Information
-
Patent Grant
-
6814034
-
Patent Number
6,814,034
-
Date Filed
Wednesday, November 19, 200320 years ago
-
Date Issued
Tuesday, November 9, 200420 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
-
CPC
-
US Classifications
Field of Search
US
- 123 48 R
- 123 48 B
- 123 78 R
- 123 78 E
- 123 78 F
-
International Classifications
-
Abstract
A variable stroke engine includes: a connecting rod connected at one end to a piston through a piston pin; a subsidiary arm turnably connected at one end to the other end of the connecting rod and connected to a crankshaft through a crankpin; and a control rod connected at one end to the subsidiary arm at a position displaced from a connection position of the connecting rod; a support position of the other end of the control rod being capable of being displaced in a plane perpendicular to an axis of the crankshaft. In the variable stroke engine, a switchover means switches over: a state in which a high expansion stroke is provided such that the stroke of the piston in an expansion stroke is larger than that in a compression stroke when an engine load is high; and a state in which a constant compression ratio is provided when the engine load is low. Thus, a reduction in fuel consumption is achieved irrespective of the level of an engine load, while putting a high value on a reduction in fuel consumption in a state in which the engine load is low.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to a variable stroke engine including: a connecting rod connected at one end to a piston through a piston pin; a subsidiary arm turnably connected at one end to the other end of the connecting rod and connected to a crankshaft through a crankpin; and a control rod connected at one end to the subsidiary arm at a position displaced from a connection position of the connecting rod; a support position of the other end of the control rod being cable of being displaced in a plane perpendicular to an axis of the crankshaft.
2. Description of the Related Art
Such an engine is conventionally known, for example, from Japanese Patent Application Laid-open No. 9-228858, U.S. Pat. No. 4,517,931 and the like, wherein the stroke of a piston in an expansion stroke is made larger than that in a compression stroke, whereby a larger expansion work is carried out in the same amount of an intake air-fuel mixture to enhance the cycle thermal efficiency.
In the above-described conventionally known engine, the stroke of the piston in the expansion stroke is made larger than that in the compression stroke irrespective of the engine load, thereby enhancing the cycle thermal efficiency. However, when the engine load is low, it is desirable that the operation of the engine is carried out while putting a high value on a reduction in fuel consumption.
SUMMARY OF THE INVENTION
The present invention has been accomplished with such circumstance in view, and it is an object of the present invention to provide a variable stroke engine, wherein a reduction in fuel consumption can be achieved irrespective of the level of the engine load, while putting a high value on a reduction in fuel consumption in a state in which the engine load is low.
To achieve the above object, the present invention provides a variable stroke engine including: a connecting rod connected at one end to a piston through a piston pin; a subsidiary arm turnably connected at one end to the other end of the connecting rod and connected to a crankshaft through a crankpin; and a control rod connected at one end to the subsidiary arm at a position displaced from a connection position of the connecting rod; a support position of the other end of the control rod being cable of being displaced in a plane perpendicular to an axis of the crankshaft, wherein the engine further includes a switchover means capable of switching over: a state in which a high expansion ratio is provided such that the stroke of the piston in an expansion stroke is larger than that in a compression stroke when an engine load is high; and a state in which a constant compression ratio is provided when the engine load is low.
With such arrangement of the invention, when the engine load is high, the high expansion ratio is provided, and when the engine load is low, the constant compression ratio is provided. Thus, it is possible to provide a reduction in fuel consumption irrespective of the engine load, while enabling the fuel consumption to be further reduced in the state in which the engine load is low.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1
is a front view of an engine according to a first embodiment of the present invention.
FIG. 2
is a sectional view taken along a line
2
—
2
in FIG.
1
.
FIG. 3
is a sectional view taken along a line
3
—
3
in FIG.
2
.
FIG. 4
is a sectional view taken along a line
4
—
4
in FIG.
3
.
FIG. 5
is an enlarged view of essential portions of FIG.
2
.
FIG. 6
is an enlarged sectional view taken along a line
6
—
6
in FIG.
5
.
FIG. 7
is an enlarged sectional view taken along a line
7
—
7
in FIG.
5
.
FIG. 8
is a sectional view taken along a line
8
—
8
in FIG.
5
.
FIG. 9
is a partially cutaway plan view taken along a line
9
—
9
in
FIG. 1
in a low load state of the engine.
FIG. 10
is a view similar to
FIG. 9
, but in a high load state of the engine.
FIG. 11
is a graph showing the relationship between the engine load and the amount of decrement in fuel consumption.
FIG. 12
is a front view of an engine according to a second embodiment of the present invention.
FIG. 13
is a sectional view taken along a line
13
—
13
in FIG.
12
.
FIG. 14
is a sectional view taken along a line
14
—
14
in FIG.
13
.
FIG. 15
is a sectional view taken along a line
15
—
15
in FIG.
13
.
FIG. 16
is an enlarged view of essential portions of FIG.
13
.
