Marine propulsion unit with hydraulic pump

Information

  • Patent Grant
  • 6176750
  • Patent Number
    6,176,750
  • Date Filed
    Tuesday, August 24, 1999
    24 years ago
  • Date Issued
    Tuesday, January 23, 2001
    23 years ago
Abstract
An improved hydraulic system for a twin propeller marine propulsion unit. A vertical drive shaft is operably connected to the engine of the propulsion unit and carries a pinion that drives a pair of coaxial bevel gears. An inner propeller shaft and an outer propeller shaft are mounted concentrically in the lower torpedo section of the gear case and each propeller shaft carries a propeller. To provide forward movement for the watercraft, a sliding clutch is moved in one direction to operably connect the first of the bevel gears with the inner propeller shaft to drive the rear propeller. A hydraulically operated multi-disc clutch is actuated when engine speed reaches a pre-selected elevated value to operably connect the second of the bevel gears to the outer propeller shaft, to thereby drive the second propeller in the opposite direction. The hydraulic system for actuating the multi-disc clutch includes a pump connected to the inner propeller shaft, and the pump has an inlet communicating with a fluid reservoir in the gear case and has an outlet which is connected through a hydraulic line to the multi-disc clutch. A strainer, a pressure regulator and a valve mechanism are disposed in the lower gear case and are located in series in the hydraulic line. At idle and slow operating speeds the valve is held by a solenoid in a position where the fluid is dumped to the reservoir, so that the pressure of the fluid being directed to the multi-disc clutch is insufficient to engage the clutch. At engine speeds above a preselected value, the solenoid is deenergized and the valve is then biased to a position where the fluid is delivered to the multi-disc clutch to engage the clutch and cause operation of the second propeller.
Description




BACKGROUND OF THE INVENTION




Certain marine propulsion units, such as outboard drives and inboard/outboard stern drives, utilize a forward-neutral-reverse transmission along with twin propellers. The typical twin propeller system includes a vertical drive shaft which is operably connected to the engine and is journaled for rotation in the lower gearcase. The lower end of the drive shaft carries a pinion which drives a pair of coaxial bevel gears that are located in the lower torpedo-shaped section of the gearcase. Inner and outer propeller shafts are mounted concentrically in the lower section and each propeller shaft carries a propeller, with the propeller of the outer shaft being located forwardly of the propeller of the inner shaft.




U.S. Pat. No. 4,793,773 is directed to a twin propeller propulsion system in which both propellers are rotated at the same speed, but in opposite directions, during forward movement of the watercraft. With this system, a mechanism is provided to disconnect the outer propeller shaft when the watercraft is moved in the reverse direction. Thus, with the system shown in the aforementioned patent, both propellers are operated during forward movement of the watercraft, but only the inner propeller shaft and the rear propeller are operated during reverse movement.




Co-pending U.S. Pat. application Ser. No. 08/719,633, filed Sep. 25, 1996, now U.S. Pat. No. 5,766,047 is directed to a twin propeller marine propulsion system in which, during forward movement of the watercraft, only one of the propellers is driven at low engine speed and the second propeller is driven when the engine speed reaches a pre-selected elevated value.




In accordance with the construction of the aforementioned patent application, a sliding clutch mechanism having forward neutral and reverse positions is employed to selectively engage the inner propeller shaft with the bevel gears to thereby rotate the inner propeller shaft and the rear propeller in both the forward and reverse directions. In addition, a hydraulically operated multiple disc clutch located in the lower torpedo section is employed to selectively cause engagement of one of the bevel gears with the outer propeller shaft when the engine speed reaches a pre-selected elevated value, normally in the range of 3,500 rpm to 7,000 rpm, to thereby cause the second or forward propeller to rotate in the opposite direction from the rear propeller. With this construction, only the rear propeller is driven at low forward speeds, while at high forward speeds both propellers are driven.




As described in the aforementioned patent application, the multiple disc clutch is moved to the engaged position at the pre-selected elevated engine speed by supplying pressurized fluid to a piston which engages the multiple clutch discs and moves the discs to a contacting or driving position. With this construction, only a single propeller is operable at low speeds, and once the pre-selected elevated engine speed has been achieved, the second propeller is then driven, resulting in a significant improvement in acceleration of the watercraft when getting on plane.




