Ignition device for personal watercraft engine

Information

  • Patent Grant
  • 6810869
  • Patent Number
    6,810,869
  • Date Filed
    Wednesday, July 3, 2002
    22 years ago
  • Date Issued
    Tuesday, November 2, 2004
    20 years ago
Abstract
An ignition device for a personal watercraft engine, which allows mounting of a four-cycle engine on the personal watercraft and prevents occurrence of leakage of current. The engine for driving a jet propelling pump is provided in a watercraft body surrounded by a hull and a deck. A spark plug for spark ignition is provided in a cylinder head of the engine, and an integral cap ignition coil having a water-proof structure is water-tightly provided in the cylinder head in such a manner as to be located on the spark plug at an uppermost portion of the engine. A water-escape groove continuous to a recess for receiving a cap is formed in an upper surface of the cylinder head. A bottom surface of the escape groove is formed into a shape tilted downwardly.
Description




CROSS-REFERENCE TO RELATED APPLICATION




The present application claims priority under 35 U.S.C. §119 to Japanese Patent Application No. 2001-213497, filed Jul. 13, 2001, the entire contents of which are hereby incorporated by reference.




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to an ignition device for a personal watercraft engine.




2. Description of Background Art




Small two-cycle engines are commonly used for personal watercraft. Typically, the ignition is disposed in a sufficient space above a cylinder head of the engine. In prior art devices, ignition current is supplied via a high-tension cord from an ignition coil disposed on a side of the watercraft body to a spark plug in a cylinder head of the engine. However, since high-tension current flows from the ignition coil to the spark plug, if water droplets adhere on a surface in the vicinity of either, current leakage may occur, and current may escape via the water droplets. Accordingly, special measures are required to prevent current leakage, for example, waterproofing high-voltage areas and arranging and waterproofing the ignition coil.




In recent years, there has been a growing demand for four-cycle personal watercraft engines to reduce environmental damage caused by exhaust gas and noise pollution. However, a disadvantage associated with four-cycle personal watercraft engines is that a four-cycle engine is substantially higher than its two-cycle counterpart with the same displacement. As a result, if a four-cycle engine is mounted in the narrow body of a personal watercraft, much less space is available above the engine than if a two-cycle engine is mounted. Clearly, it is difficult to lay a high-tension cord and the like in such a cramped space.




SUMMARY AND OBJECTS OF THE INVENTION




It is an object of the present invention is to provide an ignition device for a personal watercraft engine which allows for the mounting of a four-cycle engine and which prevents current leakage.




To achieve these objects, a personal watercraft engine ignition device is provided which includes an engine for driving a jet propelling pump disposed in the watercraft body, which body is surrounded by a hull and deck. A spark plug for spark ignition is located in a cylinder head of the engine. An ignition coil having an integral cap is provided on the spark plug, and is mounted in a watertight manner on the cylinder head, thus constituting a waterproof structure.




In one embodiment, the ignition coil is disposed on an uppermost portion of the engine at a position higher than an open opening of an intake duct for supplying air to the watercraft body.




Also included are a female case connector portion provided on the cap of the integral cap ignition coil and a recess for receiving the cap and a water-escape groove continuous to the recess formed in a upper surface of the cylinder head. The escape groove is formed so as to extend from the recess to an opening of the female case connector portion. A bottom surface of the escape groove is tilted downwardly from the recess to the opening of the female case connector portion of the cap.




As described above, the engine for driving the jet propelling pump is provided in the watercraft body surrounded by the hull and the deck, the spark plug for spark ignition is disposed in the engine cylinder head, and the integral cap ignition coil is located on the spark plug. As a result, no high voltage portion is exposed in the watercraft body.




Accordingly, even if the inside of the watercraft body gets wet, current leakage will not occur. Thus, it is possible to prevent misfiring due to current leakage and, hence, to prevent increased hydrocarbon emissions. Further, since it is not necessary to lay a high-tension cord in a space over the engine, it is possible to mount a four-cycle engine in the narrow body of a personal watercraft.