FIG. 17
is an enlarged sectional view taken along a line
17
—
17
in FIG.
16
.
FIG. 18
is an enlarged sectional view taken along a line
18
—
18
in
FIG. 16
in a high-load state of the engine.
FIG. 19
is an enlarged sectional view taken along a line
19
—
19
in
FIG. 16
in the high-load state of the engine.
FIG. 20
is a sectional view similar to
FIG. 18
, but in a low-load state of the engine.
FIG. 21
is a sectional view similar to
FIG. 19
, but in the low-load state of the engine.
FIG. 22
is a partially cutaway plan view taken along a line
22
—
22
in
FIG. 12
in the low-load state of the engine.
FIG. 23
is a view similar to
FIG. 22
, but in the high-load state of the engine.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Referring first to
FIGS. 1
to
3
, an engine is a air-cooled single-cylinder engine used in, for example, a working machine or the like, and has an engine body
21
which includes a crankcase
22
, a cylinder block
23
slightly inclined upwards and protruding from one side of the crankcase
22
, and a cylinder head
24
coupled to a head of the cylinder block
23
. A large number of air-cooling fins
23
a
and
24
a
are provided on outer surfaces of the cylinder block
23
and the cylinder head
24
. The crankcase
22
is installed, at an installation surface
22
a
on its lower surface, on a cylinder head of any of various working machines.
The crankcase
22
includes a case body
25
formed integrally with the cylinder block
23
by casting, and a side cover
26
coupled to an open end of the case body
25
. One end
27
a
of a crankshaft
27
protrudes from the side cover
26
. A ball bearing
28
and an oil seal
30
are interposed between the one end
27
a
of the crankshaft
27
and the side cover
26
. The other end
27
b
of the crankshaft
27
protrudes from the case body
25
. A ball bearing
29
and an oil seal
31
are interposed between the other end
27
b
of the crankshaft
27
and the case body
25
.
A flywheel
32
is secured to the other end
27
b
of the crankshaft
27
outside the case body
25
. A cooling fan
33
for supplying cooling air to various portions of the engine body
21
is secured to the flywheel
32
. A recoil starter
34
is disposed outside the cooling fan
33
.
A cylinder bore
39
is formed in the cylinder block
23
. A piston
38
is slidably received in the cylinder bore
39
. A combustion chamber
40
is formed between the cylinder block
23
and the cylinder head
24
, so that a top of the piston
38
faces the combustion chamber
40
.
An intake port
41
and an exhaust port
42
capable of leading to the combustion chamber
40
are formed in the cylinder head
24
. An intake valve
43
for connecting and disconnecting the intake port
41
and the combustion chamber
40
to and from each other and an exhaust valve
44
for connecting and disconnecting the exhaust port
42
and the combustion chamber
40
to and from each other are openably and closably disposed in the cylinder head
24
. A spark plug
45
is threadedly mounted to the cylinder head
24
with its electrode facing the combustion chamber
40
.
A carburetor
35
is connected to an upper portion of the cylinder head
24
. A downstream end of an intake passage
41
of the carburetor
35
communicates with the intake port
41
. An intake pipe
47
leading to an upstream end of the intake passage
46
is connected to the carburetor
35
, and also connected to an air cleaner which is not shown. An exhaust pipe
48
leading to the exhaust port
42
is connected to an upper portion of the cylinder head
24
, and also connected to an exhaust muffler
49
. Further, a fuel tank
51
is disposed above the crankcase
22
while being supported on the crankcase
22
.
A driving gear
51
and a second driving gear
52
integral with the first driving gear
51
and having an outer diameter equal to ½ of that of the first driving gear
51
, are fixedly mounted on the crankshaft
27
at positions closer to the side cover
26
of the crankcase
22
. A first driven gear
53
meshed with the first driving gear
51
is secured to a camshaft
54
which is rotatably carried in the crankcase
22
and which has an axis parallel to the crankshaft
27
. Thus, a rotating power from the crankshaft
27
is transmitted at a reduction ratio of 1/2 to the camshaft
54
by the first driving gear
51
and the first driven gear
53
meshed with each other.
An intake cam
55
and an exhaust cam
56
corresponding to the intake valve
43
and the exhaust valve
44
respectively are provided on the camshaft
54
. A follower piece operably carried in the cylinder block
23
is in sliding contact with the intake cam
55
. On the other hand, an operating chamber
58
is formed in the cylinder block
23
and the cylinder head
24
, so that an upper portion of the follower piece
57
protrudes into a lower portion of the operating chamber
58
. A lower end of a pushrod
59
disposed in the operating chamber
58
is in abutment against the follower piece
57
. On the other hand, a rocker arm
60
is swingably carried in the cylinder head
24
with one end abutting against an upper end of the intake valve
43
biased in a closing direction by a spring. An upper end of the pushrod
59
is in abutment against the other end of the rocker arm
60
. Thus, the pushrod
59
is operated axially in response to the rotation of the intake cam
55
. The intake valve
43
is opened and closed by the swinging movement of the rocker arm caused in response to the operation of the pushrod
59
.
