Engine control for watercraft

Abstract
A watercraft includes an improved engine control system that enhances the responsiveness of the watercraft and eases watercraft operation. The watercraft includes a propulsion device, such as a jet propulsion unit, and an engine that powers the propulsion device. The engine control system is configured to maintain or increase engine speed under certain operating conditions.
Description




PRIORITY INFORMATION




This invention is based on and claims priority to Japanese Patent Application Nos. 2001-038202 and 2002-013828, filed Feb. 15, 2001 and Jan. 23, 2002, respectively, the entire contents of which are hereby expressly incorporated by reference.




BACKGROUND OF THE INVENTION




1. Field of the Invention




This invention relates to a control system for an engine of a watercraft.




2. Description of Related Art




Personal watercraft have become very popular in recent years. This type of watercraft is quite sporting in nature and carries one or more riders. A hull of the personal watercraft commonly defines a rider's area above an engine compartment. An internal combustion engine powers a jet propulsion unit that propels the watercraft by discharging water rearward. The engine lies within the engine compartment in front of a tunnel, which is formed on an underside of the hull. The jet propulsion unit is placed within the tunnel and includes an impeller that is driven by the engine.




A deflector or steering nozzle is mounted on a rear end of the jet propulsion unit for steering the watercraft. A steering mast with a handlebar is linked with the deflector through a linkage. The steering mast extends upwardly in front of the rider's area. The rider remotely steers the watercraft using the handlebar.




The engine typically includes at least one throttle valve disposed in an air intake passage of the engine. The throttle valve regulates the amount of air supplied to the engine. Typically, as the amount of air increases, the engine output also increases. A throttle lever or control is attached to the handlebar and is linked with the throttle valve(s) usually through a throttle linkage and cable. The rider thus can control the throttle valve remotely by operating the throttle lever on the handlebar.




SUMMARY OF THE INVENTION




In accordance with one aspect of the present invention, a jet propelled watercraft comprises an engine having at least one throttle valve. The throttle valve is movable between an idle position and a fully open position. A throttle operator, which is remotely positioned relative to the engine and is coupled to the throttle valve, is movable between first and second positions. This movement of the throttle operator causes the throttle valve to move between the idle and fully open positions, respectively. An engine control system comprises a first sensor configured to detect an operating state of the watercraft or the engine, a second sensor configured to detect a position of the throttle operator, and a throttle valve control mechanism that includes an actuator which cooperates with the throttle valve under at least one operating state of the watercraft or the engine. A controller of the engine control system communicates with the first and second sensors and with the throttle valve control mechanism. The controller is configured to activate the throttle valve control mechanism once the operating state of the watercraft or engine is greater than a predetermined state. The controller is also configured to leave active the throttle valve control mechanism at least when the throttle operator quickly moves to the first position so as to maintain the throttle valve between the idle and fully open positions.




In accordance with another one aspect of the present invention, a jet propelled watercraft comprises an engine having at least one throttle valve. The throttle valve is movable between a closed position and a fully open position, A throttle operator is remotely positioned relative to the engine and is coupled to the throttle valve. The throttle operator can be moved between first and second positions which cause the throttle valve to move between the closed and fully open positions, respectively. An engine control system cooperates with the engine to control engine speed under at least one operating condition of either the watercraft or the engine. The control system comprises a first sensor configured to detect an operating state of either the watercraft or the engine, a second sensor configured to detect a position of the throttle operator, a throttle valve control mechanism that includes an actuator selectively cooperating with the throttle valve under at least one operating state of the watercraft or the engine, and a controller communicating with the first and second sensors and with the throttle valve control mechanism. The controller is configured to activate the throttle valve control mechanism once the operating state of either the watercraft or engine is greater than a preset state, and the controller and throttle valve control mechanism are further configured to delay closure of the throttle valve at least when the throttle operator quickly moves to the first position.




In accordance with yet another aspect of the present invention, a method of controlling a watercraft having an engine is provided. The method involves sensing a first control parameter that is indicative of the operating state of either the watercraft or the engine, sensing a position of an operator used to control engine speed to determine at least when the operator is abruptly moved to an idle position, and activating a throttle valve control mechanism when the operating state of the watercraft or engine is greater than a preset operating state. Engine speed is maintained above an idle speed when the watercraft or engine is operating above the preset operating state and the operator is abruptly moved to the idle position.




Further aspects, features and advantages of this invention will become apparent from the detailed description of the preferred embodiments which follow.











BRIEF DESCRIPTION OF THE DRAWINGS




These and other features, aspects and advantages of the present invention will now be described with reference to the drawings of preferred embodiments, which are intended to illustrate and not to limit the invention. The drawings comprise 11 figures.





FIG. 1

is a side elevational view of a personal watercraft and schematically illustrates an engine control system configured in accordance with an embodiment of the present invention.





FIG. 2

is a system diagram of the engine control system.





FIG. 3

is a control routine for the engine control system.




FIG.


4


(A) illustrates the air intake pathway with a throttle valve control mechanism of the engine control system.




FIG.


4


(B) shows a sectional view of the same mechanism taken generally along a central axis of the intake pathway.




FIG.


5


(A) illustrates a plan view of the throttle valve control mechanism of FIG.


4


(A) in an active state and engaged with a throttle lever of the mechanism, thereby maintaining a throttle opening angle above idle.




FIG.


5


(B) illustrates a plan view with the mechanism deactivated and disengaged.





FIG. 6

is a graph showing the relationship between engine rpm and time under two control conditions: (1) with the throttle valve control mechanism active and engaged for a period of time and (2) with the throttle valve control mechanism deactivated and disengaged.




FIG.


7


(A) is a schematic front view of the engine and illustrates another embodiment of the throttle valve control mechanism that employs a servomotor. A large part of the engine except for an air induction system and a throttle valve control mechanism is illustrated in phantom.




FIG.


7


(B) is a schematic view of the pulley assembly used with this embodiment of the throttle valve control mechanism.




FIG.


8


(A) is a side view of another throttle valve control mechanism configured in accordance with another preferred embodiment of the present invention that can be used in the engine control system of FIG.


2


.




FIG.


8


(B) is a sectional view of the throttle valve control mechanism taken along the line A—A of FIG.


8


(A).




FIG.


8


(C) is a front view of the throttle valve control mechanism.




FIG.


9


(A) is a side view of an additional throttle valve control mechanism configured in accordance with an additional preferred embodiment of the present invention that can be used with the engine control system of FIG.


2


.




FIG.


9


(B) is a sectional view of the throttle valve control mechanism taken along the line A—A of FIG.


9


(A).




FIG.


9


(C) is a front view of a control structure including a solenoid actuator looked in the direction of the arrow H.





FIG. 10

is a schematic view showing another embodiment of the engine control system.





FIG. 11

is a control routine of an ECU of the control system shown in FIG.


10


.











DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS




With primary reference to FIG.


1


and additionally to

FIGS. 7-10

, an overall configuration of a personal watercraft


30


will be described.




The watercraft


30


employs an internal combustion engine


32


and an engine control system


34


configured in accordance with a preferred embodiment of the present invention. This engine control system


34


has particular utility with a personal watercraft and, thus, is described in the context of the personal watercraft. The control system, however, can be applied to other types of watercraft as well, such as, for example, small jet boats and the like.




The personal watercraft


30


includes a hull


36


generally formed with a lower hull section


38


and an upper hull section or deck


40


. The lower hull section may include one or more inner liner sections to strengthen the hull or to provide mounting platforms for various internal components of the watercraft. Both the hull sections


38


,


40


are made of, for example, a molded fiberglass reinforced resin or a sheet molding compound. The lower hull section


38


and the upper hull section


40


are coupled together to define an internal cavity. A gunnel or bulwark


42


defines an intersection of both the hull sections


38


,


40


.




As seen in FIG.


