Information
-
Patent Grant
-
6810869
-
Patent Number
6,810,869
-
Date Filed
Wednesday, July 3, 200222 years ago
-
Date Issued
Tuesday, November 2, 200420 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
- Birch, Stewart, Kolasch & Birch, LLP
-
CPC
-
US Classifications
Field of Search
US
- 123 143 C
- 123 169 PA
- 123 634
- 123 635
- 123 647
- 336 96
- 440 88 R
-
International Classifications
-
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 |
|
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Number |
Name |
Date |
Kind |
5003958 |
Yoneyama et al. |
Apr 1991 |
A |
6250980 |
Ozawa |
Jun 2001 |
B1 |
6591819 |
Tscherne et al. |
Jul 2003 |
B2 |