A mechanism similar to that between the intake cam
55
and the intake valve
43
is also interposed between the exhaust cam
56
and the exhaust valve
44
, so that the exhaust valve
44
is opened and closed in response to the rotation of the exhaust cam
56
.
Referring also to
FIG. 4
, the piston
38
, the crankshaft
27
and an eccentric shaft
61
carried in the crankcase
22
of the engine body
21
for displacement in a plane passing through a cylinder axis C and perpendicular to the axis of the crankshaft
27
, are connected to one another through a link mechanism
62
.
The link mechanism
62
includes: a connecting rod
64
connected at one end to the piston
38
through a piston pin
63
; a subsidiary rod
68
connected to the crankshaft
27
through a crankpin
65
and turnably connected to the other end of the connecting rod
64
; and a control rod
69
which is turnably connected at one end to the subsidiary rod
68
at a position displaced from a connection position of the connecting rod
64
. The control rod
69
is turnably supported at the other end on the eccentric shaft
61
so that the support position can be displaced in a plane perpendicular to the axis of the crankshaft
27
.
Referring also to
FIG. 5
, the subsidiary rod
68
has, at its intermediate portion, a first semicircular bearing portion
70
which is in sliding contact with a half of a periphery of the crankpin
65
. A pair of bifurcations
71
and
72
are provided integrally at opposite ends of the subsidiary rod
68
, so that the other end of the connecting rod
64
and one end of the control rod
69
are sandwiched between the bifurcations
71
and
72
. A second semicircular bearing portion
74
of a crank cap
73
is in sliding contact with the remaining half of the periphery of the crankpin
65
. The crank cap
73
is fastened to the subsidiary rod
68
.
The connecting rod
64
is turnably connected at the other end to one end of the subsidiary rod
68
through a cylindrical connecting rod pin
75
. The subsidiary rod pin
75
press-fitted into the other end of the connecting rod
64
is turnably fitted at its opposite ends into the bifurcation
71
located at the one end of the subsidiary rod
68
.
The control rod
69
is turnably connected at one end to the other end of the subsidiary rod
68
through a cylindrical connecting rod pin
76
. The connecting rod pin
76
is relatively turnably passed through one end of the control rod
69
which is inserted into the bifurcation
72
located at the other end of the subsidiary rod
68
. The connecting rod pin
76
is clearance-fitted at its opposite ends into the bifurcation
72
located at the other end. Moreover, a pair of clips
77
,
77
are mounted to the bifurcation
72
located at the other end, and abuts against opposite ends of the subsidiary rod pin
76
to inhibit the disengagement of the subsidiary rod pin
76
from the bifurcation
72
.
Further, the crank cap
73
is fastened to the bifurcations
71
and
72
by pairs of bolts
78
disposed on opposite sides of the crankshaft
27
. The connecting rod pin
75
and the subsidiary rod pin
76
are disposed on extensions of axes of the bolts
78
.
The cylindrical eccentric shaft
61
is integrally provided at an eccentric position on a rotary shaft
81
turnably carried in the crankcase
22
of the engine body
21
and having an axis parallel to the crankshaft
27
. The rotary shaft
81
is turnably carried at one end on the side cover
26
of the crankcase
22
with a ball bearing
83
interposed therebetween, and also carried at the other end on the case body
25
of the crankcase
22
with a ball bearing
84
interposed therebetween.
A second driven gear
85
formed to have the same diameter as the first driving gear
51
and meshed with the first driving gear
51
is relatively rotatably carried on the rotary shaft
81
. A third driven gear
86
meshed with the second riving gear
52
and having an outer diameter two times that of the second driving gear
52
is mounted on the rotary shaft
81
through a one-way clutch
87
. The one-way clutch
87
permits the transmission of the rotating power from the third driven gear
86
to the rotary shaft
81
, but disables the transmission of the rotating power from the rotary shaft
81
to the third driven gear
86
.
The following states are switched over from one to another by a switchover means
88
: a state in which the power is transmitted from the crankshaft
27
through the second driving gear
52
, the third driven gear
86
and the one-way clutch
87
to the rotary shaft
81
, i.e., a state in which the rotating power is transmitted at a reduction ratio of 1/2 from the crankshaft
27
to the rotary shaft
81
; and a state in which the power is transmitted from the crankshaft
27
through the first driving gear
51
and the second driven gear
85
to the rotary shaft
81
, i.e., a state in which the rotating power is transmitted at a constant speed from the crankshaft
27
to the rotary shaft
81
. The switchover means
88
is adapted to switch over the following states in accordance with the engine load: a state in which the rotating power is transmitted at the reduction ratio of 1/2 from the crankshaft
27
to the rotary shaft
81
in order to provide a high expansion ratio in which the stroke of the piston
38
in an expansion stroke is larger than that in a compression stroke when the engine load is high; and a state in which the rotating power is transmitted at a constant speed from the crankshaft
27
to the rotary shaft
81
in order to provide a constant compression ratio when the engine load is low.
