Information
-
Patent Grant
-
6340322
-
Patent Number
6,340,322
-
Date Filed
Friday, January 5, 200124 years ago
-
Date Issued
Tuesday, January 22, 200222 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
- Arent, Fox, Kintner, Plotkin & Kahn, PLLC
-
CPC
-
US Classifications
Field of Search
US
- 440 1
- 440 2
- 440 88
- 440 89
-
International Classifications
-
Abstract
In an outboard engine system in which a passage defining member having a passage wall defining an exhaust gas passage for guiding an exhaust gas from an engine is provided at its outer wall with a recess and a seal surface surrounding the recess; a fluid passage isolated from the exhaust gas passage is defined between the recess and a lid member which is mounted to the outer wall of the passage defining member with a seal member interposed between the lid member and the seal surface; and an exhaust gas sampling pipe is inserted into the exhaust gas passage through an insertion bore provided in the passage defining member to open into the seal surface, it is arranged that the seal member is formed to surround an opening at an outer end of the insertion bore, and the exhaust gas sampling pipe is gas-tightly fixed in the lid member to extend through the lid member. Thus, the exhaust gas sampling pipe can be inserted into the exhaust gas passage, while avoiding an increase in size of the lid member.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to an outboard engine system in which a passage defining member having a passage wall defining an exhaust gas passage for guiding an exhaust gas from an engine is provided at an outer wall thereof with a recess and a seal surface surrounding the recess; a fluid passage isolated from the exhaust gas passage is defined between the recess and a lid member which is mounted to the outer wall of the passage defining member with a seal member interposed between the lid member and the seal surface; and an exhaust gas sampling pipe is inserted into the exhaust gas passage through an insertion bore which is provided in the passage defining member to open into the seal surface. The invention particularly relates to an improvement of a structure of mounting of the exhaust gas sampling pipe.
2. Description of the Related Art
Such an outboard engine system is conventionally known from Japanese Patent Application Laid-open No.6-144374, for example.
In the above conventionally known system, a cylinder block as the passage defining member is provided with a recess for defining a water jacket which is the fluid passage isolated from the exhaust gas passage by the passage wall. The recess is covered with the lid member, and the exhaust gas sampling pipe inserted into the exhaust gas passage is screwed into the insertion bore which opens into the seal surface. The lid member is provided with an opening for disposition of the exhaust gas sampling pipe.
With such conventionally known structure, the size of the opening provided in the lid member must be set at a large value to ensure that the interference with the exhaust gas sampling pipe can be avoided. As a result, the size of the lid member is correspondingly increased, and there is a possibility that the position of mounting of the lid member in the passage defining member may be limited.
SUMMARY OF THE INVENTION
The present invention has been accomplished with such circumstances in view, and it is an object of the present invention to provide a structure of mounting of an exhaust gas sampling pipe in an outboard engine system, wherein the exhaust gas sampling pipe can be inserted into the exhaust gas passage, while avoiding an increase in size of the lid member.
To achieve the above object, according to the present invention, there is provided a structure of mounting of an exhaust gas sampling pipe in an outboard engine system in which a passage defining member having a passage wall defining an exhaust gas passage for guiding an exhaust gas from an engine is provided at an outer wall thereof with a recess and a seal surface surrounding the recess; a fluid passage isolated from the exhaust gas passage is defined between the recess and a lid member which is mounted to the outer wall of the passage defining member with a seal member interposed between the lid member and the seal surface; and an exhaust gas sampling pipe is inserted into the exhaust gas passage through an insertion bore which is provided in the passage defining member to open into the seal surface, wherein the seal member is formed to surround an opening at an outer end of the insertion bore, and the exhaust gas sampling pipe is passed through and gas-tightly fixed in the lid member.
With such arrangement, the exhaust gas sampling pipe is gas-tightly fixed in the lid member to extend through the lid member. Therefore, the lid member may have a space enough to allow the exhaust gas sampling pipe to pass through the lid member, and the exhaust gas sampling pipe can be inserted into the exhaust gas passage, while avoiding an increase in size of the lid member. Moreover, the seal member is formed to surround the opening in the outer end of the insertion bore and hence, the passage defining member and the lid member can be reliably sealed from each other around the exhaust gas sampling pipe.
The above and other objects, features and advantages of the invention will become apparent from the following description of the preferred embodiment taken in conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIGS. 1
to
14
show an embodiment of the present invention.
FIG. 1
is a side view of the entire outboard engine system;
FIG. 2
is an enlarged vertical sectional view of an essential portion shown in
FIG. 1
;
FIG. 3
is an enlarged sectional view taken along a line
3
—
3
in
FIG. 2
with an engine cover eliminated;
FIG. 4
is an enlarged sectional view taken along a line
4
—
4
in
FIG. 2
with the engine cover eliminated;
FIG. 5
is an enlarged view of the essential portion shown in
FIG. 2
;
FIG. 6
is an enlarged sectional view taken along a line
6
—
6
in
FIG. 4
;
FIG. 7
is an enlarged sectional view taken along a line
7
—
7
in
FIG. 4
;
FIG. 8
is a sectional view taken along a line
8
—
8
in
FIG. 6
;
FIG. 9
is a sectional view taken along a line
9
—
9
in
FIG. 6
;
FIG. 10
is a cross-sectional view of an oil case, taken along a line
10
—
10
in
FIG. 11
;
FIG. 11
is a rear view of the oil case, taken in the direction of an arrow
11
in
FIG. 10
;
FIG. 12
is a front view of a lid member mounted to a rear surface of the oil case;
FIG. 13
is an enlarged vertical sectional view showing a structure of mounting of an exhaust gas sampling pipe; and
FIG. 14
is a sectional view taken along a line
14
—
14
in
FIG. 2
for explaining a structure of fixing of a lower end of an undercover to a casing.
