Piston oil-cooling device in an engine

Information

  • Patent Grant
  • 6481389
  • Patent Number
    6,481,389
  • Date Filed
    Tuesday, January 9, 2001
    23 years ago
  • Date Issued
    Tuesday, November 19, 2002
    21 years ago
Abstract
A piston is reliably cooled from its backside by using an oil for lubricating portions around a crank pin of a crankshaft. An engine including a crankshaft is provided with lubricating oil bores to supply an oil from journals of the crankshaft to an outer peripheral surface of a crank pin. A larger end of the connecting rod is provided with a pair of opposed axial oil grooves in its outer peripheral surface, and with an annular oil passage connected to the axial groove in its side thrust face. A pair of cooling oil injection grooves each have one end connected to the annular oil passage and the other end directed to a piston while they are provided proximate to each other.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to a piston oil-cooling device in an engine in which a crankcase that supports journals of a crankshaft is provided with lubricating oil passages to supply oil to outer peripheral surfaces of the journals. The crankshaft is provided with lubricating oil bores to supply the oil from the journals to an outer peripheral surface of a crank pin and a piston is cooled from its backside by using the oil to lubricate portions around the crank pin.




2. Description of the Related Art




Conventional piston oil-cooling devices in engines typically include a piston oil-cooling device in a horizontal engine with a crankshaft disposed horizontally. An oil dipper is formed at a larger end of a connecting rod so that oil in an oil pan at a bottom of a crankcase is scattered by the oil dipper due to the rotation of the crankshaft. The scattered oil is permitted to reach a backside of a piston to cool the piston. The conventional piston oil-cooling devices also typically include another piston oil-cooling device having an oil injection bore provided in the larger end of the connecting rod to communicate with a lubricating oil bore in the crankshaft so that a piston is cooled from its backside by the oil injected from the oil injection bore. See Japanese Utility Model Publication No.4-37211.




Unfortunately, the first-mentioned conventional device is not applicable to a vertical engine with a crankshaft that is disposed vertically. Also, the second-mentioned conventional device is applicable to either horizontal and vertical engines, but suffers from a drawback in that much labor is needed to make the oil injection bore in the larger end of the connecting rod by drilling, which results in an increase in cost, as well as manufacturing time and effort.




SUMMARY OF THE INVENTION




Accordingly, it is an object of the present invention to provide a piston oil-cooling device applicable to either horizontal and vertical engines, wherein a piston can be reliably cooled from its backside by using an oil to lubricate portions of a crank pin of a crankshaft, wherein the oil injection bore can easily be made, which reduces manufacturing time and effort, thereby reducing cost.




To achieve the above object, according to a first aspect and feature of the present invention, there is provided a piston oil-cooling device in an engine in which a crankcase that supports journals of a crankshaft is provided with lubricating oil passages to supply oil from an oil pump to outer peripheral surfaces of the journals. The crankshaft is provided with lubricating oil bores to supply the oil from the journals to an outer peripheral surface of a crank pin. A larger end of a connecting rod connected to the crank pin is provided in an inner peripheral surface with a pair of opposed axial oil grooves. The larger end is also provided in a side thrust face with an annular oil passage connected to the axial groove and a cooling oil injection groove. The cooling oil injection groove is connected at one end thereof to the annular oil passage while the other end is directed to a backside of a piston which is connected to a smaller end of the connecting rod.




With the first feature, when the lubricating oil bores in the crankshaft are aligned with the axial oil grooves in the larger end of the connecting rod, the oil in the lubricating oil bores is injected from the cooling oil injection groove via the axial oil grooves and the annular oil passage in the larger end toward the backside of the piston to effectively cool the piston. Therefore, the force of the injected oil is always strong and reaches the piston properly, thereby effectively cooling the piston. Thus, the piston oil-cooling device is applicable to either vertical and horizontal engines. Moreover, the cooling oil injection groove, the annular oil passage, and the axial oil grooves can be manufactured simultaneously with the formation of the connecting rod, thereby reducing manufacturing time and effort, as well as cost.