Referring also to
FIG. 6
, the switchover means
88
includes: a ratchet slider
89
which is carried axially slidably and relatively non-rotatably about an axis on the rotary shaft
81
so that it is brought alternatively into engagement with one of the second and third driven gears
85
and
86
; a shifter
90
which is carried axially slidably and relatively non-rotatably about an axis on the rotary shaft
81
; a transmitting shaft
91
which is axially slidably fitted into the rotary shaft
81
so that the axial movement of the shifter
90
is transmitted to the ratchet slider
89
; a turn shaft
92
carried in the case body
25
of the crankcase
22
for turning about an axis perpendicular to the rotary shaft
81
; a shift fork
93
fixed to the turn shaft
92
to embrace the shifter
90
; and a diaphragm-type actuator
94
connected to the turn shaft
92
.
Referring to
FIGS. 7 and 8
, the ratchet slider
89
is spline-coupled to the rotary shaft
81
between the second and third gears
85
and
86
. A first engagement projection
95
is integrally provided on a face of the ratchet slider
89
which is opposed to the second driven gear
85
. A second engagement projection
96
is integrally provided on a face of the ratchet slider
89
which is opposed to the third driven gear
86
.
On the other hand, the second driven gear
85
is integrally provided with a first locking portion
98
which is adapted to be brought into engagement with the first engagement projection
95
of the ratchet slider
89
slid toward the second driven gear
85
in response to the rotation of the second driven gear
85
in a rotational direction shown by an arrow
97
by the transmission of the rotating power from the crankshaft
27
. The third driven gear
86
is integrally provided with a second locking portion
99
which is adapted to be brought into engagement with the second engagement projection
96
of the ratchet slider
89
slid toward the third driven gear
86
in response to the rotation of the third driven gear
86
in a rotational direction shown by an arrow
97
by the transmission of the rotating power from the crankshaft
27
.
Namely, when the ratchet slider
89
is slid toward the second driven gear
85
, the rotating power from the crankshaft
27
is transmitted at a constant speed through the first driving gear
51
, the second driven gear
85
and the ratchet slider
89
to the rotary shaft
81
. In this process, the third driven gear
86
is raced by the action of the one-way clutch
87
. When the ratchet slider
89
is slid toward the third driven gear
86
, the rotating power from the crankshaft
27
is reduced at a reduction ratio of 1/2 and transmitted through the second driving gear
52
, the third driven gear
86
and the ratchet slider
89
to the rotary shaft
81
. In this process, the second driven gear
85
is raced.
The shifter
90
is spline-coupled to the rotary shaft
81
at a position where the second driven gear
85
is sandwiched between the shifter
90
and the ratchet slider
89
. An annular groove
100
is provided around an outer periphery of the shifter
90
.
A slide bore
101
is provided in the rotary shaft
81
to coaxially extend from one end of the rotary shaft
81
to a point corresponding to the shifter
90
. The transmitting shaft
91
is slidably fitted in the slide bore
101
. The transmitting shaft
91
and the shifter
90
are connected to each other by a connecting pin
102
having an axis extending along one diametrical line of the rotary shaft
81
, so that the transmitting shaft
91
is slid axially in the slide bore
101
in response to the axial sliding of the shifter
90
. Moreover, an elongated bore
103
for permitting the movement of the connecting pin
102
in response to the axial sliding of the shifter
90
and the transmitting shaft
91
is provided in the rotary shaft
81
so that the connecting pin
102
is inserted through the elongated bore
103
. Further, the transmitting shaft
91
and the ratchet slider
89
are connected to each other by a connecting pin
104
having an axis extending along one diametrical line of the rotary shaft
81
, so that the ratchet slider
89
is slid axially in response to the axial movement of the transmitting shaft
91
. Moreover, an elongated bore
105
for permitting the movement of the connecting pin
104
in response to the axial sliding of the transmitting shaft
91
and the ratchet slider
89
is provided in the rotary shaft
81
so that the connecting pin
104
is inserted through the elongated bore
105
.
A bottomed cylindrical shaft-supporting portion
108
and a cylindrical shaft-supporting portion
109
are integrally provided on the case body
25
of the crankcase
22
so that they are opposed to each other at a distance on the same axis perpendicular to the axis of the rotary shaft
81
. The turn shaft
92
with one end disposed on the side of the shaft-supporting portion
108
is turnably carried on the shaft-supporting portions
108
and
109
, and the other end of the turn shaft
92
protrudes outwards from the shaft-supporting portion
109
.
The shift fork
93
is fixed to the turn shaft
92
between the shaft-supporting portions
108
and
109
by a pin
110
, and engaged in the annular groove
100
in the shifter
90
. Therefore, the shifter
90
is slid in an axial direction of the rotary shaft
81
by turning the shift fork
93
along with the turn shaft
92
, whereby the alternative engagement of the ratchet slider
89
with the second or third driven gears
85
or
86
is switched over.
