Output shaft structure of personal watercraft

Information

  • Patent Grant
  • 6716076
  • Patent Number
    6,716,076
  • Date Filed
    Tuesday, July 9, 2002
    22 years ago
  • Date Issued
    Tuesday, April 6, 2004
    20 years ago
Abstract
To provide an output shaft structure of a personal watercraft, which is capable of enhancing the durability of the engine. An engine is mounted on a watercraft body with a crankshaft extending in the longitudinal direction of the watercraft body. A shaft of a propulsion device is coupled to a rear end of the crankshaft in such a manner as to be disposed on an extension of the crankshaft. The crankshaft is supported by an engine case via plain metal. An output shaft is provided separately from the crankshaft and is coupled to the rear end of the crankshaft. The shaft of the propulsion device is coupled to the rear end of the output shaft. The output shaft is supported by the engine case via rolling bearings immovable in a thrust direction. A spline is formed on or in each of the rear end of the crankshaft and the front end of the output shaft, and a spline to be engaged with these splines is formed in or on an inner surface of a connection pipe. The rear end of the crankshaft is coupled to the front end of the output shaft via the connection pipe. A gap is formed between opposed faces of the rear end of the crankshaft and the front end of the output shaft.
Description




CROSS-REFERENCE TO RELATED APPLICATIONS




This nonprovisional application claims priority under 35 U.S.C. § 119(a) on Patent Application No. 2001-219318 filed in Japan on Jul. 19, 2001, the entirety of which is hereby incorporated by reference.




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to an output shaft structure of a personal watercraft.




2. Description of Background Art




Two-cycle engines have been used as power sources of general personal watercrafts. In recent years, however, to meet a requirement to lower environmental pollution and reduce noise, personal watercrafts using four-cycle engines as power sources have been proposed (see Japanese Patent No. 2880691).




Since integral type crankshafts are generally used for four-cycle engines, plain metal is used as bearings for the crankshafts.




In personal watercrafts of this type, as shown in FIGS.


10


(


a


) and


10


(


b


) of the present invention, an engine


1


is mounted on a watercraft body


2


with a crankshaft


1




a


of the engine


1


extending along the longitudinal direction of the watercraft body


2


. A shaft


3




a


of a propulsion device (for example, a jet pump)


3


is coupled via a coupling


4


to a rear end


1




b


of the crankshaft


1




a


in such a manner as to be disposed on an extension of the crankshaft


1




a.






Accordingly, power from the crankshaft of the engine


1


is transmitted to the propulsion device via the shaft


3




a


of the propulsion device


3


, to propel the watercraft body


2


.




In the personal watercraft as shown in FIGS.


10


(


a


) and


10


(


b


), a reaction force from the propulsion device


3


is transmitted to the crankshaft


1




a


of the engine


1


.




To be more specific, the crankshaft la receives an anti-torque, a thrust force, a bending force (for deflecting the crankshaft), and vibration from the shaft


3




a


of the propulsion device


3


via the coupling


4


. These forces and vibration are applied in a complex combination to the crankshaft


1




a.






In the conventional personal watercraft as shown in FIGS.


10


(


a


) and


10


(


b


), if a two-cycle engine is used as the power source, there occurs no problem. This is because a crankshaft of the two-cycle engine is of a built-up type and uses a ball bearing having high durability as a bearing therefor.




In the conventional personal watercraft as shown in FIGS.


10


(


a


) and


10


(


b


); however, if a four-cycle engine is used as the power source, there occurs a problem. The reason for this is that since a crankshaft of the four-cycle engine is of an integral type and plain metal is used as a bearing therefor as described above, the above-described anti-torque, thrust force, bending force, and vibration are applied in a complex combination to the crankshaft. Accordingly, the crankshaft rotating at a high speed causes torsion, compression, bending (deflection), and vibration in complex combination. This results in the fatigue of the plain metal becoming severe, to degrade durability of the engine.