According to a second aspect and feature of the present invention, in addition to the first feature, a pair of the cooling oil injection grooves are disposed in proximity to the pair of axial oil grooves on the same side thrust face, respectively.




With the second feature, the pair of cooling oil injection grooves are in proximity to the pair of axial oil grooves, respectively. Therefore, when the lubricating oil bores in the crankshaft are aligned with each of the axial oil grooves, the oil is injected, having a particularly strong force, from the cooling injection groove closer to the axial groove. Such a situation occurs once per rotation of the crankshaft and hence, the oil cooling of the piston can be carried out more effectively.




According to a third aspect and feature of the present invention, in addition to the first or second feature, when the engine is of a vertical type with a crankshaft disposed vertically, the cooling oil injection groove is provided in a lower side thrust face of the larger end.




With the third feature, the opposed side thrust faces of the larger end and the crankshaft are brought into close contact by the weight of the connecting rod. Therefore, leakage of the cooling oil from the cooling oil injection groove in the larger end of the connecting rod between both of the side thrust faces is eliminated to maintain the injection force of the oil from the cooling oil injection groove. Also, oil injected from the cooling oil injection groove is permitted to easily reach the piston without being obstructed by the connecting rod, thereby further effectively achieving the oil cooling of the piston.




According to a fourth aspect and feature of the present invention, in addition to the first or second feature, a side thrust face of the crankshaft opposed to the side thrust face of the larger end is formed to cover the entire open surface of the cooling oil injection groove.




With the fourth feature, the open surface of the cooling oil injection groove in the larger end of the connecting rod is closed by the side thrust face of the crankshaft. Therefore, it is possible to prevent a wasteful flowing-out of the cooling oil from the open surface of the cooling oil injection groove and to maintain the injection force of the oil from the cooling oil injection groove, thereby more effectively achieving the oil cooling of the piston.




According to a fifth aspect and feature of the present invention, in addition to the first or second feature, the larger end is comprised of a semi-cylindrical larger end body integrally formed at a rod portion, and a semi-cylindrical cap coupled to the larger end body, and the pair of axial oil grooves are provided at a boundary between the larger end body and the cap.




With the fifth feature, it is possible to avoid the damage to the outer peripheral surface of the crank pin by the boundary between the larger end body and the cap by using the axial oil grooves.




The above and other objects, features and advantages of the present invention will become apparent from the following description taken in conjunction with the accompanying drawings.











BRIEF DESCRIPTION OF DRAWINGS





FIG. 1

is a side view of an outboard engine system including an engine to which the present invention is applied;





FIG. 2

is a vertical sectional view of the engine;





FIG. 3

is an enlarged view of a portion shown in

FIG. 2

;





FIG. 4

is a view taken in the direction of an arrow


4


in

FIG. 3

;





FIG. 5

is a sectional view taken along a section line


5





5


in

FIG. 4

;





FIG. 6

is a sectional view taken along a section line


6





6


in

FIG. 4

;





FIG. 7

is an enlarged vertical sectional view of a crankshaft shown in

FIG. 3

;





FIG. 8

is a plan view of one of connecting rods shown in

FIG. 7

; and





FIGS. 9A and 9B

illustrate operation of the invention.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT




Referring to

FIG. 1

, an outboard engine system O includes a stern bracket


1


clamped at a transom T of a hull. A vertically extending casing


3


that swings in a lateral direction relative to the hull is connected to the stern bracket


1


through a swivel shaft


2


. An engine E is mounted at an upper portion of the casing


3


and an engine cover


4


is coupled to the casing


3


to cover the engine E. Power output from a crankshaft


5


of the engine E is transmitted to a propeller shaft


8


supported at a lower portion of the casing


3


through a drive shaft


6


disposed in the casing


3


and a bevel gear transmitting device


7


capable of switching-over the forward and rearward movements from each other, thereby driving a propeller


9


mounted at a rear end of the propeller shaft


8


.