Because the integral cap ignition coil is watertightly mounted in the cylinder head, water does not enter the area around the spark plug. This makes it possible to prevent engine misfiring due to soaking by water.




In addition, the integral cap ignition coil has a waterproof structure. As a result, it is possible to prevent water from soaking the ignition coil. By keeping out water out, engine misfiring can be prevented.




Since the integral cap ignition coil is provided on an uppermost portion of the engine and located at the remotest position from the water, even if water enters the watercraft body, it is possible to more positively prevent engine misfiring due to leakage of current.




Further, the intake duct for supplying intake air in the watercraft body is provided in the watercraft body and the integral cap ignition coil is provided at a position higher than that of the opening of the intake duct formed in the watercraft body. As a result, less of the water which may be splashed into the watercraft body via the intake duct reaches the ignition coil, again preventing engine misfire due to current leakage.




As described earlier, the female case connector portion is provided on the cap of the integral cap ignition coil, the recess for receiving the cap and the water-escape groove continuous to the recess are formed in an upper surface of the cylinder head, and the escape groove is formed so as to extend from the recess to an opening of the female case connector portion. Further, a bottom surface of the escape groove is tilted downwardly from the recess to the opening of the female case connector portion of the cap. As a result of this configuration, even if water splashes around the integral cap ignition coil onto the upper portion of the engine, the water can be readily discharged via the escape groove.




Since the escape groove tilts downwardly from the recess to the opening of the female case connector portion of the cap, when water is discharged, the water is not directed toward the opening of the connector portion. This feature further contributes to preventing engine misfire due to current leakage.




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 sectional view showing one example of a personal watercraft to which one embodiment of an ignition device for a personal watercraft engine according to the present invention is applied;





FIG. 2

is a plan view of the personal watercraft shown in

FIG. 1

;





FIG. 3

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

FIG. 1

(with parts partially omitted);





FIG. 4

is a partial, enlarged sectional view mainly showing the engine


20


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 partial, perspective side view of the engine


20


; and





FIG. 7

is a plan view of the engine


20


, equivalent to the front view of

FIG. 6

, showing a cylinder head and a cover thereof.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




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




Referring to the drawings, and to

FIG. 1

in particular, a personal watercraft


10


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


12


provided on a watercraft body


11


and holds a steering handlebar


13


provided with a throttle lever.




The watercraft body


11


has a floating structure such that a hull


14


is joined to a deck


15


so as to form a space


16


therein. In space


16


, an engine


20


is mounted on the hull


14


. A jet pump or jet propelling pump


30


, functioning as propelling means to be 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 on the watercraft body


11


.




The jet pump


30


has a flow passage


33


extending from a water inlet


17


opened in a bottom of the hull


14


to both a jet port


31


opened in a rear end portion of the hull


14


and a nozzle


32


, and an impeller


34


disposed in the flow passage


33


. A shaft


35


of the impeller


34


is connected to an output shaft


20




a


of the engine


20


. When the impeller


34


is rotated by the engine


20


, water taken in via the water inlet


17


is jetted from the jet port


31


via the nozzle


32


, thus propelling the watercraft body


11


forward. 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


14


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


13


, to change a running course.





FIGS. 1-3

also show a fuel tank


40


and a storing chamber


41


.




The engine


20


is a DOHC type in-line four-cylinder/four-cycle engine, wherein as shown in

FIG. 1

, a crankshaft (see output shaft


20




a


) of the engine


20


extends along the longitudinal direction of the watercraft body


11


.




Referring to

FIG. 4

, an intake port


21


is disposed on a left side of the engine


20


in the running direction of the watercraft


11


. Further, and exhaust port


24


is disposed on a right side of the engine


20


in the running direction of the watercraft


11


.




The intake duct


22


and a surge tank (intake chamber)


23


are connected to the intake port


21


. An intercooler


50


disposed immediately under the surge tank


23


is connected to the surge tank


23


.

