Valve system for engine

Information

  • Patent Grant
  • 6634330
  • Patent Number
    6,634,330
  • Date Filed
    Friday, November 16, 2001
    23 years ago
  • Date Issued
    Tuesday, October 21, 2003
    21 years ago
Abstract
To provide a valve system for an engine, in which a rocker arm is interlocked with an engine valve and is supported on a rocker shaft fixedly mounted to a cylinder head such that it is rockable with the rotation of a camshaft. Accordingly, the size and weight of the engine can be reduced. The posture of a rocker shaft is set to have an axial line crossing an axial line of a crankshaft on the projection plane perpendicular to an axial line of a cylinder bore. A rocker arm is rockably supported by the rocker shaft and is provided with an input arm extending, on the above projection plane, from the rocker arm to the camshaft side. A pull rod reciprocates in the axial direction with the rotation of the camshaft and is connected to the input arm.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to a valve system for an engine. In particular, the present invention relates to an improved valve system for an engine, wherein a rocker arm is interlocked with an engine valve and is supported by a rocker shaft fixedly supported by a cylinder head such that it is rockable with the rotation of a camshaft of the engine.




2. Description of Background Art




A valve system of this type has been known, for example, from Japanese Patent Laid-open No. Hei 2000-110516.




The above-described background art valve system is of an overhead cam type, wherein a camshaft is disposed over a cylinder head. In this valve system, to transmit rotational power of the crankshaft to the camshaft at a reduction ratio of 1/2, it is required to ensure a space on one end of the crankshaft for disposing power transmission means, such as a cam chain. This results in the width of the engine increasing in the direction along the axial line of the crankshaft. Accordingly, the weight of the engine is increased.




SUMMARY OF THE INVENTION




In view of the foregoing, the present invention has been made, and an object of the present invention is to provide a valve system of an engine, which is capable of reducing the size and weight of the engine.




To achieve the above object, according to a first aspect of the present invention, a valve system for an engine includes a crankshaft rotatably supported by a crankcase such that it is connected to a piston slidably fitted in a cylinder bore. A camshaft has an axial line parallel to an axial line of the crankshaft and is interlocked with the crankshaft at a reduction ratio of 1/2. A rocker arm is interlocked with engine valves and is supported by a rocker shaft fixedly supported by a cylinder head such that it is rockable with the rotation of the camshaft. The camshaft disposed on one side of the crankshaft is rotatably supported by the crankcase. The posture of the rocker shaft is set to have an axial line crossing the axial line of the crankshaft on the projection plane perpendicular to an axial line of the cylinder bore. An input arm extending on the projection plane from the rocker arm to the camshaft side is provided on the side of the rocker arm which is rockably supported by the rocker shaft. A pull rod reciprocating in the axial direction with the rotation of the camshaft is connected to the input arm in order to rock the rocker arm in the valve opening direction when the pull rod is moved to the camshaft side.




With this configuration, since the posture of the rocker shaft is set to have an axial line crossing the axial line of the crankshaft on the projection plane perpendicular to an axial line of the cylinder bore, a space required for disposing the rocker shaft, the rocker arm, and the like constituting part of the valve system can be made smaller in the direction along the axial line of the crankshaft. Also, since the input arm extends from the rocker arm to the camshaft disposed on one side of the crankshaft, and the pull rod reciprocating in the axial direction with the rotation of the camshaft is connected to the input arm, it is not required to enlarge the width of the cylinder head in the direction along the axial line of the crankshaft for disposing the pull rod. This results in the possibility of reducing the size and weight of the engine in the direction along the axial line of the crankshaft.




To achieve the above object, according to the second aspect of the present invention, a valve system for an engine includes a crankshaft which is rotatably supported by a crankcase such that it is connected to a piston slidably fitted in a cylinder bore. A camshaft has an axial line parallel to an axial line of the crankshaft and is interlocked with the crankshaft at a reduction ratio of 1/2. A first rocker arm is interlocked with first engine valves and a second rocker arm is interlocked with second engine valves different in kind from the first engine valves. The first and second rocker arms are respectively supported by a first rocker shaft and a second rocker shaft, which are fixedly supported by a cylinder head, such that they are rockable with the rotation of the camshaft. The camshaft is disposed on one side of the crankshaft and is rotatably supported by the crankcase. The first rocker arm corresponding to a pair of the first engine valves and the second rocker arm corresponding to a pair of the second engine valves are disposed in the cylinder head such that they face the combustion chamber. The first and second rocker arms are rockably supported by the first rocker shaft and the second rocker shaft, respectively. The first and second rocker shafts have axial lines crossing the axial line of the crankshaft on the projection plane perpendicular to an axial line of the cylinder bore and are disposed in parallel to each other. A first input arm and a second input arm extend on the projection plane from the first rocker arm and the second rocker arm to the camshaft side and are provided on the first rocker arm and the second rocker arm, respectively. A push rod reciprocating in the axial direction with the rotation of the camshaft is connected to the first input arm in order to rock the first rocker arm in the valve opening direction when the push rod is moved on the side opposite to the camshaft. A pull rod reciprocating in the axial direction according to the rotation of the camshaft is connected to the second input arm in order to rock the second rocker arm in the valve opening direction when the pull rod is moved on the camshaft side.




With this configuration, since the pair of first engine valves and the pair of second engine valves are disposed in the cylinder head such that they face the combustion chamber, it is possible to improve the suction efficiency and increase the output torque in a low speed rotational range. Since the postures of the first and second rocker shafts are set to have axial lines thereof crossing the axial line of the crankshaft on the projection plane perpendicular to the axial line of the cylinder bore, a space required in the cylinder head for disposing the first and second rocker shafts, the first and second rocker arms, and the like constituting part of the valve system can be made smaller in the direction along the axial line of the crankshaft. Furthermore, since the input arms extend from the first and second rocker arms to the camshaft disposed on one side of the crankshaft and the pull rod and the push rod reciprocating in the axial direction according to the rotation of the camshaft are connected to the input arms of both the rocker arms, it is not required to enlarge the width of the cylinder head in the direction along the axial line of the crankshaft for disposing the pull rod and the push rod. Accordingly, a drive system between the camshaft and the rocker arms can be disposed in good balance. This results in the possibility of reducing the size and weight of the engine in the direction along the axial line of the crankshaft.




Further scope of applicability of the present invention will become apparent from the detailed description given hereinafter. However, it should be understood that the detailed description and specific examples, while indicating preferred embodiments of the invention, are given by way of illustration only, since various changes and modifications within the spirit and scope of the invention will become apparent to those skilled in the art from this detailed description.