SUMMARY OF THE INVENTION




The invention is directed to an improved hydraulic system for a twin propeller marine propulsion unit of the type described in pending U.S. patent application, Ser. No. 08/719,633, filed Sep. 25, 1996 now U.S. Pat. No. 5,766,047.




The propulsion unit includes a vertical drive shaft that is journaled in the lower gearcase. The lower end of the drive shaft carries a beveled pinion gear that drives a pair of coaxial annular bevel gears located in the lower torpedo section of the gearcase. Inner and outer propeller shafts are journaled concentrically within the torpedo section and each propeller shaft carries a propeller with the propeller on the inner shaft being located to the rear of the propeller on the outer shaft.




A sliding clutch mechanism having forward, neutral and reverse positions is employed to selectively engage the inner propeller shaft with the bevel gears to thereby rotate the inner propeller shaft and the rear propeller in both forward and reverse directions. In addition, a hydraulically operated multiple disc clutch located in the lower torpedo section is employed to selectively cause engagement of one of the bevel gears with the outer propeller shaft when the engine reaches a pre-selected elevated value normally in the range of about 3,500 rpm to 7,000 rpm, to thereby cause the second or forward propeller to rotate in the opposite direction from the rear propeller. Thus, at low forward speeds only the rear propeller is driven, while at high forward speeds, both propellers are driven.




In accordance with the invention, an improved hydraulic system located within the gearcase is employed to supply pressurized fluid to a piston which acts to engage the multiple disc clutch and move the clutch to a contacting or driving position. The hydraulic fluid is pressurized through operation of a pump that is operably connected to the inner propeller shaft, so that rotation of the inner propeller shaft in the forward direction of watercraft movement will drive the pump to pressurize the fluid. The inlet to the pump communicates with a fluid reservoir or sump which is located in the gearcase, while the outlet of the pump is connected through a hydraulic line or conduit to the piston of the multiple disc clutch. As a feature of the invention, a strainer, pressure regulator, and valve mechanism are mounted within the gearcase and are located in series in the hydraulic line.




The strainer includes a generally cylindrical screen element which serves to filter out foreign particles in the hydraulic fluid. In addition, the strainer incorporates a provision for by-passing the fluid around the screen element when there is a substantial pressure drop across the screen element which can occur at low ambient temperatures or if the screen element is clogged.




The pressure regulator, which is located downstream from the strainer, includes a generally cylindrical casing which houses a plunger having a flat face which is exposed to the pressure of the fluid in the hydraulic line. On an increase in pressure in the fluid above a pre-selected value, the plunger will be moved outwardly against a spring biasing force to expose an outlet in the casing, thereby diverting fluid to the sump or reservoir in the gearcase.




The valve mechanism, which is located downstream of the pressure regulator, includes a valve body which is preferably formed integrally with the casing of the pressure regulator. The valve mechanism includes a solenoid operated valve member. At idle or low engine speed, the valve member is held in a dumping position by the energized solenoid so that the fluid is dumped to the reservoir and the pressure of the fluid being supplied to the piston of the multi-disc clutch is insufficient to actuate the piston and engage the clutch. When the engine speed increases to a preselected elevated value, a conventional engine speed sensor acts to deenergize the solenoid, and the valve member will then be biased to a second or clutching position where the fluid will be delivered to the piston of the multi-disc clutch to cause engagement of the clutch and thus effect operation of the outer propeller shaft and its propeller.




As a feature of the invention, a pair of concentrically mounted springs interconnect the valve member and the valve body. A first of the springs has a substantially lesser force than the second spring and the first spring acts to urge the valve to the clutching position. When the valve member is moved toward the dumping position by operation of the solenoid, the initial movement of the solenoid plunger will compress the lighter spring and further movement of the plunger will cause compression of the heavier spring. The use of the two springs results in the combined spring force throughout the stroke of the solenoid plunger being a substantial portion of the force of the solenoid throughout the stroke of the solenoid plunger, so that the clutch will be actuated with a minimum time lag.




The invention provides a compact unit with the strainer, pressure regulator and valve mechanism being contained within the lower unit of the outboard or stern drive.




The system effectively filters foreign particles from the hydraulic fluid and yet permits by-pass of the screen element when a predetermined pressure drop occurs across the screen element, such as for example, when the hydraulic fluid is at a low temperature causing the fluid to be very viscous, or in case the screen becomes clogged. The pressure regulator provides a substantially uniform pressure for the fluid being delivered to the clutch when the valve is in the clutching position. The system is designed without need for a shut-off valve to the clutch when the valve is in the dumping position, thus permitting use of a less expensive valve structure.