FIG. 4

also shows mounting brackets


52


and


53


of the intercooler


50


, to be mounted to the engine


20


.




As shown in

FIGS. 4 and 5

, the intercooler


50


includes 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


, and the outlet


51




o


is connected, via a tube


51




c


, to an intake inlet


23




a


of the surge tank


23


. The cooling unit


60


is a heat exchange unit accommodated in the case


51


(see FIG.


4


).





FIG. 5

shows cooling water hoses


91


and


92


connected to the intercooler


50


.




Referring to

FIG. 4

, an exhaust manifold


25


is connected to the exhaust port


24


of the engine


20


. Also, an exhaust outlet


25




o


(see

FIG. 5

) of the exhaust manifold


25


is connected to a turbine portion


73


of the turbo-charger


70


.




As shown is

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


, a water muffler


76


, and an exhaust/drainage pipe


77


. The anti-counterflow chamber


75


is designed to prevent the counterflow of water in cases when the watercraft turns-over.





FIG. 6

shows a spark plug


27


for spark ignition provided in each cylinder head


26


of the engine


20


, and an integral cap ignition coil


80


provided on the spark plug


27


.




The integral cap ignition coil


80


includes a cap


81


and an ignition coil portion


82


integrated with the cap


81


. The ignition coil portion


82


is electrically connected to the spark plug


27


by inserting the ignition coil portion


82


in a hole


26




a


of the cylinder head


26


and connecting a lower portion


82




a


of the ignition coil portion


82


to a head portion


27




a


of the spark plug


27


.




A switching circuit for operating the ignition coil portion


82


is contained in the cap


81


.




Referring to

FIGS. 6 and 7

, a connector portion


83


having a female case is formed on a right side surface of the cap


81


. A connector


84


having a male case, which is connected to a control circuit (not shown), is inserted in the connector portion


83


, to connect the switching circuit to the control circuit. In this case, any of a connector pin of the connector portion


83


and a connection pin of the connector


84


may be a male type pin.




With respect to the insertion hole


26




a


of the cylinder head


26


, a water-proof ring


85


is interposed between and edge portion


26




b


of the insertion hole


26




a


and a lower portion of the cap


81


, to prevent soak of water in the insertion hole


26




a


. Accordingly, the integral cap ignition coil


80


is water-tightly mounted to the cylinder head


26


of the engine


20


.




The ignition coil portion


82


is contained in a cylindrical case


82




b.


Accordingly, the integral cap ignition coil


80


has a water-proof structure.




The integral cap ignition coil


80


configured as described above is mounted to the cylinder head


26


by initially mounting the water-proof ring


85


on an upper portion of the ignition coil portion


82


(immediately under the cap


81


). Next, the ignition coil portion


82


is inserted into the hole


26




a


of the cylinder head


26


, connecting the lower portion


82




a


of the ignition coil portion


82


to the head portion


27




a


of the spark plug


27


as described above. Lastly, a flange portion


81




a


, which is integrally formed on a side surface of the front portion of the cap


81


, is fixed to the cylinder head


26


with a bolt


86


.




As is apparent from

FIGS. 4

to


7


, the integral cap ignition coil


80


is provided on an uppermost portion of the engine


20


. As is also apparent from

FIG. 1

, the integral cap ignition coil


80


is provided at position higher than that of an opening


18




a


, opened in the watercraft body, of the intake duct


18


.




Referring to

FIGS. 4

,


6


and


7


, a recess


26




c


for receiving the cap


81


is formed in an upper surface of the cylinder head


26


, and a water-escape groove


26




d


continuous to the recess


26




c


is also formed in the upper surface of the cylinder head


26


. As can be seen in

FIG. 7

, the escape groove


26




d


is formed in such a manner as to extend from the recess


26




c


to and opening


83




a


of the female case connector portion


83


of the cap


81


. As shown in

FIG. 4

, a bottom surface


26




e


of the escape groove


26




d


(part of the upper surface of the cylinder head) is tilted downwardly (in the direction from the recess


26




c


to the opening


83




a


of the female case connector portion


83


of the cap


81


).