Referring to

FIGS. 2 and 3

, the engine E is mounted in the casing


3


in an attitude in which the crankshaft


5


has been turned vertically and a cylinder block


11


has been turned rearwards of the hull. The engine E includes an engine block


12


with a crankcase


10


and the cylinder block


11


formed integrally with each other. Two upper and lower cylinder bores


13


,


13


having axes turned horizontally are provided in the cylinder block


11


.




The crankcase


10


has a closed bottom wall and an upper wall having an opening


14


for assembling the crankshaft


5


. A case cover


15


is coupled to the crankcase


10


to cover the opening


14


.




First and second bearing bores


20


and


21


are provided in the bottom wall of the crankcase


10


and the case cover


15


. A lower first journal


25


and an upper second journal


26


of the crankshaft


5


are carried by first and second bearing bushes


22


and


23


which are fitted in the bearing bores


20


and


21


, respectively. Connecting rods


28


,


28


are connected at their smaller ends


28




a


(

FIG. 8

) to a pair of upper and lower pistons


27


,


27


reciprocally movable in the cylinder bores


13


,


13


, and at their larger ends


28




b


(

FIG. 7

) to a pair of upper and lower crank pins


5




a


,


5




a


of the crankshaft


5


, respectively.




A working bore


10




a


is provided in a sidewall of the crankcase


10


opposite to the cylinder bores


13


,


13


for assembling the connecting rods


28


,


28


. The working bore


10




a


is closed by a side lid


10




b.






The structure of coupling the crankcase


10


and the case cover


15


will be described with reference to

FIGS. 4

to


6


.




The crankcase


10


and the case cover


15


are each provided with a pair of positioning bores


32


and


33


;


34


and


35


, respectively, which open into a joint face


30


,


31


thereof. The positioning bores


32


,


33


,


34


and


35


are disposed at locations closer to the cylinder block


11


than the second bearing bush


23


and spaced equidistantly on opposite sides of a plane P including an axis Y of the crankshaft


5


and axes X of the cylinder bores


13


,


13


. Halves of a pair of knock pins


36


and


37


are press-fit into the positioning bores


32


and


33


in the crankcase


10


, and the positioning bores


34


and


35


in the case cover


15


are fit over the other halves of the knock pins


36


and


37


, respectively. Thus, the joint positions of the crankcase


10


and the case cover


15


are defined to coaxially arrange the first and second bearing bushes


22


and


23


.




A plurality of threaded bores


38


are provided in the crankcase


10


and open into the joint face


30


to surround the opening


14


. A corresponding number of bolt-insertion bores


39


are provided in the case cover


15


. Thus, the crankcase


10


and the case cover


15


are coupled to each other by threadedly fitting bolts


40


through the bolt-insertion bores


39


into the threaded bores


38


and then tightening the bolts


40


. A liquid packing is then applied to at least one of the joint faces


30


and


31


of the crankcase


10


and the case cover


15


.




Thus, when an explosion load is applied from the pistons


27


,


27


to the crankshaft


5


through the connecting rods


28


,


28


during an explosion stroke of the engine E, a shearing load is applied to the joint faces


30


and


31


of the crankcase


10


and the case cover


15


. However, a shearing stress generated on the knock pins


36


and


37


and a frictional force applied to the joint faces


30


and


31


by the plurality of bolts


40


resist the shearing load.




Furthermore, because the pair of knock pins


36


and


37


are positioned closer to the cylinder block


11


than the second bearing bushes


23


, when the explosion load is applied from the crankshaft


5


to the case cover


15


, a tensile stress is generated in a wide area between the second bearing bush


23


and the pair of knock pins


36


and


37


. Therefore, because the case cover


15


is strongly resistant to the tensile stress, the case cover


15


exhibits a high rigidity in cooperation with the dispersion of the tensile stress.