DESCRIPTION OF THE PREFERRED EMBODIMENT
The present invention will be described by way of an embodiment with reference to the accompanying drawings. Referring first to
FIGS. 1 and 2
, a vertically extending casing
16
is mounted to a stern plate
15
a
of a hull
15
, and a 2-cylinder, 4-cycle engine E, for example, is mounted at an upper end of the casing
16
. At least an upper portion of the engine E (upper half, in this embodiment) is covered with an engine cover
13
made of a synthetic resin, and at least a lower portion, e.g., lower half of the engine E in this embodiment and an upper portion of the casing
16
are covered with an undercover
14
made of a synthetic resin. A propeller
17
is rotatably carried at a lower end of the casing
16
, so that power from the engine E is transmitted to the propeller
17
through a driving-force transmitting means
18
accommodated in the casing
16
.
The casing
16
is comprised of an oil case
19
, an extension case
20
coupled to a lower end of the oil case
19
, and a gear case
21
coupled to a lower end of the extension case
20
. The engine E has an engine body
22
, which is coupled to the oil case
19
in such a manner that a crankshaft
23
extends vertically, and the propeller
17
is rotatably carried on the gear case
21
.
The driving-force transmitting means
18
comprises a forward and backward movement switchover mechanism
26
mounted between a lower end of a drive shaft
24
connected to the crankshaft
23
and extending vertically within the casing
16
and a rear end of a propeller shaft
25
connected to the propeller
17
.
An upwardly and downwardly extending pipe-shaped swivel case
27
is disposed on a front side of the casing
16
, i.e., on a side closer to the hull
15
, and a swinging arm
28
is provided at an upper portion of the swivel case
27
to extend toward the hull
15
. On the other hand, an inversed J-shaped mounting bracket
29
is detachably attached from the above and fixed to the stern plate
15
a
of the hull
15
by tightening a setscrew
30
threadedly engaged with the mounting bracket
29
. The swinging arm
28
is pivotally supported at its front end on the mounting bracket
29
through a pivot
31
having a horizontal axis.
A plurality of pinholes
32
are provided in the mounting bracket
29
, so that the tilting angle of the casing
16
and thus the outboard engine system about the axis of the pivot
31
can be regulated by inserting a pin
34
through a pinhole (not shown) defined in a locking plate
33
secured to the swivel case
27
and through any of the pinholes
32
in the mounting bracket
29
.
A swivel shaft
35
is inserted through the swivel case
27
and rotatably supported by the swivel case
27
. A mount arm
36
is provided at an upper end of the swivel shaft
35
, and a mount block
37
is provided at a lower end of the swivel shaft
35
.
Referring also to
FIG. 3
, the oil case
19
of the casing
16
is integrally provided at an upper end of its front portion with a support arm
19
a
disposed above the mount arm
36
. The mount arm
36
is resiliently connected to the support arm
19
a
through a pair of left and right upper mounts
38
,
38
, and the mount block
37
is resiliently connected to the extension case
20
through a lower mount
39
. A steering handlebar
40
is fixed to the mount arm
36
to extend toward the hull
15
, so that the casing
16
can be turned laterally about an axis of the swivel shaft
35
by laterally operating the steering handlebar
40
to steer the outboard engine system.
Referring also to
FIGS. 4 and 5
, the engine body
22
includes an engine block
43
integrally provided with a crankcase
43
a
and coupled to an upper surface of the oil case
19
, a cylinder head
44
coupled to the engine block
43
, and a head cover
45
made of a synthetic resin and coupled to the cylinder head
44
. A valve operating chamber
46
is defined between the cylinder head
44
and the head cover
45
.
A pair of upper end lower cylinder bores
47
,
47
are provided in the engine block
43
and each have a cylinder axis extending in a longitudinal direction of the outboard engine system, and pistons
48
,
48
are slidably received in the cylinder bores
47
,
47
, respectively. On the other hand, the crankshaft
23
extending vertically within the crankcase
43
a
is rotatably supported by a support member
50
coupled to an upper portion of the crankcase
43
a
and by a lower portion of the crankcase
43
a
, and the pistons
48
,
48
are connected to the crankshaft
23
through connecting rods
49
,
49
, respectively.
A power generator
51
and a recoiled starter
52
are coaxially connected to an upper end of the crankshaft
23
protruding upwards from the support member
50
, and are covered with a common cover
53
.
A valve operating mechanism
55
including a camshaft
54
having an axis parallel to the crankshaft
23
is accommodated in the valve operating chamber
46
. The camshaft
54
is rotatably supported by the cylinder head
44
. Power is transmitted to the camshaft
54
through a belt transmitting means
56
, which comprises an endless timing belt
59
wound around a driving pulley
57
fixed to the crankshaft
23
above the support member
50
and a driven pulley
58
fixed to an upper end of the camshaft
54
above the cylinder head
44
.