BRIEF DESCRIPTION OF THE DRAWINGS




The present invention will become more fully understood from the detailed description given hereinbelow and the accompanying drawings which are given by way of illustration only, and thus are not limitative of the present invention, and wherein:





FIG. 1

is a vertical sectional rear view of an engine;





FIG. 2

is an enlarged sectional view along line


2





2


of

FIG. 1

;





FIG. 3

is an enlarged sectional view along line


3





3


of

FIG. 2

;





FIG. 4

is an enlarged sectional view along line


4





4


of

FIG. 2

;





FIG. 5

is a sectional view along line


5





5


of

FIG. 1

showing a cylinder head;





FIG. 6

is a sectional view along line


6





6


of

FIG. 5

showing the cylinder head in a state in which a head cover is removed;





FIG. 7

is a view along an arrow


7


of

FIG. 6

;





FIG. 8

is a sectional view along line


8





8


of

FIG. 7

;





FIG. 9

is a sectional view along line


9





9


of

FIG. 1

;





FIG. 10

is an exploded perspective view of a structure for connecting a pull rod to a cam follower;





FIG. 11

is a side elevational view showing an engine installed in an airplane;





FIG. 12

is a sectional view along line


12





12


of

FIG. 11

;





FIG. 13

is an enlarged sectional view along line


13





13


of

FIG. 11

; and





FIG. 14

is an exploded perspective view, corresponding to

FIG. 10

, showing another embodiment of the present invention.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




Hereinafter, embodiments of the present invention will be described with reference to the accompanying drawings.





FIGS. 1

to


10


show one embodiment in which the present invention is applied to a four-cycle horizontally opposed type two-cylinder engine, wherein

FIG. 1

is a vertical sectional rear view of the engine;

FIG. 2

is an enlarged sectional view along line


2





2


of

FIG. 1

;

FIG. 3

is an enlarged sectional view along line


3





3


of

FIG. 2

;

FIG. 4

is an enlarged sectional view along line


4





4


of

FIG. 2

;

FIG. 5

is a sectional view along line


5





5


of

FIG. 1

showing a cylinder head;

FIG. 6

is a sectional view along line


6





6


of

FIG. 5

showing the cylinder head in a state in which a head cover is removed;

FIG. 7

is a view along an arrow


7


of

FIG. 6

;

FIG. 8

is a sectional view along line


8





8


of

FIG. 7

;

FIG. 9

is a sectional view along line


9





9


of

FIG. 1

;

FIG. 10

is an exploded perspective view of a structure for connecting a pull rod to a cam follower;

FIG. 11

is a side elevational view showing an engine installed in an airplane;

FIG. 12

is a sectional view along line


12





12


of

FIG. 11

; and

FIG. 13

is an enlarged sectional view along line


13





13


of FIG.


11


.




Referring first to

FIG. 1

, a four-cycle horizontally opposed type engine E is shown. The engine is mountable on an automobile, a motorcycle, aircraft, and the like. A main body


11


of the engine E includes a left engine block


12


L disposed on the left side as seen from the rear side of the engine E and a right engine block


12


R disposed on the right side as seen from the rear side of the engine E.




The left engine block


12


L includes a left cylinder block


13


L, a left crankcase


14


L formed integrally with the left cylinder block


13


L, and a left cylinder head


15


L connected to the side, opposite to the left crankcase


14


L, of the left cylinder block


13


L. Similarly, the right engine block


12


R includes a right cylinder block


13


R, a right crankcase


14


R formed integrally with the right cylinder block


13


R, and a right cylinder head


15


R connected to the side, opposite to the right crankcase


14


R, of the right cylinder block


13


R.




The cylinder block


13


L (or


13


R) has a cylinder bore


16


L (or


16


R). A piston


18


L (or


18


R) is slidably fitted in the cylinder bore


16


L (or


16


R) in such a manner as to form a combustion chamber


17


L (or


17


R) between the cylinder bore


16


L (or


16


R) and the cylinder head


15


L (or


15


R).




Both of the engine blocks


12


L and


12


R are oppositely disposed with axial lines of the cylinder bores


16


L and


16


R arranged substantially in the horizontal direction. The left and right crankcases


14


L and


14


R are fastened to each other to form a crankcase


19


in cooperation with each other. A crankshaft


21


connected to the pistons


18


L and


18


R via connecting rods


20


L and


20


R is rotatably supported between the left and right crankcases


14


L and


14


R.




Referring to

FIG. 2

, the crankcase


19


is provided with a front journal wall


22


F, an intermediate journal wall


22


M, and a rear journal wall


22


R, which are spaced from each other in the longitudinal direction. The journal walls


22


F,


22


M and


22


R rotatably support three portions spaced from each other in the axial direction of the crankshaft


21


. The crankshaft


21


is housed in a crank chamber


24


formed in the crankcase


19


. A partition wall


25


defining the bottom of the crank chamber


24


is provided on the inner wall of the crankcase


19


.




A rear end portion (left end portion in

FIG. 2

) of the crankshaft


21


projects rearwardly from the rear journal wall


22


R. A rotor


27


of a generator


26


is coaxially connected to the rear end portion of the crankshaft


21


. A stator


28


of the generator


26


is disposed behind the rear journal wall


22


R and is fixedly supported by a supporting plate


29


fixed to the crankcase


19


. A cover


30


for covering the generator


26


is fastened to a rear portion of the crankcase


19


.




A drive gear


31


is fixed to the crankshaft


21


at a position between the rear journal wall


22


R and the supporting plate


29


. A rotating shaft


33


, to which a first intermediate gear


32


meshing with the drive gear


31


, is rotatably supported by the rear journal wall


22


R and the supporting plate


29


. A second intermediate gear


34


, which is integrally provided on the rotating shaft


33


, meshes with a gear


35


provided on a camshaft


36


. The camshaft


36


having an axial line parallel to the crankshaft


21


is rotatably supported by the crankcase


19


at a position under the partition wall


25


.




In this way, power is transmitted from the crankshaft


21


to the camshaft


36


, at a reduction ratio of 1/2, via the drive gear


31


, first intermediate gear


32


, second intermediate gear


34


, and gear


35


.




A water pump


37


is mounted to the cover


30


. A pump shaft


38


of the water pump


37


is coaxially connected to the rotating shaft


33


such that it does not rotate relative to the rotating shaft


33


, whereby rotational power is transmitted from the crankshaft


21


to the water pump


37


.




Referring to

FIGS. 3 and 4

, an oil pan


42


is connected to a lower portion of the crankcase


19


such that an oil reservoir chamber


43


is formed under the camshaft


36


. An oil pump


44


is configured as a trochoide pump and is housed in the oil pan


42


.




A pump housing


45


of the oil pump


44


is formed by connecting a pair of housing halves


46


and


47


to each other. A drive shaft


48


having an axial line parallel to the crankshaft


21


and the camshaft


36


is rotatably supported by the housing half


46


. The drive shaft


48


is connected to a rotor


49


disposed between the housing halves


46


and


47


.




A partition wall


46




a


is integrally provided on the housing half


46


, whereby a power transmission chamber


50


partitioned from the oil reservoir chamber


43


formed in the oil pan


42


is formed between the partition wall


46




a


and a side wall of the oil pan


42


. A gear


51


meshing with the gear


35


of the camshaft


36


, which is rotated by power transmitted from the crankshaft


21


, is fixed to an end portion, on the power transmission chamber


50


side, of the drive shaft


48


. In this way, rotational power is transmitted from the crankshaft


21


to the oil pump


44


.