SUMMARY OF THE INVENTION




An object of the present invention is to solve the above-described problem and to provide an output shaft structure of a personal watercraft, which is capable of enhancing durability of an engine.




To achieve the above object, according to a first aspect of the present invention, there is provided an output shaft structure of a personal watercraft, wherein an engine is mounted on a watercraft body with a crankshaft of the engine extending in the longitudinal direction of the watercraft body. A shaft of a propulsion device is coupled to a rear end of the crankshaft of the engine in such a manner as to be disposed on an extension of the crankshaft. The crankshaft is supported by an engine case via plain metal. This output shaft structure includes an output shaft, which is provided separately from the crankshaft and is coupled to the rear end of the crankshaft. The shaft of the propulsion device is coupled to a rear end of the output shaft. The output shaft is supported by the engine case via a rolling bearing, which is immovable in a thrust direction.




With the above construction according to the first aspect of the present invention, a thrust force from the shaft of the propulsion device is mainly received by the output shaft and the rolling bearing. Therefore, the thrust force is not directly applied to the crankshaft. However, if the thrust force is applied to the crankshaft, it is transmitted thereto indirectly (in a moderated state).




Since the output shaft provided separately from the crankshaft is coupled to the rear end of the crankshaft and the shaft of the propulsion device is coupled to the rear end of the output shaft, an anti-torque, a bending force, and vibration from the shaft of the propulsion device are not directly applied to the crankshaft. However, if applied to the crankshaft, they are transmitted thereto indirectly (in a moderated state). In particular, a bending force applied to the crankshaft is significantly reduced.




As a result, according to the output shaft structure of a personal watercraft according to the first aspect of the present invention, it is possible to reduce fatigue of the plain metal for supporting the crankshaft, and hence to improve the durability of the engine.




According to a second aspect of the present invention, a spline is formed on or in the rear end of the crankshaft. Furthermore, a spline is formed on or in the front end of the output shaft. A spline for engageing with the splines is formed in or on an inner surface of a connection pipe. The rear end of the crankshaft is coupled to the front end of the output shaft via the connecting pipe.




With the above construction according to the second aspect of the present invention, it is possible to certainly transmit power from the crankshaft to the output shaft via the connection pipe.




An anti-torque, a bending force, and vibration from the shaft of the propulsion device are transmitted from the output shaft to the crankshaft via the connection pipe. In this case, since each of the crankshaft and the output shaft is coupled to the connection pipe by a spline-fitting, the reaction force, particularly, the bending force and vibration can be significantly reduced in the course of transmission from the output shaft to the crankshaft via the connection pipe.




As a result, according to the output shaft structure of a personal watercraft according to the second aspect of the present invention, it is possible to certainly transmit a power from the crankshaft to the output shaft via the connection pipe and to improve durability of the engine.




According to a third aspect of the present invention, a gap is formed between opposed faces of the rear end of the crankshaft and the front end of the output shaft.




With the above construction according to the third aspect of the present invention, an anti-torque, a thrust force, a bending force, and vibration, particularly, a thrust force and a bending force can be significantly reduced. Accordingly, it is possible to more certainly improve the durability of the engine.




Further scope of applicability of the present invention will become apparent from the detailed description given hereinafter. However, it should be understood that the detailed description and specific examples, while indicating preferred embodiments of the invention, are given by way of illustration only, since various changes and modifications within the spirit and scope of the invention will become apparent to those skilled in the art from this detailed description.