A portion of the belt transmitting means
56
corresponding to the driven pulley
58
is covered with a belt cover
60
. More specifically, a side of the belt transmitting means
56
corresponding to the driving pulley
57
is covered with a cover
53
, and the belt cover
60
is disposed to cover a portion which cannot be covered with the cover
53
. A pair of arms
60
a
,
60
a
are integrally provided at a rear portion of the belt cover
60
to protrude rearwards, and pins
45
a
,
45
a
integrally provided on the head cover
45
to protrude upwards are fitted into the arms
60
a
,
60
a
with elastic members interposed therebetween, whereby the rear portion of the belt cover
60
is positioned and supported on the head cover
45
. The support member
50
is integrally provided with a support arm
50
a
extending toward the belt cover
60
, and the belt cover
60
is fastened to the support arm
50
a
and thus supported at its front portion to the support member
50
.
Referring carefully to
FIG. 3
, a pair of intake ports
62
are provided in a left side of the cylinder head
44
in an attitude to face rearwards of the outboard engine system, and can be connected to combustion chambers
61
, which are defined between the engine block
43
and the cylinder head
44
with the pistons
48
,
48
facing the combustion chambers
61
, respectively. A pair of exhaust ports
63
are provided in a right side of the cylinder head
44
in an attitude to face rearwards of the outboard engine system, and can be connected to the combustion chambers
61
.
The valve operating mechanism
55
is operable to open and close a pair of intake valves
64
for switching over the connection and disconnection between the combustion chambers
61
and the intake ports
62
and a pair of exhaust valves
65
for switching over the connection and disconnection between the combustion chambers
61
and the exhaust ports
63
. The valve operating mechanism
55
includes the camshaft
54
, a rocker shaft
66
supported by the cylinder head
44
and having an axis parallel to the camshaft
54
, a pair of intake rocker arms
67
operatively connected to the intake valves
64
and swingably carried on the rocker shaft
66
, and a pair of exhaust rocker arms
68
operatively connected to the exhaust valves
65
and swingably carried on the rocker shaft
66
.
Referring carefully to
FIG. 5
, the camshaft
54
is provided with intake cams
69
corresponding to the intake rocker arms
67
, and exhaust cams
70
corresponding to the exhaust rocker arms
68
, so that the intake valves
64
and the exhaust valves
65
are opened and closed with operational characteristics depending on cam profiles of the cams
69
and
70
by swinging the intake rocker arms
67
and the exhaust rocker arms
68
to follow the cams
69
and
70
, respectively.
An intake device
73
is connected to the intake ports
62
in the cylinder head
44
and includes a carburetor
74
disposed on one side of the engine block
43
(i.e., on a left side at an attitude to face rearwards of the outboard engine system) on a side where the intake ports
62
are disposed, an intake silencer box
75
connected to an upstream end of the carburetor
74
, and an intake manifold
76
which interconnects the upstream end of the carburetor
74
and the intake ports
62
. The intake manifold
76
is formed integrally with the cylinder head
44
and has a pair of intake passages
76
a
and
76
b
individually leading to the intake ports
62
and commonly connected to the carburetor
74
. The carburetor
74
is formed into a variable Venturi type, particularly, a so-called constant vacuum type utilizing vacuum, and has a bypass-type starting device
77
.
Referring to
FIG. 6
, the carburetor
74
has a carburetor body
78
which is provided with an intake passageway
79
communicating at its downstream end with the intake manifold
76
, and a throttle valve
80
is disposed at a downstream location in the intake passageway
79
, and a Venturi portion
81
is disposed in the intake passageway
79
at an intermediate location upstream of the throttle valve
80
.
A float chamber member
82
is coupled to the carburetor body
78
immediately below the intake passageway
79
, and a float
84
is accommodated in a float chamber
83
, which is defined between the carburetor body
78
and the float chamber member
82
. A fuel oil can be supplied from a fuel pump
72
mounted to the cylinder head
44
to the float chamber
83
.
A fuel nozzle
85
is mounted at a lower portion of the carburetor body
78
and opens into the Venturi portion
81
, so that it leads to a portion of the float chamber
83
below a fuel oil surface through a fuel jet
86
. A valve needle
87
is inserted into the fuel nozzle
85
from the above to regulate the effective opening area of the fuel nozzle
85
. The valve needle
87
is mounted at a lower end of a valve piston
88
liftably supported at an upper portion of the carburetor body
78
to vary the opening area of the Venturi portion
81
. The valve piston
88
is connected at its upper end to the central portion of a diaphragm
90
, a peripheral edge of which is sandwiched between the carburetor body
78
and a cap
89
mounted at an upper end of the carburetor body
78
.
A Venturi pressure chamber
91
is defined between the diaphragm
90
and the cap
89
, and an upstream pressure chamber
92
is defined between the diaphragm
90
and the carburetor body
78
. The Venturi pressure chamber
91
leads to the Venturi portion
81
through a communication bore (not shown) provided in a lower end of the valve piston
88
, and a return spring
93
for biasing the valve piston
88
downwards is accommodated in the Venturi pressure chamber
91
. The upstream pressure chamber
92
communicates with the inside of the intake silencer box
75
upstream of the carburetor
74
.
An air bleed pipe
94
having a large number of injection bores is connected to a lower portion of the fuel nozzle
85
, and an annular chamber
95
is defined between the air bleed pipe
94
and the carburetor body
78
to lead to the upstream pressure chamber
92
. An amount of air depending on a difference in pressure between the Venturi portion
81
and the annular chamber
95
is injected from the large number of injection bores into the air bleed pipe
94
to emulsify the fuel in the air bleed pipe
94
, thereby promoting the atomization or nebulization of the fuel injected from the fuel nozzle
85
of which effective opening area is regulated by the valve needle
87
.