Other objects and advantages will appear in the course of the following description.











DESCRIPTION OF THE DRAWINGS




The drawings illustrate the best mode presently contemplated of carrying out the invention.




In the drawings:





FIG. 1

is a longitudinal section of the lower drive unit of an outboard marine drive incorporating the invention;





FIG. 2

is an enlarged fragmentary section showing the forward portion of the drive mechanism;





FIG. 3

is a longitudinal section of the strainer unit with the screen element being shown in the screening position;





FIG. 4

is a view similar to

FIG. 3

with the screen element being shown in the by-pass position;





FIG. 5

is a section taken along line


5





5


of

FIG. 4

;





FIG. 6

is a longitudinal section of the pressure regulator with the plunger of the pressure regulator being in the non-dumping position;





FIG. 7

is a view similar to

FIG. 6

with the plunger in a dumping position;





FIG. 8

is a transverse section taken along line


8





8


of

FIG. 6

;





FIG. 9

is a section taken along line


9





9


of of

FIG. 8

, and showing the valve in the clutching position;





FIG. 10

is a view similar to FIG.


9


and showing the valve in the dumping position;





FIG. 11

is a section taken along line


11





11


of

FIG. 10

;





FIG. 12

is a horizontal section taken along line


12





12


of FIG.


8


and showing the pressure regulator and the valve mechanism;





FIG. 13

is an enlarged fragmentary longitudinal section showing the multidisc clutch construction;





FIG. 14

is an enlarged fragmentary section of the seal between the valve body and the clutch housing; and





FIG. 15

is a graph showing the combined spring force acting on the valve as compared to the solenoid force.











DESCRIPTION OF THE ILLUSTRATED EMBODIMENT





FIG. 1

shows a twin propeller marine outboard engine


1


for a boat or watercraft that incorporates the invention. The drive mechanism for driving the twin propellers of the outboard engine


1


is the same as that described in copending U.S. application Ser. No. 08,719,633, filed Sep. 25, 1996, now U.S. Pat. No. 5,766,047, and the description of that patent application is incorporated herein by reference. It is contemplated that the invention can also be utilized with an inboard/outboard stern drive, or other marine drive.




Outboard engine


1


includes a vertical drive shaft


2


which is journaled for rotation in gear case


3


by a bearing assembly


4


. The lower end of drive shaft


2


carries a bevel pinion gear


5


that is located within the lower torpedo-shaped section


6


of the gearcase.




Pinion gear


5


drives a pair of coaxial, annular bevel gears


7


and


8


. As best shown in

FIG. 2

, an inner propeller shaft


9


extends through aligned openings in bevel bears


7


and


8


and the forward end of shaft


9


is journaled within the hub of bevel gear


7


by a suitable bearing assembly. The central portion of inner propeller shaft


9


is provided with an axial passage


10


which merges into an enlarged forward passage


12


.




Secured to the rear end of propeller shaft


9


is a hub


13


of a propeller


14


, and propeller


14


includes a plurality of blades which are located at a rearward rake angle, preferably in the range of 20° to 30°.




An annular sliding clutch


15


is located within torpedo section


6


and includes a series of forwardly facing teeth


16


which are adapted to engage teeth on bevel gear


7


. Clutch


15


is also formed with a series of rearwardly facing teeth


17


adapted to engage teeth


18


on the forward end of a clutch housing


19


that is threaded to the hub portion of bevel gear


8


and rotates with the bevel gear. Clutch


15


can be moved between three positions, namely a central or neutral position, a forward position where teeth


16


engage the teeth on bevel gear


7


, and a rearward position in which the teeth


17


engage the teeth


18


of housing


19


.




To move clutch


15


between the three positions, a pin


20


extends diametrically across the clutch and extends through elongated slots


22


formed in the inner propeller shaft


9


. Pin


20


also extends through a pair of aligned holes in a sleeve


23


that is mounted in the forward passage


12


of inner propeller shaft


9


. As shown in

FIG. 2

, the forward end of sleeve


23


is enlarged and is provided with a circumferential groove


24


which receives a crank


25


mounted on the lower end of actuating rod


26


. Rotation of rod


26


will pivot crank


25


to thereby move sleeve


23


axially, and thus move clutch


15


between the neutral, forward and reverse positions. When clutch


15


is moved forwardly to engage teeth


16


with the teeth on bevel gear


7


, the clutch will rotate with bevel gear


7


and impart rotation to the inner propeller shaft


9


to drive the propeller


14


.