The partition wall


46




a


has an approximately U-shaped transverse cross-section, which is opened upwardly. The upper end of the partition wall


46




a


is located at a position higher than the oil level L of oil in the oil reservoir chamber


43


, so that oil does not flow from the oil reservoir chamber


43


side to the power transmission chamber


50


side. On the other hand, oil flows from the crank chamber


24


side into the power transmission chamber


50


via a gear train disposed in the power transmission route from the crankshaft


21


to the gear


51


. The oil in the power transmission chamber


50


splashes to the oil reservoir chamber


43


side across the upper end of the partition wall


46




a


by rotation of the gear


51


.




A pair of boss-like mounting portions


52


are integrally provided on a portion, corresponding to the housing half


46


, of the bottom of the oil pan


42


in such a manner as to project therefrom. The housing half


46


is removably mounted on the mounting portions


52


with bolts


53


. Similarly, a pair of boss-like mounting portions


52


are integrally provided on a portion, corresponding to the housing half


47


, of the bottom of the oil pan


42


in such a manner as to project therefrom. The housing half


47


is removably mounted on the mounting portions


52


with bolts


53


. Specifically, the pump housing


45


is removably mounted on the mounting portions


52


provided on the bottom of the oil pan


42


.




An inlet


54


is provided in the housing half


46


of the pump housing


45


. An oil strainer


55


connected to the inlet


54


is fixedly held between the housing half


46


and the oil pan


42


. To be more specific, an upper portion of the oil strainer


55


is inserted from below in a lower portion of the housing half


46


such that it is continuous with the inlet


54


. A lower peripheral edge of the oil strainer


55


is received on a receiving portion


56


provided on the bottom of the oil pan


42


.




An outlet


57


is provided in the housing half


47


of the pump housing


45


. A relief valve


58


connected to the outlet


57


is fixedly held between the housing half


47


and the oil pan


42


, while being kept in a posture parallel to that of the oil strainer


55


. To be more specific, an upper portion of the relief valve


58


is inserted from below in a lower portion of the housing half


47


such that it is continuous with the outlet


57


. A lower end of the relief valve


58


is received by a raised portion


59


provided on the bottom of the oil pan


42


.




An oil passage


61


in communication with the outlet


57


is provided in the housing half


47


. An oil passage


62


in communication with the oil passage


61


is provided in the lower portion of the oil pan


42


when the pump housing


45


is mounted to the oil pan


42


. An oil filter


63


connected to the oil passage


62


is removably mounted to an outer surface of a side wall of the oil pan


42


. An oil passage


64


for oil cleaned by passing through the oil filter


63


is provided in the oil pan


42


and the crankcase


19


. The oil passage


64


is in communication with a main gallery


65


provided in the crankcase


19


.




A front portion of the crankshaft


21


is formed into a cylindrical hollow shape for reducing the weight of the crankshaft


21


. A cylindrical spacer


66


, having an annular chamber


67


formed between the inner surface of the crankshaft


21


and the outer surface of the spacer


66


, is fitted in the cylindrical hollow portion of the crankshaft


21


. The annular chamber


67


extends at least between portions corresponding to the front and intermediate journal walls


22


F and


22


M of the crankcase


19


. Both axial ends of the annular chamber


67


are sealed in a fluid tight manner by mounting seal members to both ends of the spacer


66


or press-fitting both the ends of the spacer


66


in the crankshaft


21


.




An oil passage


68


for supplying oil to a portion to be lubricated between the intermediate journal wall


22


M and the crankshaft


21


is provided in the crankcase


19


in communication with the main gallery


65


. The crankshaft


21


has a passage hole


69


for supplying oil from the portion to be lubricated between the intermediate journal wall


22


M and the crankshaft


21


to the annular chamber


67


. The crankshaft


21


also has a passage hole


70


for supplying oil from the annular chamber


67


to a portion to be lubricated between the front journal wall


22


F and the crankshaft


21


.




The crankshaft


21


integrally includes a crank pin


21


L connected to the connecting rod


20


L on the left engine block


12


L side and a crank pin


21


R connected to the connecting rod


20


R on the right engine block


12


R side. An oil passage


71


for supplying oil from the annular chamber


67


to a portion to be lubricated between the connecting rod


20


L and the crank pin


21


L is provided in the crankshaft


21


. Oil is supplied from the main gallery


65


to a portion to be lubricated between the rear journal wall


22


R and the crankshaft


21


. An oil passage


72


for supplying oil from the portion to be lubricated between the rear journal wall


22


R and the crankshaft


21


to a portion to be lubricated between the connecting rod


20


R and the crank pin


21


R is provided in the crankshaft


21


.




In addition, in order to supply oil to the portion to be lubricated between the connecting rod


20


L and the crank pin


21


L, the entire cylindrical hollow portion of the crankshaft


21


can be used as an oil passage. However, in this case, since the volume of the oil passage may become excessively large, the hydraulic pressure rising time upon start-up of the engine E may be retarded and a residual amount of oil upon oil exchange may be increased. According to this embodiment, the annular chamber


67


formed between the cylindrical hollow portion of the crankshaft


21


and the spacer


66


is, as described above, used as the oil passage. Accordingly, the passage volume can be set to a suitable value, to prevent the retardation of the hydraulic pressure rising time and to prevent the increase in residual amount of oil upon oil exchange. Also, since the inside diameter of the cylindrical hollow portion of the crankshaft


21


can be set to a relatively large value without increasing the passage volume, it is not required to increase the accuracy of the penetrating depths of the passage holes


69


and


70


. Furthermore, by making the spacer


66


from a material lighter in weight than that of the crankshaft


21


, the entire crankshaft


21


can be made lighter in weight.




The oil, which has lubricated the portion to be lubricated between the connecting rod


20


L and the crank pin


21


L and the portion to be lubricated between the connecting rod


20


R and the crank pin


21


R, is released into the crank chamber


24


and is accumulated on the partition wall


25


. Oil through-holes


73


for directing the oil accumulated on the partition wall


25


to portions of the crankcase


19


for supporting both ends of the camshaft


36


are provided in the partition wall


25


. As a result, the oil is supplied to portions to be lubricated between the camshaft


36


and the crankcase


19


.




Referring to

FIGS. 5 and 6

, a pair of intake valve ports


76


and a pair of exhaust valve ports


77


are provided in the cylinder head


15


R of the right engine block


12


R in such a manner as to be positioned on both sides of a first virtual plane


78


containing the axial line of the cylinder bore


16


R and passing through the center of the combustion chamber


17


R. The pair of intake valve ports


76


and the pair of exhaust valve ports


77


face toward the combustion chamber


17


R. The first virtual plane


78


crosses an axial line C of the crankshaft


21


at an angle α on the projection plane perpendicular to the axial line of the cylinder bore


16


R (parallel to the paper in FIG.