In such carburetor
74
, when the amount of air drawn into the intake passageway
79
is increased to a certain value or more, the pressure in the Venturi pressure chamber
91
is dropped along with the pressure in the Venturi portion
81
, and a difference in pressure is produced between the Venturi pressure chamber
91
and the upstream pressure chamber
92
, whereby the valve piston
88
is pulled up to a position in which a pull-up force of the diaphragm
90
provided by the difference in pressure and a push-down force provided by the return spring
93
are balanced with each other, leading to an increase in opening area of the Venturi portion
81
. Thus, the pressure in the Venturi portion
81
is about to return to an original value and hence, after the amount of air drawn has reached the certain value or more, the pressure in the Venturi portion
81
is controlled to a substantially constant value.
Referring to
FIG. 7
, the carburetor body
78
is provided with a starting passage
96
, which extends around the throttle valve
80
and the Venturi portion
81
and connects the upstream end and lower end of the intake passageway
79
. The bypass-type starting device
77
is mounted to the carburetor body
78
to regulate the concentration of a fuel in an air-fuel mixture flowing through the starting passage
96
around the throttle valve
80
and the Venturi portion
81
during starting and warming of the engine E.
The bypass-type starting device
77
includes a starting fuel nozzle
97
mounted on the carburetor body
78
and opening into an intermediate portion of the starting passage
96
, a valve needle
98
inserted from the above to regulate the effective opening area of the starting fuel nozzle
97
, and a starting air bleed pipe
99
which is inserted into a starting fuel chamber
100
defined between the carburetor body
78
and the float chamber member
82
and which leads to the starting fuel nozzle
97
. The starting fuel chamber
100
has a lower end communicating with the float chamber
83
, and an upper portion communicating with the upstream air chamber
92
, and a large number of through-bores
101
are provided in the starting air bleed pipe
99
.
The bypass-type starting device
77
includes a case
102
fastened to the carburetor body
78
and extending upwards. A PTC heater and a wax (not shown) are accommodated in the case
102
, so that the valve needle
98
is lifted and lowered to regulate the effective opening area of the starting fuel nozzle
97
by heating and expanding the wax by the PTC heater. A coupler
103
is mounted at an upper end of the case
102
to perform the electric connection with PTC heater.
Such bypass-type starting device
77
is attached to the carburetor body
78
between the intake passageway
79
in the carburetor body
78
of the carburetor
74
and the engine block
43
, and the coupler
103
is disposed with its upper surface located at substantially the same level as the upper surface of the cap
89
in the carburetor
74
.
Further, another heater
104
such as a PTC heater different from the PTC heater of the bypass-type starting device
77
is embedded in the carburetor body
78
, as shown in
FIGS. 3 and 4
, so that the icing of the carburetor
74
is prevented by the heater
104
.
Referring also to
FIGS. 8 and 9
, the intake silencer box
75
is comprised of a first case member
105
made of a synthetic resin and connected to the upstream end of the carburetor
74
, a second case member
106
made of a synthetic resin and detachably connected to the first case member
105
, and a third case member
107
made of a synthetic resin and detachably connected to the second case member
106
.
The first case member
105
is integrally provided with a connecting tubular portion
105
a
connected to the upstream end of the intake passageway
79
in the carburetor
74
and extending within the first case member
105
. A frame trap
108
having a large number of through-bores is mounted to an inner end, i.e., an upstream end of the connecting tubular portion
105
a.
A first air passage
109
is defined between the first and second case members
105
and
106
for guiding air in a direction along the cylinder axis in the engine block
43
, i.e., in a direction substantially along the longitudinal direction of the outboard engine system. The first air passage
109
is connected at its downstream end to the carburetor
74
through the frame trap
108
and the connecting tubular portion
105
a.
The third case member
107
is detachably connected to an end of the second case member
106
at a longitudinally front side of the outboard engine system, and a second air passage
110
is defined in the third case member
107
to extend vertically with its upstream end, i.e., its lower end being opened to the outside. Moreover, the direction of flowing of air in the second air passage
110
is set so as to be substantially perpendicular to the direction of flowing of air in the first air passage
109
at least at the downstream end, i.e., the upper end, as shown by arrows in
FIGS. 8 and 9
, and in this embodiment, the direction of flowing of air in the second air passage
110
is set at a lateral direction of the outboard engine system.
A cleaner element
112
is disposed on a plane extending in a vertical direction of the outboard engine system substantially in parallel to the direction of flowing of the air in the first air passage
109
, and is accommodated and fixed in the intake silencer box
75
in such a manner that it is interposed between an upstream end of the first air passage
109
and a downstream end of the second air passage
110
.
The cleaner element
112
is clamped between the second and third case members
106
and
107
, and the second member
106
is integrally provided, at its portion connected to the third case member
107
, with a supporting tubular portion
106
a
of a square cross section. The supporting tubular portion
106
a
is integrally provided, at its end closer to the first air passage
109
, with a lattice portion
111
. In addition, the third case member
107
is integrally provided at its downstream end with a plurality of retaining portions
114
extending in the longitudinal direction of the outboard engine system. A frame trap
113
having a large number of through-bores is inserted into the supporting tubular portion
106
a
in such a manner to abut against the lattice portion
111
, and the cleaner element
112
is also inserted into the supporting tubular portion
106
a
in such a manner that it is sandwiched between the frame trap
113
and the retaining portions
114
.