An outer propeller shaft


27


is mounted concentrically around the inner propeller shaft. To provide support for the propeller shafts


9


and


27


, an annular bearing carrier


28


is threaded on the rear end of torpedo section


6


, and is positioned between the outer propeller shaft


27


and the torpedo section


6


, as described in detail in the aforementioned patent application. A hub


29


of propeller


30


is secured to the outer propeller shaft


27


, and propeller


30


is located forwardly of propeller


14


.




The hub portion


32


of housing


19


is threaded to bevel gear


8


and rotates with the bevel gear. Housing


19


also includes an enlarged rear portion


33


that houses a multiple disc clutch


34


. Clutch


34


, when engaged, functions to connect the housing


19


with the outer propeller shaft


27


, to thereby drive propeller


30


.




Clutch


34


, as described in detail in the aforementioned patent application, includes a series of clutch discs


35


each having a plurality of circumferentially spaced, outwardly extending ears or lugs


36


, which are engaged with slots


37


formed in the rear portion


33


of housing


19


. A second group of generally flat clutch discs


38


are interdigitated with discs


35


and opposite faces of the discs


38


are provided with a friction coating. Discs


38


are connected to outer propeller shaft


27


through a splined connection.




Discs


35


and


38


are contained within the enlarged rear portion


33


of housing


19


by a pressure plate


40


having circumferentially spaced peripheral ears or lugs that engage the slots


37


in housing portion


33


. The cap is retained in position by a suitable snap ring


42


.




Spaced outwardly of section


33


of housing


19


is a cylindrical metal sleeve


43


having a longitudinal slot


44


which registers with a series of holes


45


in gearcase


3


. Holes


45


communicate with a sump or reservoir


46


formed in the gearcase. Oil or hydraulic fluid can flow between reservoir


46


and torpedo section


6


through holes


45


and slot


44


. In addition, holes


45


a also provide communication between the reservoir


46


and the interior of torpedo section


6


.




Clutch discs


35


and


38


are moved into driving engagement by an annular piston


47


which is mounted in the rear section


33


of housing


19


. Piston


47


has a rear face which is adapted to engage the discs


35


and


38


and is also provided with a generally flat forward face


48


. The piston is urged forwardly by a series of springs


49


, each of which is mounted in a longitudinal hole in outer propeller shaft


27


. The rear end of each spring


49


engages the bottom of a hole, while the forward end of each spring bears against a shoulder on pin


50


which, in turn, bears against the piston


47


. Thus, the force of springs


49


urge the piston


47


forwardly. In this position, the peripheral edge of forward face


48


will engage a shoulder on housing


19


, as best seen in

FIG. 13

to space the face


48


away from the bottom of housing


19


.




Piston


47


is adapted to be moved rearwardly to engage clutch discs


35


and


38


by pressurized hydraulic fluid or oil. The rotating housing


19


is provided with a series of axial holes


52


which communicate with the space between piston face


48


and the bottom of housing


19


. The forward ends of holes


52


connect with an annular groove


53


formed in the outer surface of hub portion


32


of housing


19


, and grooves


53


, in turn, communicate with radial holes


54


in ring


55


. Ring


55


is fixed to gear case


3


and the outer ends of radial holes


54


communicate with a circumferential groove


56


, which receives the pressurized hydraulic fluid as will be described in greater detail.




The hydraulic system of the invention includes a pump


57


, as shown in

FIG. 2

, which is operably connected to inner propeller shaft


9


and rotates with the shaft. Pump


57


can be constructed as described in the aforementioned patent application Ser. No. 08/719,633, now U.S. Pat. No. 5,766,047. Chamber


58


located at the forward portion of torpedo section


6


of the gearcase is normally filled with oil and during operation of pump


57


oil will be drawn from chamber


58


through inlet


59


to the pump and fluid will be discharged from the pump through outlet


60


to the forward chamber


62


. The hydraulic fluid will then flow through passage


63


in gearcase


3


to hydraulic line or conduit


64


. Hydraulic line


64


is connected to the inlet


65


of a strainer or filter casing


66


, which is located within gearcase


3


. Inlet


65


communicates with the lower end of a vertical passage


67


which, in turn, is connected to a horizontal passage


68


that leads to a central chamber


69


in casing


66


, as best seen in FIG.