In this way, the pair of knock pins


36


and


37


define the position for coupling of the crankcase


10


and the case cover


15


to each other, but also contribute to increasing the rigidity of the case cover


15


. Therefore, it is possible to increase the supporting strength of the crankshaft


5


, reduce the weight of the case cover


15


, and decrease the number of bolts


40


used.




In addition, the knock pins


36


and


37


are positioned equidistantly from the plane P including the axis of the crankshaft


5


and the axes X of the cylinder bores


13


,


13


. Therefore, it is possible to effectively provide the equalization of the shearing load applied to both of the knock pins


36


and


37


and disperse the tensile stress generated on the case cover


15


, thereby enhancing the durability of the knock pins


36


and


37


and the case cover


15


.




The bearing bore


20


for mounting of the first bearing bush


22


to support the first journal


25


of the crankshaft


5


is provided in the engine block


12


, and the bearing bore


21


for mounting of the bearing bush


23


to support the second journal


26


of the crankshaft


5


is provided in the case cover


15


. Therefore, it is not necessary to machine the two members while in a coupled state to form the bearing bores


20


and


21


as is common in conventional engines. Thus, a step of coupling the two members to each other and a step of separating them from each other is not required, which reduces the manufacturing cost, but also permits replacement of either the engine block


12


and the case cover


15


, leading to an enhanced interchangeability of parts.




Moreover, the supplying of a lubricating oil to the second journal


26


of the crankshaft


5


is conducted from the oil pump


53


through the oil passages


42


and


43


provided in the engine block


12


and the case cover


15


. Therefore, it is not necessary to define an oil passage for lubricating the second journal


26


in the crankshaft


5


, which also simplifies the structure of the oil passage in the crankshaft


5


.




In

FIG. 4

, reference character U designates an igniting CDI device mounted on the side lid


10




b


and a boss formed on the case cover


15


. Reference character S is a starting motor, and R is a regulator rectifier for a power supply, both of which are mounted on an upper wall of the engine block


12


.




Referring again to

FIG. 3

, a valve operating camshaft


48


is disposed parallel relative to the crankshaft


5


and is carried in the cylinder head


16


coupled to a rear end of the cylinder block


11


. Driving and driven pulleys


50


and


51


are secured to the crankshaft


5


and the camshaft


48


above the cylinder head


16


and the case cover


15


, respectively, and a timing belt


52


is reeved around the driving and driven pulleys


50


and


51


, so that the crankshaft


5


drives the camshaft


48


at a reduction ratio of ½.




The oil pump


53


is mounted at a lower rear portion of the cylinder block


11


and driven by the camshaft


48


. The oil pump


53


pumps an oil from an oil case


54


(see

FIG. 2

) coupled to a lower portion of the engine block


12


and accommodated in the casing


3


to supply the oil to a first lubricating oil passage


41


defined through a lower wall of the cylinder block


11


and a second lubricating oil passage


42


defined through one sidewall of the cylinder block


11


and extends upwards.




As shown in

FIG. 7

, each of the first and second bearing bushes


22


and


23


is provided with an annular lubricating groove


60


that opens into an inner surface thereof, and a through-bore


61


that permits the lubricating groove


60


to communicate with an outer peripheral surface of the bearing bushes


22


and


23


. The first lubricating oil passage


41


communicates with the through-bore


61


in the first bearing bush


22


, and the second lubricating oil passage


42


is connected to a third lubricating oil passage


43


defined in the case cover


15


through a hole


36




a


in the hollow knock pin


36


. The third lubricating oil passage


43


communicates with the through-bore


61


in the second bearing bush


23


.