1


and best seen in

FIG. 10

, a steering mast


46


extends generally upwardly almost atop the upper hull section


40


to support a handlebar


48


. The handlebar


48


is provided primarily for a rider to control the steering mast


46


so that a thrust direction of the watercraft


30


is properly changed. The handlebar


48


also carries other control devices such as, for example, a throttle lever


52


for manually operating throttle valves


54


(

FIGS. 4-5

, and


7


-


9


) of the engine


32


. The throttle lever


52


is one type of a throttle operator that can be used with the present engine control system


32


and is remotely positioned relative to the engine


32


. A rider can move the throttle lever


52


between a first, fully-released position, which corresponds to an idle position of the throttle valves, and a second, fully-depressed position, which corresponds to a fully open position of the throttle valves. In the fully open position, the throttle valves need not be wide open for some engine designs. In the illustrated arrangement, the steering must


46


is covered with a padded steering cover member


56


.




A seat


60


extends longitudinally fore to aft along a centerline of the hull


36


at a location behind the steering mast


46


. This area, in which the seat


60


is positioned, is a rider's area. The seat


60


has generally a saddle shape so that the rider can straddle it. Foot areas are defined on both sides of the seat


60


and at the top surface of the upper hull section


40


. A cushion, which has a rigid backing and is supported by a pedestal section of the upper hull section


40


, forms part of the seat


60


. The pedestal forms the other portion of the seat. The seat cushion is detachably attached to the pedestal of the upper hull section


40


. An access opening is defined on the top surface of the pedestal, under the seat cushion, through which the rider can access an engine compartment defined in an internal cavity formed between the lower and upper hull sections


38


,


40


. The engine


32


is placed in the engine compartment. The engine compartment may be an area within the internal cavity or may be divided from one or more other areas of the internal cavity by one or more bulkheads.




A fuel tank is placed in the internal cavity under the upper hull section


40


and preferably in front of the engine compartment. The fuel tank is coupled with a fuel inlet port positioned at a top surface of the upper hull section


40


through a filler duct. A closure cap closes the fuel inlet port.




At least a pair of air ducts or ventilation ducts is provided on both sides of the upper hull section


40


so that the ambient air can enter the internal cavity through the ducts. Except for the air ducts, the engine compartment is substantially sealed so as to protect the engine


32


and a fuel supply system (including the fuel tank) from water.




A jet propulsion system


64


propels the watercraft


30


. The jet propulsion system


64


includes a tunnel


66


formed on the underside of the lower hull section


38


. In some hull designs, the tunnel is isolated from the engine compartment by a bulkhead. The tunnel


66


has a downward facing inlet port


68


opening toward the body of water. A jet pump unit


70


is disposed within a portion of the tunnel


66


and communicates with the inlet port


68


. An impeller


72


is rotatably supported within the housing of the unit


70


. An impeller shaft extends forwardly from the impeller


72


and is coupled with a crankshaft of the engine


32


so as to be driven by the crankshaft. The rear end of the unit


70


includes a discharge nozzle


74


. A deflector or steering nozzle


76


is affixed to the discharge nozzle


74


for pivotal movement about a steering axis


78


that extends generally vertically. A cable connects the deflector


76


with the steering mast


46


so that the rider can rotate the deflector


76


about the steering axis


78


. A steering mechanism


80


for the watercraft thus preferably comprises the steering mast


46


, the handlebar


48


, the cable and the deflector


76


.




When the crankshaft of the engine


32


drives the impeller shaft and hence the impeller


72


rotates, water is drawn from the surrounding body of water through the inlet port


68


. The pressure generated in the jet pump unit


70


by the impeller


72


produces a jet of water that is discharged through the discharge nozzle


74


and the deflector


76


. The water jet produces thrust to propel the watercraft


30


. Maneuvering of the deflector


76


changes the direction of the water jet, thus providing forces having both lateral and longitudinal vectors to affect the heading of the watercraft


30


. The rider thus can turn the watercraft


30


in either a right or a left direction by operating the steering mechanism


80


.




As schematically shown in

FIG. 1

, the engine control system


34


preferably includes an ECU (electronic control unit) or control device


86


, a steering position sensor


88


, a throttle lever position sensor


89


, a throttle position sensor


90


, an engine rpm sensor


91


, and a watercraft velocity sensor


92


. The ECU


86


is preferably mounted on the engine


32


or disposed in proximity to the engine


32


. The steering position sensor


88


is preferably positioned adjacent to the steering mast


46


so as to sense an angle of the steering mast


46


when the rider operates it. The throttle lever position sensor


89


is positioned at the throttle lever


52


or is located along the cable and/or linkage that connects the throttle lever


52


to the throttle valve


54


. For example, the throttle lever position sensor


89


could be attached to the throttle pulley


120


(see FIG.


4


A), which is directly connected to the throttle lever


52


by a cable


118


in the illustrated embodiment. The throttle position sensor


90


is preferably affixed at one end of throttle valve shafts


94


(

FIGS. 4A and 4B

) so as to sense a position of the throttle valves


54


. The engine rpm sensor may be located at an end of the crankshaft or along the impeller shaft. The watercraft velocity sensor


92


is preferably located at a rear bottom portion of the watercraft


30


, which is submerged during normal running conditions of the watercraft


30


. The respective sensors


88


,


89


,


90


,


91


,


92


are connected to the ECU


86


through signal lines


96


,


97


,


98


,


99


,


100


, respectively. Of course, the signals can be sent through hard-wired connections, emitter and detector pairs, infrared radiation, radio waves or the like. The type of signal and the type of connection can be varied between sensors or the same type can be used with all sensors.




The illustrated control system


34


preferably is configured as schematically shown in FIG.


2


and operates in accordance with a control routine shown in

FIG. 3

, although other control routines are applicable inasmuch as they comply with the control strategy of the present invention. The exemplary control routine as well as the control system


34


will be described in greater detail shortly.




The engine


32


preferably operates on a two-cycle crankcase compression principle and has three cylinders spaced apart from one another along the longitudinal centerline. The illustrated engine, however, merely exemplifies one type of engine on which various aspects and features of the present invention can be used. The invention can be used with engines having other number of cylinders, having other cylinder arrangements, other cylinder orientations (e.g., upright cylinder banks) and operating on other combustion principles (e.g., four cycle or rotary).




The engine


32


generally has a typical and conventional construction. The engine


32


includes a cylinder block defining three cylinder bores in which pistons reciprocate. At least one cylinder head member is affixed to the upper end of the cylinder block to close respective upper ends of the cylinder bores and defines combustion chambers with the cylinder bores and the pistons. Separate cylinder heads for each cylinder bore also can be used. A crankcase member is also affixed to the lower end of the cylinder block to close the respective lower ends of the cylinder bores and to define crankcase chambers with the cylinder block. The crankshaft is rotatably connected to the pistons through connecting rods and is journaled for rotation within the crankcase. The cylinder block, the cylinder head and the crankcase member preferably are made of aluminum alloy and together define an engine body


102


.




Engine mounts


104


(

FIG. 7A

) extend from both sides of the engine body


102


. The engine mounts


104


preferably include resilient portions made of, for example, rubber material. The engine body


102


is mounted on the lower hull section


38


(or possibly on the hull liner) by the engine mounts


104


so that vibration of the engine body


102


is inhibited from conducting to the hull section


38


.




The engine


32


preferably includes an air induction system


108


to introduce air to the combustion chambers. As seen in

FIG. 8

, in the illustrated embodiment, the air induction system is disposed on the starboard side of the engine body


102


. The induction system


108


includes one or more throttle bodies


110


affixed to the crankcase member, and a plenum chamber member or air intake box


112


. The plenum chamber member


112


defines a plenum chamber


114


into which the air in the engine compartment enters. Preferably, the plenum chamber


114


smoothes the intake air flow and attenuates intake noise. The throttle bodies


110


each communicate with a respective individual chamber within the crankcase that communicates with one of the combustion chambers through scavenge passages defined within the engine body


102


. The throttle bodies


110


define intake passages


116


through which the air flows to the individual crankcase chambers.




The respective throttle valves


54


are disposed within the intake passages


116


so as to regulate the amount of air passing through the intake passages


116


. Because the throttle valve shafts


94


are journaled on the throttle bodies


110


for rotatable movement about axes of the respective valve shafts


94


, the respective throttle valves


54


can rotate to change opening degrees thereof. The foregoing throttle lever


52


preferably is connected to the throttle valve shafts


94


through a throttle wire or cable


118


. In the illustrated embodiment, the individual throttle valve shafts


94


are linked together so that the throttle wire


118


can be connected with only one of the shafts


94


or at a point along the resulting throttle shaft linkage. As seen in

FIG. 4B

, the throttle valve shaft


94


has a pulley


120


and the throttle wire


118


is affixed to the pulley


120


so as to coil around it. By operating the throttle lever


52


, the opening degrees of the respective throttle valves


54


change so as to regulate air flow to the combustion chambers. In the illustrated embodiment, the throttle pulley


120


and the cable


118


provide a throttle drive mechanism that link the throttle lever


52


to the throttle valve assembly.




