971 |
Current U.S.
Class: |
440/42 |
Current CPC
Class: |
B63H
11/113 (20130101) |
Current International
Class: |
B63H
11/113 (20060101); B63H 11/00 (20060101); B63h
011/00 () |
Field of
Search: |
;115/12R,12A,11,14,15,16
;60/221,232 ;114/151 ;239/127.1,265.11,265.35 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Halvosa; George E. A.
Assistant Examiner: Basinger; S. D.
Claims
What is claimed is:
1. A jet propulsion system for a boat, comprising:
a jet producing nozzle;
said nozzle comprising a substantially spherically configurated
bearing surface;
direction control means for pivoting said nozzle horizontally
around a vertically oriented azimuth pivot axis, for controlling
the direction of said boat;
trim angle control means for pivoting said nozzle vertically around
a horizontally oriented elevation pivot axis, for controlling the
attitude of said boat;
a housing having a flared housing portion adapted to partially
enclose said bearing surface of said nozzle;
a support ring positioned to peripherally encircle said housing
portion;
means for pivotally attaching said support ring on said housing
portion for causing said support ring to pivot in only a first
manner;
means for attaching said nozzle to said support ring for causing
said nozzle to pivot in said first manner.
2. The combination of claim 1 including;
means for attaching said nozzle to said support ring for causing
said nozzle to pivot in a second manner.
3. The combination of claim 2 including means comprising a
directional control rod and a directional control linkage
interlinking said directional control rod and said support ring,
for causing said nozzle to pivot in said first manner.
4. The combination of claim 2 including means, comprising a trim
angle control rod and a trim angle control linkage interlinking
said trim angle control rod and said nozzle, for causing said
nozzle to pivot in said second manner.
5. The combination of claim 2 wherein said first pivotal manner is
horizontal, and said second pivotal manner is vertical.
6. A jet propulsion system for a boat, comprising;
a jet producing nozzle having a substantially spherically
configurated bearing surface;
a housing having a flared housing portion adapted to partially
enclose said bearing surface of sai nozzle;
means, comprising a sealing O-ring positioned in the interior
surface of said housing portion for providing a seal between the
interior surface of said housing portion and said bearing surface
of said nozzle;
direction control means for pivoting said nozzle horizontally
around a vertically oriented azimuth axis, for controlling the
horizontal direction of said jet from said nozzle;
said direction control means comprising a support ring positioned
to peripherally encircle said housing portion;
said direction control means further comprising pivot means,
including a pivot pin arrangement between said support ring and
said housing portion, for causing said support ring to be limited
to a pivotal movement in only a horizontal direction;
said direction control means further comprising means for attaching
said nozzle to said support ring, for causing said nozzle to pivot
in said horizontal direction;
means, comprising a direction control rod and a direction control
linkage interlinking said direction control rod and said support
ring, for actuating said direction control means;
trim angle control means for pivoting said nozzle vertically around
a horizontally oriented elevation axis, for controlling the
vertical direction of said jet from said nozzle;
said trim angle control means comprising pivot means, including a
pivot pin arrangement between said support ring and said nozzle,
for causing said nozzle to pivot in a vertical direction;
means, comprising a trim angle rod and a trim angle linkage
interlinking said trim angle rod and said nozzle, for actuating
said trim angle control means.
Description
BACKGROUND
In using and handling speedboats, there are many factors that enter
into the pleasure obtained from these water craft and one of the
most exhilarating factors is their high speeds. One way of
obtaining even higher speeds is to use a more powerful engine, but
there is a practicable limit to the engine size that is feasible
for each boat. Therefore, as a practical matter, the power input
cannot be continuously increased to too great an extent.
However, as is well known, speedboats experience an appreciable
amount of water drag, especially up to the speed at which the boat
begins to "plane." It would therefore be advantageous to cause the
boat to begin its planing operation at a lower speed.
Unfortunately, the planing characteristic of a boat or its "trim
angle" that controls the planing characteristic is inherent in a
boat's design and construction, but if this trim angle were able to
be changed, it would improve the boat's efficiency, increase the
boat's speed, and improve the boat's stability for various
different boating conditions.
OBJECTS AND DRAWINGS
It is therefore the principal object of the present invention to
provide an improved speedboat.
It is another object of the present invention to provide an
improved propulsion system for a speedboat.
It is still another object of the present invention to provide an
improved jet propulsion system for a speedboat.
It is a further object of the present invention to provide an
improved jet propulsion system that, in part, controls the boat's
attitude.
