Lubrication system for two-cycle engine

Information

  • Patent Grant
  • 6792900
  • Patent Number
    6,792,900
  • Date Filed
    Thursday, September 26, 2002
    21 years ago
  • Date Issued
    Tuesday, September 21, 2004
    19 years ago
Abstract
A lubrication system for two-cycle engine includes a lubricant recess formed in a wall of a crankcase. Oil that becomes deposited within the intake passageway is directed to the lubricant recess preferably by a guide groove and pools adjacently below a connecting rod endcap. As the crankshaft with attached connecting rod rotates, pooled oil is drawn into the interior of the connecting rod endcap. Preferably, oil holes are formed radially outward through the connecting rod endcap to throw collected oil around the crankcase chamber when exposed to a centrifugal force.
Description




PRIORITY INFORMATION




This application is based on and claims priority to Japanese Patent Application No. 2001-301620, filed Sep. 28, 2001 the entire contents of which is hereby expressly incorporated by reference.




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to oil injection lubrication for engines and more particularly to oil injection systems and methods for lubricating a two-cycle engine.




2. Description of the Related Art




In two-cycle engines, it is a common practice to mix lubricating oil with induction air to lubricate engine parts. Typically, the intake air is pre-compressed inside a crank chamber before being sent into the cylinders. In this type of two-cycle engine, oil is guided to an intake passage and further into the engine by the intake air. More specifically, the oil encounters the intake air inside the intake passage and is misted therein. The misted oil is then drawn into the crank chamber as the piston ascends and a valve opens to allow intake air to enter the crank chamber. The misted oil lubricates rotating parts in and around the crankshaft and within the interior wall of the cylinder.




In conventional two-cycle engines, fuel mixes with the intake air inside the intake passageway to reduce the viscosity of the oil which promotes misting of the oil. However, in direct injection-type two-cycle engines in which the fuel is directly sprayed into the combustion chamber, the viscosity of the oil drawn into the crank chamber is not reduced by dilution with the fuel. The undiluted liquid oil is, therefore, more difficult to convert into a mist. Since the oil may not be sufficiently misted in the intake air, the amount of oil supplied to the engine may be reduced. Insufficiently misted oil results in liquid oil depositing onto the interior wall surface inside the intake passageway. More liquid oil deposits on the wall surfaces of the intake passageway when the flow of intake air decreases, such as during low speed operation.




SUMMARY OF THE INVENTION




One aspect of the present invention includes the realization that the rotation of the crankshaft of an internal combustion engine can be used to redistribute oil that has condensed in the crankcase chamber. For example, a lubricant recess can be preferably located adjacent, and generally below, a throw of a vertically-oriented crankshaft, such that a connecting rod endcap attached to the crankshaft throw passes over the recess during at least a portion of its rotational travel. The endcap is preferably configured with radial oil holes to help establish a flow path caused by a pressure differential due to rotation of the crankshaft. In at least one embodiment, the pressure differential is sufficient to draw oil from the recess into the endcap and throw the oil about the crankcase chamber.




According to another aspect of the present invention, a lubrication system for a two-cycle engine is provided. The engine, which may be of the direct fuel injection type, has a vertical crankshaft and a lubrication recess disposed generally adjacent to a throw of the crankshaft. The lubrication recess opens upwardly such that at least a portion of a connecting rod endcap passes over the recess.




The lubrication recess is preferably formed in an interior wall of the engine crankcase. Liquid oil may be directed to the lubrication recess by a guide groove that extends from an air intake of the crankcase to the lubrication recess.




The endcap preferably has one or more holes formed therethrough and providing an opening in an interior surface of the endcap and an opening in the exterior surface of the endcap. As the crankshaft rotates, the opening in the interior surface of the endcap preferably passes over the lubrication recess during a predetermined range of crankshaft rotation.




According to another aspect, a two-stroke engine has one or more cylinders with each cylinder having a piston, a vertical crankshaft, and a connecting rod that connects the piston to a throw of the crankshaft. The connecting rod has an endcap that allows it to connect to the crankshaft throw, the endcap having one or more oil holes formed therethrough thus providing fluid communication between an opening in an interior peripheral surface and an opening in an exterior peripheral surface of the endcap. A lubrication recess is formed adjacent the crankshaft and generally below a crankshaft throw. As the crankshaft rotates, each opening in the interior peripheral surface of the endcap to pass over the lubrication recess.




The crankshaft rotation can cause a pressure differential between the interior and exterior surfaces of the endcap sufficient to draw oil from within the lubrication recess upwardly and into the interior peripheral surface opening. The oil is then thrown through the exterior peripheral surface opening.