As described above, one of the throttle valve shafts


94


in the illustrated embodiment shown in

FIG. 4B

has the throttle position sensor


90


at one end thereof. The throttle position sensor


90


thus can sense an angular position of each throttle valve


54


, i.e., an opening degree of each throttle valve


54


.




The throttle valves


54


can be closed so as to bring the engine


32


to an idle state. Even at this idle state, the engine


32


still needs a small amount of air to maintain the idle state. The throttle valves


54


thus usually lie slightly skewed or have a bypass opening to permit a small amount of air to pass through the intake passage


116


when in an idle, “closed” position. Alternatively, an idle air supply mechanism can be provided such as a sub-passage bypassing the throttle valves


54


. A control valve for controlling the idle air amount can be provided at the sub-passage.




The engine


32


also includes a fuel supply system. The fuel supply system includes the fuel tank, a charge forming device and a fuel delivery mechanism that connects the fuel tank with the charge forming device. The charge forming device can take various structures such as a carburetor, a fuel injection mechanism or the like. If the fuel injection mechanism is employed, fuel can be sprayed either directly or indirectly to the combustion chambers. In the illustrated embodiment, an indirect fuel injection mechanism is employed.




The fuel injection mechanism includes one or more fuel injectors directed toward the respective intake passages and one or more fuel pumps to pressurize the fuel delivered to the fuel injectors. Each fuel injector has an injection nozzle that is exposed to the intake passage. The injection nozzle preferably is opened and closed by an electromagnetic unit that is slideable within an injection body. The electromagnetic unit has a solenoid coil controlled by electrical signals. When the nozzle is opened, pressurized fuel is sprayed into the intake passage. The sprayed fuel is drawn to the combustion chambers with the air passing through the intake passages.




The ECU


86


preferably controls an amount of fuel sprayed into each intake passage


116


. Alternatively, another ECU can control the fuel injector because a pressure regulator strictly regulates the fuel pressure, the ECU


86


can vary the fuel amount by varying the duration of each injection. The ECU also can advance injection timing and initiation timing in order to increase the engine output.




The engine


32


further includes an ignition or firing system. Spark plugs of the ignition system are affixed to the cylinder head. A spark gap of each spark plug is exposed within an associated combustion chamber. Each spark plug ignites an air/fuel charge at an ignition timing controlled by the ECU or by another ECU. The ignition system preferably has an ignition mechanism including an ignition coil and an igniter. The ignition coil preferably is a combination of a primary coil element and a secondary coil element that are wound around a common core. The secondary coil element is connected to the spark plugs while the primary coil element is connected to the igniter. The primary coil element also is coupled with a power source (e.g. a battery). The igniter abruptly cuts off the current flow in response to an ignition timing control signal from the ECU. A high voltage current flow consequently occurs in the secondary coil element. The high voltage current flow forms a spark at each spark plug. The ECU


86


controls an ignition timing of the spark plugs in this manner.




The engine


32


further includes an exhaust system to discharge burnt charges, i.e., exhaust gases, from the combustion chambers. Exhaust ports are defined in the cylinder block and communicate with the associated combustion chambers. An exhaust manifold is connected to the cylinder block and communicates with the exhaust ports. Multiple exhaust conduits


122


(

FIG. 1

) are further coupled with the exhaust manifold in series so as to extend around the engine body


102


and then toward the tunnel


66


. A discharge exhaust conduit


122


is connected to the tunnel


66


so that the exhaust gases are discharged into the tunnel


66


in a known manner.




With reference to

FIGS. 1-10

, and especially to

FIGS. 2-6

, the control system


34


and an exemplary control routine will now be described. It is to be noted that the control system


34


may be in the form of a hard wired feedback control circuit or may be constructed of a dedicated processor and a memory for storing a computer program and data. Additionally, the control system


34


may be constructed of a general purpose computer having a general purpose processor and the memory for storing the computer program for performing the control routine. Preferably, however, the control system


34


utilizes the engine ECU


86


, which may be constructed in any of the above-mentioned forms.





FIG. 2

illustrates a block diagram of the control system


34


in which the ECU


86


controls a throttle valve control mechanism


130


. In the illustrated embodiment, the ECU receives signals from the throttle lever position


89


sensor and the engine rpm sensor


91


. It also preferably receives signals from the other sensor, but need not to for the purposes of the control routine illustrated in FIG.


3


. Generally, a throttle opening angle (i.e., throttle position) will correspond with a given engine rpm, although variances are expected due to, among other factors, engine load and air/fuel mixture. The ECU


86


controls the throttle valve control mechanism


130


which may be activated to control the opening angle of the throttle valves


54


and, hence, to control the engine output (for at least some period of time or until certain control parameters occur). The throttle valves


54


are also controlled by the user-controlled throttle lever


52


mounted on the handlebar of the watercraft


30


which is the usual circumstance; however, under some circumstances (described below) the throttle valve control mechanism temporarily overrides the user-controlled mechanism. Thus, the throttle valve


54


opening angle is controlled by the throttle lever


52


, yet is still under the overriding control of the ECU via the throttle valve control mechanism


130


. In this way, the ECU


86


may override the throttle opening angle provided by the throttle lever


52


, based upon signals received either from the rpm sensor


91


and the throttle lever position sensor


89


. The throttle valve control mechanism


130


is preferably a mechanical control disposed adjacent the throttle valve shaft


94


and will be discussed in greater detail with specific reference to

FIGS. 4 and 5

.





FIG. 3

illustrates an exemplary control routine for the ECU


86


. The routine begins at S


1


when the engine is started. At S


2


, the ECU receives a signal from the rpm sensor


91


and determines if the engine speed is greater than a reference rpm, which may be, for example, within the range of from about 2,000 rpm to about 5,000 rpm, and more preferably within the range of from about 3,500 to about 4,500, and in one embodiment, is 4,000 rpm. This comparison is repeatedly carried out until the engine rpm sensor


91


reports a value above the reference rpm. The ECU


86


then proceeds, at S


3


, and determines if the engine rpm is maintained at an rpm above the reference rpm for a given time, for example, but without limitation, 3-5 seconds. If the engine rpm has not been maintained for a period of time longer than the reference time, the ECU


86


continues to receive signals from the rpm sensor


91


until the reported value is greater than the reference rpm. If the engine rpm maintains a speed above the reference rpm for greater than the predetermined amount of time, at S


4


, the ECU sends instructions to actuate the throttle valve control mechanism


130


. At S


5


, the ECU


86


then monitors the position of the throttle lever


52


via the throttle lever sensor


89


to determine when the throttle lever


52


returns to an idle position. Once the throttle lever


52


is returned to an idle position, the ECU


86


receives the corresponding signal from the throttle lever sensor


89


and, at S


5


, waits for a predetermined amount of time to elapse, such as, for example, but without limitation, 3 seconds. During this time, the throttle valve control mechanism


130


holds open the throttle valves to maintain the engine at a speed above idle, such as, for example, but without limitation, at 3000 rpm. Once the predetermined amount of time elapses, the ECU


86


releases (i.e. deactivates) the throttle valve control mechanism


130


at S


7


and the throttle valve


54


is allowed to return to a closed, idle position.




It should be understood that the above routine can be part of a larger control routine and can include additional control step, including those discussed below in connection with the control routine diagramed in FIG.


11


. In addition, the control parameter used to determine when to activate the throttle valve control mechanism


130


can be any parameter that is indicative of the operating state of the watercraft


30


or the engine


32


. For example, control parameters, such as, for example, watercraft speed or throttle position can be used in addition or in the alternative to engine speed. In addition, the control parameter used to determine when to turn off the throttle control mechanism


130


can involve parameters other than time, such as, for example, steering angle, watercraft speed, and engine speed. For instance, the ECU can determine if the steering angle is less than a preset angle (e.g., 30 degrees), and if so, can cause the throttle valve control mechanism


130


to release the throttle valve


54


. This can be done in addition or in the alternative to a timing control.