A working bore


43




a


of the third lubricating oil passage


43


opens into one side of the case cover


15


, as shown in

FIGS. 4 and 5

. A hydraulic pressure sensor


46


is threadedly mounted in the working bore


43




a


to detect a pressure discharged from an oil pump


53


through the third lubricating oil passage


43


. With such a structure, it is not necessary to especially provide an exclusive bore for mounting the hydraulic pressure sensor


46


in the case cover


15


, thereby leading to a reduction in cost. In this case, the disposition of the hydraulic pressure sensor


46


, with a tip end turned laterally and rearwards of the outboard engine system O, decreases the overhanging of the hydraulic pressure sensor


46


in an outward direction of the engine block


12


, which avoids increasing the size of the engine cover


4


.




As shown in

FIG. 8

, the larger end


28




b


of each of the connecting rods


28


includes a semi-cylindrical larger end body


66


integrally formed at a rod portion


28




a


and a semi-cylindrical larger end cap


67


coupled to the semi-cylindrical larger end body


66


by bolts


68


. A crank pin hole


69


that supports the corresponding crank pin


5




a


is defined within inner peripheral surfaces of the semi-cylindrical larger end body


66


and the semi-cylindrical larger end cap


67


. Annular oil passages


71


,


71


defined in upper and lower side thrust faces


70


,


70


conically extend down into the crank pin hole


69


.




Axial oil grooves


72


,


72


are provided within an inner peripheral surface of the crank pin hole


69


and connect the oil passages


71


,


71


to each other. Each axial oil groove


72


,


72


has a U-shape in section with a large width so that it passes through a boundary between the larger end body


66


and the larger end cap


67


. In this manner, a large path area of each axial oil groove


72


can be ensured even though it is a narrow portion between the inner peripheral surface of the crank pin hole


69


and the bolt


68


. Each axial oil groove


72


,


72


is used as a recess to prevent the boundary between the larger end body


66


and the larger end cap


67


from coming into contact with the outer peripheral surface of the crank pin


5




a.






The axial oil grooves


72


,


72


in the lower connecting rod


28


communicate with the first lubricating oil bore


62


at predetermined different angles of rotation of the crankshaft


5


, respectively. The axial oil grooves


72


,


72


in the upper connecting rod


28


align and communicate with the second lubricating oil bore


63


at predetermined different angles of rotation of the crankshaft


5


, respectively.




The lower side thrust face


70


of the larger end


28




b


of each connecting rod


28


is provided with a pair of cooling oil injection grooves


73


,


73


connected at one end thereof to the annular oil passage


71


and with the other end directed toward a backside of the corresponding piston


27


. The cooling oil injection grooves


73


,


73


are disposed in proximity to the pair of axial oil grooves


72


,


72


, respectively. The cooling oil injection grooves


73


,


73


, the annular oil passages


71


,


71


and the axial oil grooves


72


,


72


are manufactured upon the formation of the connecting rod


28


by either one of a casting process, a forging process, or a sintering process. Hence, a special process or machine is not required to produce them.




The side thrust face


75


of the crankshaft


5


opposed to the lower side thrust face


70


of the larger end


28




b


of each connecting rod


28


is formed to bulge toward the smaller end


28




a


, so that it covers the open surfaces of the cooling oil injection groove


73


substantially over the entire length.




As shown in

FIGS. 2

to


4


, a large number of mounting bosses are provided on and project from the outer surface of the case cover


15


. A recoiled starting device


58


is bolted to mounting bosses,


55




a


to


55




c


disposed at apexes of a triangle at locations farthest from the crankshaft


5


. In the present embodiment, a measure is taken so that the parts or components can be used commonly in any outboard engine system having a specification of 6 volts or 12 volts in power-generating and charging systems.




For example, in the specification of 12 volts, a circular annular multi-pole power-generating coil C (see

FIG. 2

) is secured to bosses


56




a


to


56




c


disposed at apexes of a triangle at locations closest to the crankshaft


5


. In the specification of 6 volts, a semicircular igniting power coil is bolted at its opposite ends to bosses


57




a


and


57




b


disposed at intermediate locations, and a semicircular charging coil is bolted at its opposite ends to bosses


57




c


and


57




d.