3


.




Mounted within chamber


69


is a generally cup-shaped screen element


70


which includes an outer cylindrical perforated metal member


72


, and an inner cylindrical screen or mesh


73


, preferably formed of stainless steel. In the normal screening position, the open end of screen element


70


is biased against the bottom of an annular recess


74


formed in casing


66


by a coil spring


75


which is interposed between the closed end of the screen element and a cap


76


which is secured to the open end of casing


66


by bolts


77


. In the screening position the hydraulic fluid enters the hollow interior of screen element


70


through passage


68


and flows radially outward through the screen element to outlet


78


in casing


66


.




The screening system also includes a provision to bypass the screen element


70


in the event there is a substantial pressure differential between the interior and exterior of the screen element as could occur if the screen element is clogged, or if the hydraulic fluid is at a low temperature and is very viscous. If the pressure differential exceeds a preselected value, the internal pressure in screen element


70


will move the filter element axially against the force of the spring


75


to a bypass position, as shown in FIG.


4


. The inner wall of casing


66


is provided with a series of longitudinal grooves or splines


79


, and when the end of the screen element


70


is unseated from the recess


74


, the fluid will pass through the grooves or splines


79


to the outlet


78


, thus bypassing the screen element


70


. If the pressure differential resulting in the bypass is caused by low temperature oil, the heating of the oil through operation of the engine will reduce the pressure differential, causing the screen element


70


to move to the right, as shown in

FIG. 3

, to close off the bypass.




The hydraulic fluid is not only employed to operate to the multi-disc clutch


34


, but is also used to lubricate the various operating or moving elements contained within torpedo section


6


. As the valve which controls the flow of fluid in the hydraulic system has close tolerances, it is important that any foreign particulate material be removed from the fluid before it passes to the valve and to the clutch


6


.




Outlet


78


in the filter or strainer casing


66


is connected by nipple


80


to a passage


81


in the upper surface of a housing


82


of a pressure regulator


83


, which is also mounted within the gearcase


3


, and is located upstream of a control or dump valve


84


.




Pressure regulator


83


includes a plunger or slide


85


which is mounted for axial sliding movement in a bore


86


of housing


82


. As best shown in

FIG. 7

, the central portion of plunger


85


is provided with a radially extending flange or collar


87


which is biased against a shoulder


88


formed in the pressure regulator housing


82


by a coil spring


89


. The outer end of spring


89


bears against a snap ring


90


which is mounted within a circumferential groove in the inner surface of housing


82


. Thus, the force of spring


89


will urge the flange


87


into engagement with shoulder


88


and the inner face


91


of plunger


85


will be exposed to the pressure of the fluid in passage


81


.




Pressure regulator housing


82


is also formed with a radial outlet


92


which communicates with bore


86


. At idle and slow engine speeds, outlet


92


is normally closed off by plunger


85


, as shown in FIG.


7


. However, at higher engine speeds when the valve is supplying fluid to the multi-disc clutch, if the pressure of the fluid in passage


81


exceeds a pre-selected value, the pressure will force the plunger


85


axially against the force of spring


89


to thereby expose the outlet


92


and dump fluid to the reservoir


64


.




Valve unit


84


includes a valve body


93


, which is formed integrally with housing


82


of pressure regulator


83


. Housing


82


and valve body


93


are located in a generally side-by-side relation, as best shown in FIG.


8


. Valve body


93


includes a valve chamber


94


, and a generally horizontal passage


95


connects passage


81


in pressure regulator housing


82


with valve chamber


94


.




A valve


96


is mounted for sliding movement within chamber


94


, and is connected to the plunger


97


of a solenoid


98


by a pin


99


. To provide the connection, plunger


97


is provided with a bifurcated end


100


which straddles a lug


101


on valve


96


and pin


99


extends through aligned holes in end


100


and the lug


101


to provide the connection.




To mount solenoid


98


on valve body


93


, an externally threaded sleeve


102


projects outwardly from the end of the solenoid and surrounds the plunger


97


. Sleeve


102


is threaded within a suitable opening in valve body


93


, as best shown in

FIGS. 9 and 10

, thus supporting the solenoid


98


from the valve body


93


.