BRIEF DESCRIPTION OF THE DRAWINGS




The present invention will become more fully understood from the detailed description given hereinbelow and the accompanying drawings which are given by way of illustration only, and thus are not limitative of the present invention, and wherein:





FIG. 1

is a schematic side view showing one example of a personal watercraft to which one embodiment of an output shaft structure of a personal watercraft according to the present invention is applied;





FIG. 2

is a plan view of the personal watercraft of

FIG. 1

;





FIG. 3

is a partial, enlarged sectional view taken on line III—III of

FIG. 1

(with parts partially omitted);





FIG. 4

is a view mainly showing the engine


20


, which is a partial, enlarged sectional view taken on line IV—IV of

FIG. 1

(with parts partially omitted);





FIG. 5

is a schematic perspective view of the engine


20


as seen from an obliquely rearward direction;





FIG. 6

is a sectional side view of the engine


20


;





FIG. 7

is a partial, enlarged view of

FIG. 6

;





FIG. 8

is an enlarged view showing the crankshaft


21


, a connection pipe


23


, and the ball bearings


27




a


and


27




b;






FIGS.


9


(


a


) and


9


(


b


) are views showing the output shaft


22


, wherein FIG.


9


(


a


) is an end view seen from rear, and FIG.


9


(


b


) is a sectional view taken on line b—b of FIG.


9


(


a


); and




FIGS.


10


(


a


) and


10


(


b


) are views illustrating a background art personal watercraft.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




Hereinafter, an embodiment of the present invention will be described with reference to the accompanying drawings.





FIG. 1

is a schematic side view showing one example of a personal watercraft to which one embodiment of an output shaft structure of a personal watercraft according to the present invention is applied.

FIG. 2

is a plan view of the personal watercraft of FIG.


1


.

FIG. 3

is a partial, enlarged sectional view taken on line III—III of

FIG. 1

(with parts partially omitted).




Referring to these figures (particularly to FIG.


1


), a personal watercraft


10


is a small saddle type watercraft, which is operable by a driver who sits on a seat


12


disposed on a watercraft body


11


and holds a steering handlebar


13


provided with a throttle lever.




The watercraft body


11


has a floating structure, wherein a hull


14


is joined to a deck


15


to form a space


16


therein. In the space


16


, an engine


20


is mounted on the hull


14


with a crankshaft


21


(see

FIG. 6

) extending in the longitudinal direction of the watercraft body


11


. A jet pump or jet propulsion pump


30


functioning as a propulsion device driven by the engine


20


is provided on a rear portion of the hull


14


. An intake duct


18


for supplying intake air in the watercraft body


11


(space


16


) is provided in the watercraft body


11


.




The jet pump


30


has a flow passage


33


extending from a water inlet


17


opened in a bottom shell to both a jet port


31


opened in a rear end portion of the hull


14


and a nozzle


32


. An impeller


34


is disposed in the flow passage


33


. A shaft


35


of the impeller


34


is coupled to an output shaft


22


(to be described below) of the engine


20


via a coupling


80


. When the impeller


34


is rotated by drive of the engine


20


, water taken in via the water inlet


17


is jetted from the jet port


31


via the nozzle


32


, to propel the watercraft body


11


. A rotational speed of the engine


20


, that is, a propelling force of the jet pump


30


is controlled by a turning operation of a throttle lever


13




a


(see

FIG. 2

) of the steering handlebar


13


. The nozzle


32


is coupled to the steering handlebar


13


via a steering wire (not shown), and is turned by operation of the steering handlebar


13


, to change a running direction of the watercraft body


11


.




In the figures, reference numeral


40


denotes a fuel tank, and reference numeral


41


denotes a containing chamber.





FIG. 4

is a view mainly showing the engine


20


, which is a partial, enlarged sectional view taken on line IV—IV of

FIG. 1

(with parts partially omitted).

FIG. 5

is a schematic perspective view of the engine


20


as seen from an obliquely rearward direction.

FIG. 6

is a sectional side view of the engine


20


.

FIG. 7

is a partial, enlarged view of FIG.


6


.




The engine


20


is a DOHC type in-line four-cylinder/four-cycle engine. As is apparent from

FIGS. 1 and 4

, the crankshaft


21


of the engine


20


extends along the longitudinal direction of the watercraft body


11


. Referring to

FIG. 4

, an intake port


20




a


is disposed on a left side of the engine


20


in the running direction of the watercraft body


11


. An exhaust port


20




b


is disposed on a right side of the engine


20


in the running direction of the watercraft body


11


.