5


).




Referring to

FIGS. 7 and 8

, a pair of ignition plugs


80


is mounted in the cylinder head


15


R in such a manner that the end portions thereof project into the combustion chamber


17


R. The axial lines of the ignition plugs


80


pass through the center of the combustion chamber


17


R and are disposed on the first virtual plane


78


.




The ignition plugs


80


are disposed symmetrically with respect to the second virtual plane


79


perpendicular to the first virtual plane


78


, and are mounted in the cylinder head


15


R such that they are tilted with a distance therebetween becoming smaller towards the combustion chamber


17


R. The end portions, projecting in the combustion chamber


17


R, of both the ignition plugs


80


are disposed in a region surrounded by both of the intake valve ports


76


and both of the exhaust valve ports


77


.




Both of the ignition plugs


80


are connected to an ignition circuit (not shown) and are usually operated in synchronization with each other by the ignition circuit.




Inner ends of plug insertion cylinders


81


, in which the ignition plugs


80


are to be inserted, are fixedly fitted in the cylinder head


15


R. Outer ends of the plug insertion cylinders


81


are located in opening portions


83


formed in the head cover


82


R fastened to the cylinder head


15


R. Spaces between the outer ends of the plug insertion cylinders


81


and the head cover


82


R are sealed.




A single intake port


84


, in communication with both of the intake valve ports


76


and having its axial line disposed on the second virtual plane


79


, is provided in the cylinder head


15


R such that it is opened in an upper side surface of the cylinder head


15


R. A single exhaust port


85


, in communication with both of the exhaust valve ports


77


and having its axial line disposed on the second virtual plane


79


, is provided in the cylinder head


15


R such that it is opened in a lower side surface of the cylinder head


15


R.




An intake pipe


74


R is connected to the upper side surface of the cylinder head


15


R such that it is in communication with the intake port


84


. A fuel injection valve


75


R is provided in the intake pipe


74


R.




Each of the intake valve ports


76


is openable/closable by an intake valve VI as an engine valve. A valve stem


86


of the intake valve VI is slidably fitted in a guide cylinder


87


provided in the cylinder head


15


R. The intake valve VI is elastically biased in the valve closing direction by a valve spring


89


provided between the cylinder head


15


R and a retainer


88


fixed to an end, projecting from the guide cylinder


87


, of the valve stem


86


.




Each of the exhaust valve ports


77


is openable/closable by an exhaust valve VE as an engine valve. A valve stem


90


of the exhaust valve VE is slidably fitted in a guide cylinder


91


provided in the cylinder head


15


R. The exhaust valve VE is elastically biased in the valve closing direction by a valve spring


93


provided between the cylinder head


15


R and a retainer


92


fixed to an end, projecting from the guide cylinder


91


, of the valve stem


90


.




Like the right cylinder head


15


R, the left cylinder head


15


L on the left engine block


12


L side is provided with a pair of intake valves VI and a pair of exhaust valves VE, and is also provided with a pair of ignition plugs


80


. A head cover


82


L is fastened to the cylinder head


15


L. An intake pipe


74


L provided with a fuel injection valve


75


L is connected to an upper side surface of the cylinder head


15


L.




The pair of the intake valves VI and the pair of the exhaust valves VE disposed in the right cylinder head


15


R are opened/closed by a valve system


94


R. The pair of the intake valves VI and the pair of the exhaust valves VE disposed in the left cylinder head


15


L are opened/closed by a valve system


94


L. The configuration of the valve system


94


R is the same as that of the valve system


94


L. Accordingly, only the configuration of the valve system


94


R on the right cylinder head


15


R side will be hereinafter described.




The valve system


94


R includes a holder


97


which integrally includes cylindrical lifter housings


95


coaxial with valve stems


86


of both of the intake valves VI and cylindrical lifter housings


96


coaxial with valve stems


90


of both of the exhaust valves VE. The holder


97


is fastened to the cylinder head


15


R. An intake side rocker shaft


98


and an exhaust side rocker shaft


99


have axial lines parallel to each other and are fixedly supported by the holder


97


. An intake side rocker arm


100


is rockably supported by the intake side rocker shaft


98


and an exhaust side rocker arm


101


is rockably supported by the exhaust side rocker shaft


99


. Lifters


102


are slidably fitted in the lifter housings


96


such that they are interposed between the intake rocker arm


100


and both of the intake valves VI. Lifters


103


are slidably fitted in the lifter housings


97


such that they are interposed between the exhaust side rocker arm


101


and both of the exhaust valves VE. The camshaft


36


is interlocked with the crankshaft


21


at a reduction ratio of 1/2. A push rod


104


imparts a valve opening force to the intake side rocker arm


100


according to the rotation of the camshaft


36


. A pull rod


105


imparts a valve opening force to the exhaust side rocker arm


101


according to the rotation of the camshaft


36


.




The intake side and exhaust side rocker shafts


98


and


99


are mounted to the cylinder head


15


such that they are disposed on both sides of the pair of ignition plugs


80


. To be more specific, the intake side rocker shaft


98


is disposed between the pair of the intake valves VI, i.e., the lifter housings


95


and both of the ignition plugs


80


. The exhaust side rocker shaft


99


is disposed between the pair of exhaust valves VE, i.e., the lifter housings


96


and both of the ignition plugs


80


. On the projection plane perpendicular to the axial line of the cylinder bore


16


R (parallel to the paper in FIG.


7


), the postures of both of the rocker shafts


98


and


99


are set such that axial lines thereof extend in parallel to the first virtual planes


78


on both sides of the first virtual plane


78


while crossing the axial line C of the crankshaft


21


.




The lifter


102


(or


103


) is formed into a cylindrical shape with its bottom closed. The lifter


102


(or


103


) has a diameter larger than an outside diameter of the valve stem


86


of the intake valve VI (or the valve stem


90


of the exhaust valve VE). The lifter


102


(or


103


) is slidably fitted in the lifter housing


95


(or


96


) with the closed end thereof directed toward the rocker arm


100


(or


101


) side. The closed end of the lifter


102


(or


103


) has a plurality of through-holes


106


(or


107


) arranged along a circular line for reducing the weight of the lifter


102


(or


103


).




A pair of drive arms


100




a


and


100




b


extending to the lifters


102


is integrally provided on the intake side rocker arm


100


. The leading ends of the drive arms


100




a


and


100




b


are in contact with the outer surfaces of the closed ends of the lifters


102


in order to impart driving forces for pressing the intake valves VI in the valve opening direction to the valve stems


86


of the intake valves VI via the lifters


102


.




A pair of drive arms


101




a


and


101




b


extending to the lifters


103


are integrally provided on the exhaust side rocker arm


101


. The leading ends of the drive arms


101




a


and


101




b


are in contact with the outer surfaces of the closed ends of the lifters


103


in order to impart driving forces for pressing the exhaust valves VE in the valve opening direction to the valve stems


90


of the exhaust valves VE via the lifters


103


.