Another aspect of the present invention is directed to an outboard motor having a powerhead, a driveshaft housing depending from the powerhead, and a lower unit connect to and disposed below the driveshaft housing. The powerhead includes an internal combustion engine coupled to a propeller of the lower unit through a driveshaft extending through the driveshaft housing for propelling a watercraft. The internal combustion engine further has a cylinder block defining a cylinder bore and a cylinder head connected to the cylinder block. The cylinder head has a recess in one of its surfaces which cooperates with a piston surface and the cylinder bore to define a combustion chamber.




A vertical crankshaft is configured for rotation within a crankcase chamber formed, in part, by a crankcase member, and is coupled to the piston through a connecting rod that has a large end engaging the crankshaft and a small end engaging the piston. The crankcase member further defines an air intake passageway having an air and oil regulating valve disposed therein.




A lubrication recess is formed by the crankcase member and is disposed generally below the large end of the connecting rod during at least a range of the crankshaft rotation. The crankcase member further defines a guide groove configured to urge deposited lubricant to flow toward the lubricant recess.




The large end of the connecting rod draws lubricant from the lubricant recess and throws the lubricant within the crankcase chamber.




According to yet another aspect, a two-stroke internal combustion engine includes one or more cylinders and a piston for reciprocating within each cylinder. A connecting rod is rotatably coupled to each piston and is further coupled to a throw of a vertical crankshaft by an endcap. The crankshaft and connecting rod are disposed within a crankcase chamber.




One or more oil holes are formed radially through the endcap thereby providing fluid communication between a first opening disposed inwardly from an outer peripheral surface and a second opening in the outer peripheral surface of the endcap.




A lubrication recess can be disposed adjacent the crankshaft and generally below a throw of the crankshaft during at least a range of its rotation. Rotation of the crankshaft may cause lubricant from within the lubrication recess to be drawn into the first opening and discharged out of the second opening. Rotation of the crankshaft can cause a pressure differential sufficient to draw lubricant into the first opening. The lubricant can further be used to lubricate the coupling between the connecting rod and the throw of the crankshaft.




The crankshaft rotation can additionally or alternatively cause the endcap to splash the lubricant within the lubrication recess thereby forcing lubricant into the first opening.




A guide groove may be provided in a lower surface of the crankcase and extend generally from an air intake of the crankcase to the lubrication recess.




According to another aspect, a two-stroke internal combustion engine has one or more cylinder each having a piston for reciprocation therein. Each piston is rotatably coupled to a connecting rod which is, in turn, coupled to a throw of a crankshaft by an endcap. The crankshaft is disposed generally vertically within a crankcase chamber of the engine. A lubrication recess is disposed adjacent to the crankshaft and generally below a throw of the crankshaft.




Liquid oil within the crankcase chamber may collect within the lubrication recess, after which the endcap and/or connecting rod can throw the collected oil about the crankcase chamber.




According to yet another aspect, an outboard motor has an internal combustion engine with a crankshaft journaled for rotation within a crankcase and couple to a driveshaft for rotating a propeller connect to the driveshaft. The internal combustion engine includes means for causing oil to pool adjacent a throw of the crankshaft and means for redistributing pooled oil around the crankcase.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a schematic diagram illustrating the fuel and oil supply system of an engine in which one embodiment of the lubrication system of the present invention is invented.





FIG. 2

is a partial top plan and a cross-sectional view of the outboard motor illustrated in

FIG. 1

, showing a crankshaft and piston rod assembly with in a case of the engine.





FIG. 3

is an enlarged cross-sectional view of the crankshaft and piston rod assembly of FIG.


2


.





FIG. 4

is a partial sectional and side elevational view of the engine showing the crankshaft, piston rod assembly, and reed valves mounted to the crankcase of the engine.





FIG. 5

is an enlarged cross-sectional view of

FIG. 4

schematically showing a flow of air and oil through the reed valve and connecting rod assembly.





FIG. 6

is a front elevational view of the crankcase and crankshaft.





FIG. 7

is a front elevational view of a portion of the crankshaft removed from the engine.





FIG. 8A

is a top plan view of a connecting rod removed from the engine.





FIG. 8B

is a cross-sectional view taking along line B—B of FIG.


8


A.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT




In the following description, reference is made to the accompanying drawings which form a part of this written description which show, by way of illustration, specific embodiments in which the invention can be practiced. It is to be understood that other embodiments may be utilized and structural changes may be made without departing from the scope of the present invention. Where possible, the same reference numbers will be used throughout the drawings to refer to the same or like components. Numerous specific details are set forth in order to provide a thorough understanding of the present invention; however, it would be obvious to one skilled in the art that the present invention may be practiced without the specific details or with certain alternative equivalent devices and methods to those described herein. In other instances, well-known methods, procedures, components and devices have not been described in detail so as not to unnecessarily obscure aspects of the present invention.