Referring also to
FIG. 9
, the actuator
94
includes: a casing
112
mounted to a support plate
111
fastened to an upper portion of the case body
25
of the crankcase
22
; a diaphragm
115
supported in the casing
112
to partition the inside of the casing
112
into a negative pressure chamber
113
and an atmospheric pressure chamber
114
; a spring
116
mounted under compression between the casing
112
and the diaphragm
115
to exhibit a spring force in a direction to increase the volume of the negative pressure chamber
113
; and an actuating rod
117
connected to a central portion of the diaphragm
115
.
The casing
112
includes: a bowl-shaped first case half
118
mounted to the support plate
111
; and a bowl-shaped second case half
119
connected by crimping to the case half
118
. A peripheral edge of the diaphragm
115
is clamped between open ends of the case halves
118
and
119
. The negative pressure chamber
113
is defined between the diaphragm
115
and the second case half
119
, and accommodates the spring
116
therein.
The atmospheric pressure chamber
114
is defined between the diaphragm
115
and the first case half
118
. The actuating rod
117
protrudes into the atmospheric pressure chamber
114
through a through-bore
120
provided in a central portion of the first case half
118
, and is connected at one end to a central portion of the diaphragm
115
. The atmospheric pressure chamber
114
communicates with the outside through a clearance between an inner periphery of the through-bore
120
and an outer periphery of the actuating rod
117
.
A conduit
121
leading to the negative pressure chamber
113
is connected to the second case half
119
of the casing
112
, and also connected to a downstream end of the intake passage
46
in the carburetor
35
. Namely, an intake negative pressure in the intake passage
46
is introduced into the negative pressure chamber
113
in the actuator
94
.
The other end of the actuating rod
117
of the actuator
94
is connected to a driving arm
122
carried on the support plate
111
for turning about an axis parallel to the turn shaft
92
. A driven arm
123
is fixed to the other end of the turn shaft
92
protruding from the crankcase
22
. The driving arm
122
and the driven arm
123
are connected to each other through a connecting rod
124
. A spring
125
is mounted between the driven arm
123
and the support plate
111
for biasing the driven arm
123
to turn in a clockwise direction in FIG.
9
.
When the engine is in a low-load operational state in which the negative pressure in the negative pressure chamber
113
is high, the diaphragm
115
is flexed to decrease the volume of the negative pressure chamber
113
against spring forces of the return spring
116
and the spring
125
, so that the actuating rod
117
is contracted, as shown in FIG.
9
. In this state, the turned positions of the turn shaft
92
and the shift fork
93
are positions in which the first engagement projection
95
of the ratchet slider
89
is in abutment and engagement with the first locking portion of the second driven gear
85
.
On the other hand, when the engine is brought into a high-load operational state in which the negative pressure in the negative pressure chamber
113
is low, the diaphragm
115
is flexed to increase the volume of the negative pressure chamber
113
by the spring forces of the return spring
116
and the spring
125
, so that the actuating rod
108
is expanded, as shown in FIG.
10
. Thus, the turn shaft
92
and the shift fork
93
are turned to the positions at which the second engagement projection
96
of the ratchet slider
89
is in abutment and engagement with the second locking portion
99
of the third driven gear
86
.
By turning the shift fork
93
by the actuator
94
in the above manner, the rotating power from the crankshaft
27
is transmitted at the constant speed to the rotary shaft
81
during the low-load operation of the engine, and the rotating power from the crankshaft
27
is reduced at the reduction ratio of 1/2 and transmitted to the rotary shaft
81
during the high-load operation of the engine.
The operation of the first embodiment will be described below. During the high-load operation of the engine, the eccentric shaft
61
is rotated at a rotational speed equal to ½ of that of the crankshaft
27
about the axis of the rotary shaft
81
. Therefore, the position of the other end of the control rod
69
in the link mechanism
62
can be displaced at 180 degree about the axis of the rotary shaft
81
in the expansion stroke and the compression stroke, thereby providing a high expansion ratio in which the stroke of the piston
38
in the expansion stroke is larger than that in the compression stroke, when the engine load is high.
On the other hand, during the low-load operation of the engine, the eccentric shaft
61
is rotated at the speed equal to that of the crankshaft
27
about the axis of the rotary shaft
81
. Therefore, when the engine load is low, the stroke of the piston
38
can be made constant, and the compression ratio can be made constant.
If the high-load ratio operation, in which the stroke of the piston in the expansion stroke is larger than that in the compression stroke irrespective of the engine load, is carried out, the amount of decrement in fuel consumption can be relatively increased irrespective of the engine load, as shown by a dashed line in FIG.
11
. However, according to the present invention, if the compression ratio is made constant when the engine load is low, the fuel consumption can be further reduced in a state in which the engine load is low, as shown by a solid line in FIG.