A throttle body


42


and a surge tank (intake chamber)


43


are connected to the intake port


20




a


. An inter-cooler


50


disposed immediately under the surge tank


43


is connected to the surge tank


43


. In

FIG. 4

, reference numerals


52


and


53


denote mounting brackets of the inter-cooler


50


. the mounting brackets


52


and


53


are mountable to the engine


20


.




The inter-cooler


50


includes, as shown in

FIGS. 4 and 5

, a case


51


having an intake inlet


51




i


and an outlet


51




o


, and a cooling unit


60


. The intake inlet


51




i


is connected and communicated, via piping


72


, to a compressor portion


71


of a supercharger (turbo-charger)


70


disposed immediately behind the engine


20


. The outlet


51




o


is connected, via a tube


51




c


, to an intake inlet


43




a


of the surge tank


43


. The cooling unit


60


is a heat exchange unit accommodated in the case


51


.




In

FIG. 5

, reference numerals


91


and


92


denote cooling water hoses connected to the inter-cooler


50


.




Referring also to

FIG. 4

, an exhaust manifold


44


is connected to the exhaust port


20




b


of the engine


20


. An exhaust outlet


44




o


(see

FIG. 5

) of the exhaust manifold


44


is connected to a turbine portion


73


of the turbo-charger


70


.




In addition, as shown in

FIGS. 1 and 2

, exhaust gas, which has been used for rotating a turbine in the turbine portion


73


, is discharged in water stream generated by the jet pump


30


via an exhaust pipe


74


, an anti-counterflow chamber


75


for preventing counterflow of water (permeation of water in the turbo-charger


70


and the like) at the time of turn-over, a water muffler


76


, and an exhaust/drainage pipe


77


.




Referring to

FIGS. 6 and 7

, the crankshaft


21


of the engine


20


is rotatably supported, via plain metal


26


, by a bearing portion


20




e


provided in a lower case


20




c


and an upper case


20




d


of the engine


20


.




A rear end


21




a


of the crankshaft


21


is located between the engine cases


20




c


and


20




d


. The output shaft


22


is provided separately from the crankshaft


21


and is coupled to the rear end


21




a


of the crankshaft


21


. A shaft


35


of the jet pump


30


, which is the above-described propulsion device, is coupled to a rear end of the output shaft


22


via the coupling


80


.




The output shaft


22


is rotatably supported by two rolling bearings (ball bearings in the example shown in the figures)


27




a


and


27




b


, which are mounted in the engine cases


20




c


and


20




d


in such a manner as to be immovable in a thrust direction (in the direction from right to left or from left to right in FIGS.


6


and


7


). In the figure, reference numeral


28


denotes a seal member for preventing permeation of water in the engine


20


, and


29




a


,


29




b


and


29




c


denote thrust receiving members interposed between the ball bearings and the engine cases.





FIG. 8

is an enlarged view showing the crankshaft


21


, a connection pipe


23


, and the ball bearings


27




a


and


27




b


. FIGS.


9


(


a


) and


9


(


b


) are views showing the output shaft


22


, wherein FIG.


9


(


a


) is an end view seen from rear, and FIG.


9


(


b


) is a sectional view taken on line b—b of FIG.


9


(


a


).




Referring to

FIG. 7

to FIG.


9


(


b


), a spline


21




a


is formed on or in the rear end of the crankshaft


21


. A spline


22




a


is formed on or in a front end of the output shaft


22


. The connection pipe


23


has, in or on its inner surface, a spline


23




a


for being engaged with the splines


21




a


and


22




a


. The rear end of the crankshaft


21


is thus coupled to the front end of the output shaft


22


via the connection pipe


23


.