In such intake silencer box
75
, the direction of flowing of the air at the downstream end of the second air passage
110
is set at the lateral direction of the outboard engine system, and the second air passage
110
is disposed between the cleaner element
112
disposed on the plane extending substantially in the vertical direction of the outboard engine system and the engine block
43
. One of the frame traps
108
and
113
accommodated in the intake silencer box
75
, e.g., the frame trap
108
, may be omitted.
Referring carefully to
FIG. 5
, a partition plate
117
is fixed to the head cover
45
within the valve operating chamber
46
to define a breather chamber
118
at a distance from the valve operating chamber
46
between the partition plate
117
and the head cover
45
. A reed valve
119
is mounted at a portion of the partition plate
117
facing the breather chamber
118
for permitting the flowing of a breather gas from the valve operating chamber
46
to the breather chamber
118
.
A connection pipe
120
leading to the breather chamber
118
is integrally provided in an upward rising attitude at that substantially central portion of the head cover
45
in the lateral direction of the outboard engine system, which is displaced rearwards from the belt cover
60
. A breather pipe
121
is connected at one end to the connection pipe
120
and at the other end to the first case member
105
of the intake silencer box
75
to lead to the first air passage
109
in the intake silencer box
75
in the intake device
73
.
Moreover, the breather pipe
121
is disposed above the intake manifold
76
and the carburetor
74
to extend along an outer surface of the belt cover
60
, and fixed at its intermediate portion to the outer surface of the belt cover
60
by a fixing member
122
fastened to the outer surface of the belt cover
60
.
Referring carefully to
FIG. 2
, the oil case
19
is integrally provided with an oil pan
123
, which opens upwards, i.e., toward the engine E, and an oil strainer
124
is mounted at a lower end of a suction pipe
125
inserted into the oil pan
123
.
The suction pipe
125
is connected at its upper end to an oil intake passage
126
provided in the engine block
43
and the cylinder head
44
. The oil intake passage
126
is connected to an oil pump
127
, which is mounted in the cylinder head
44
, so that it is driven by the camshaft
54
. Thus, the oil discharged from the oil pump
127
is supplied to a crankshaft support portion at a lower portion of the crankcase
43
a
and to a crankshaft support portion of the support member
50
through an oil supply passage
128
(see
FIG. 7
) provided in the engine block
43
and the support member
50
.
Referring also to
FIG. 10
, a middle of a front portion of the oil pan
123
is formed as a partition wall
123
a
curved rearwards, and an upper drive shaft chamber
130
is defined at a front portion of the oil case
19
to extend vertically and isolated from the inside of the oil pan
123
by the partition wall
123
a
. The drive shaft
24
connected to the crankshaft
23
to extend downwards is inserted into the upper drive shaft chamber
130
.
The oil pan
123
has a rear portion formed as a partition wall
123
b
extending laterally of the outboard engine system, and a first cooling wall passage
131
is defined in the oil case
19
to extend vertically in the rear of the oil pan
123
and isolated from the inside of the oil pan
123
by the partition wall
123
b
. Further, a passage wall
132
is provided integrally with the oil pan
123
in the rear of the first cooling water passage
131
to form a portion of a rear outer wall of the oil case
19
at its rear portion, and has a partition wall portion
132
a
by which the passage wall
132
is spaced apart from the first cooling wall passage
131
, and a first exhaust gas passage
133
is defined in the passage wall
132
to extend vertically.
The inside of the extension case
20
coupled to the lower end of the oil case
19
is divided by a partition wall
136
into an exhaust gas expansion chamber
134
leading to a lower end of the first exhaust gas passage
133
, and a lower drive shaft chamber
135
disposed in front of the exhaust gas expansion chamber
134
to lead to lower ends of the first cooling water passage
131
and the drive shaft chamber
130
.
Referring also to
FIG. 11
, the oil case
19
is provided at an outer wall of its rear portion with a rectangular recess
137
faced by an intermediate portion of a rear portion of the passage wall
132
defining the first exhaust gas passage
133
. The recess
137
is covered with a flat plate-shaped member
138
, and a second cooling water passage
139
is defined in the recess
137
between the oil case
19
and the plate member
138
.
A lid member
140
is fastened to the outer wall of the rear portion of the oil case
19
to sandwich the plate member
138
between the lid member
140
and the oil case
19
, and a second exhaust gas passage
141
is defined between the lid member
140
and the plate member
138
and isolated from the second cooling water passage
139
. Moreover, the plate member
138
is formed from a material having an elasticity and comes into close contact with a seal face
159
provided on the oil case
19
to surround the recess
137
, thereby performing a sealing function.
Thus, an exhaust gas discharged from the exhaust ports
63
in the cylinder head
44
is permitted to flow through a main exhaust gas passage
142
provided in the engine block
44
via the first exhaust gas passage
133
into the exhaust gas expansion chamber
134
, and discharged into the external water via a hollow portion around the propeller shaft
25
.
On the other hand, the oil case
19
is provided with a passage
143
for turning a portion of the exhaust gas from the upper portion of the exhaust gas expansion chamber
134
toward the second exhaust gas passage
141
to guide it to the second exhaust gas passage
141
. The passage
143
communicates to the second exhaust gas passage
141
.