11
. Thus, it is possible to further reduce the fuel consumption, when the load of the engine is low, while providing a reduction in fuel consumption in a state in which the engine load is high.
FIGS. 12
to
23
show a second embodiment of the present invention. In the description of the second embodiment of the present invention with reference to
FIGS. 12
to
23
, portions or components corresponding to those in the first embodiment shown in
FIGS. 1
to
11
are designated by the same numerals and symbols, and the detailed description of them is omitted.
Referring to
FIGS. 12
to
16
, a crankshaft
22
′ of an engine body
21
′ includes a case body
25
′ formed integrally with a cylinder block
23
by casting, and a side cover
26
coupled to an open end of the case body
25
′. A third driving gear
131
is fixedly mounted on the crankshaft
27
at a position closer to the side cover
26
of the crankcase
22
′, and meshed with the first driven gear
53
secured to the camshaft
54
. Thus, the rotating power from the crankshaft
27
is transmitted at a reduction ratio of 1/2 to the camshaft
54
by the third driving gear
131
and the first driven gear
53
meshed with each other.
A piston
38
and the crankshaft
27
are connected to the each other through a link mechanism
62
. The link mechanism
62
includes: a connecting rod
64
connected at one end to the piston
38
through a piston pin
63
; a subsidiary rod
68
connected to the crankshaft
27
through a crank pin
65
and also turnably connected to the other end of the connecting rod
64
; and a control rod
69
turnably connected at one end to the subsidiary rod
68
at a position displaced from a connection position of the connecting rod
64
. The other end of the control rod
69
is turnably supported at a support position capable of being displaced in a plane perpendicular to the axis of the crankshaft
27
.
An eccentric shaft
61
′ is integrally provided at an eccentric position on a rotary shaft
81
which is rotatably carried in the crankcase
22
′ of the engine body
21
′ with ball bearings
83
and
84
interposed therebetween and which has an axis parallel to the crankshaft
27
. The eccentric shaft
61
′ is relatively rotatably passed through the other end of the control rod
69
.
A fourth driven gear
132
having an outer diameter two times that of the third driving gear
131
and adapted to be meshed with the third driving gear
131
, is relatively non-rotatably mounted on the rotary shaft
81
′. Thus, during operation of the engine, the rotating power from the crankshaft
27
is always transmitted at a reduction ratio of 1/2 to the rotary shaft
81
′.
The support center of the other end of the control rod
69
in the link mechanism
62
is switched over by a switchover means
133
between a state in which it has been displaced from the axis of the rotary shaft
81
′, i.e., from the rotational center in a plane perpendicular to the axis of the rotary shaft
81
′, and a state in which it is aligned with the axis of the rotary shaft
81
′, i.e., from the rotational center. The switchover means
133
is adapted to switch over the following states in accordance with the engine load: a state in which the support center of the other end of the control rod
69
is displaced from the rotational center of the rotary shaft
81
′ in order to provide a high expansion ratio in which the stroke of the piston
38
in an expansion stroke is larger than that in a compression stroke when the engine load is high; and a state in which the support center of the other end of the control rod
69
is aligned with the rotational center of the rotary shaft
81
′ in order to provide a constant compression ratio when the engine load is low.
Referring also to
FIG. 17
, the switchover means
133
includes: an eccentric sleeve
134
having an outer periphery which is eccentric from the eccentric shaft
61
′ and surrounding the eccentric shaft
61
′; a one-way clutch
139
interposed between the eccentric sleeve
134
and the eccentric shaft
61
′; a ratchet slider
136
which is carried on the rotary shaft
81
′ for sliding in an axial direction and for relative non-rotation about an axis, so that it can be brought into engagement with the eccentric sleeve
134
alternatively at two points whose rotated phases are different from each other; a shifter
137
relatively non-rotatably connected to the ratchet slider
136
and surrounding the eccentric sleeve
134
; a turn shaft
92
′ carried in the case body
25
′ of the crankcase
22
′ for turning about an axis perpendicular to the rotary shaft
81
′; a shift fork
138
fixed to the turn shaft
92
′ and connected to the shifter
137
; and a diaphragm-type actuator
94
connected to the turn shaft
92
′. The one-way clutch
139
is interposed between the other end of the control rod
69
in the link mechanism
62
and the eccentric sleeve
134
.
When the other end of the control rod
69
is turned about the eccentric sleeve
134
in response to the sliding of the piston
38
in the cylinder bore
39
, the one-way clutch
139
transmits the turning force, in a direction opposite from the a direction
140
of the rotation of the rotary shaft
81
′, from the control rod
69
to the eccentric sleeve
134
, but does not transmit the turning force in the same direction as the rotational direction
140
from the control rod
69
to the eccentric sleeve
134
, nor the turning power from the rotary shaft
81
′ to the eccentric sleeve
134
.