FIG. 7

shows a breather pipe


26




f.






As summarized below, the ignition device for a personal watercraft engine configured in the present invention affords numerous effects and benefits:




(a) Since the engine


20


for driving the jet propelling pump


30


is provided in the watercraft body


11


surrounded by the hull


14


and the deck


15


, and spark plug


27


for spark ignition is provided in the cylinder head


26


of the engine


20


and integral cap ignition coil


80


is provided on the spark plug


27


, a high voltage portion is not exposed in the watercraft body


11


.




Accordingly, even if the inside of the watercraft body


11


becomes wet, leakage of current is prevented. As a result, it is possible to prevent misfire due to leakage of current, and hence to prevent an increased amount of hydrocarbon in the exhaust.




Further, since there is no requirement to lay a high-tension cord in a space over the engine


20


, it is possible to mount a four-cycle engine in the narrow watercraft


11


of a personal watercraft.




(b) Since the integral cap ignition coil


80


is water-tightly mounted in the cylinder head


26


of the engine


20


, water does not enter the area of the spark plug


27


.




Accordingly, it is possible to prevent misfiring of the engine due to soaking by water.




(c) Since the integral cap ignition coil


80


has a water-proof structure, it is possible to prevent the ignition coil


80


form getting soaked by water.




(d) Since the integral cap ignition coil


80


is provided on an uppermost portion of the engine


20


, even if water enters the watercraft body


11


, the integral cap ignition coil


80


is located at the remotest position from the water.




Accordingly, it is possible to more positively prevent engine misfiring due to leakage of current.




(e) Since the intake duct


18


for supplying intake air in the watercraft body


11


is provided in the watercraft body


11


and the integral cap ignition coil


80


is provided at a position higher than that of the opening


18




a


of the intake duct


18


, less of the water which may have entered the watercraft body


11


via the intake duct


18


is likely to reach the ignition coil


80


.




Accordingly, it is possible to more certainly prevent engine misfiring due to leakage of current.




(f) Since the water-escape groove


26




d


continuous to the recess


26




c


is formed in an upper surface of the cylinder head


26


, and the escape groove


26




d


extends from the recess


26




c


to an opening


83




a


of the female case connector portion


83


of the cap


81


, and a bottom surface


26




e


of the escape groove


26




d


is tilted downwardly in the direction from the recess


26




c


to the opening


83




a


of the female case connector portion


83


of the cap


81


, even if water is splashed around the integral cap ignition coil


80


, the water can be readily discharged from via the escape groove


26




d


. This can be clearly seen by an arrow W in FIG.


7


.




Since the escape groove


26




d


is formed tilting downwardly in the direction from the recess


26




c


to the opening


83




a


of the female case connector portion


83


of the cap


81


, when water is discharged (in the direction of arrow W), it is directed away from the opening


83




a


of the connector portion


83


.




Accordingly, it is possible to more positively prevent engine misfiring due to leakage of current.