Referring to
FIG. 12
, the second exhaust gas passage
141
includes a flow-in chamber
144
leading to the passage
143
, an upper expansion chamber
145
and a lower expansion chamber
146
. The chambers
144
,
145
and
146
are partitioned by a wall portion
140
a
provided on an inner surface of the lid member
149
. The flow-in chamber
144
is defined in a lower portion of the lid member
140
, and communicates with the upper expansion chamber
145
disposed above the flow-in chamber
144
through flow grooves
147
provided in the wall portion
140
a
. The upper expansion chamber
145
and the lower expansion chamber
146
disposed below the upper expansion chamber
145
communicate with each other through flow grooves
148
provided in the wall portion
140
a
. Moreover, the lid member
140
is integrally provided with an exhaust pipe
150
, which protrudes rearwards to define a discharge passage
149
leading to an upper portion of the inside of the lower expansion chamber
146
, so that a portion of an exhaust gas guided from the upper portion of the exhaust gas expansion chamber
134
to the second exhaust gas passage
141
flows within the second exhaust gas passage
141
and is discharged to the outside through the exhaust pipe
150
, as indicated by a broken arrow in FIG.
12
.
A return chamber
151
is defined in the lid member
140
below the flow-in chamber
144
. Moreover, a return groove
152
is provided in the wall portion
140
a
for permitting the lower end of the inside of the lower expansion chamber
146
to communicate with the return chamber
151
, so that water separated from the exhaust gas in the lower expansion chamber
136
and accumulated in the lower expansion chamber
146
is permitted to flow through the return groove
152
into the return chamber
151
. Further, a return passage
153
is provided in the oil case
19
for permitting the return chamber
151
to lead to the exhaust gas expansion chamber
134
, so that the water separated from the exhaust gas in the lower expansion chamber
146
is returned to the exhaust gas expansion chamber
134
.
On the other hand, cooling water pumped by a cooling water pump (not shown) is supplied through a cooling water inlet
154
provided in the oil case
19
to a lower portion within the second cooling water passage
139
and flows upwards within the second cooling water passage
139
and to a third cooling water passage
155
provided in the oil case
19
at a location above the cooling water inlet
154
. In this case, a baffle plate
156
is provided in the oil case
19
for allowing the cooling water to flow in a zigzag manner, as indicated by an arrow in
FIG. 11
to prevent the cooling water from flowing in the second cooling water passage
139
from the cooling water inlet
154
directly toward the third cooling water passage
155
. Thus, the cooling water can be permitted to flow all over along that portion of the passage wall
132
defining the first exhaust gas passage
133
, which faces the second cooling water passage
139
. Moreover, a communication groove
156
a
is provided in a lower end of the baffle plate
156
. When the cooling water pump is in operation, a portion of the cooling water from the cooling water inlet
154
flows upwards from the communication groove
156
a
toward the inside of the second cooling water passage
139
, as indicated by the arrow in
FIG. 11
, but when the cooling water pump is in stoppage, the cooling water can be returned from the second cooling water passage
139
via the communication groove
156
a
to the cooling water inlet
154
, thereby avoiding that the water is accumulated above the baffle plate
156
.
The cooling water flowing to the third cooling water passage
155
is introduced into a water jacket
157
(see
FIGS. 3 and 5
) provided in the engine block
43
and the cylinder head
44
, and the cooling water discharged from the water jacket
157
flows down in the first cooling water passage
131
into the lower drive shaft chamber
135
. A water-examining withdrawal pipe
158
is mounted to the oil case
19
to lead to an intermediate portion of the third cooling water passage
155
.
Referring also to
FIG. 13
, the oil case
19
is provided in its outer wall with an insertion bore
161
whose outer end opens into an upper portion of the seal surface
159
surrounding the recess
137
, and whose inner end opens into the first exhaust gas passage
133
. An exhaust gas sampling pipe
162
for sampling the exhaust gas is inserted at its inner end through the insertion bore
161
into the first exhaust gas passage
133
. The exhaust gas sampling pipe
162
is mounted to extend through the lid member
140
and is fixed air-tightly to the lid member
140
by threadedly fitting an external threaded section
164
provided on an outer surface of an intermediate portion of the exhaust gas sampling pipe
162
into a threaded bore
163
provided in the lid member
140
in correspondence to the insertion bore
161
.
A portion of the external threaded section
164
protrudes outwards from the lid member
140
, a bottomed cylindrical plug
165
is threadedly fitted over external threaded section
164
at its portion protruding from the lid member
140
to cover an outer end of the exhaust gas sampling pipe
162
. The plug
165
has an engage groove
166
provided in its outer surface at a closed end for engagement by a rotating tool such a screwdriver or the like, and a washer
167
is clamped between an open end of the plug
165
and the outer surface of the lid member
140
.
The plate member
138
is provided with a through-bore
168
corresponding to an outer end of the insertion bore
161
, and the periphery of the outer end of the insertion bore
161
is sealed by the flat plate member
138
.
Referring also to
FIG. 14
, the undercover
14
comprises a pair of cover halves
170
and
171
made of a synthetic resin connected to each other to cover lower half of the engine E and an upper portion of the casing
16
from opposite sides. One of the cover halves
170
has a fitting groove
170
a
provided in its joint surface to the other half
171
, and the other half
171
has a fitting projection
171
a
provided on its joint surface to the one cover half
170
and fitted into the fitting groove
170
a.
A notch
172
is provided at an upper end of a front portion of the undercover
14
, as shown in
FIG. 3
, and the support arm
19
a
provided on the oil case
19
is disposed in the notch
172
, so that its front end is exposed to the outside.
A through-bore
173
is provided in a portion corresponding to the exhaust pipe
150
in the rear portion of the undercover
14
with the rear end of the exhaust pipe
150
being permitted to protrude in order to discharge the exhaust gas from the exhaust passage
149
in the exhaust pipe
150
rearwards of the undercover
14
.