The eccentric sleeve
134
is integrally provided with a cylindrical portion
134
a
which extends coaxially with the eccentric shaft
61
′ and towards the ratchet slider
136
. The one-way clutch
139
is interposed between the cylindrical portion
134
a
and the eccentric shaft
61
′.
A load in a direction to compress the control rod
69
and a load in a direction to expand the control rod
69
are applied alternately to the control rod
69
depending on the operation cycle of the engine. When the eccentric sleeve
134
is at the eccentric position on the rotary shaft
81
′, the rotating force from the control rod
69
toward one side and the rotating force toward the other side are also applied alternately to the control rod
69
. Therefore, because the one-way clutch
139
is interposed between the eccentric sleeve
134
and the eccentric shaft
61
′, the eccentric sleeve
134
can be turned only in the direction opposite from the rotational direction
140
of the rotary shaft
81
′ depending on the application of the force from the control rod
69
.
A third engagement projection
141
is integrally formed at an end of the cylindrical portion
134
a
of the eccentric sleeve
134
closer to the ratchet slider
136
, to protrude radially outwards at circumferentially one point.
On the other hand, the ratchet slider
136
is spline-coupled to the rotary shaft
81
′ between the cylindrical portion
134
a
of the eccentric sleeve
134
and the fourth driven gear
132
. Third and fourth locking portions
142
and
143
capable of being engaged alternatively with the third engagement projection
141
are integrally provided on a surface of the ratchet slider
136
opposed to the cylindrical portion
134
a.
Referring to
FIG. 18
, the third locking portion
142
is provided on an outer periphery of the ratchet slide
136
, so that it is brought into engagement with the third engagement projection
141
in response to the rotation of the ratchet slider
136
slid toward the fourth driven gear
132
in the rotational direction
140
by the transmission of the rotating power from the crankshaft
27
.
In a state in which the third locking portion
142
has been brought into engagement with the third engagement projection
141
in the above manner, the rotational center C
1
of the rotary shaft
81
′, the center C
2
of the eccentric shaft
61
′ and the center of the eccentric sleeve
134
, i.e., the support center C
3
of the other end of the control rod
69
are at relative positions shown in FIG.
19
. If the distance between the rotational center C
1
of the rotary shaft
81
′ and the center C
2
of the eccentric shaft
61
′ is represented by B, the distance A between the rotational center C
1
of the rotary shaft
81
′ and the support center C
3
of the other end of the control rod
69
is set so that an equation, A=B×2 is established.
Referring to
FIG. 20
, the fourth locking portion
143
is provided on an inner periphery of the ratchet slider
136
, so that it is brought into engagement with the third engagement projection
141
in response to the rotation of the ratchet slider
136
slid toward the eccentric sleeve
134
in the rotational direction
140
by the transmission of the rotating power from the crankshaft
27
.
In a state in which the fourth locking portion
143
has been brought into engagement with the third engagement projection
141
in the above manner, the rotational center C
1
of the rotary shaft
81
′, the center C
2
of the eccentric shaft
61
′ and the center of the eccentric sleeve
134
, i.e., the support center C
3
of the other end of the control rod
69
are at relative positions shown in
FIG. 21
, and the rotational center C
1
of the rotary shaft
81
′ and the support center C
3
of the other end of the control rod
69
are at the same position. Namely, the third and fourth locking portions
142
and
143
are provided on the ratchet slider
136
at positions whose rotated phases are different from each other by 180 degree.
A bottomed cylindrical shaft-supporting portion
144
and a cylindrical shaft-supporting portion
145
are integrally provided on the case body
25
′ of the crankcase
22
′ so that they are opposed to each other at a distance on the same axis perpendicular to the axis of the rotary shaft
81
′. The turn shaft
92
′ with one end disposed on the side of the shaft-supporting portion
144
is turnably carried on the shaft-supporting portions
144
and
145
, and the other end of the turn shaft
92
′ protrudes outwards from the shaft-supporting portion
145
.
The shift fork
138
is fixed by a pin
146
to the turn shaft
92
′ between the shaft-supporting portions
144
and
145
. A pair of pins
148
,
148
are embedded in the shift fork
138
so that they are engaged in an annular grooves
147
provided around the outer periphery of the shifter
137
. Therefore, the shifter
137
is slid in an axial direction of the rotary shaft
81
′ by turning the shift fork
138
along with the turn shaft
92
′, whereby the alternative engagement of the third engagement projection
141
with the third or fourth locking portions
142
or
143
of the ratchet slider
136
is switched over.
Referring also to
FIG. 22
, the actuating rod
117
of the actuator
94
is connected to a driving arm
122
which is carried on a support plate
111
for turning about an axis parallel to the turn shaft
92
′. A drive arm
123
is fixed to the other end of the turn shaft
92
′ protruding from the crankcase
22
′. The driving arm
122
and the driven arm
123
are connected to each other through a connecting rod
124
. A spring
125
for biasing the driven arm
123
to turn in a clockwise direction in
FIG. 22
is mounted between the driven arm
123
and the support plate
111
.