The operation of the engine E will be described below.




When the oil pump


53


driven by the camshaft


48


supplies oil to the first and second lubricating oil passages


41


and


42


during operation of the engine E, the oil supplied to the first lubricating oil passage


41


is permitted to flow through the through-bore


61


in the first bearing bush


22


into the lubricating groove


60


in the inner periphery to lubricate the first journal


25


of the crankshaft


5


. The oil supplied to the second lubricating oil passage


42


is permitted to flow via the third lubricating oil passage


43


through the through-bore


61


in the second bearing bush


23


into the lubricating groove


60


in the inner periphery to lubricate the second journal


26


of the crankshaft


5


.




A portion of the oil supplied to each of the lubricating grooves


60


,


60


in the first and second bearing bushes


22


and


23


as described above flows toward each of the first and second lubricating oil bores


62


and


63


. When the first and second lubricating oil bores


62


and


63


are aligned with one of the axial oil grooves


72


in the larger end


28




b


of the corresponding connecting rod at the predetermined angles of rotation of the crankshaft


5


in the above manner, as shown in

FIG. 9A

, the oil in each of the first and second lubricating oil bores


62


and


63


is passed from the one axial oil groove


62


into the upper and lower annular oil passages


71


,


71


in the larger end


28




b


to lubricate the crank pin hole


69


and the upper end lower side thrust faces


70


,


70


of the larger end


28




b


, as well as the crank pin


5




a.






A portion of the oil flowing into the annular oil passage


71


,


71


is permitted to flow through the annular oil passages


71


into the pair of cooling oil injection grooves


73


,


73


in the larger end


28




b,


and is injected therefrom toward the backside of the piston


27


. Particularly, the force of the oil is less abated in the cooling oil injection groove


73


, which is closer to the corresponding lubricating oil bore


62


or


63


. Therefore, a relatively large amount of oil is injected forcefully from the cooling oil injection groove


73


and thus, reliably reaches the backside of the corresponding piston


27


, thereby effectively cooling the piston


27


.




When the first and second lubricating oil bores


62


and


63


are aligned with the axial oil groove


72


in the larger end


28




b


of the corresponding connecting rod


28


at the different predetermined angles of rotation of the crankshaft


5


, as shown in

FIG. 9B

, the crank pin hole


69


and the upper and lower side thrust faces


70


,


70


of the larger end


28




b


are lubricated by the oil passing from the first and second lubricating oil bores


62


and


63


via the other axial oil groove


72


to the annular oil grooves


71


,


71


in the same manner as that described above. Thus, a relatively large amount of oil is injected forcefully, particularly from the other cooling oil injection groove


73


closer to the other axial oil groove


72


, thereby effectively cooling the corresponding piston


27


from the backside.




Notwithstanding that the axial oil grooves


72


,


72


formed into the U-shape in section with the large width in the larger end


28




b


of each connecting rod


28


are narrow portions between the inner peripheral surface of the crank pin hole


69


and the bolt


68


, a large path area is provided therein, and the duration of communication between the first and second lubricating oil bores


62


and


63


and the axial oil grooves


72


,


72


in each connecting rod


28


is thereby prolonged. Therefore, a large amount of oil is supplied to the lubricating oil bores


62


and


63


, thereby enhancing the oil-cooling effect for the piston


27


.




In the vertical engine as described above, the cooling oil injection grooves


73


,


73


in each of the connecting rods


28


are provided in the lower side thrust face


70


of the larger end


28




b


of the connecting rod


28


. Thus, the opposed side thrust faces


70


and


75


of the larger end


28




b


and the crankshaft


5


are in closed contact with each other under the weight of the connecting rod


28


. Therefore, it is possible to inhibit the leakage of the cooling oil from the cooling oil injection grooves


73


,


73


in the connecting rod


28


between both side thrust faces


70


and


75


to maintain the force of the oil injected from the cooling oil injection grooves


73


,


73


. Moreover, it is possible to ensure that the oil injected from the cooling oil injection grooves


73


,


73


easily reaches the corresponding piston


27


without being obstructed by the connecting rod


28


. As a result, the piston


27


can effectively be further cooled.