The undercover
14
is fixed to the upper portion of the casing
16
, and the cover halves
170
and
171
are fastened at their rear portions to a pair of mounting bosses
19
b
,
19
b
projectingly provided at the lower portion of the outer wall of the rear portion of the oil case
19
which is an upper portion of the casing
16
, by screw members
174
,
174
, respectively. Additionally, the cover halves
170
and
171
are fastened at their front portions to the upper portion of the front portion of the oil case
19
by screw members
175
, respectively, and also fastened at their front portions to the upper end of the front portion of the extension case
20
by screw members
176
, respectively. Thus, the undercover
14
is fixed to the oil case
19
which is the upper portion of the casing
16
, as well as to the upper end of the extension case
20
.
An support projection
45
b
is provided centrally at the rear portion of the head cover
45
forming a portion of the engine body
22
to protruding rearwards, and a figment
177
is embedded in the rear end of the support projection
45
b
and has a threaded bore with opposite ends opened. On the other hand, the cover halves
170
and
171
forming the undercover
14
are integrally provided in their upper areas with portions to be mounted
170
b
and
171
b
, which sandwich the support projection
45
b
from opposite sides. The portions to be mounted
170
b
and
171
b
are fastened to the support projection
45
b
by screw members
178
,
178
threadedly fitted in the figment
177
. Thus, the undercover
14
is detachably fixed at its upper portion to the head cover
45
which is a portion of the engine body
22
.
An inverted J-shaped arm
45
c
is integrally connected to the rear end of the support projection
45
b
to extend upwards from the support projection
45
b
, and a throttle cable
179
for operating the throttle valve
80
of the carburetor
74
is retained at its intermediate portion between the support projection
45
b
and the arm
45
c.
The engine cover
13
is formed from a synthetic resin into a dish shape covering upper half of the engine E, and a hook
180
is fixed to the engine cover
13
in the front portion of the outboard engine system and engaged from the rear side into an engage bore
181
provided in the front end of the support arm
19
a
of the oil case
19
. A hook lever
182
is pivotally carried at the upper portion of the undercover
14
in the rear portion of the outboard engine system for turning movement about a horizontal axis, and a hook
183
mounted on the hook lever
182
is engaged into an engage portion
184
provided at the rear portion of the engine cover
13
. Thus, the undercover
14
is detachably connected at its upper end to the lower end of the engine cover
13
.
A tilting-up grip portion
13
a
is provided at the upper portion of the engine cover
13
in the rear portion of the outboard engine system in such a manner to become recessed forwards, and an air introducing pipe
185
leading to an inner end of the grip portion
13
a
is integrally provided in the engine cover
13
to introduce air into the engine cover
13
. Moreover, the air introducing pipe
185
extends vertically immediately above the belt cover
60
with its lower end opened, and a dish-shaped portion
186
with its upper surface opened is integrally provided at the upper portion of the belt cover
60
to surround the lower end of the air introducing pipe
185
in order to avoid that water entering the belt cover
60
from the air introducing pipe
185
collides with the upper surface of the belt cover
60
to become scattered.
The operation of this embodiment will be described below. The undercover
14
fixed to the upper portion of the casing
16
is detachably fixed at its upper portion to the head cover
45
of the engine body
22
, and the engine cover
13
is detachably connected at its lower end to the upper end of the undercover
14
. Therefore, the upper portion of the undercover
14
is firmly supported on the engine body
22
, and the lower portion of the engine cover
13
is firmly supported on the engine body
22
through the upper portion of the undercover
14
. Thus, when an operator has grasped the grip portion
13
a
provided at the upper portion of the engine cover
13
to conduct the tilting-up operation, the deformation of the lower portion of the engine cover
13
and the upper portion of the undercover
14
can be suppressed to the minimum and hence, the impression of rigidity of the engine cover
13
and the undercover
14
can be obtained.
The breather pipe
121
leading to the breather chamber
118
within the head cover
45
in the engine E and connected at one end to the upper end of the head cover
45
is connected at the other end to the intake silencer box
75
of the intake device
73
disposed on one side of the engine block
43
. The breather pipe
121
is disposed along the outer surface of the belt cover
60
disposed above the cylinder head
44
to cover at least that portion of the belt transmitting means
56
interconnecting the camshaft
54
and the crankshaft
23
, which corresponds to the driven pulley
58
, and is fixed at its intermediate portion to the belt cover
60
by the fixing member
122
. Therefore, the breather pipe
121
can be disposed in proximity to the belt cover
60
to such an extent that it is in contact with the belt cover
60
, but cannot overhang sideways from the intake device
73
. Even if the engine cover
13
covering the upper half of the engine E is relatively small, the breather pipe
121
can be disposed compactly within the engine cover
13
.
The carburetor
74
of the intake device
73
is formed into the variable Venturi type, particularly, to the so-called constant vacuum type utilizing vacuum, so that the area of the opening in the Venturi portion
81
in the intake passageway
79
can be varied depending on the operational state of the engine E, thereby achieving both of low-speed and high-speed performances and at the same time, enhancing the accuracy of the air-fuel ratio and providing a reduction in fuel consumption and an enhancement in nature of the exhaust gas.
Moreover, the bypass-type starting device
77
is mounted to the carburetor body
78
of the carburetor
74
between the intake passageway
79
and the engine block
43
. Therefore, the bypass-type starting device
77
cannot overhang outwards from the carburetor body
78
, thereby avoiding an increase in size of the engine cover
13
in order to avoid any interference with the bypass-type starting device
77
.