When the engine is in a low-load operational state in which the negative pressure in the negative pressure chamber is high, the diaphragm
115
has been flexed to decrease the volume of the negative pressure chamber
113
against the spring forces of the return spring
116
and the spring
125
, so that the actuating rod
117
is contracted, as shown in FIG.
22
. In this state, the turn shaft
92
′ and the shift fork
138
are at turned positions in which the ratchet slider
136
is in proximity to the eccentric sleeve
134
so that the third engagement projection
141
is engaged with the fourth locking portion
143
.
On the other hand, when the engine is brought into a high-load operational state in which the negative pressure in the negative pressure chamber is low, the diaphragm
115
is flexed to increase the volume of the negative pressure chamber
113
by the spring forces of the return spring
116
and the spring
125
, so that the actuating rod
117
is expanded. Thus, the turn shaft
92
′ and the shift fork
138
are at turned positions in which the ratchet slider
136
is in proximity to the fourth driven gear
132
so that the third engagement projection
141
is engaged with the third locking portion
143
.
By turning the shift fork
138
by the actuator
94
in the above manner, the turning power of the crankshaft
27
is reduced to ½ and transmitted to the rotary shaft
81
′ in a state in which the support center C
3
of the other end of the control rod
69
is aligned with the axis of the rotary shaft
81
′, i.e., the rotational center C
1
, during the low-load operation of the engine, and the turning power of the crankshaft
27
is reduced to ½ and transmitted to the rotary shaft
81
′ in a state in which the support center C
3
of the other end of the control rod
69
is displaced from the axis of the rotary shaft
81
′, i.e., the rotational center C
1
, during the high-load operation of the engine.
The operation of the second embodiment will be described below. During the high-load operation of the engine, the eccentric shaft
61
′ is rotated at a rotational speed equal to ½ of that of the crankshaft
27
about the axis of the rotary shaft
81
′ in the state in which the support center C
3
of the other end of the control rod
69
is displaced from the axis of the rotary shaft
81
′, i.e., the rotational center C
1
. Therefore, the position of the other end of the control rod
69
in the link mechanism
62
can be displaced through 180 degree about the axis of the rotary shaft
81
′ in the expansion stroke and the compression stroke, thereby providing a high expansion ratio in which the stroke of the piston
38
in the expansion stroke is larger than the stroke in the compression stroke, when the engine load is high.
On the other hand, during the low-load operation of the engine, the eccentric shaft
61
′ is rotated at a rotational speed equal to ½ of that of the crankshaft
27
about the axis of the rotary shaft
81
′ in the state in which the support center C
3
of the other end of the control rod
69
is aligned with the axis of the rotary shaft
81
′, i.e., the rotational center C
1
. Therefore, when the engine load is low, the high compression ratio can be made constant.
In this way, the engine can be operated at the constant compression ratio when the engine load is low, and the engine can be operated at the high expansion ratio when the engine load is high. Thus, it is possible to further reduce the fuel consumption in the state in which the engine load is low, while providing a reduction in fuel consumption in the state in which the engine load is high.
In the second embodiment, the third and fourth locking portions
142
and
143
are provided on the ratchet slider
136
at the locations whose rotated phases are different from each other by 180 degree, but in the low-load operational state of the engine, a difference between the rotated phases of the third and fourth locking portions
142
and
143
may be set at a value smaller than 180 degree, while ensuring that the support center C
3
of the other end of the control rod
69
is aligned with the axis of the rotary shaft
81
′, i.e., the rotational center C
1
.
Although the embodiments of the present invention have been described, it will be understood that the present invention is not limited to the above-described embodiments, and various modifications in design may be made without departing from the subject matter of the invention defined in the claims.
Claims
- 1. A variable stroke engine including: a connecting rod connected at one end to a piston through a piston pin; a subsidiary arm turnably connected at one end to the other end of the connecting rod and connected to a crankshaft through a crankpin; and a control rod connected at one end to the subsidiary arm at a position displaced from a connection position of the connecting rod; a support position of the other end of the control rod being capable of being displaced in a plane perpendicular to an axis of the crankshaft,wherein the engine further includes a switchover means capable of switching over: a state in which a high expansion ratio is provided such that the stroke of the piston in an expansion stroke is larger than that in a compression stroke when an engine load is high; and a state in which a constant compression ratio is provided when the engine load is low.
Priority Claims (2)
Number |
Date |
Country |
Kind |
2002-336292 |
Nov 2002 |
JP |
|
2003-270282 |
Jul 2003 |
JP |
|
US Referenced Citations (2)
Number |
Name |
Date |
Kind |
1786423 |
Cady |
Dec 1930 |
A |
4517931 |
Nelson |
May 1985 |
A |
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Number |
Date |
Country |
1 197 647 |
Oct 2001 |
EP |
1 215 380 |
Dec 2001 |
EP |
9-228858 |
Sep 1997 |
JP |