The invention being thus described, it will be obvious that the same may be varied in may ways. Such variations are not to be regarded as a departure from the spirit and scope of the invention, and all such modification 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 ignition device of an engine for a personal watercraft, comprising:an engine for driving a jet propelling pump is provided in a watercraft body surrounded by a hull and a deck; a spark plug for spark ignition is provided in a cylinder head of said engine; and a ignition coil with integral cap is provided on said spark plug; a recess for receiving said cap; and a water escape groove continuous to said recess formed in an upper surface of said cylinder head.
  • 2. The ignition device of an engine for a personal watercraft according to claim 1, wherein said ignition coil with integral cap is water-tightly mounted in said cylinder head of said engine.
  • 3. The ignition device of an engine for a personal watercraft according to claim 1, wherein said ignition coil with integral cap has a water-proof structure.
  • 4. The ignition device of an engine for a personal watercraft according to claim 3, further comprising a water-proof ring interposed between an edge portion of an insertion hole in said cylinder head and a lower portion of a cap to prevent water from entering said insertion hole.
  • 5. The ignition device of an engine for a personal watercraft according to claim 3, further comprising a flange portion on said cap and a bolt for fixing said flange portion to said cylinder head.
  • 6. The ignition device of an engine for a personal watercraft according to claim 1, wherein said ignition coil with integral cap is provided on an uppermost portion of said engine.
  • 7. The ignition device of an engine for a personal watercraft according to claim 1, wherein an intake duct for supplying intake air in said watercraft body is provided in said watercraft body, and said ignition coil with integral cap is provided at a position higher than that of an opening, opened in said watercraft body, of said intake duct.
  • 8. The ignition device of an engine for a personal watercraft according to claim 1, further comprising:a female case shaped connector portion provided on a cap of said ignition coil with integral cap, wherein said escape groove is formed in said recess in such a manner as to extend from said recess to an opening of said female case shaped connector portion, and a bottom surface of said escape groove being tilted downwardly in the direction from said recess to the opening of said female case shaped connector portion of said cap.
  • 9. The ignition device of an engine for a personal watercraft according to claim 8, wherein said female case shaped connector portion tilts downwardly from said cap, and extends over said bottom surface of said escape groove and in a direction toward an exhaust manifold of said engine.
  • 10. An ignition device of an engine for a personal watercraft, comprising:an engine for driving a jet propelling pump is provided in a watercraft body surrounded by a hull and a deck; a spark plug for spark ignition is provided in a cylinder head of said engine; a ignition coil with integral cap is provided on said spark plug; and a female case shaped connector portion provided on said integral cap of said ignition coil with integral cap, wherein said female case shaped connector portion tilts downwardly from said cap, and extends over a bottom surface of an water escape groove formed in a recess of the cylinder head.
  • 11. The ignition device of an engine for a personal watercraft according to claim 10, wherein said ignition coil with integral cap is water-tightly mounted in said cylinder head of said engine.
  • 12. The ignition device of an engine for a personal watercraft according to claim 10, wherein said ignition coil with integral cap has a water-proof structure.
  • 13. The ignition device of an engine for a personal watercraft according to claim 12, further comprising a water-proof ring interposed between an edge portion of an insertion hole in said cylinder head and a lower portion of a cap to prevent water from entering said insertion hole.
  • 14. The ignition device of an engine for a personal watercraft according to claim 12, further comprising a flange portion on said cap and a bolt for fixing said flange portion to said cylinder head.
  • 15. The ignition device of an engine for a personal watercraft according to claim 10, wherein said ignition coil with integral cap is provided on an uppermost portion of said engine.
  • 16. The ignition device of an engine for a personal watercraft according to claim 10, wherein an intake duct for supplying intake air in said watercraft body is provided in said watercraft body, and said ignition coil with integral cap is provided at a position higher than that of an opening, opened in said watercraft body, of said intake duct.
  • 17. The ignition device of an engine for a personal watercraft according to claim 10, wherein said water escape groove is continuous to said recess formed in an upper surface of said cylinder head, said escape groove being is formed in such a manner as to extend from said recess to an opening of said female case shaped connector portion, and a bottom surface of said escape groove being tilted downwardly in the direction from said recess to the opening of said female case shaped connector portion of said cap.
  • 18. The ignition device of an engine for a personal watercraft according to claim 10, wherein said female case shaped connector portion extends tilted downwardly in a direction toward an exhaust manifold of said engine.
Priority Claims (1)
Number Date Country Kind
2001-213497 Jul 2001 JP
US Referenced Citations (3)
Number Name Date Kind
5003958 Yoneyama et al. Apr 1991 A
6250980 Ozawa Jun 2001 B1
6591819 Tscherne et al. Jul 2003 B2