The output shaft


22


also has, on or in its rear end, a spline


22




b


. An output side coupling


81


(see

FIG. 7

) has, in or on an inner surface of a boss, a spline


81




a


for being engaged with the spline


22




b


. The output side coupling


81


is thus coupled to the rear end of the output shaft


22


by engaging the spline


22




b


on the output shaft


22


with the spline


81




a


on the output side coupling


81


.




The output shaft


22


, the connection pipe


23


, and the bearings


27




a


and


27




b


are mounted to the crankshaft


21


by mounting the connection pipe


23


and the bearings


27




a


and


27




b


to the rear end of the crankshaft


21


as shown in FIG.


8


. The output shaft


22


is then mounted in a rear portion of the connection pipe


23


as shown in

FIG. 7. A

bolt B is then inserted in a bolt insertion hole


22




c


formed in the output shaft


22


(see FIGS.


9


(


a


) and


9


(


b


)), and an external thread portion B


1


at a leading end portion of the bolt B is threaded in a threaded hole


21




b


formed in the rear end of the crankshaft


21


(see FIG.


8


). It should be noted that any threaded portion, in which the external thread portion B


1


of the bolt B is to be screwed, is not formed in the output shaft


22


(see FIGS.


9


(


a


) and


9


(


b


)), and that the bolt B is only inserted in the output shaft


22


.




The lower case


20




c


and the upper case


20




d


of the engine


20


are thus fastened to each other with bolts (not shown). This results in the crankshaft


21


, the output shaft


22


, the connection pipe


23


, and the bearings


27




a


and


27




b


being assembled in the engine


20


as shown in

FIGS. 6 and 7

.




In such an assembled state, the connection pipe


23


is slightly clamped between a stepped portion


21




d


at the rear portion of the crankshaft


21


in the axial direction and a flange portion


22




d


of the output shaft


22


. The wording “slightly clamped” means a state where the connection pipe


23


is clamped to such a degree as to allow the connection pipe


23


to be positioned without the occurrence of looseness between the stepped portion


21




d


at the rear portion of the crankshaft


21


and the flange portion


22




d


of the output shaft


22


. On the other hand, the bearings


27




a


and


27




b


are slightly clamped between a flange portion


23




d


of the connection pipe


23


and the flange portion


22




d


of the output shaft


22


. The wording “slightly clamped” means a state where the bearings


27




a


and


27




b


are clamped to such a degree as to allow the bearings


27




a


and


27




b


to be positioned between the flange portion


23




d


of the connection pipe


23


and the flange portion


22




d


of the output shaft


22


. A gap C (see

FIG. 7

) is formed between opposed faces


21




e


and


22




e


of the rear end of the crankshaft


21


and the front end of the output shaft


22


.




Accordingly, a thrust force F (see

FIG. 7

) from the shaft


35


of the jet pump


30


is mainly received, via the coupling


80


and the flange portion


22




d


of the output shaft


22


, by the bearings


27




a


and


27




b


(and consequently, by the engine cases). In other words, the thrust force F is not directly applied to the crankshaft


21


. However, if the thrust force is applied, it is slightly transmitted thereto via the connection pipe


23


, i.e., indirectly (in a moderated state).




Referring again to

FIGS. 6 and 7

, a transmission chamber


20




g


, which accommodates a transmission mechanism (to be described below) for transmitting power of the crankshaft


21


to a cam shaft


20




f


of the engine


20


, is provided in a rear portion of the engine


20


, i.e., in a rear portion of the crankshaft


21


. In the transmission chamber


20




g


, the rear end (


21




a


) of the crankshaft


21


is coupled to the front end (


22




a


) of the output shaft


22


.




The transmission mechanism for transmitting power of the crankshaft


21


to the cam shaft


20




f


includes a drive sprocket


23




s


(see

FIG. 8

) integrated with the connection pipe


23


. A driven sprocket


20




s


is provided on the cam shaft


20




f


in such a manner as to be rotatable with the cam shaft


20




f


. An endless chain (transmission chain)


20




h


is stretched between the drive sprocket


23




s


and the driven sprocket


20




s


. It is to be noted that the transmission mechanism may be configured by using a gear train. In this case, a drive gear may be integrally provided on the connection pipe


23


, in place of the drive sprocket


23




s.