With reference to

FIG. 1

, and initially Section A, an outboard motor constructed and operated in accordance with a preferred embodiment of the invention is depicted in a side elevational view and is identified generally by the reference numeral


100


. The entire outboard motor


100


is not depicted in that the swivel bracket and the clamping bracket which are associated with the driveshaft housing indicated generally by the reference numeral


102


are not illustrated. These components are well known in the are and thus the specific method by which the outboard motor


100


is mounted to the transom of an associated watercraft is not necessary to permit those skilled in the art to understand or practice the invention.




The outboard motor


100


includes a powerhead indicated generally by the reference numeral


104


. The powerhead


104


is positioned above the driveshaft housing


102


and includes a powering internal combustion engine indicated generally by the reference numeral


106


. The engine


106


is shown is more detail in the remaining three views of FIG.


1


and is described below with reference thereto.




The powerhead


104


is completed by a protective cowling formed by a main cowling member


108


and a lower tray


110


. The main cowling member


108


is detachably connected to the lower tray


110


. The lower tray


110


encircles an upper portion of the driveshaft housing


102


and a lower end of the engine


106


.




Positioned beneath the driveshaft housing


102


and coupled thereto is a lower unit


112


in which a propeller


114


which forms the propulsion device for the associated watercraft is journaled. As is typical with outboard motor practice, the engine


106


is supported in the powerhead


104


so that its crankshaft


116


(see Section B of

FIG. 1

) rotates about a vertically extending axis. This facilitates connection of the crankshaft


116


to a driveshaft which extends into the lower unit


112


and which drives the propeller


114


through a conventional forward-neutral-reverse transmission contained in the lower unit


112


.




The details of the construction of the outboard motor


100


and the components which are not illustrated may be considered to be conventional or of any type known to those wishing to utilize the invention disclosed herein. Those skilled in the art can readily refer to any known constructions of such with which to practice the invention.




With reference now in detail to the construction of the engine


106


still by primary reference to

FIG. 1

, the illustrated embodiment of the engine


106


is of the V6-type and operates on a two-stroke crankcase compression principal. Although the invention is described in conjunction with an engine having a particular cylinder number and cylinder configuration, it will be readily apparent that the invention can be utilized with engines having other cylinder numbers and other cylinder configurations. Also, although the engine


106


is described as operating on a two-stroke principal, it will also be apparent to those skilled in the art that certain facets of the invention can be employed in conjunction with four-stroke engines. Some features of the invention may also be employed with rotary-type engines.




With reference primarily to Sections B and D of

FIG. 1

, the engine


106


comprises a cylinder block


118


that is formed with a pair of cylinder banks


120


. Each of the cylinder banks


120


comprises three vertically spaced, horizontally extending cylinder bores


122


. The cylinder bores


122


are numbered #


1


-


6


from top to bottom and will be referred to individually as cylinder


1


, cylinder


2


, etc. Pistons


124


reciprocate in the cylinder bores


122


. The pistons


124


are in turn connected to the upper or small ends of connecting rods


126


. The big ends of these connecting rods are journaled on the throws of the crankshaft


116


in a manner that is well-known in the art.




The crankshaft


116


is journaled in a suitable manner for rotation within a crankcase chamber


128


that is formed by part of the cylinder block


118


and by the crankcase member


130


. The crankcase member


130


is affixed to the cylinder block


118


in a suitable manner. As is typical with two-cycle engines, the crankshaft


116


, cylinder block


130


, and crankcase member


130


are formed with seals so that each section of the crankcase


128


which is associated with one of the cylinder bores


122


, is sealed from the other sections. This type of construction is well-known in the art.




With additional reference to

FIG. 2

, a cylinder head assembly, indicated generally by the reference numeral


202


, is affixed to an end of each cylinder bank


120


that is spaced from the crankcase chamber


128


. The cylinder head assemblies


202


comprise a main cylinder head member


204


that defines a plurality of recesses


206


on its inner face. Each of these recesses


206


cooperate with a respective cylinder bore


122


and the head of the piston


124


to define the combustion chambers of the engine as is well known in the art. A cylinder head cover member


208


completes the cylinder head assembly


202


. The cylinder head members


204


,


208


are affixed to each other and to the respective cylinder banks


120


in a suitable known manner.




With reference again primarily to

FIG. 1

, Sections B and C, an air induction system indicated generally by the reference numeral


132


is provided for delivery of an air charge to the sections of the crankcase chamber


128


associated with each of the cylinder bores


122


. This communication is via an intake port


134


formed in the crankcase member


130


and registering with each such crankcase chamber section.