Valve


96


is provided with a generally cylindrical section


103


and an outer section


104


of reduced diameter, which is connected to the cylindrical section


103


by a tapered area


105


. A head or cap


106


is secured to the outer end of the valve section


104


.




Valve


96


is biased to a non-dumping or clutching position, as shown in

FIG. 9

, where the valve will not restrict the flow of pressurized fluid from passage


95


, through valve chamber


94


to outlet


107


. Outlet


107


is located at 90° from passage


81


and is connected to a diagonal passage


108


in gear case


3


. Diagonal passage


108


, in turn, communicates with circumferential groove


56


, so that in this position of valve


95


, pressurized fluid will be supplied through holes


54


and axial passages


52


against the face


48


of piston


47


, thus moving the piston against the force of spring


49


to engage the clutch


34


. Valve


96


is biased to this position by a coil spring


109


which is interposed between valve body


93


and head


106


of the valve. With this construction, the force of spring


109


will urge the valve


96


to the position shown in

FIG. 9

to effect engagement of clutch


34


. The pressure regulator


83


comes into play when the valve


96


is in the clutching position, serving to dump fluid through outlet


92


to reservoir


46


when the fluid pressure exceeds a preselected value.




As a feature of the invention, a second coil spring


110


is located concentrically around the spring


109


and the inner end of spring


110


is seated within an annular recess in valve body


93


. When the valve


96


is in the position as shown in

FIG. 9

, the outer end of spring


110


will be spaced from an annular flange


112


on head


106


. In the preferred form of the invention, spring


110


has a greater spring force than spring


109


.




With solenoid


98


deenergized, the low rate spring


109


will urge valve


96


to the position shown in

FIG. 9

to permit the hydraulic fluid to pass through the valve body


93


to the passage


108


and hence to the piston


47


of multi-disc clutch


34


to engage the clutch. When the solenoid is energized, plunger


97


will be drawn inwardly, thus compressing spring


109


. Continued inward movement of solenoid plunger


97


will bring the flange


112


of head


106


into contact with the high rate spring


110


, compressing the spring


110


, so that at this stage the force of both springs will oppose the force of the solenoid. With plunger


97


fully retracted, valve


96


will be in the position shown in

FIG. 10

, in which the tapered section


105


of the valve will be aligned with the fluid passage in the valve body. In this position of the valve, the fluid will be dumped through the annular gap


113


between valve section


104


and the valve body to the reservoir


46


. Thus, the pressure of the fluid in outlet


107


will be insufficient to move piston


47


against the force of springs


49


, so that the clutch


34


will remain disengaged.




The use of the two springs


109


and


110


with different spring rates, enables the combined spring rate to be a substantial portion of the force of the solenoid throughout the stroke of the solenoid plunger.

FIG. 15

includes a curve showing the solenoid force in lbs. versus the stroke in inches of the solenoid plunger. The solenoid force is low on initial retraction of the plunger and then increases dramatically as the plunger moves to its fully retracted position.

FIG. 15

also includes a curve illustrating the combined force of springs


109


and


110


during movement of the solenoid plunger. The spring force acting against the valve will be relatively low on initial retraction of the solenoid plunger due to the fact that only the low rate spring


109


is acting on the valve. When the head


106


of the valve engages the high rate spring


110


, the combined force of the two springs will be relatively high and will, in general, follow the solenoid force. By approximating the spring force to the solenoid force, clutch


34


will be actuated with a minimum time lag, and this provides better control over the clutching in of the second propeller mounted on the outer propeller shaft.




To prevent leakage of fluid at the joint between the fixed ring


55


and the rotating clutch housing


19


, a flexible lip-type seal


115


is mounted in a recess in the inner diameter of ring


55


and is held in the recess by plate


116


that is secured to a face of ring


55


, as shown in FIG.


14


. Seal


115


is provided with a pair of diverging flexible lips


117


and the pressure of the fluid in passage


54


will tend to force the lips apart, urging the inner lip into tight engagement with the hub


32


of rotating clutch housing


19


to prevent leakage at the joint between ring


55


and housing


33


.




In operation, the watercraft or boat is moved forwardly by rotating the rod


26


, causing crank


25


to move sleeve


23


and clutch


15


forwardly to cause engagement of the clutch teeth


16


with the teeth on bevel gear


7


, thus transmitting rotation of bevel gear


7


to the inner propeller shaft


9


to drive the propeller


14


.