It is a still further object of the present invention to provide an
improved structure for a boat's propulsion system.
The attainment of these objects and others will be realized from a
study of the following description, taken in conjunction with the
drawings of which:
FIG. 1 shows a side view of a speedboat utilizing a jet propulsion
system;
FIG. 2 shows a cutaway horizontal cross sectional view of the
subject jet propulsion system in a dead -ahead driving
orientation;
FIG. 3 shows a cutaway horizontal cross sectional view of the
subject jet propulsion system in a turning orientation;
FIG. 4 shows a cutaway vertical cross sectional view of the subject
jet propulsion system in a flat attitude; and
FIG. 5 shows a schematic rear view of the pivoting arrangement of
subject jet propulsion system.
SYNOPSIS
The present invention discloses a dual purpose jet propulsion
system for a speedboat; the jet nozzle being mounted in such a way
that it may be pointed upwards, downwards, to the right, to the
left, and in any desired intermediate combination of directions.
This result is accomplished, in part, by forming part of the nozzle
into a substantially spherically configurated bearing surface and
by having this bearing surface coact with a suitable positioned
O-ring. In this way, the O-ring provides a seal regardless of the
direction in which the nozzle happens to be pointing.
A nozzle supporting ring is mounted on the propulsion system
housing in such a way that the support ring can pivot only in a
horizontal direction, thus causing the nozzle to also pivot in the
horizontal direction so that independent direction control is thus
obtained.
The nozzle is simultaneously mounted on the support ring in such a
manner that the nozzle can pivot in a vertical direction; so that
the independent attitude control is thus obtained.
In this way, the disclosed structure provides either pure
directional control, pure attitude control, or any desired
combination thereof.
Operation of a Jet Propulsion System
In the past, most speedboats used underwater propellers to propel
the boat through the water and in response to the constant demand
for greater speed the propellers were made larger, were made to
rotate faster, were designed with different angles, etc. While
these modifications tended to achieve their purpose, they also
introduced new problems -- such as cavitation of the propeller,
undue breakage, undesirable slippage, wastage of power, etc. Thus,
while these propeller modifications provided a limited increase in
speed, they were not completely satisfactory.
The newer trend for speedboats is the use of a "jet propulsion"
technique. This uses a water pump that forces a jet of high speed
water rearward from the stern of the boat; this rearwardly directed
water jet causing the boat to move in the opposite (forward)
direction. As will be obvious, the jet propulsion technique --
since it does not use propeller blades -- does no have the problem
associated with them; and the jet propulsion technique therefore
offered many speedboat advantages.
As the speeds of the boats increased, their trim angle became much
more important then previously, because this angle controlled the
speed at which the boat began to plane, i.e., to rise from the
surface of the water. This trim angle was usually conservatively
designed for safety during average boating conditions, but if the
boat was used under unusual boating conditions, this angle tended
to be a disadvantage -- in many cases causing the boat to
"porpoise" or bounce on the water. This behaviour is, of course,
not only undesirable, but may become dangerous at high speed.
The present application discloses means for controlling this trim
angle without impairing the boat's efficiency.
Overall Operation
FIG. 1 shows a boat 10 having a symbolically illustrated jet
propulsion system 11 that produces a high speed jet of water that
is forced out of the propulsion system 11 in a rearward direction.
It is, of course, essential to be able to control the direction of
the water jet and this horizontal direction control has been
accomplished in a number of ways.
The disclosed apparatus achieves control of the water jet in an
improved manner that may be understood from FIG. 2; which is a
horizontal cross sectional view of the disclosed propulsion system
15, as viewed from above. In FIG. 2, a water pump (not shown)
produces a high volume flow of water that moves in the direction
indicated by arrow 17a; the water flow being contained by the walls
of a housing 19, housing 19 terminating in a substantially
spherical portion 20.
The Jet Nozzle
Housing portion 20 partially encloses a jet nozzle 25 having a
constricting passageway that further accelerates the water flow,
whose direction in the nozzle 25 is indicated by arrow 17b; the
water jet emerging from nozzle 25 being indicated by the
directional arrow 17c. Since the water jet is shown to emerge in an
exact rearward direction in FIG. 2, the boat to which the
propulsion system 15 is attached will move forward in a
"dead-ahead" manner.
It should be noted that nozzle 25 comprises a substantially
spherically configurated bearing surface 27 that is partially
enclosed by the flared housing portion 20.