The output shaft structure of the personal watercraft according to the present invention, configured as described above, has the following functions and effects:




The engine


20


is mounted on the watercraft body


11


with the crankshaft


21


of the engine


20


extending in the longitudinal direction of the watercraft body


11


. The shaft


35


of the propulsion device


30


is coupled to the rear end of the crankshaft


21


in such a manner as to be disposed on an extension of the crankshaft


21


. The crankshaft


21


is supported by the cases


20




c


and


20




d


of the engine


20


via plain metal


26


. With this structure, the output shaft


22


provided separately from the crankshaft


21


is coupled to the rear end of the crankshaft


21


. The shaft


35


of the propulsion device


30


is coupled to the rear end of the output shaft


22


. The output shaft


22


is supported by the cases


20




c


and


20




d


of the engine


20


via the rolling bearings


27




a


and


27




b


immovable in a thrust direction. As a result, a thrust force F from the shaft


35


of the propulsion device


30


is mainly received by the output shaft


22


and the rolling bearings


27




a


and


27




b


. Therefore, the thrust force is not directly applied to the crankshaft


21


. However, if the thrust force is applied to the crankshaft


21


, it is transmitted thereto indirectly (in a moderated state).




Since the output shaft


22


provided separately from the crankshaft


21


is coupled to the rear end of the crankshaft


21


and the shaft


35


of the propulsion device


30


is coupled to the rear end of the output shaft


22


, an anti-torque, a bending force, and vibration from the shaft


35


of the propulsion device


30


are not directly applied to the crankshaft


21


. However, if applied to the crankshaft, they are transmitted thereto indirectly (in a moderated state). In particular, a bending force applied to the crankshaft


21


is significantly reduced.




As a result, according to this configuration of the output shaft structure of a personal watercraft, it is possible to reduce fatigue of the plain metal


26


for supporting the crankshaft


21


, and hence to improve the durability of the engine


20


.




The spline


21




a


is formed on or in the rear end of the crankshaft


21


and the spline


22




a


is also formed on or in the front end of the output shaft


22


. The spline


23




a


for engaging with the splines


21




a


and


22




a


is formed in or on an inner surface of the connection pipe


23


. The rear end of the crankshaft


21


is coupled to the front end of the output shaft


22


via the connecting pipe


23


. As a result, it is possible to certainly transmit a power from the crankshaft


21


to the output shaft


22


via the connection pipe


23


.




An anti-torque, a bending force, and vibration from the shaft


35


of the propulsion device


30


are transmitted from the output shaft


22


to the crankshaft


21


via the connection pipe


23


. In this case, since each of the crankshaft


21


and the output shaft


22


is coupled to the connection pipe


23


by spline-fitting, the reaction force from the shaft


35


of the propulsion device


30


, particularly, the bending force and vibration can be significantly reduced in the course of transmission from the output shaft


22


to the crankshaft


21


via the connection pipe


23


.




As a result, according to this configuration of the output shaft structure of a Personal watercraft, it is possible to certainly transmit power from the crankshaft


21


to the output shaft


22


via the connection pipe


23


and to improve durability of the engine


20


.




The gap C is formed between opposed faces


21




e


and


22




e


of the rear end of the crankshaft


21


and the front end of the output shaft


22


. Accordingly, an anti-torque, a thrust force, a bending force, and vibration, particularly, a thrust force and a bending force transmitted from the shaft


35


of the propulsion device


30


to the crankshaft


21


can be significantly reduced. As a result, it is possible to more certainly improve the durability of the engine


20


.