It should be noted that according to this embodiment, to adjust a tappet clearance, as shown in

FIG. 6

, a shim


121


is held between the valve stem


86


and the lifter


102


and a shim


122


is held between the valve stem


90


and the lifter


103


. In place of the shim


121


(or


122


), a tappet screw screwed in the leading end of the drive arm


100




a


(or


100




b


,


101




a


, or


101




b


) such that it is adjustable in the forward or backward direction may be brought into contact with the lifter


102


(or


103


).




An oil passage


108


, to which oil is supplied from the oil pump


44


, is provided in both the cylinder head


15


R and the holder


97


connected to the cylinder head


15


R. An oil hole


109


, which is in communication with the oil passage


108


and annular recesses


110


and


111


provided in inner surfaces of the lifter housings


95


and


96


, is provided in the holder


97


and in the lifter housings


95


and


96


.




Referring to

FIG. 9

, the camshaft


36


disposed under the crankshaft


21


is provided with an intake side cam


112


R corresponding to the intake valves VI on the right engine block


12


R side, an intake side cam


112


L corresponding to the intake valves VI on the left engine block


12


L side, an exhaust side cam


113


R corresponding to the exhaust valves VE on the right engine block


12


R side, and an exhaust side cam


113


L corresponding to the exhaust valves VE on the left engine block


12


L side.




Cam followers


114


R and


114


L following the intake side cams


112


R and


112


L and cam followers


115


R and


115


L following the exhaust side cams


113


R and


113


L are rockably supported by the crankcase


19


. The cam followers


114


R and


115


L are disposed on the right engine block


12


R side with respect to the camshaft


36


, and are rockably supported by a common supporting shaft


118


mounted to the crankcase


19


. The cam followers


114


L and


115


R are disposed on the left engine block


12


L side with respect to the camshaft


36


, and are rockably supported by a common supporting shaft


119


mounted to the crankcase


19


.




Referring to

FIG. 7

, input arms


100




c


and


101




c


extending, on the projection plane perpendicular to the axial line of the cylinder bore


16


R, from the intake side rocker arm


100


and the exhaust side rocker arm


101


to the camshaft


36


side (lower side of FIG.


7


), are provided on the rocker arms


100


and


101


, respectively. The input arm


100




c


of the intake side rocker arm


100


is connected to the cam follower


114


R by means of a push rod


104


. The input arm


101




c


of the exhaust side rocker arm


101


is connected to the cam follower


115


R by means of the pull rod


105


. The push rod


104


acts, upon movement thereof in the direction opposite to the camshaft


36


, to push up the input arm


100




c


for rocking the intake side rocker arm


100


in the valve opening direction. The pull rod


105


acts, upon movement thereof on the camshaft


36


side, to pull the input arm


101




c


for rocking the exhaust side rocker arm


101


in the valve opening direction.




A rod chamber


120


extending from the crankcase


19


to both of the cylinder heads


15


R and


15


L is formed under the engine main body


11


. The push rod


104


and the pull rod


105


are contained and disposed in the rod chamber


120


. In addition, since the tensile strength of a material for forming both of the rods


104


and


105


is higher than the compression strength thereof, the diameter of the pull rod


105


is set to be smaller than that of the push rod


104


.




Spherical portions


104




a


and


104




b


are provided on both ends of the push rod


104


. The spherical portion


104




a


at one end of the push rod


104


is swingably received on the cam follower


114


R. The spherical portion


104




b


at the other end of the push rod


104


is swingably received on the leading end of the input arm


100




c


provided on the intake side rocker arm


100


.




As shown in

FIG. 10

, an approximately U-shaped fork


116


opened toward the side opposite to the camshaft


36


is integrally provided on the cam follower


115


R. A pin


123


fixed in one end of the pull rod


105


by press-fitting or the like is engaged with the fork


116


. Furthermore, an approximately U-shaped fork


117


opened on the side opposite to the camshaft


36


is integrally provided on the leading end of the input arm


101




c


provided on the exhaust side rocker arm


101


. A pin


124


fixed in the other end of the pull rod


105


is engaged with the fork


117


. With this configuration, both of the ends of the pull rod


105


can be connected to the input arm


101




c


provided on the exhaust side rocker arm


101


and the cam follower


115


R only by engaging both of the ends of the pull rod


105


with the forks


116


and


117


. Accordingly, one end of the pull rod


105


can be connected to the cam follower


115


R from the cylinder head


15


R side without disassembly of the oil pan


42


. This results in the maintenance being improved.




It should be noted that when an engine E as described above is installed in an air plane


150


as shown in

FIG. 11

, the engine E is accommodated in a cowl


152


attached to a front portion of a body


151


such that an axial line of the crankshaft


21


extends in the forward and backward direction. Furthermore, the engine E is resiliently supported on a support frame


153


disposed in the cowl


152


.




A spinner


155


having a plurality of propellers


154


is disposed forwardly of the cowl


152


, and the crankshaft


21


of the engine E is coupled coaxially to the spinner


155


.




Referring also to

FIG. 12

, an intake manifold


156


is disposed above the engine E and extends in the forward and backward direction. A pair of intake pipes


74


L and


74


R are connected to the opposite sides of a front portion of the intake manifold


156


such that they communicate with the intake ports


84


of the cylinder heads


15


L and


15


R of the cylinder blocks


12


L and


12


R of the engine E.




An air cleaner


157


is disposed below a rear portion of the intake manifold


156


on the rear side of the engine E and is connected to a rear portion of the intake manifold


156


. In addition, a suction pipe


158


is connected to a lower portion of the air cleaner


157


and extends forwardly below the engine E. The forward end of the suction pipe


158


is open to a screen


159


provided at a lower portion of the front end of the cowl


152


.




A pair of radiators


160


,


160


is disposed on the opposite left and right sides of a lower portion of the engine E. The radiators


160


,


160


are accommodated in a pair of first air ducts


161


,


161


, which extends forwardly upwards. The lower ends of the first air ducts


161


,


161


are open obliquely rearwards in the cowl


152


. A second air duct


162


is connected in common to the upper ends of the two first air ducts


161


,


161


. The second air duct


162


includes a common duct portion


162




a


extending leftwardly and rightwardly below a front portion of the engine E and having, at a front and central portion thereof, and air intake opening


163


opposed to the screen


159


. A pair of branch duct portions


162




b


,


162




b


extend rearwardly upwards from the opposite left and right end portions of the common duct portion


162




a


and connect to the upper ends of the first air ducts


161


,


161


.




In particular, the radiators


160


,


160


disposed on the opposite left and right sides of a lower portion of the engine E are cooled by air fed from the screen


159


at the front end of the cowl


152


to the air intake opening


163


by the propellers


154


and flowing through the left and right first air ducts


161


,


161


separately from the second air duct


162


.