The Sealing Arrangement
Since the water in housing 19 and in nozzle 25 is under pressure, a
seal is desirable between the exterior surface 27 of nozzle 25 and
the interior surface 28 of housing portion 20. For reasons that
will become apparent from a later discussion, the disclosed
structure uses a seal comprising an "O-ring" 29 that is fitted into
a peripheral recess of the housing portion 20. Thus, sealing O-ring
29 prevents the leakage of water and the loss of water pressure
between the housing 19 and the nozzle 25.
Horizontal Directional Control
In order to provide horizontal directional control for the boat,
the emerging water jet -- whose direction is indicated by aroow 17c
-- must be diverted from its exact rearward direction. This
diversion is accomplished by means of a steering control rod 31 and
a steering control linkage 32, both of which will be more fully
discussed later.
For the moment, attention is directed to the horizontal cross
sectional view of the FIG. 3. This illustration corresponds to FIG.
2 except that nozzle 25 has been pivoted and shows that the
emerging jet now takes a new direction as indicated by arrow
17c.
This result has been achieved as follows. The steering control rod
31 has been moved leftward in the illustrating of FIG. 3, causing
the nozzle 25 to pivot around a vertically oriented "azimuth" pivot
axis 33; so that the water jet now emerges at an angle relative to
the center line of the boat -- thus causing the boat to turn from
its original dead-ahead course.
Thus, the nozzle 25 may be pivoted horizontally to any desired
extent and in either direction; the movement of the steering
control rod 31 in either of the directions indicated by the double
ended arrow 34 causing the nozzle 25 to pivot horizontally in a
corresponding direction as indicated by the double ended curved
arrow 35.
It should be noted that during the above discussed horizontal
pivoting of the nozzle 25, the previously mentioned O-ring 29
continues to provide the desired sealing function. This is
accomplished because O-ring 29 is always in arcuate peripheral
contact with the spherical bearing surface 27 of the nozzle 25. It
should be noted in passing, that the sealing O-ring 29 establishes
an "O-ring plane" whose significance will be discussed later.
In this way, the horizontal direction of the boat's movement is
readily controlled by the jet propulsion system; without danger of
losing water pressure at any particular angle, and without losing
overall efficiency.
Boat Attitude
As indicated above, it is frequently desirable to control, and to
change, the boat's attitude in order to prevent "boat squatting" or
"boat plowing" and this attitude control is accomplished in a
manner that is similar to that explained above in connection with
the horizontal direction control. The attitude control will be
better understood from FIG. 4, which is a vertical cross sectional
view, looking at the side of the subject propulsion system 15.
As indicated previously, the arrows 17 indicate the direction of
the water and jet flow, and it will be noted that the vertical
cross section of FIG. 4 shows the emerging jet flow to be in a
horizontal direction, as indicated by arrow 17c, so that the boat's
attitude is substantially the angle built into the boat by its
design and construction.
It should be noted that the previously discussed FIG. 2 illustrated
a dead-ahead horizontal orientation of the nozzle 25, and that the
FIG. 4 illustration about to be discussed illustrates a flat-out
vertical orientation of the nozzle.
Referring again to FIG. 4, an attitude control rod 36 and an
attitude control linkage 37 provide for vertically pivoting the
nozzle 25 around a horizontally oriented "elevation" pivot axis 38,
as indicated by the curved double ended arrow 39.
The vertical pivoting action is similar to the horizontal pivoting
action previously described, except that a total of only about
twenty degrees of vertical movement is needed to provide the
desired change of attitude angle.
It is readily apparent that as nozzle 25 is vertically pivoted
around this elevation axis 38, the water jet will be directed
either upwards or downwards. Thus, by controlling the vertical
angle of the water jet, the effective attitude of the boat may be
quickly and easily adjusted for changing boating conditions;
without adversely affecting the boat's forward direction, the
boat's speeds, or the boat's efficiency during the vertical
pivoting action.
It will be noted, as indicated above, that the sealing O-ring 29
establishes an O-ring plane and that during the vertical pivoting,
the O-ring 29 continues to seal the housing 19 and the nozzle 25 in
the same manner as for the horizontal pivoting of the nozzle. Thus,
a relatively simple O-ring and a substantially spherically
configurated bearing surface provide a simple solution to the
sealing problem.
The Horizontal Pivoting Mechanism
In order to provide coordinated horizontal and vertical pivoting,
it has been found desirable to use a ring and pivot arrangement
that will be best understood by referring back to FIG. 2. This
shows a support ring 40 that is positioned to peripherally encircle
the end portion 20 of housing 19 and -- in a manner and for reasons
to be discussed later -- supporting ring 40 is affixed to housing
portion 20 in such a way that the supporting ring 40 cannot rotate,
it can only pivot around the vertically oriented "azimuth" axis 33.