The rear end of the crankshaft


21


is located between the engine cases


20




c


and


20




d


. The output shaft


22


is provided separately from the crankshaft


21


and is coupled to the rear end of the crankshaft


21


. The shaft


35


of the propulsion device


30


is coupled to the rear end of the output shaft


22


. As a result, the crankshaft


21


can be shortened because the rear end of the crankshaft


21


is located between the engine cases


20




c


and


20




d.






Accordingly, even if an anti-torque, a thrust force, a bending force, and vibration are applied in a complex combination to the crankshaft


21


, the crankshaft


21


is bent less (less deflected).




As a result, the crankshaft


21


rotating at a high speed, the bearing portion


20




e


thereof, and the like are less fatigued. This makes it possible to further improve the durability of the engine


20


.




The engine


20


is a four-cycle DOHC engine. The transmission chamber


20




g


where the transmission mechanism for transmitting a power from the engine


20


to the cam shaft


20




f


of the engine


20


is provided in a rear portion of the crankshaft


21


. In the transmission chamber


20




g


, the rear end of the crankshaft


21


is coupled to the front end of the output shaft


22


. As a result, it is possible to couple the rear end of the crankshaft


21


to the front end of the output shaft


22


by making effective use of a space in the transmission chamber


20




g.






A drive sprocket


23




s


(or drive gear) of the transmission mechanism is integrally provided on the connection pipe


23


. The provision of the drive sprocket


23




s


(or drive gear) of the transmission mechanism on the connection pipe


23


is easier than the provision of the drive sprocket


23




s


(or drive gear) of the transmission mechanism on the crankshaft


21


.




The invention being thus described, it will be obvious that the same may be varied in many ways. Such variations are not to be regarded as a departure from the spirit and scope of the invention, and all such modifications as would be obvious to one skilled in the art are intended to be included within the scope of the following claims.