The support frame


153


is formed from; for example, a plurality of pipe members combined in such a manner as to embrace the engine E from the rear. In addition; for example, mounting arms


164


,


164


are inclined such that the distances between them increase rearwardly at four locations of a rear portion of the crankcase


19


of the engine E. The mounting arms


164


,


164


are provided such that they may be positioned at the corners of an imaginary rectangular parallelepiped centered at the axial line of the crankshaft


21


in a plane perpendicular to the axial line. The mounting arms


164


,


164


, are mounted on the support frame


153


through resilient mounts


165


,


165


.




Referring to

FIG. 13

, each resilient mount


165


includes a cylindrical collar


166


, a cylindrical support tube


167


fixed to the support frame


153


and coaxially surrounding the collar


166


, and a mount rubber member


168


interposed between the collar


166


and the support tube


167


with inner and outer peripheries thereof baked to an outer periphery of the collar


166


and an inner periphery of the support tube


167


. Opposite ends of the collar


166


project from the opposite ends of the support tube


167


.




The collar


166


has one end contacting with a mounting arm


164


. The collar


166


contacts, at the other end thereof, with a holding down plate


169


. A bolt


170


has an increased diameter head portion


170




a


for engaging with an outer face of the holding down plate


169


and extending through the holding down plate


169


and the collar


166


. The bolt


170


is screwed in the mounting arm


164


such that the mounting arm


164


, i.e., the engine E, is resiliently mounted on the support frame


153


by tightening the bolt


170


.




The function of this embodiment will be described below. Since the pump housing


45


of the oil pump


44


for supplying lubricating oil to various portions of the engine E is removably mounted on the mounting portions


52


provided on the bottom of the oil pan


42


connected to the lower portion of the crankcase


19


, it is possible to set the oil pump


44


at a relatively low position in the engine E. Accordingly, the center of gravity of the engine E can be lowered and the suction efficiency and maintenance performance of the oil pump


44


can be improved.




Since the oil strainer


55


connected to the inlet


54


of the oil pump


44


is fixedly held between the oil pan


42


and the pump housing


45


, it is possible to fix the oil strainer


55


between the oil pan


42


and the pump housing


45


without use of parts specialized for fixture thereof such as bolts. Accordingly, the number of parts and the number of assembling steps can be reduced. Furthermore, since an oil suction passage between the inlet


54


of the oil pump


44


and the oil strainer


55


can be shortened, the pumping loss of the oil pump


44


can be reduced.




Since the relief valve


58


connected to the outlet


57


of the oil pump


44


is fixedly held between the oil pan


42


and the pump housing


45


while being kept in a posture parallel to that of the oil strainer


55


, the relief valve


58


can be disposed by making effective use of a space which is formed on a side of the oil strainer


55


by holding the oil strainer


55


between the pump housing


45


and the oil pan


42


. In addition, the relief valve is directly connected to the pump housing


45


of the oil pump


44


. Accordingly, it is possible to shorten and simplify the oil discharge passage, composed of the oil passages


61


and


62


extending from the oil filter


63


mounted on the outer surface of the side wall of the oil pan


42


, to the oil pump


44


. Furthermore, since a relief port of the relief valve


58


can be easily set in the oil in the oil pan


42


, it is possible to prevent the oil from bubbling.




In addition, the partition wall


46




a


forming the power transmission chamber


50


, which is partitioned from the oil reservoir chamber


43


formed in the oil pan


42


, between the side wall of the oil pan


42


and the partition wall


46




a


, is formed on the housing half


46


constituting part of the pump housing


45


. The gear


51


rotated by power transmitted from the crankshaft


21


is fixed to the end portion, on the power transmission chamber


50


side, of the drive shaft


48


rotatably supported by the pump housing


45


. Accordingly, since the gear


51


rotated for transmitting a power from the crankshaft


21


to the drive shaft


48


does not agitate the oil reserved in the oil reservoir chamber


43


in the oil pan


42


, it is possible to prevent the occurrence of friction loss and oil mist due to agitation of the oil.




The lifter


102


(or


103


) is formed into a cylindrical shape with its bottom closed. The lifter


102


(or


103


) has a diameter larger than that of the valve stem


86


(or


90


) and is interposed between the valve stem


86


of the intake valve VI (or the valve stem


90


of the exhaust valve VE) and the intake side rocker arm


100


(or exhaust side rocker arm


101


) which is interlocked to rock with the rotation of the camshaft


36


. The lifter


102


(or


103


) is slidably fitted in the cylindrical lifter housing


95


(or


96


), which is integrally provided on the holder


97


fixed to the cylinder heads


15


R and


15


L, and which is coaxial with the valve stem


86


(or


90


).




With this configuration, a drive force from the intake side rocker arm


100


(or the exhaust side rocker arm


101


) is applied to the valve stem


86


of the intake valve VI (or the valve stem


90


of the exhaust valve VE) via the lifter


102


(or


103


), so that a bending load is not applied to the valve stem


86


(or


90


), which has a relatively small diameter. As a result, it is possible to prevent the occurrence of partial wear, galling, and the like in the guide cylinder


87


(or


91


). Furthermore, the lifter


102


(or


103


) has a relatively large diameter. Accordingly, even if a bending load is applied from the intake side rocker arm


100


(or exhaust side rocker arm


101


), it is possible to minimize the occurrence of partial wear, galling, and the like between the lifter housing


95


(or


96


) and the lifter


102


(or


103


). Therefore, the reliability of the valve systems


94


R and


94


L can be improved.




The oil hole


109


is opened in the inner surfaces of the lifter housings


95


and


96


and is provided in the holder


97


and in the lifter housings


95


and


96


. Accordingly, it is possible to make the sliding motion of the lifter


102


(or


103


) in the lifter housing


95


(or


96


) smoother. Therefore, the occurrence of partial wear, galling, and the like between the lifter housing


95


(or


96


) and the lifter


102


(or


103


) can be more surely prevented.




In this case, if a point of the lifter


102


(or


103


), to which a drive force is applied from the intake side rocker arm


100


(or


101


), is offset from the center of the lifter


102


(or


103


), the lifter


102


(or


103


) can be rotated around its axial line. Correspondingly, the intake valve VI (or exhaust valve VE) can be rotated, to thereby prevent seizing on one side of the intake valve VI (or exhaust valve VE). From this viewpoint, according to this embodiment, the intake valve VI (or exhaust valve VE) can be easily rotated by smoothly sliding the lifter


102


(or


103


) in the lifter housing


95


(or


96


).




The pair of intake valve ports


76


and the pair of exhaust valve ports


77


are provided in the cylinder head


15


R (or


15


L) such that they are located on both sides of the first virtual plane


78


containing the axial line of the cylinder bore


16


R (or


16


L) and passing through an approximately center of the combustion chamber


17


R (


17


L). The pair of intake valve ports


76


and the pair of exhaust valve ports


77


face toward the combustion chamber


17


R (


17


L). The pair of ignition plugs


80


is mounted in the cylinder head


15


R (or


15


L). Both of the ignition plugs


80


are approximately symmetrical with respect to the second virtual plane


79


passing through the center of the combustion chamber


17


R (or


17


L) and are perpendicular to the first virtual plane


78


. Furthermore, the ignition plugs


80


are disposed in the cylinder head


15


R (or


15


L) in such a manner that the axial lines thereof extend substantially along the first virtual plane


78


and are tilted with a distance therebetween becoming smaller toward the combustion chamber


17


R (or


17


L). The ends of the ignition plugs


80


, projecting in the combustion chamber


17


R (or


17


L), are disposed in the region surrounded by both of the intake valve ports


76


and both of the exhaust valve ports


77


.