At idle speed, as well as low speeds below the preselected high speed of about 3,000 to 6,000 rpm, pump


57


will operate to deliver fluid through strainer


66


and pressure regulator


83


to the dump valve


84


. However, at this time, solenoid


98


will be energized and valve


96


will be in the position shown in

FIG. 10

, so that hydraulic fluid will be dumped through gap


113


to the sump or reservoir


46


. As the fluid is dumped to the sump, the pressure of the fluid being delivered to the piston


47


will not be sufficient to overcome the force of the springs


49


on piston


47


, so that the piston


47


will be in a disengaged condition.




When the engine speed reaches the preselected elevated value, an electronic control unit, not shown but described in the aforementioned patent application, will deenergize solenoid


98


, so that the valve


96


will be moved by spring force to the position shown in

FIG. 9

, and pressurized fluid will be delivered to clutch


34


, as previously described, to engage the clutch and provide driving engagement between the rotating housing


19


and the outer propeller shaft


27


. Thus, both propellers


14


and


30


will rotate in opposite directions and at the same speed. On slowing down from the high speed, both propellers will continue to operate at reduced engine rpm down to a second pre-selected value, generally in the range of about 1,400 to 1,800 rpm. The electronic control unit will then energize solenoid


98


to move valve


96


to the position shown in FIG.


10


and dump fluid to reservoir


46


. This permits the springs


49


to move the clutch


34


to the disengaged position to disengage the drive of the outer propeller shaft


27


and propeller


30


.




In reverse operation of the watercraft, clutch


15


is moved to the left, as shown in

FIG. 2

, through operation of rod


26


, causing the clutch teeth


17


to engage the teeth


18


on housing


19


. As housing


19


is threaded to bevel gear


8


, clutch


15


, along with the inner propeller shaft


9


will rotate in the opposite direction to move the watercraft in reverse. At this time, the forward propeller


30


will free-wheel. If the engine speed is increased above the preselected value of about 3,000 to 6,000 rpm while clutch


15


is in the reverse position, the solenoid operated valve


96


will be moved to the position shown in

FIG. 9

, connecting the outlet line


108


to the clutch


34


, but as the pump


57


, which is connected to the inner propeller shaft


9


, is rotating in the opposite direction, the pump will not operate to pressurize the hydraulic fluid, so that the multiple disc clutch


34


will not be engaged, even at high speed when the watercraft is operating in reverse.




If clutch


15


is in the neutral position, and the engine is revved to a high speed above the pre-selected value, the control unit will cause the solenoid operated valve


96


to be moved to the position shown in

FIG. 9

, connecting the valve outlet


107


with the multi-disc clutch


34


, but in the neutral position of clutch


15


, pump


57


will not be operated. Thus, even if the engine speed is increased to above the pre-selected value when clutch


15


is in neutral, clutch


34


will not be engaged and the outer propeller shaft


20


, along with its propeller will not be operated.