The act of maintaining engine speed above idle also can involve either holding a generally constant speed (see, e.g., graph


171


in

FIG. 6

) or gradually decreasing the engine speed at a rate slower than normal if the throttle valve were allowed to closed under spring bias (as usually is the case). A gradual decrease can take the throttle valve back to its idle position at the end of the controlled closing process (under the control of the throttle valve control mechanism) or can slow the rate of closure until the end of the controlled closing process, at which time the throttle valve will close (i.e., return to its idle position) under the spring bias.





FIGS. 4A and 4B

illustrate an embodiment of a throttle valve control mechanism


130


. A throttle valve stop housing


131


houses an actuator, which may be a solenoid, a step motor, or other similar device to displace a slidable plunger


133


protruding from the throttle stop housing


131


. In one variation, the plunger


133


can be replaced by a linkage assembly. The throttle shaft


94


fixedly carries a throttle shaft lever


139


that is permanently oriented relative to the throttle valves


54


. At least one throttle body


110


includes a protruding boss


141


having a first torsion spring


145


mounted circumferentially thereon. As seen in

FIG. 4B

, a static end


143


the spring


145


is held in place, such as by a flange


147


protruding from the throttle body


110


. The biasing end


149


of the spring


145


fits within a hole or notch


151


formed in pulley


120


, such that the spring


145


biases the pulley to rotate in a direction corresponding with a closed throttle position. The pulley


120


is rotatably attached to the throttle valve shaft


94


, and is retained thereon by a clip


155


; however, under normal conditions, the pulley


120


is biased to rotate with the throttle valve shaft


94


by a second torsion spring


157


. The pulley


120


has one end of the second torsion spring


157


connected to it. The second torsion spring


157


wraps around the throttle valve shaft


94


and has a second biasing end


159


projecting adjacent to the throttle shaft lever


139


, such that the biasing end


159


of the second spring


157


biases the throttle shaft lever


139


and the pulley


120


to rotate together. The result is a lost motion coupling that allows concurrent rotation of the throttle shaft lever


139


, throttle shaft


94


, and pulley


120


, but also permits the pulley


120


to return to the idle position while the throttle lever


139


and throttle shaft are held open by the throttle valve control mechanism


130


. When the throttle valve control mechanism


130


is activated, the plunger


133


inhibits the throttle shaft lever


139


for rotating with the pulley


120


back towards an idle position under the bias of the first torsion spring


145


. Consequently, the throttle valve control mechanism


130


prevents the throttle valve lever


139


from rotating to its maximum range of movement corresponding with a throttle valve closed position. The throttle valve


54


is maintained in a partially opened position and the engine is maintained at an output level above idle.




In the illustrated embodiment, as best seen in

FIGS. 5A and 5B

, a drive arrangement is provided as part of the lost motion coupling to cause the throttle pulley


120


to rotate the throttle shaft


94


in a direction


163


opening the throttle valve


54


. The pulley


120


contains an inward protrusion


156


that projects toward the rotational axis of the pulley


120


and that nests within a pocket


158


formed into the side of the pulley


120


. A pin


154


is mounted in the throttle valve shaft


94


and perpendicular thereto such that it protrudes into the pocket


158


. In one embodiment, the pulley


120


is not constrained to rotate with the throttle valve shaft


94


, but is free to rotate independently thereof. However, when the throttle lever


52


is depressed and the throttle wire


118


imparts rotational motion to the pulley


120


, the inward protrusion


156


has a contacting surface


160


that contacts the pin


154


and causes the throttle shaft


94


to rotate. In this way, the throttle opening angle is controlled directly by the throttle lever


52


.




The first and second torsion springs


145


,


157


can, in addition or in the alternative to the drive arrangement, have different spring constants, such that the spring constant of the first torsion spring


145


is greater than the spring constant of the second spring


157


. This type of lost motion mechanism allows the pulley


120


to rotate about the throttle valve shaft


94


independently of the shaft lever


139


. Therefore, when the throttle lever


52


mounted on the handlebar is released and returns to a position corresponding with an engine idle position, the pulley is able to rotate to accept the slack of the throttle cable


118


, while the throttle valve


54


is forced to maintain a partially opened position (i.e. held partially open). Accordingly, once the ECU


86


activates the throttle valve control mechanism


130


and the plunger


133


is extended, even if an operator releases the throttle lever


52


, the throttle valve


54


remains in a partially opened position to provide a thrust above idle to provide for sharp steering of the watercraft. As described in relation to

FIG. 3

, the ECU


86


deactivates the throttle valve control mechanism


130


after a prescribed amount of time and the engine is allowed to return to an idle state. In another variation, the ECU could turn off the throttle valve control mechanism


130


after the watercraft slows to a particular speed or the engine speed (rpm) slows to a particular lever.




The torsion springs


149


,


157


(

FIG. 4B

) bias the pulley in a clockwise direction


161


, which corresponds to a direction that tends to close the throttle valves


54


and place the engine in an idle state. (It should be understood that other types of biasing devices can be used in place of the torsion springs


149


,


157


used in the illustrated embodiment.) The clockwise biasing


161


also tensions the throttle wire


118


thus providing some resilience to the throttle lever


52


on the handlebar


48


. The throttle wire


118


is connected at one end to the throttle lever


52


and the other end to the pulley


120


. The throttle wire


118


is preferably at least partially wound around the pulley


120


so as to translate a linear displacement of the wire


118


into an angular displacement of the pulley


120


.




As shown in

FIG. 5B

with continued reference to

FIGS. 4A and 4B

, when the throttle lever


52


is depressed, the throttle wire


118


is tensioned, which causes the pulley


120


to rotate about its center, thereby rotating the throttle valve shaft


94


and the throttle valve


54


located thereon. As the throttle lever


52


is released, such as in

FIG. 5A

, the biasing of the torsion springs


149


,


157


cause the pulley


120


, throttle shaft lever


139


, throttle shaft


94


, and throttle valve


54


to rotate in unison to return the throttle valve


54


to a position corresponding with an engine idle state. However, the throttle control mechanism


130


is under the control of the ECU


86


, and when activated, interferes with the rotational movement of the throttle valve


54


by inhibiting further clockwise movement of the throttle shaft lever


139


. The throttle valve control mechanism


130


includes the plunger


133


that, when extended, prevents the throttle valve


54


from fully closing and thus returning the engine


32


to an idle state. In this way, the engine is maintained at an rpm level elevated above an idle rpm level to provide higher thrust to allow a watercraft operator to turn the watercraft more sharply. The length of the plunger


133


directly controls the throttle valve


54


position, and hence, the engine rpm. By simply varying the length of the extended plunger


133


, the maintained engine rpm may also be varied. Similarly, the relative position of the shaft lever


139


vis-a-vis the throttle shaft


94


position at idle can be changed to increase or decrease the rpm level of the engine


32


when the plunger


133


is deployed. It is anticipated that the engaged throttle valve control mechanism


130


will, at least, provide an engine rpm above an idle rpm.




As is shown in relation to

FIG. 5B

, the throttle valve lever


139


is still rotatable in an rpm increasing direction


163


regardless of the engaged or disengaged status of the throttle valve control mechanism


130


.




When the throttle lever


52


is released, the pulley


120


is biased to rotate in a direction


161


corresponding with a throttle closed position, thus drawing in the slack in the throttle wire


118


. The throttle valve shaft


94


is able to rotate independently of the pulley


120


, but is also biased in a direction corresponding with a throttle closed position by a spring


157


. If the throttle valve control mechanism


130


has been actuated and the plunger


133


has been positioned into the path of the throttle shaft lever


139


, the plunger interferes with further rotational movement of the throttle shaft lever


139


. However, the pulley


120


is free to continue to rotate as shown in FIG.


5


A. Specifically, the inward protrusion


156


no longer contacts the pin


154


and the pulley is free to continue its rotation to draw in any slack in the throttle wire


118


.




The effect of the throttle valve control mechanism


130


being activated on the engine rpm is graphically depicted in relation to FIG.