With this configuration, the ends of the pair of ignition plugs


80


, projecting in the combustion chamber


17


R (or


17


L), are disposed in proximity to an approximately central portion in the combustion chamber


17


R (or


17


L). Accordingly, it is possible to ideally propagate flame in the combustion chamber


17


R (or


17


L). Furthermore, even if an accidental firing of either of the ignition plugs


80


occurs, since the other ignition plug


80


is located at the approximately central portion of the combustion chamber


17


R (or


17


L), it is possible to minimize the deterioration of the flame propagation condition.




Both of the ignition plugs


80


are disposed in an approximately V-shape opened in the direction opposite to the combustion chamber


17


R (or


17


L), as seen from the direction perpendicular to the first virtual plane


78


. Furthermore, both of the ignition plugs


80


can be easily mounted in the cylinder head


15


R (or


15


L) with the ends of the ignition plugs


80


, projecting in the combustion chamber


17


R (or


17


L). Accordingly, the ignition plugs


80


are allowed to be disposed in proximity to an approximately central portion of the combustion chamber


17


R (or


17


L).




Both of the ignition plugs


80


are collectively disposed in the vicinity of the central portion of the combustion chamber


17


R (or


17


L). Accordingly, it is possible to enhance the degree of freedom of the shape of a water jacket on the cylinder head


15


R (or


15


L) side and the degree of freedom of disposition of fastening bolts for fastening the cylinder head


15


R (or


15


L) to the cylinder block


13


R (or


13


L). Accordingly, the sealing performance between the cylinder head


15


R (or


15


L) and the cylinder block


13


R (or


13


L) as well as the cooling performance can be improved.




The intake side and exhaust side rocker arms


100


and


101


are rockably supported by the intake side and exhaust side rocker shafts


98


and


99


having the axial lines extending along the first virtual plane


78


. The virtual plane


78


contains the axial line of the cylinder bore


16


R and passes through the center of the combustion chamber


17


R and crosses the axial line of the crankshaft


21


at the angle on the projection plane perpendicular to the axial line of the cylinder bore


16


R. The intake side and exhaust side rocker shafts


98


and


99


are mounted to the cylinder head


15


R (or


15


L) such that they are disposed on both of the sides of the ignition plugs


80


. With this configuration, it is possible to set the width of the cylinder head


15


R (or


15


L) at a relatively small value in the direction along the second virtual plane


79


. Accordingly, the engine E can be made more compact.




The input arm


101




c


extends on the projection plane perpendicular to the axial line of the cylinder bore


16


R (or


16


L) from the rocker arm


101


to the camshaft


36


side. The input arm


101




c


is provided on the exhaust side rocker arm


101


. The pull rod


105


reciprocates in the axial direction according to the rotation of the camshaft


36


. The pull rod


105


is connected to the input arm


101




c


in order to rock the exhaust side rocker arm


101


in the valve opening direction when the pull rod


105


is moved to the camshaft


36


side. With this configuration, it is not required to enlarge the width of the cylinder head


15


R (


15


L) in the direction along the axial line of the crankshaft


21


for disposing the pull rod


105


. Accordingly, the size and weight of the engine E in the direction along the axial line of the crankshaft


21


can be reduced.




The input arm


100




c


extends on the projection plane perpendicular to the axial line of the cylinder bore


16


R (or


16


L), from the rocker arm


101


to the camshaft


36


side. The input arm


100




c


is provided on the intake side rocker arm


100


. The push rod


104


reciprocates in the axial direction according to the rotation of the camshaft


36


. The push rod


104


is connected to the input arm


100




c


in order to rock the intake side rocker arm


100


in the valve opening direction when the push rod


104


is moved to the camshaft


36


side.




The intake and exhaust side rocker shafts


98


and


99


and the intake side and exhaust side rocker arms


100


and


101


are disposed as described above. Furthermore, an opening/closing force is imparted to the intake side rocker arm


100


by the pull rod


105


and to the exhaust side rocker arm


101


by the push rod


104


. Accordingly, the space in the cylinder head


15


R (or


15


L) necessary for disposing the rocker shafts


98


and


99


and the rocker arms


100


and


101


constituting parts of the valve system


94


R (or


94


L) can be can be decreased in size in the direction along the axial line of the crankshaft


21


.




Furthermore, it is not required to enlarge the width of the cylinder head


15


R (or


15


L) in the direction along the axial line of the crankshaft


21


for disposing the pull rod


105


and the push rod


104


. Accordingly, a drive system between the camshaft


36


and both the rocker arms


100


and


101


can be disposed in good balance. This makes it possible to reduce the size and weight of the engine E in the direction along the axial line of the crankshaft


21


.




As mentioned above, the pair of the intake valves VI and the pair of the exhaust valves VE are disposed in the cylinder head


15


R (or


15


L) in such a manner as to face the combustion chamber


17


R (or


17


L). Accordingly, it is possible to improve the suction efficiency and thereby increase the output torque in a low speed rotational range of the engine E.





FIG. 14

shows another embodiment of the present invention. A spherical portion


105




a


is provided at one end of a pull rod


105


. An engagement portion


126


is formed into a bowl shape and has a slit


127


allowing the insertion of the pull rod


105


. The engagement portion


126


is provided on a cam follower


115


R for being connected to the one end of the pull rod


105


. The one end of the pull rod


105


is connected to the cam follower


115


R by engaging the spherical portion


105




a


with the engagement portion


126


.




In this embodiment, since the one end of the pull rod


105


can be connected to the cam follower


115


R from the cylinder head


15


R side without disassembly of the oil pan


42


, it is possible to improve the maintenance of the device.




While the preferred embodiments have been described above, the present invention is not limited thereto, and it is to be understood that various changes in design may be made without departing from the scope of the claims.




For example, the present invention can be widely applied to engines other than the horizontally opposed type two-cylinder engine described above.




As described above, according to the first aspect of the present invention, a space required for disposing the rocker shaft, the rocker arm, and the like constituting part of the valve system can be made smaller in the direction along the axial line of the crankshaft. Furthermore, since it is not required to enlarge the width of the cylinder head in the direction along the axial line of the crankshaft for disposing the pull rod, it is possible to reduce the size and weight of the engine in the direction along the axial line of the crankshaft.