The side thrust face


75


of the crankshaft


5


opposed to the side thrust face


70


of the larger end


28




b


of each connecting rod


28


is formed to cover the entire open surfaces of the cooling oil injection grooves


73


,


73


. Thus, the open surfaces of the cooling oil injection grooves


73


,


73


in the larger end


28




b


of the connecting rod


28


are closed by the side thrust faces


75


of the crankshaft


5


. Thus, wasteful leakage of the cooling oil from the open surfaces of the cooling oil injection grooves


73


,


73


is prevented to maintain the force of the oil injected from the cooling oil injection grooves


73


,


73


, thereby more effectively cooling the piston


27


.




Further, the axial oil grooves


72


,


72


in each of the connecting rods


28


are provided in the boundary between the larger end body


66


and the cap


67


constituting the larger end


28




b.


Accordingly, damage to the outer peripheral surfaces of the crank pins


5




a


,


5




a


by the boundary between the larger end body


66


and the cap


67


is avoided.




Although the preferred embodiment of the present invention has been described above in detail, it will be understood that the present invention is not limited to the above-described embodiment, and various modifications in design may be made without departing from the subject matter of the invention. For example, the engine E may be formed into a horizontal type with its crankshaft disposed horizontally, or into a single-cylinder type.



Claims
  • 1. A piston oil-cooling device in an engine comprises:a crankshaft; a crankcase that supports journals of said crankshaft, said crankcase is provided with lubricating oil passages to supply oil from an oil pump to outer peripheral surfaces of said journals, wherein said crankshaft is provided with lubricating oil bores to supply the oil from said journals to an outer peripheral surface of a crank pin; a connecting rod including a larger end connected to said crank pin, said larger end being provided with a pair of opposed axial oil grooves in an inner peripheral surface of the larger end and an annular oil passage formed in a side thrust face of the larger end and connected to said axial oil grooves; and a cooling oil injection groove formed in said side thrust face and having one end thereof connected to said annular oil passage and the other end directed to a backside of a piston which is connected to a smaller end of said connecting rod.
  • 2. The piston oil-cooling device in an engine according to claim 1, wherein a pair of said cooling oil injection groves are disposed proximate to said pair of axial oil grooves on the same side thrust face.
  • 3. The piston oil-cooling device in an engine according to either one of claim 1 or claim 2, whereinwhen the engine is of a vertical type with said crankshaft disposed vertically, said side thrust face in which said cooling oil injection groove is provided is a lower one of side thrust faces of said larger end.
  • 4. The piston oil-cooling device in an engine according to either one of claim 1 or claim 2, wherein a side thrust face of said crankshaft opposite said side thrust face of said larger end is configured to cover an entire open surface of said cooling oil injection groove.
  • 5. The piston oil-cooling device in an engine according to either one of claim 1 or claim 2, wherein said larger end is comprised of a semi-cylindrical larger end body integrally formed at a rod portion and a semi-cylindrical cap coupled to the larger end body, and said pair of axial oil grooves are provided at a boundary between said larger end body and said cap.
Priority Claims (1)
Number Date Country Kind
2000-010370 Jan 2000 JP
US Referenced Citations (4)
Number Name Date Kind
3739657 Patchen et al. Jun 1973 A
3785459 Patchen Jan 1974 A
5482380 Corrati et al. Jan 1996 A
6032635 Moorman et al. Mar 2000 A
Foreign Referenced Citations (1)
Number Date Country
437211 Feb 2002 JP