Variable stroke engine

Information

  • Patent Grant
  • 6814034
  • Patent Number
    6,814,034
  • Date Filed
    Wednesday, November 19, 2003
    20 years ago
  • Date Issued
    Tuesday, November 9, 2004
    20 years ago
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
Foreign Referenced Citations (3)
Number Date Country
1 197 647 Oct 2001 EP
1 215 380 Dec 2001 EP
9-228858 Sep 1997 JP