Information
-
Patent Grant
-
6716076
-
Patent Number
6,716,076
-
Date Filed
Tuesday, July 9, 200222 years ago
-
Date Issued
Tuesday, April 6, 200420 years ago
-
Inventors
-
Original Assignees
-
Examiners
- Morano; S. Joseph
- Vasudeva; Ajay
Agents
- Birch, Stewart, Kolasch & Birch, LLP
-
CPC
-
US Classifications
Field of Search
US
- 440 38
- 440 75
- 440 83
- 440 111
- 440 112
- 123 1921
- 123 1922
- 464 104
- 464 105
- 464 179
- 464 182
- 464 183
-
International Classifications
-
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)
Foreign Referenced Citations (2)
Number |
Date |
Country |
2880691 |
Jan 1999 |
JP |
2002227696 |
Aug 2002 |
JP |