6


. At an initial time T


0


, the engine rpm is above a reference rpm, such as for example, 4000 rpm. While this diagram depicts the engine rpm as a steady value, this is not a requirement for the throttle valve control mechanism


130


to become activated. As described relative to

FIG. 3

, the throttle valve control mechanism


130


is activated when the engine rpm maintains a speed above a reference speed for a given amount of time. A first reference line


169


shows the normal engine behavior when the throttle lever


52


abruptly returns to a position corresponding with an engine idle state at T


1


. Generally, time is required for the motion of the throttle lever


52


to translate through the throttle system and eventually close the throttle valves


54


. Furthermore, the engine does not abruptly return to an idle state, as the engine inertia must be dissipated over time. Accordingly, the first reference line


169


shows a gradual decrease in engine rpm between the time the throttle lever


54


is released at T


1


until the engine returns to an idle state which may take on the order of several seconds.




A second reference line


171


denotes how the engine rpm is affected by the activation of the throttle valve control mechanism


130


. When the throttle lever


52


is abruptly released at T


1


, the engine rpm begins to decrease, generally following the first reference line


169


, until the throttle valve lever


139


contacts the plunger


133


of the throttle valve control mechanism


130


and is prevented from fully closing the throttle valve


54


. Consequently, the second reference curve


171


begins to level out at a higher rpm corresponding with an rpm when the throttle valve


54


is maintained in a partially opened position. This increased rpm maintains an elevated thrust to allow the watercraft to be sharply turned after the operator has completely released the throttle lever


52


. After a predetermined amount of time, such as, for example, 3 seconds, the throttle valve control mechanism


130


is disengaged at T


2


and the throttle valve


54


is allowed to fully close to an idle position.




Thus, in one aspect, there is provided a throttle control mechanism


130


that maintains an engine rpm above an idle rpm for a predetermined amount of time (or until a certain control parameter occurs) following an abrupt release of the throttle lever


52


.




The throttle valve control mechanism


130


can comprise a step motor or an electric motor employed in a feedback system. A servomotor also can be used in place of the step motor. Although a servomotor is usually larger than the step motor, the servomotor may be desirable in some applications because it eliminates the need for the throttle valve position sensor


90


. Further, a solenoid may be used to provide the necessary linear displacement of the plunger


133


.




In the servomotor variation, as illustrated in

FIGS. 7A and 7B

, the servomotor


132




a


preferably is disposed apart from the engine body


102


. The servomotor


132




a


has a pulley


136


on a shaft


138


that rotates about an axis (e.g., a vertical axis), while the throttle valve


54


has a corresponding pulley


140


on its shaft


94


next to the pulley


120


that is coupled to the throttle wire


118


. A control wire


142


connects the pulleys


136


,


140


with each other. The servomotor


132




a


moves the throttle shaft


94


in a controlled manner through this pulley system. The pulleys


140


,


120


, which are connected to the servomotor


132




a


and the throttle wire


118


, respectively, can of course be positioned on different throttle shafts


94


.




The throttle valve control mechanism


130


is connected to the ECU


86


by a control line. Normally, the operator operates the throttle valves


54


by the throttle lever


52


. The ECU


86


, however, overrides the control of the throttle lever


52


and causes the throttle valve control mechanism


130


to maintain (or to increase under other control strategies) the opening degree of the throttle valves


54


under certain operating conditions.




In the illustrated embodiment shown in

FIGS. 1-5

, five sensors or sensing mechanisms, i.e., the throttle valve position sensor


90


, the steering position sensor


88


, the throttle lever position sensor


89


, the engine rpm sensor


91


, and a watercraft velocity sensor


92


, are employed for sensing the respective states or velocity of the watercraft and its engine. However, as described herein, only two sensors may be used to provide the appropriate engine control contemplated herein. In the illustrated embodiment, the throttle lever position sensor


89


and engine rpm sensor


91


may be all that is required to provide the ECU


86


enough feedback to appropriately control the engine output. But as noted above, other control parameters can be used in addition or in the alternative to engine speed and, thus, these other sensors can be used in place of the engine speed sensor in some applications of the present engine control system.




The throttle valve position sensor


89


preferably is a proximity sensor (e.g., a reed switch) to detect when the throttle lever is in a position corresponding to idle. Other sensors or sensing mechanisms such as a potentiometer can also be used.




The steering position sensor


88


preferably is a proximity sensor positioned adjacent to the steering mast


46


and senses an angular position of the steering mast


46


. Other types of sensors or sensing mechanisms also can be used.




The velocity sensor


92


of the watercraft


30


preferably is a paddle-wheel type sensor positioned at a bottom portion or a submerged stern portion of the watercraft


30


. Any other sensors acting as velocity sensors such as a dynamic pressure sensor disposed with the tunnel


66


or a Pitot tube type sensor disposed toward the body of water can replace the paddle-wheel type sensor


92


. It would also be possible to use a GPS (global positioning system) that uses an artificial satellite and includes a GPS antenna comprises a velocity sensing mechanism. The sensing mechanism using the GPS is described in, for example, Japanese Laid Open Publication No. Hei 11-43093.




The ECU


86


has stored in its memory a reference watercraft engine rpm. In the illustrated embodiment, the reference rpm is selected from speeds greater than those that cause the watercraft


30


to start planing. In general, the jet type watercraft


30


transfers from a displacement (trolling) range to a transient range at a velocity of 10-15 Km/h (at an engine speed of 2,000-2,500 rpm) and then transfers to the planing range at a velocity of 30-35 Km/h (at an engine speed of 4,500 rpm). The watercraft


30


can stay in a complete planing range when the velocity is 35 Km/h or more (at the engine speed is 4,500 rpm or more). In the illustrated embodiment, the maximum speed of the engine


32


is about 7,000 rpm. Embodiments of the present invention, however, can be used with engines having greater or lesser top-end speeds. The velocity of the watercraft when it starts planing also depends upon the size and shape of its hull, the weight of the watercraft, the location of the watercraft's center of gravity, and the performance of the jet propulsion unit, to name a few additional factors. The reference engine speed can be determined empirically for a particular watercraft design and then stored in the ECU


86


of each watercraft made in accordance with such design. The predetermined reference engine speed of 4,000 rpm in this embodiment thus is merely an example.




As understood from the following embodiments, the ECU can also use other control parameters and, thus, store other reference parameters in its memory. For example, in accordance with one preferred embodiment, a reference throttle opening degree (Thθs) preferably is selected to correspond to a watercraft engine rpm that generates a thrust force sufficient to change sharply the direction of travel of the watercraft


30


. The reference throttle opening degree (Thθs) increases with watercraft velocity. In the illustrated embodiment, where the throttle opening degree ranges from 0 to 90 degrees, the reference throttle opening degree (Thθs) preferably is not less than 30 degrees and increases with increasing watercraft speed. At throttle angles less than 30 degrees, the engine output may not be sufficient to produce enough thrust to turn the watercraft


30


sharply.




A reference steering position (Sds) also is preferably selected to correspond to a watercraft velocity. Unless the reference steering position (Sds) is large enough relative to the watercraft velocity, the watercraft


30


may not be as responsive as the rider would like at low speeds. The reference steering position (Sds) is variable and generally increases with increasing watercraft velocity. In the illustrated embodiment, the steering mast


46


rotates from a neutral position (for straight-ahead travel) by forty degrees (40°) to a fully turned position to each side. In other words, the steering mast


46


rotates from its neutral position (0°) by plus forty degrees (40°) when moved from the neutral position to a fully turned position to the right and by minus forty degrees (−40°) when moved from the neutral position to a fully turned position to the left. For such an embodiment, the reference steering position (Sds) preferably is not less than twenty degrees (20°) and varies relative to watercraft speed.




The ECU


86


may have stored in its memory at least one map that relates the reference throttle opening degrees (Thθs) to watercraft velocities (V) and at least another map that relates the reference steering positions (Sds) to the watercraft velocities (V). These maps are used for selecting the reference throttle opening degree (Thθs) and the steering positions (Sds) in response to a continually sensed watercraft velocity (V).