Claims
  • 1. A marine propulsion unit comprising a housing, a vertical drive shaft journalled in said housing and operably connected to an engine, a lower horizontal propeller shaft journalled for rotation in said housing and selectively driven by said vertical drive shaft, a hydraulic pump located within said housing and operatively driven by said engines, wherein said hydraulic pump in said housing is operatively connected to one of said shafts and driven by rotation thereof, wherein said housing includes a lower torpedo in which said propeller shaft is rotatably journalled, and wherein said hydraulic pump is in said torpedo and driven by said propeller shaft.
  • 2. The invention according to claim 1 wherein said propeller shaft extends fore to aft in said torpedo, said propeller shaft having an aft end for mounting a propeller, said propeller shaft being driven by said drive shaft at a bevel gear, and wherein said hydraulic pump in said torpedo is forward of said bevel gear.
  • 3. The invention according to claim 2 wherein said hydraulic pump is a rotary pump coaxially aligned with and rotating about the same rotational axis as said propeller shaft.
  • 4. By The invention according to claim 3 wherein said torpedo has first and second hydraulic fluid chambers respectively fore and aft of said hydraulic pump.
  • 5. The invention according to claim 4 wherein said second hydraulic fluid chamber is between said bevel gear and said hydraulic pump, and wherein said hydraulic pump has an aft inlet receiving hydraulic fluid from said second chamber, and a forward outlet supplying pressurized hydraulic fluid to said first chamber.
  • 6. The invention according to claim 2 comprising a vertical shift rod in said housing and extending downwardly between said bevel gear and said hydraulic pump, said bevel gear being axially aft of said shift rod, said hydraulic pump being axially forward of said shift rod.
  • 7. The invention according to claim 6 wherein said torpedo has first and second hydraulic fluid chambers respectively fore and aft of said hydraulic pump, said second hydraulic fluid chamber being between said bevel gear and said hydraulic pump, and comprising a shift sleeve axially slidable along said propeller shaft, and wherein said shift rod engages said shift sleeve in said second chamber.
  • 8. The invention according to claim 1 comprising a hydraulic fluid reservoir located within said housing, and wherein said hydraulic pump has an inlet communicating with said reservoir, and an outlet supplying pressurized hydraulic fluid to actuate a movable member.
  • 9. The invention according to claim 8 comprising in combination a strainer, a pressure regulator and a valve connected in series and all located within said housing.
  • 10. The invention according to claim 9 wherein said pressure regulator is located downstream of said strainer, and said valve is located downstream of said pressure regulator.
  • 11. The invention according to claim 8 comprising a conduit in said housing carrying pressurized hydraulic fluid from said pump, and a strainer in said conduit and located within said housing downstream of said pump.
  • 12. The invention according to claim 11 wherein said strainer comprises a casing, and a screen element disposed within the casing and having an inlet and an outlet whereby fluid enters said inlet and passes through said screen element to said outlet, said strainer also including a bypass for permitting said fluid to bypass said screen element when the pressure differential across said screen element exceeds a pre-selected value.
  • 13. The invention according to claim 12 including a biasing element for urging said screen element to a first screening position when said screen element is positioned between said inlet and said outlet, said pressure differential acting to move said screen element against the force of said biasing element to a bypass position where said fluid flows directly from said inlet to said outlet.
  • 14. The invention according to claim 13 wherein said screen element is generally cylindrical and has an open end engaged with said casing when said screen element is in said screening position, said screen element also having an outer cylindrical surface that rides against an inner surface of said casing, one of said surfaces having a plurality of longitudinal grooves to permit direct flow of said fluid from said inlet and through said grooves to said outlet when said screen element is in said bypassed position.
  • 15. The invention according to claim 8 comprising a conduit in said housing carrying pressurized hydraulic fluid from said pump, and a pressure regulator in said conduit and located within said housing downstream of said pump.
  • 16. The invention according to claim 15 wherein said pressure regulator comprises a sub-housing and a plunger mounted for movement in said sub-housing and having a surface exposed to the pressure of said fluid in said conduit, said sub-housing having an outlet communicating with said reservoir, a biasing element for biasing the plunger to a first position where the plunger closes off said outlet, said plunger being constructed and arranged such that a pressure of said fluid exceeding a pre-selected value will move said plunger against the force of said biasing element to open said outlet and permit fluid to be dumped to said reservoir.
  • 17. The invention according to claim 8 comprising a conduit in said housing carrying pressurized hydraulic fluid from said pump, and a valve in said conduit and located within said housing downstream of said pump.
  • 18. The invention according to claim 17 wherein said valve comprises a valve body and a valve member movable within said valve body, and a solenoid having a solenoid plunger operably connected to said valve member for moving said valve member from a first position to a second position.
  • 19. The invention according to claim 18 and including one or more resilient members connected to said valve member for biasing said valve member to said first position.
  • 20. The invention according to claim 19 wherein said one or more resilient members comprise a pair of concentrically mounted springs disposed to interconnect said valve body and said valve member, the first of said springs having a lesser spring force than the second of said springs, and said first spring acting to hold said valve member in said first position, and said second spring constructed and arranged to act on said valve member after said valve member has moved a predetermined distance toward said second position under the influence of said solenoid.
CROSS REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. application Ser. No. 08/904,072, filed Jul. 31, 1997, now U.S. Pat. No. 6,062,926 which is a continuation-in-part of U.S. application Ser. No. 08/719,633, filed Sep. 25, 1996, now U.S. Pat. No. 5,766,047.

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Continuations (1)
Number Date Country
Parent 08/904072 Jul 1997 US
Child 09/379758 US
Continuation in Parts (1)
Number Date Country
Parent 08/719633 Sep 1996 US
Child 08/904072 US