According to the second aspect of the present invention, it is possible to improve the suction efficiency and increase the output torque in a low speed rotational range. Also, a space required in the cylinder head for disposing the first and second rocker shafts, the first and second rocker arms, and the like constituting part of the valve system can be made smaller in the direction along the axial line of the crankshaft. Furthermore, since it is not required to enlarge the width of the cylinder head in the direction along the axial line of the crankshaft for disposing the pull rod and the push rod, a drive system between the camshaft and both the rocker arms can be disposed in good balance. This results in the possibility of reducing the size and weight of the engine in the direction along the axial line of the crankshaft.




The invention being thus described, it will be obvious that the same may be varied in many ways. Such variations are not to be regarded as a departure from the spirit and scope of the invention, and all such modifications as would be obvious to one skilled in the art are intended to be included within the scope of the following claims.



Claims
  • 1. An engine, comprising:a cylinder block having a crankcase formed integrally therewith and a cylinder bore formed therein; a cylinder head connected to said cylinder block; a crankshaft rotatably supported by said crankcase; a piston, said piston being slidably fitted in said cylinder bore and being operatively connected to said crankshaft; a camshaft having an axial line parallel to an axial line of said crankshaft, said camshaft being interlocked with said crankshaft at a reduction ratio of 1/2, said camshaft being disposed on one side of said crankshaft and being rotatably supported by said crankcase; a rocker shaft fixedly supported by said cylinder head; a rocker arm supported by said rocker shaft for rocking motion thereon in accordance with rotation of said camshaft, said rocker arm being operatively connected to engine valves; said rocker shaft is arranged to have an axial line thereof crossing an axial line of said crankshaft on a projection plane perpendicular to an axial line of said cylinder bore; and an input arm extending on said projection plane from said rocker arm to said one side of said crankshaft is provided on said rocker arm rockably supported by said rocker shaft; and a rod reciprocating in an axial direction in accordance with the rotation of said camshaft is connected to said input arm to rock said rocker arm in a valve opening direction.
  • 2. The engine according to claim 1, wherein said rod is a pull rod, said rocker arm being rocked in the valve opening direction when said pull rod is moved in a direction toward said camshaft.
  • 3. The engine according to claim 1, wherein said rod is a push rod, said rocker arm being rocked in the valve opening direction when said push rod is moved in a direction away from said camshaft.
  • 4. The engine according to claim 1, further comprising a holder, said holder supporting said rocker shaft and being connected to said cylinder head.
  • 5. A valve system for an engine, the engine including a cylinder block having a crankcase formed integrally therewith and a cylinder bore formed therein, a cylinder head connected to the cylinder block, a crankshaft rotatably supported by the crankcase, a piston slidably fitted in the cylinder bore and being operatively connected to the crankshaft, and a camshaft having an axial line parallel to an axial line of the crankshaft, the camshaft being interlocked with the crankshaft at a reduction ratio of 1/2 and being disposed on one side of the crankshaft rotatably supported by the crankcase, said valve system comprising:a rocker shaft fixedly supportable by the cylinder head; a rocker arm supported by said rocker shaft for rocking motion thereon in accordance with rotation of the camshaft, said rocker arm being operatively connected to engine valves of the engine; said rocker shaft is arranged to have an axial line thereof crossing an axial line of the crankshaft on a projection plane perpendicular to an axial line of the cylinder bore; and an input arm extending on said projection plane from said rocker arm to said one side of said crankshaft is provided on said rocker arm rockably supported by said rocker shaft.
  • 6. The valve system according to claim 5, further comprising a rod reciprocating in an axial direction in accordance with the rotation of said camshaft, said rod being connected to said input arm to rock said rocker arm in a valve opening direction.
  • 7. The valve system according to claim 6, wherein said rod is a pull rod, said rocker arm being rocked in the valve opening direction when said pull rod is moved in a direction toward said camshaft.
  • 8. The valve system according to claim 6, wherein said rod is a push rod, said rocker arm being rocked in the valve opening direction when said push rod is moved in a direction away from said camshaft.
  • 9. The valve system according to claim 5, further comprising a holder, said holder supporting said rocker shaft and being connectable to said cylinder head.
  • 10. An engine, comprising:a cylinder block having a crankcase formed integrally therewith and a cylinder bore formed therein; a cylinder head connected to said cylinder block; a crankshaft rotatably supported by said crankcase; a piston, said piston being slidably fitted in said cylinder bore and being operatively connected to said crankshaft; a camshaft having an axial line parallel to an axial line of said crankshaft, said camshaft being interlocked with said crankshaft at a reduction ratio of 1/2, said camshaft being disposed on one side of said crankshaft and being rotatably supported by said crankcase; a first rocker shaft fixedly supported by said cylinder head; a second rocker shaft fixedly supported by said cylinder head a first rocker arm supported by said first rocker shaft for rocking motion thereon in accordance with rotation of said camshaft, said rocker arm being operatively connected to a pair of first engine valves; a second rocker arm supported by said second rocker shaft for rocking motion thereon in accordance with rotation of said camshaft, said rocker arm being operatively connected to a pair of second engine valves, said second engine valves being different than said first engine valves; said first rocker shaft and said second rocker shaft are arranged to have axial lines thereof crossing an axial line of said crankshaft on a projection plane perpendicular to an axial line of said cylinder bore; a first input arm and a second input arm extending on said projection plane from said first rocker arm and said second rocker arm, respectively, to said one side of said crankshaft are provided on said first rocker arm and said second rocker arm, respectively; a first rod and a second rod reciprocating in axial directions in accordance with the rotation of said camshaft, said first rod and said second rod being connected to said first input arm and said second input arm, respectively, to rock said first rocker arm and said second rocker arm in valve opening directions, respectively.
  • 11. The engine according to claim 10, wherein said first rod is a push rod, said first rocker arm being rocked in the valve opening direction when said push rod is moved in a direction away from said camshaft.
  • 12. The engine according to claim 10, wherein said second rod is a pull rod, said second rocker arm being rocked in a valve opening direction when said pull rod is moved in a direction toward said camshaft.
  • 13. The engine according to claim 11, wherein said second rod is a pull rod, said second rocker arm being rocked in a valve opening direction when said pull rod is moved in a direction toward said camshaft.
  • 14. The engine according to claim 10, wherein said first rocker shaft and said second rocker shaft are disposed parallel to each other.
  • 15. The engine according to claim 10, further comprising a holder, said holder supporting said first rocker shaft and said second rocker shaft and being connected to said cylinder head.
Priority Claims (2)
Number Date Country Kind
2000-349952 Nov 2000 JP
2001-333341 Oct 2001 JP
CROSS-REFERENCES TO RELATED APPLICATIONS

This nonprovisional application claims priority under 35 U.S.C. §119(a) on Patent Application No. 2000-349952 filed in Japan on Nov. 16, 2000, and Patent Application No. 2001-333341 filed in Japan on Oct. 30, 2001, the entirety of each of which is herein incorporated by reference. This nonprovisional application further claims priority under 35 U.S.C. §119(e) on U.S. Provisional Application No. 60/248,551, filed on Nov. 16, 2000, the entirety of which is herein incorporated by reference.

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60/248551 Nov 2000 US