More thrust generally is required to turn the watercraft


30


sharply at higher speeds. The present control system


32


thus is adapted to maintain or increase the throttle angle to a desired throttle opening degree in order to enhance the responsiveness of the watercraft


30


and to ease watercraft operations during such turns. For this purpose, the ECU


86


has stored in its memory a map of objective throttle opening degrees (Thθm), i.e., desired throttle opening degrees, versus watercraft speed. In general, the throttle opening degree (Thθm) increases with increases in watercraft speed.




With reference to FIGS.


8


(A)-(C), another embodiment of the throttle valve control mechanism


130


B will be described below. The same reference numerals will be assigned to the same components and members that have been already described and further detailed description of such components and members will be omitted.




The engine in this embodiment also operates on a two cycle crankcase compression principle and has three cylinders. Three throttle bodies


110




a


,


110




b


,


110




c


are separately formed and coupled together by a lower linkage rail


210


and an upper linkage rail


212


. That is, each throttle body


110




a


,


110




b


,


110




c


has a lower flange


214


that extends downward from the bottom thereof and defines a vertical face. Each throttle body


110




a


,


110




b


,


110




c


also includes an upper flange


216


that extends upward and defines a horizontal face. The respective lower flanges


214


are affixed to the vertical faces of the lower linkage rail


210


by screws


218


, while the respective upper flanges


216


are affixed to the respective horizontal faces of the upper linkage rail


212


by screws


220


. The linked throttle bodies


110




a


,


110




b


,


110




c


are affixed to the crankcase member of the engine body one side of the engine (e.g., the starboard side). One end


222


of each throttle body


110




a


,


110




b


,


110




c


communicates with the crankcase chamber through an appropriate intake manifold and the other end


224


communicates with the plenum chamber via an appropriate sleeve. The throttle valve shafts


94




a


,


94




b


,


94




c


, which support the throttle valves


54




a


,


54




b


,


54




c


, are journaled by bearing portions


228


of the throttle bodies


110




a


,


110




b


,


110




c


for pivotal movement. Coupling members


230


couple the throttle valve shafts


94




a


,


94




b


,


94




c


with one another so that all of the valve shafts


94




a


,


94




b


,


94




c


rotate together. Return springs are provided around the respective throttle valve shafts


94




a


,


94




b


,


94




c


in the bearing portions


228


to bias the shafts


94




a


,


94




b


,


94




c


toward a position in which the throttle valves


54




a


,


54




b


,


54




c


are closed. In other words, the throttle valves


54




a


,


54




b


,


54




c


are urged toward the closed position unless an actuation force acts on the valve shafts


94




a


,


94




b


,


94




c.






The fuel injectors


232


are affixed to the throttle bodies


94




a


,


94




b


,


94




c


so that each nozzle portion of the injector


232


is directed to the intake passage


116




a


,


116




b


,


116




c


downstream of the throttle valve


54




b


. A fuel rail


234


is affixed to the throttle bodies


94




a


,


94




b


,


94




c


so as to support the fuel injectors


232


and also to form a fuel passage


236


therein through which the fuel sprayed by the injectors


232


is delivered.




In the illustrated embodiment, lubricant oil


238


is also injected toward the journaled portions of the valve shafts


94




a


,


94




b


,


94




c


in the intake passages


116




a


,


116




b


,


116




c


through oil injection nozzles


240


. Lubricant injection at this point tends to inhibit salt water from depositing on the valve shafts and at the journaled portions of the valve shaft.




A motor flange


244


is unitarily formed with the most forward portion of the throttle body


110




c


and a valve control motor


246


is affixed thereto. The throttle valve shafts


94




a


,


94




b


,


94




c


in this arrangement are actuated only by this motor


246


in either a manual control mode by the rider or the engine output control mode by the ECU


86


. No mechanical control wire or cable connects the throttle lever


52


and the valve shafts


94




a


,


94




b


,


94




c


. Instead, the throttle lever


52


is connected to a throttle lever position sensor that sends a signal to the ECU


86


through a signal line.




The engine output control mechanism


130


B needs no throttle position sensor because the motor


246


has a built-in position sensor by which a signal indicating a position of the throttle shafts


94




a


,


94




b


,


94




c


is sent to the ECU


86


. A watertight cover protects the motor


246


. Because of the arrangements and constructions of the throttle bodies and valve control motor, the engine output control mechanism


130


B is simple, accurate and durable.




With reference to FIGS.


9


(A)-(C), a further embodiment of the throttle valve control mechanism


130


C will be described below. The same reference numerals will also be assigned to the same components and members that have been already described and further detailed description of these components and members will be omitted.




In this arrangement, a pulley


250


is affixed to the middle throttle shaft


94




b


and a throttle wire


252


is affixed to the pulley


250


. The throttle wire


252


also is connected to the throttle lever


52


so that the rider can manually operate the valve shafts


94




a


,


94




b


,


94




c


through the throttle wire


252


. In the illustrated embodiment, the pulley


250


is disposed between the front throttle body and the middle throttle body. The pulley


250


, however, can be disposed between the middle throttle body and the rear throttle body, and can be connected to any of the throttle shafts.




In the illustrated embodiment, the coupling


230


is positioned between the middle throttle body


110




b


and the rear throttle body


110




a


and has a lever portion


254


extending outward. The coupling


230


preferably lies on one side of the middle throttle body and the pulley


250


lies on the other side in order to simplify construction and provide a compact arrangement of these components.




A solenoid actuator


256


is disposed in a space between the middle throttle body


110




b


and the rear throttle body


110




a


. The solenoid actuator


256


depends from the upper linkage


212


and is affixed thereto. Also, a bracket


258


, which is affixed to the rear throttle body


110




a


, extends forwardly from the rear throttle body to support a body of the actuator


256


. The solenoid actuator


256


has a plunger


260


that extends toward the lever portion


254


of the coupling


230


. The plunger


260


extends when a solenoid of the actuator


256


is activated to push or hold the lever portion


254


downward under control of the ECU


86


.




The throttle position sensor


90


is affixed to a forward end of the throttle valve shaft


94




c


that is placed at the most forward position. The position sensor


90


senses the opening degree of the throttle valves


54




a


,


54




b


,


54




c


and send a signal to the ECU


86


as described above.




Normally, the rider manually operates the throttle shafts


94




a


,


94




b


,


94




c


through the wire


252


and the pulley


250


. When the ECU


86


starts the engine output control mode, the plunger


260


pushes the lever portion


254


. Under this condition, the throttle valve shafts


94




a


,


94




b


,


94




c


rotate to increase the throttle opening degree. The manual operation of the shafts


94




a


,


94




b


,


94




c


is regulated not to decrease the opening degree and is only allowed to increase further the opening degree. The plunger


260


also can be extended to prevent closing rotation of the throttle valves beyond the objective opening degree.




Because the solenoid actuator


256


is disposed between the throttle bodies


110




a


,


110




b


and hence is protected thereby, the engine output control mechanism


130


C is durable and is protected, particularly against water.




With reference to

FIGS. 10 and 11

, a further embodiment of the control system will now be described. The same reference numerals will again be assigned to the same components and members that have been already described and further detailed description of such components and members will be omitted.





FIG. 10

illustrates a further control system


34


A. The steering mast


46


includes a steering shaft


380


, the handlebar


48


, a steering arm


382


and a tubular steering column


384


. While the handlebar


48


is formed atop the steering shaft


380


, the steering arm


382


is rigidly affixed to the bottom portion of the steering shaft


380


. The steering column


384


is affixed to the upper hull section


40


. The steering column


384


supports the steering shaft


380


for steering movement. With the rider steering with the handlebar


48


, the steering arm


382


moves generally in a plane normal to the steering shaft


380


. The steering arm


382


is connected to the deflector


76


through a deflector cable


386


, and the deflector


76


pivots about the vertical axis


78


with the movement of the steering arm


382


in a known manner. A sensor arm


388


on which the steering position sensor


88


is disposed is rigidly affixed to the steering column


384


. A lever


390


extends from the sensor


88


and a linkage member


392


couples the lever


390


with the steering arm


382


. Because the lever


390


pivots with the movement of the steering arm


382


, the steering position sensor


88


senses an angular position of the steering shaft


380


. The sensed signal is set to the ECU


86


through a signal line


396


.