Claims
  • 1. An output shaft structure of a personal watercraft, wherein an engine is mounted on a watercraft body with a crankshaft of the engine extending in a longitudinal direction of the watercraft body, a shaft of a propulsion device is coupled to a rear end of the crankshaft of said engine in such a manner as to be disposed on an extension of the crankshaft, and the crankshaft is supported by an engine case via plain metal, said output shaft structure comprising:an output shaft provided separately from the crankshaft, said output shaft being coupled to the rear end of the crankshaft, the shaft of the propulsion device being coupled to a rear end of said output shaft, and said output shaft is supported by the engine case via a rolling bearing immovable in a thrust direction; a first spline being formed on or in the rear end of the crankshaft; a second spline being formed on or in a front end of said output shaft; and a third spline engaging with said first and second splines and being formed in or on an inner surface of a connection pipe, and the rear end of the crankshaft is coupled to the front end of said output shaft via said connecting pipe.
  • 2. The output shaft structure of a personal watercraft according to claim 1, wherein a gap is formed between opposed faces of the rear end of said crankshaft and the front end of said output shaft.
  • 3. The output shaft structure of a personal watercraft according to claim 2, wherein the crankshaft includes a stepped portion formed thereon, said output shaft including a flange portion formed thereon, and said connection pipe is slightly clamped between said stepped portion and said flange portion.
  • 4. The output shaft structure of a personal watercraft according to claim 1, wherein said output shaft includes a bolt insertion hole formed therein, the rear end of the crank shaft includes a threaded bolt hole formed therein, said output shaft structure further comprising a bolt inserted through said bolt insertion hole and into said threaded bolt hole, said bolt including a thread portion formed at a leading end portion thereof, said thread portion being threaded in said threaded bolt hole to couple said output shaft to the crankshaft.
  • 5. The output shaft structure of a personal watercraft according to claim 1, wherein said output shaft includes a bolt insertion hole formed therein, the rear end of the crank shaft includes a threaded bolt hole formed therein, said output shaft structure further comprising a bolt inserted through said bolt insertion hole and into said threaded bolt hole, said bolt including a thread portion formed at a leading end portion thereof, said thread portion being threaded in said threaded bolt hole to couple said output shaft to the crankshaft.
  • 6. The output shaft structure of a personal watercraft according to claim 5, wherein the crankshaft includes a stepped portion formed thereon, said output shaft including a flange portion formed thereon, and said connection pipe is slightly clamped between said stepped portion and said flange portion.
  • 7. The output shaft structure of a personal watercraft according to claim 1, wherein the crankshaft includes a stepped portion formed thereon, said output shaft including a flange portion formed thereon, and said connection pipe is slightly clamped between said stepped portion and said flange portion.
  • 8. A personal watercraft, comprising:a watercraft body; an engine mounted on said watercraft body with a crankshaft of said engine extending in the longitudinal direction of said watercraft body, said crankshaft being supported by an engine case via plain metal; an output shaft, said output shaft being provided separately from said crankshaft and coupled to a rear end of said crankshaft, said output shaft being supported by said engine case via a rolling bearing immovable in a thrust direction; a propulsion device, a shaft of said propulsion device being coupled to a rear end of said crankshaft in such a manner as to be disposed on an extension of said crankshaft, said shaft of said propulsion device being coupled to a rear end of said output shaft; and a first spline being formed on or in the rear end of said crankshaft; a second spline being formed on or in a front end of said output shaft; and a third spline engaging with said first and second splines and being formed in or on an inner surface of a connection pipe, and the rear end of said crankshaft is coupled to the front end of said output shaft via said connecting pipe.
  • 9. The personal watercraft according to claim 8, wherein a gap is formed between opposed faces of the rear end of said crankshaft and the front end of said output shaft.
  • 10. The personal watercraft according to claim 9, wherein said crankshaft includes a stepped portion formed thereon, said output shaft including a flange portion formed thereon, and said connection pipe is slightly clamped between said stepped portion and said flange portion.
  • 11. The personal watercraft according to claim 8, wherein said output shaft includes a bolt insertion hole formed therein, the rear end of said crank shaft includes a threaded bolt hole formed therein, said personal watercraft further comprising a bolt inserted through said bolt insertion hole and into said threaded bolt hole, said bolt including a thread portion formed at a leading end portion thereof, said thread portion being threaded in said threaded bolt hole to couple said output shaft to said crankshaft.
  • 12. The personal watercraft according to claim 8, wherein said output shaft includes a bolt insertion hole formed therein, the rear end of said crank shaft includes a threaded bolt hole formed therein, said personal watercraft further comprising a bolt inserted through said bolt insertion hole and into said threaded bolt hole, said bolt including a thread portion formed at a leading end portion thereof, said thread portion being threaded in said threaded bolt hole to couple said output shaft to said crankshaft.
  • 13. The personal watercraft according to claim 12, wherein said crankshaft includes a stepped portion formed thereon, said output shaft including a flange portion formed thereon, and said connection pipe is slightly clamped between said stepped portion and said flange portion.
  • 14. The personal watercraft according to claim 8, wherein said crankshaft includes a stepped portion formed thereon, said output shaft including a flange portion formed thereon, and said connection pipe is slightly clamped between said stepped portion and said flange portion.
Priority Claims (1)
Number Date Country Kind
2001-219318 Jul 2001 JP
US Referenced Citations (10)
Number Name Date Kind
4722707 Murase Feb 1988 A
4813898 Nakase et al. Mar 1989 A
5282444 Ito et al. Feb 1994 A
5405276 Kato Apr 1995 A
5558549 Nakase et al. Sep 1996 A
6394860 Nanami et al. May 2002 B1
6475046 Muramatsu et al. Nov 2002 B2
6488553 Bourret Dec 2002 B2
6537115 Suganuma et al. Mar 2003 B2
20030075089 Matsuda et al. Apr 2003 A1
Foreign Referenced Citations (2)
Number Date Country
2880691 Jan 1999 JP
2002227696 Aug 2002 JP