Further, defined in the intake silencer box
75
disposed at the upstream end of the intake device
73
are the first air passage
109
connected at its downstream end to the carburetor
74
for guiding the air in the direction substantially along the cylinder axis of the engine block
43
extending in the longitudinal direction of the outboard engine system, and the second air passage
110
provided with its upstream end opened to the outside, so that the direction of flowing of the air at least in its downstream end is substantially perpendicular to the direction of flowing of the air in the first air passage
109
. The cleaner element
112
, which is disposed on the plane substantially in parallel to the direction of flowing of the air in the first air passage
109
and interposed between the upstream end of the first air passage
109
and the downstream end of the second air passage
110
, is accommodated and fixed in the intake silencer box
75
.
Therefore, the air is purified in the cleaner element
112
while flowing from the second air passage
110
to the first air passage
109
. Moreover, the first air passage
109
is provided, so that the air flows therethrough in the direction substantially along the cylinder axis of the engine block
43
, i.e., in the substantially longitudinal direction of the outboard engine system, and the cleaner element
112
is disposed in the plane substantially in parallel to the direction of flowing of the air in the first air passage
109
. Therefore, the size of the intake silencer box
75
cannot be increased in the lateral direction of the outboard engine system due to the disposition of the cleaner element
112
, and it is possible for the intake device
73
to have an air purifying function, while avoiding an increase in size of the intake device
73
.
The direction of flowing of the air in the downstream end of the second air passage
110
is set in the lateral direction of the outboard engine system, and the second air passage
110
is disposed between the engine block
43
and the cleaner element
112
disposed on the plane extending substantially vertically of the outboard engine system. Therefore, the opening at the upstream end of the intake silencer box
75
can be disposed at the location where the opening is covered with the intake silencer box
75
itself, thereby preventing, to the utmost, the water entering the engine cover
13
and the undercover
14
covering the engine E from being drawn into the intake device
73
.
The recess
137
and the seal surface
159
surrounding the recess
137
are provided on the outer wall of the oil case
19
integrally provided with the passage wall
132
defining the first exhaust gas passage
133
for guiding the exhaust gas from the engine E. The second cooling water passage
139
isolated from the first exhaust gas passage
133
and the second exhaust gas passage
141
are defined between the recess
137
and the lid member
140
mounted to the outer wall of the oil case
19
with the plate member
138
interposed between the lid member
140
and the seal surface
159
, and the exhaust gas sampling pipe
162
is inserted into the first exhaust gas passage
133
through the insertion bore
161
provided in the oil case
19
to open into the seal surface
159
. Moreover, the plate member
138
performing the sealing function is formed to surround the opening at the outer end of the insertion bore
161
, and the exhaust gas sampling pipe
162
is provided to extend through the lid member
140
and air-tightly fixed to the lid member
140
.
Therefore, the lid member
140
may have a space enough to ensure that the exhaust gas sampling pipe
162
is passed through the lid member
140
. Thus, the exhaust gas sampling pipe
162
can be inserted into the first exhaust gas passage
133
, while avoiding an increase in size of the lid member
140
, and the oil case
19
and the lid member
140
can be reliably sealed from each other around the exhaust gas sampling pipe
162
.
Moreover, a portion of the outer wall of the oil case
19
is formed by the passage wall
132
, and the recess
137
provided on the outer wall of the oil case
19
with a portion of the passage wall
132
facing the recess
137
is covered with the plate member
138
, and the second cooling water passage
139
is defined between the plate member
138
and the recess
137
. Therefore, the passage wall
132
can be cooled effectively by the cooling water flowing through the second cooling water passage
137
to prevent the rising of the temperature of the oil pan
123
integral with the passage wall
132
, and it is unnecessary to take account of a draft in the molding for forming the second cooling water passage
137
, thereby avoiding increases in size and weight of the oil case
19
.
Although the embodiment of the present invention has been described in detail, it will be understood that the present invention is not limited to the above-described embodiment, and various modifications in design may be made without departing from the spirit and scope of the invention defined in claim.
For example, the embodiment has been described in the case where the passage defining member is the oil case, but the present invention is applicable to a case where the passage defining member is an engine block, as described in Japanese Patent Application Laid-open No. 6-144374.
Claims
- 1. A structure of mounting of an exhaust gas sampling pipe in an outboard engine system in which a passage defining member having a passage wall defining an exhaust gas passage for guiding an exhaust gas from an engine is provided at an outer wall thereof with a recess and a seal surface surrounding said recess; a fluid passage isolated from the exhaust gas passage is defined between said recess and a lid member which is mounted to the outer wall of said passage defining member with a seal member interposed between the lid member and said seal surface; and an exhaust gas sampling pipe is inserted into said exhaust gas passage through an insertion bore which is provided in said passage defining member to open into said seal surface, wherein said seal member is formed to surround an opening at an outer end of said insertion bore, and said exhaust gas sampling pipe is passed through and gas-tightly fixed in said lid member.
Priority Claims (1)
Number |
Date |
Country |
Kind |
2000-010386 |
Jan 2000 |
JP |
|
US Referenced Citations (1)
Number |
Name |
Date |
Kind |
5111609 |
Fujimoto et al. |
May 1992 |
A |
Foreign Referenced Citations (2)
Number |
Date |
Country |
769290 |
Jul 1995 |
JP |
8207892 |
Aug 1996 |
JP |