The throttle lever


52


on the handlebar


48


is connected to a pulley


400


affixed to a shaft of a throttle lever position sensor


402


through a throttle wire


404


. This throttle position sensor


402


is not affixed to the throttle valve shafts


94


but rather is separately provided for remotely sensing a position of the throttle lever


52


. The sensed signal is sent to the ECU


86


through a signal line


406


. Because the throttle valves


54


desirably are controlled by the throttle lever


52


, the position of the throttle valves


54


should generally correspond to the position of this lever


52


. A return spring


408


is provided at the throttle position sensor


402


so as to return the shaft of the position sensor


402


to an initial position unless the rider operates the throttle lever


52


.




The control system


34


A employs another engine output control mechanism


130


E. This control mechanism


130


E includes an electric motor


412


having a motor shaft


414


. A first gear


416


is coupled with the motor shaft


414


via a clutch


418


. Unless the clutch


418


is activated, the motor


412


does not rotate the first gear


416


and the first gear


416


merely idles. The first gear


414


meshes with a second gear


420


that in turn is coupled to a second shaft


422


. Because a diameter of the second gear


420


is larger than a diameter of the first gear


414


, a rotational speed of the second shaft


422


will be reduced relative to the rotational speed of the motor shaft


414


.




A pulley


426


is affixed to the second shaft


422


. The throttle bodies


110


(schematically illustrated in

FIG. 10

) also have a pulley


424


that actuates the throttle shafts. An actuator cable


426


connects together the pulleys


422


,


424


. A return spring


428


is affixed to one end of the second shaft


422


so as to return the first and second gears


416


,


420


to their initial positions unless the clutch


418


is connected. A position sensor


430


is affixed to the other end of the reduction shaft


422


to sense an angular position of the shaft


422


. The position sensor


430


sends a signal, which is indicative of the angular position of the shaft


422


, to the ECU


86


through a signal line


432


for feedback control of the clutch


418


and/or the motor


412


. The signal sensed by the position sensor


430


corresponds to the position of the throttle valves


54


.




The position sensor


430


as well as the throttle lever position sensor


402


can be any type of angular position sensors such as a potentiometer type like the sensor


90


used in the preceding embodiments or a Hall IC type sensor.




The ECU


86


controls the motor


412


through a control line


434


. A pulse width modulator or power amplifier


436


preferably is provided between the ECU


86


and the motor


412


to directly control the motor


412


.




The ECU


86


also controls the clutch


418


through a control line


438


. A switch


440


, e.g., FET switch, preferably is provided between the ECU


86


and the clutch


418


to actuate the clutch


418


. When a power switch, i.e., main switch, of the watercraft


30


is off, the ECU


86


is off and the switch


440


is disconnected. In the event of malfunction of the motor


412


, the switch


440


is biased off and accordingly the clutch


418


is disconnected so that the throttle valves


54


can be manually operated.




The ECU


86


has a ROM to store at least a reference position of the steering shaft


380


and also has a RAM to store at least a current position signal of the throttle lever


52


and a change rate of the position signal. The ECU


86


also has a timer.





FIG. 11

illustrates a control routine of the control system


34


A. The control routine starts at Step S


21


when the rider turns on the main power switch. At Step S


22


, the ECU initializes stored data of the RAM and proceeds to Step S


23


. The timer starts to count time (T


0


) at Step S


23


. At Step S


24


, the ECU


86


determines a closed position of the throttle valves


54


from the signal of the throttle valve position sensor


430


. The ECU then determines whether the time (T


0


) counted by the timer exceeds 0.25 seconds (Step S


25


). If 0.25 seconds has not elapsed, the ECU returns to Step S


24


to repeat this step. If the time has elapsed, the ECU instructs the switch


440


to connect the clutch


418


(Step S


26


). Steps S


21


through S


26


comprise an initializing phase of the routine and are not repeated until engine is stopped and restarted.




At Step S


27


, the ECU


86


reads a current throttle lever position from the signal sensed by the throttle lever position sensor


402


. The ECU then calculates the rate of change of the throttle lever position (Step S


28


). If the rate of change is zero, the rider wants to maintain the current throttle position. A large rate of change indicates quick movement of the throttle lever (e.g., when accelerating from rest) and a small rate of change indicates slow movement of the throttle lever (e.g., when docking the watercraft at which time the rider may more precisely control the throttle lever for slow speed maneuvering).




The ECU


86


then determines (at Step S


29


) whether the closed position of the throttle valves, which was read and stored into memory at Step S


24


, falls within a range defined between a reference upper limit (RUL) and a reference lower limit (RLL). If it does, the ECU proceeds to Step S


31


. If not, the ECU performs Step S


30


.




At the step S


30


, the ECU


86


selects either the reference upper limit (RUL) or the reference lower limit (RLL) as a hypothetical closed position. For example, the ECU may be programmed to determine which one of the RUL or RLL is closer to measured value, and then use the closest one as the hypothetical closed position. The ECU then proceeds to the Step


31


.




At Step S


31


, the ECU


86


determines whether the engine


32


is in an idle state, i.e., whether the throttle valves


54


are closed. This determination uses either the actual closed position sensed by the throttle valve position sensor


430


or the hypothetical closed position replaced at the step S


30


, depending upon the conclusion reached at Step S


29


. The idle engine speed of the engine


32


is, for example, 1,200 rpm. If the engine is operating above idle, the ECU proceeds to Step S


39


to instruct the pulse width modulator


436


to practice a normal control mode for controlling the throttle drive motor


412


. If, however, the engine is at idle, the ECU proceeds to Step S


32


.




The pulse width modulator


436


practices the following two controls at the step S


39


. The first control (i.e., Control (1)) involves bringing the actual throttle opening degree sensed by the throttle valve position sensor


430


close to the desired throttle opening sensed by the throttle lever position sensor


402


. For this purpose, any deviation between these two sensed values preferably is minimized to the extent possible by actuating the motor


412


to move the throttle valves.




The second control (i.e., Control (2)) involves controlling the motor


412


through the pulse width modulator


436


in response to the change rate calculated at Step S


28


. If the rate of change is large, the modulator


436


supplies the motor


412


with a relatively high power level so that the motor


412


rotates at a relatively high speed. If the rate of change is small, then the modulator


436


supplies the motor


412


with a relatively low power level so that the motor


412


rotates at a relatively low speed. After performing Step S


39


, the program returns to Step S


27


.




If the ECU determines that the throttle valves are closed (Step S


31


), the ECU


86


then determines at Step S


32


whether the steering position sensed by the steering position sensor


88


is greater than a reference steering position (RS). If no, the ECU does not begin its engine output control mode and proceeds to control the modulator


436


in its normal manner (Step S


39


). If, however, the sensed steering position is greater than the reference steering position (RS), i.e., the rider has turned the steering bar


48


by more than a predetermined degree, the ECU proceeds to Step S


33


for a further calculation before deciding whether to begin its engine output control mode.




The ECU


86


at Step S


33


determines whether the throttle valve opening, and consequently the engine output, is increasing. The assessment of this situation can be determined from whether the actual throttle opening degree is increasing from the closed position under the rider's own control. If yes, the program proceeds to Step S


39


. If not, the ECU begins its engine output control mode (Step S


34


). This step S


33


is advantageous if a manual control or an independent control of the throttle valves is employed. This step S


33


, however, can be omitted in the illustrated control system


34


A.




At Step S


34


, the ECU


86


instructs the pulse width modulator


436


to drive the motor


412


in a direction that increases the throttle valve opening degree. Under this control, the throttle valves are opened to a predetermined throttle opening that corresponds with a desired engine speed. In one embodiment, the engine speed preferably is increased to within the range of about 1,500 to about 4,000 rpm, and more preferably to within the range of about 2,500 to 3,500 rpm, and in one embodiment, to 3,000 rpm. The desired engine speed preferably is sufficient to effect sharp turning of the watercraft. The ECU


86


then starts the timer (Step S


35


) to count off a predetermined amount of time (i.e., starts a count down).




At Step S


36


, the ECU


86


determines whether the throttle lever position is greater than the idle position. If yes, the rider is operating the throttle lever


52


to increase the engine output and the program proceeds to Step S


38


to stop the engine output control mode. If no, the ECU proceeds to Step S


37


.