The support ring 40 therefore pivots in a first, horizontal
mode.
The peripheral support ring 40 is shown to have diametrically
oppositely positioned ring sockets for accepting pivot pins 42a and
42b that are fixed in respective ring sockets in any suitable
manner; e.g., pins, threaded arrangements, adhesives, etc. Thus,
the pivot pins 42a and 42b are affixed in supporting ring 40 at
diametrically opposite locations and these pivot pin locations
always remain in the same horizontal plane as the support ring 40
pivots around the vertically oriented azimuth axis 33.
FIG. 3 indicates that support ring 40 has been pivoted horizontally
around the vertically oriented azimuth axis 33. The nozzle 25 has
pair of diametrically oppositely positioned horizontally oriented
"radials" 44 that carry longitudinal nozzle arms 45 having bearing
recesses for receiving respective pivot pins 42a and 42
respectively. A suitable bearing material, such as a sleeve of
Teflon or Nylon, may be inserted between the pivot pins 42 and
their recesses.
The Horizontal Pivoting Action
The resultant horizontal pivoting action may be understood by
briefly referring back to FIG. 2, which shows the nozzle 25 in its
dead-ahead horizontal orientation. The horizontal pivoting shown in
FIG. 3 has been accomplished by moving the steering control rod 31
leftward; the horizontal linkage 32 pulling though the pivot-pin
426 on its attached portion of ring 40, which -- acting through,
the nozzle arms 45, and the radials 44 -- causes support ring 40
and the nozzle 25 to pivot horizontally around the vertically
oriented azimuth axis 33 to the horizontal orientation indicated in
FIG. 3. Thus, the amount and direction of horizontal pivoting is
controlled by the steering control rod 31.
Since nozzle 25 is exposed to appreciable water flow and water
pressure, the steering control rod 31 is preferably provided with
suitable holding or clamping means (not shown).
The Horizontal Linkage
it will be noted from FIG. 3 that the lower shown pivot pin 42b
extends outside of the support ring 40, and is indicated to
terminate in a ball. FIG. 3 further shows that the end portion of
the steering control rod 31 contains a cutout that is adapted to
receive the ball; a set screw causing a pair of pressure pads to
contact the ball, and to hold it in place. Of course, many such
type of ball joints are commercially available.
A threaded rod and a lock nut are used to provide length adjustment
of the steering control rod 31.
Vertical Pivoting
It was pointed out above in connection with FIG. 2 and 3, that
support ring 40 was pivoted horizontally around an azimuth axis 33,
but could not rotate. Therefore, the pivot pins 42 mounted on
support ring 40 are always in and always remains in the same
horizontal plane regardless of the instantaneous position of the
support ring 40.
As a result of this always horizontal orientation of the pivot pins
42, nozzle 25 -- which is mounted on pivot pins 42, -- is adapted
to pivot vertically around the always horizontal pivot pins 42.
Therefore, these pivot pins 42 define the above mentioned elevation
axis 38 around which the nozzle 25 pivots vertically and the pivot
pins 42 will therefore be designated as the "elevation pivot pins
42."
The vertical pivoting action may be better understood by referring
back to the vertical cross sectional view of FIG. 4. From this
illustration, it will be recalled that the vertical pivoting action
of nozzle 25 takes place around a horizontally oriented elevation
axis 38. The operation of this horizontally oriented elevation axis
38 will be understood by referring back to FIGS. 2 and 3 and
visualizing the vertically oriented elevation axis 38 as being
defined by the elevation pivot pins 42.
Since the elevation axis 38 and the elevation pins 42 are always in
the same horizontal plane, the vertical pivoting of nozzle 25 will
therefore cause the nozzle to point upward, point downward, or
point horizontally as indicated in FIG. 4, regardless of the
instantaneous direction of the nozzle 25/support ring 40
combination.
FIG. 4 also shows a pair of diametrically oppositedly positioned
pivot pins 48 that are affixed to housing portion 20 and are seated
in bearing recesses of the support ring 40 -- suitable bearing
sleeves being used as previously discussed. These pivot pins 48
define the ends of the vertically oriented azimuth axis 33, and
will therefore be referred to as "azimuth pivot pins 48." Thus, the
azimuth pivot pins 48 attach the support ring 40 to housing portion
20; preventing support ring 40 from rotating, and limiting the
support ring 40 to a horizontal pivoting movement.