At Step S


37


, the ECU determines whether the timer has finished the count down. The time period of this count down is preferably within the range of from about 1 second to 5 seconds, and in one embodiment, is about 3 seconds. If this time has not elapsed, the ECU repeats Step S


36


. If the time has expired, the ECU ceases the engine output control mode (Step S


38


), and returns to the main control routine at Step S


27


.




Although this engine control system has been described in terms of certain preferred embodiments, other embodiments and variations of the foregoing examples will be readily apparent to those of ordinary skill in the art. For example, the output of the throttle valve position sensor in the described embodiments can be directly or indirectly used as a control parameter of the ECU. That is, for example, a sensed throttle opening degree, an absolute value of the sensed opening degree, an increase or decrease amount of the opening degree and a rate of change of the opening degree can all be used as the control parameter(s).




Additionally, the output of the steering position sensor can be directly or indirectly used as another control parameter of the ECU. That is, for example, a sensed angular position, an absolute value of the sensed angular position, an increase or decrease amount of the angular position and a rate of change of the angular position are all applicable as the control parameter(s).




The output of the velocity sensor can be directly or indirectly used as a further control parameter of the ECU. That is, for example, a sensed velocity, an absolute value of the velocity, an increase or decrease amount of the velocity and a change rate of the velocity are all applicable as the control parameter.




The sensors can be positioned not only in close proximity to thing that they are measuring but also at a remote place. If the sensors are remotely disposed, an appropriate mechanical, electrical or optical linkage mechanism can be applied.




Conventional sensors are all applicable as the sensor described above whether they are given as examples or not. Additionally, conventional actuators using, for example, electrical power or fluid power (e.g., air pressure, water pressure or hydraulic oil pressure) are all applicable as the actuator for the engine output control whether they are exemplified or not.




Although this invention has been disclosed in the context of certain preferred embodiments and examples, it will be understood by those skilled in the art that the present invention extends beyond the specifically disclosed embodiments to other alternative embodiments and/or uses of the invention and obvious modifications and equivalents thereof. In addition, while a number of variations of the invention have been shown and described in detail, other modifications, which are within the scope of this invention, will be readily apparent to those of skill in the art based upon this disclosure. It is also contemplated that various combination or sub-combinations of the specific features and aspects of the embodiments may be made and still fall within the scope of the invention. Accordingly, it should be understood that various features and aspects of the disclosed embodiments can be combine with or substituted for one another in order to form varying modes of the disclosed invention. Thus, it is intended that the scope of the present invention herein disclosed should not be limited by the particular disclosed embodiments described above, but should be determined only by a fair reading of the claims that follow.



Claims
  • 1. A jet propelled watercraft comprising:an engine having at least one throttle valve, the throttle valve being movable between an idle position and a fully open position; a throttle operator remotely positioned relative to the engine and coupled to the throttle valve, the throttle operator being movable between first and second positions whereby the throttle operator causes the throttle valve to move between the idle and fully open positions, respectively; and an engine control system comprising a first sensor configured to detect an operating state of the watercraft or the engine, a second sensor configured to detect a position of the throttle operator, a throttle valve control mechanism including an actuator cooperating with the throttle valve under at least one operating state of the watercraft or the engine, and a controller communicating with the first and second sensors and with the throttle valve control mechanism, the controller being configured to activate the throttle valve control mechanism once the operating state of the watercraft or engine is greater than a predetermined state for a preset period of time and to leave active the throttle valve control mechanism at least when the throttle operator quickly moves to the first position so as to maintain the throttle valve between the idle and fully open positions.
  • 2. The watercraft of claim 1, wherein the throttle operator is coupled to the throttle valve by a throttle drive mechanism, and the actuator is coupled to the throttle valve independently of the throttle drive mechanism.
  • 3. The watercraft of claim 2, wherein the throttle drive mechanism comprises a throttle pulley.
  • 4. The watercraft of claim 3, wherein the throttle drive mechanism additionally comprises a cable linking the throttle operator to the throttle pulley and a biasing member arranged to bias the throttle operator towards the first position.
  • 5. The watercraft of claim 1, wherein the first sensor is an engine speed sensor configured to output a signal to the controller that is indicative of engine rotational speed.
  • 6. The watercraft of claim 1, wherein the first sensor is a watercraft speed sensor configured to output a signal to the controller that is indicative of a vehicle speed of the watercraft.
  • 7. The watercrafi of claim 1, wherein the first sensor is a throttle valve position sensor configured to output a signal to the controller that is indicative of the position of the throttle valve.
  • 8. The watercraft of claim 1, wherein throttle valve control mechanism is configured to maintain the throttle valve open to a degree corresponding to a trolling condition of the watercraft.
  • 9. The watercraft of claim 1, wherein throttle valve control mechanism is configured to maintain the throttle valve open to a degree corresponding to a transient condition of the watercraft between a displacement mode of operation and a planing mode of operation.
  • 10. The watercraft of claim 1, wherein the engine control system additionally comprises a steering angle sensor, and wherein the controller is configured to deactivate the throttle valve control mechanism so as to permit the throttle valve to return to an idle position when a steering angle is less than a preset degree.
  • 11. The watercraft of claim 1, wherein the controller and the throttle valve control mechanism are configured to maintain the throttle valve at a preset position between the idle and fully open positions.
  • 12. The watercraft of claim 1, wherein the controller and the throttle valve control mechanism are configured to retard movement of the throttle valve from a preset position, which lies between the idle and fully open positions, to the idle position.
  • 13. The watercraft of claim 12, wherein the controller and the throttle valve control mechanism are configured to gradually decrease the opening degree of the throttle valve at least over a range of movement between the preset position and the idle position.
  • 14. A jet propelled watercraft comprising:an engine having at least one throttle valve, the throttle valve being movable between a closed position and a fully open position; a throttle operator remotely positioned relative to the engine and coupled to the throttle valve, the throttle operator being movable between first and second positions whereby the throttle operator causes the throttle valve to move between the closed and fully open positions, respectively; a steering mast comprising a handlebar rotatably carried by the steering mast and configured to steer the watercraft; and an engine control system comprising a first sensor configured to detect an operating state of the watercraft or the engine, a second sensor configured to detect a position of the throttle operator, a third sensor configured to detect an angular orientation of the handlebar, a throttle valve control mechanism including an actuator cooperating with the throttle valve under at least one operating state of the watercraft or the engine, and a controller communicating with the first and second sensors and with the throttle valve control mechanism, the controller being configured to activate the throttle valve control mechanism once the operating state of the watercraft or engine is greater than a predetermined state, and the controller and throttle valve control mechanism further being configured to delay closure of the throttle valve at least when the throttle operator moves to the first position and the handlebar exceeds a predetermined angular orientation, wherein the first sensor is an engine speed sensor configured to output a signal to the controller that is indicative of engine rotational speed.
  • 15. A jet propelled watercraft comprising:an engine having at least one throttle valve, the throttle valve being movable between a closed position and a fully open position; a throttle operator remotely positioned relative to the engine and coupled to the throttle valve, the throttle operator being movable between first and second positions whereby the throttle operator causes the throttle valve to move between the closed and fully open positions, respectively; a steering mast comprising a handlebar rotatably carried by the steering mast and configured to steer the watercraft; and an engine control system comprising a first sensor configured to detect an operating state of the watercraft or the engine, a second sensor configured to detect a position of the throttle operator, a third sensor configured to detect an angular orientation of the handlebar, a throttle valve control mechanism including an actuator cooperating with the throttle valve under at least one operating state of the watercraft or the engine, and a controller communicating with the first and second sensors and with the throttle valve control mechanism, the controller being configured to activate the throttle valve control mechanism once the operating state of the watercraft or engine is greater than a predetermined state, and the controller and throttle valve control mechanism further being configured to delay closure of the throttle valve at least when the throttle operator moves to the first position and the handlebar exceeds a predetermined angular orientation, wherein the controller is configured to activate the throttle valve control mechanism once the operating state of the watercraft or engine is greater than a predetermined state for a preset period of time.
  • 16. The watercraft according to claim 1, wherein the controller is configured to prevent actuation of the throttle valve control mechanism until the operating state of the watercraft or engine is greater than a predetermined state for the preset period of time.
Priority Claims (2)
Number Date Country Kind
2001-038202 Feb 2001 JP
2002-013828 Jan 2002 JP
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