The Vertical Linkage
FIG. 4 shows a vertical linkage 37 that is quite similar to the
horizontal linkage 32 previously discussed in connection with FIG.
3. The vertical, or attitude control linkage 37, comprises an
attitude control rod 36 that accepts a ball which is affixed to a
longitudinal arm 50 attached to a nozzle radial 51.
However, it should be noted that, unlike the previously discussed
horizontal linkage, the vertical linkage 36 has its ball/rod
connection separated from the support ring 40. Thus, as the
attitude control rod 36 is moved forward or backward, it does not
affect the support ring 40, rather it causes the nozzle 25 to pivot
vertically around its elevation axis 38 -- which is carried on
support ring 40.
The principal difference between the horizontal linkage and the
vertical linkage is as follows. The horizontal linkage is attached
to the support ring 40, and provides a horizontal pivoting around
the azimuth axis 33; whereas the vertical linkage is attached to
the nozzle 25 and provides vertical pivoting around elevation axis
38.
Attention is now directed to FIG. 5, which is partially cutaway
rear view that schematically illustrates the overall structure and
the pivoting support. FIG. 5 shows support ring 40 to be supported
on housing 20 by means of the pair of vertically oriented
oppositely positioned azimuth pivot pins 48 that are affixed in a
vertical plane on housing portion 20. Due to the fact that the pair
of azimuth pivot pins 48 are located in a vertical plane, and are
fixedly positioned with respect to the housing portion 20, support
ring 40 cannot rotate peripherally; but, rather, is restricted to a
horizontal pivoting motion around the vertically oriented azimuth
axis 38. Thus, as indicated previously, support ring 40 pivots
horizontally as indicated in FIG. 2 and 3 -- to produce horizontal
direction control.
FIG. 5 also shows that nozzle 25 is supported on support ring 40 by
means of a pair of oppositely positioned elevation pivot pins 42
that are always located in a horizontal plane on ring 40. Due to
the fact that the pair of elevation pivot pins 42 are located in a
horizontal plane, and are fixedly positioned with respect to the
ring, nozzle 25 cannot rotate peripherally, but, rather, is
restricted to a vertical pivotal motion around the horizontally
oriented elevation axis 33 to provide vertical attitude
control.
The steering control rod 31, and the attitude control rod 36 are
indicated to be at the near side and the top side respectively of
the overall structure, but these locations may be varied as
desired.
It can now be understood that nozzle 25 may assume a dead-ahead
horizontal direction as illustrated in FIG. 2, and that entire
nozzle 25 may be horizontally pivoted around its vertically
oriented azimuth axis 38 defined azimuth pivot pins 42. As a result
of this horizontal pivoting, the nozzle 25 may be pivoted rightward
or leftward, depending upon the movement of the steering control
rod 31. In this way, directional control is achieved.
It may also be understood that nozzle 25 may assume a level
vertical orientation as indicated in FIG. 4; and that the nozzle 25
may be pivoted vertically about its horizontally oriented elevation
axis 33 defined by elevation pivot pins 42. As a result of the
vertical pivoting, the nozzle 25 may be pivoted upward or downwad
depending upon the movement of attitude control rod 36. In this
way, attitude control is achieved.
Thus, the disclosed boat propulsion system controls boat direction
and the boat's attitude.
It should be noted that the disclosed support ring pivoting
arrangement gives the same mechanical effect as though the nozzle
were rotating on its peripheral sealing O-ring, but has the
additional advantage that the much stronger ring structure is
adapted to take all of the necessary stresses, while still assuring
a desired spherical relationship between the nozzle and the
housing. In this way, the O-ring has the sole function of providing
a sealing effect; being completely relieved from the mechanical
loading effects produced by the boat's driving jet propulsion
system.
SUMMARY
The subject invention has many advantages over prior art propulsion
systems. First of all, it controls both the horizontal direction
and the vertical attitude. Second, the structure is quite simple.
Third, the sealing system is extremely efficient. Fourth, there is
no feedback between the horizontal control system and the vertical
control system; each is substantially independent of the other, and
yet their actions may be combined to any extent desired. Fifth, on
a given boat the planing speed was reduced from 25 miles per hour
to 17 miles per hour; thus providing improved overall efficiency.
Sixth, the boat's top speed was increased by 7 miles per hour.
Seventh, boat's attitude may be adjusted instantaneously, as soon
as a different boating condition makes such a change desirable. And
finally, these improved results are achieved without increasing the
size of the engine.
* * * * *