The induction system


132


includes an air silencing and inlet device shown schematically in this FIG.


1


and indicated by the reference numeral


136


. The device


136


is typically contained within the cowling


108


at the forward end thereof and has a rearwardly facing air inlet opening


138


through which air is drawn. Air is admitted into the interior of the cowling


108


in a known manner such as primarily through a pair of rearwardly positioned air inlets as is generally well-known in the art.




The air inlet device


136


supplies the induced air through a plurality of throttle bodies


140


, each of which includes a throttle valve


142


positioned therein. The throttles valves


142


are supported for rotation on throttle valve shafts (not shown). The throttle valve shafts are linked to each other for simultaneous opening and closing of the throttle valves


142


in a manner well-known in the art.




As is also typical in two-cycle engine practice, the intake ports


134


are provided with reed-type check valves


144


. The check valves


144


permit air to flow into the sections of the crankcase chamber


128


when the pistons


124


are moving toward the recesses


206


in their respective cylinder bores


122


. As the pistons


124


move toward the crankcase


128


, the charge is compressed in the sections of the crankcase chamber


128


. At that time, the reed-type check valve


144


closes so as to permit the charge to be compressed.




In accordance with at least one preferred embodiment of the present invention, an oil pump


146


pumps oil to a solenoid valve unit


150


through an oil delivery hose


151


. In one preferred embodiment, the oil pump


146


is driven by the crankshaft


116


; however, an electric oil pump may be used in the alternative. The solenoid valve unit


150


may regulate the delivery of oil to the throttle body


140


of each cylinder


122


, in which case, the oil passes through the throttle body


140


and into the crankcase chamber


128


to lubricate the components of each cylinder


122


. The air charge, which is compressed in the sections of the crankcase chamber


128


, is then transferred to the combustion chamber through a scavenging system (not shown) in a manner that is well known.




A sparkplug


152


is mounted in the cylinder head assembly


202


for each cylinder bore. The sparkplug


152


is fired under control of an ECU


148


(electronic control unit). The ECU


148


receives certain signals for controlling the timing of firing of the sparkplugs


152


in accordance with any desired control strategy.




The sparkplug


152


ignites a fuel-air charge that is formed by mixing the intake air with fuel supplied from a fuel delivery system


154


. With reference to Section C and D of

FIG. 1

, the fuel supply system


154


is configured to supply fuel to the combustion chambers through fuel injectors


156


. In the illustrated embodiment, the fuel system


154


comprises a main fuel supply tank


158


that is provided in the hull of the watercraft with which the outboard motor


100


is associated. Fuel is drawn from this tank


158


through a conduit


160


by a first low pressure pump


162


and a plurality of second low pressure pumps


164


. The first low pressure pump


162


is a manually operated pump and the second low pressure pumps


164


are diaphragm-type pumps operated by variations in pressure in the sections of the crankcase chamber


128


and thus provide a relatively low pressure. A quick disconnect coupling is provided in the conduit


160


and a fuel filter


166


is positioned in the conduit


160


in an appropriate location.




From the low pressure pump


164


fuel is supplied through a vapor separator


168


which is mounted on the engine


106


or within the cowling


108


at an appropriate location. This fuel is supplied through a line


169


and a float valve regulates fuel flow through the line


169


. The float valve is operated by a float that is disposed within the vapor separator


168


so as to maintain a generally constant level of fuel in the vapor separator


168


.




A high pressure electric fuel pump


170


is provided in the vapor separator


168


and pressurizes fuel that is delivered through a fuel supply line


171


to a high pressure fuel pump indicated generally by the reference numeral


172


. The electric fuel pump


170


which is driven by an electric motor develops a pressure such as within the range of from about 3 to about 10 kg/cm


2


. A low pressure regulator


170


A is positioned in the line


171


at the vapor separator


168


and limits the pressure that is delivered to the high pressure fuel pump


172


by dumping the fuel back to the vapor separator


168


.




With reference to Section D of

FIG. 1

, fuel is supplied from the high pressure fuel pump


172


to a pair of vertically extending fuel rails


173


through a flexible pipe


173


A. The pressure in the high pressure pump


172


is regulated by a high pressure regulator


174


which dumps fuel back to the vapor separator


168


through a pressure relief line


175


in which a fuel heat exchanger or cooler


176


may be provided.




After the fuel charge has been formed in the combustion chamber by the injection of fuel from the fuel injectors


156


, the charge is fired by firing sparkplugs


152


. The injection timing and duration, as well as the control for the timing of firing of the sparkplugs


152


are controlled by the ECU


148


.




As the charge burns and expands, the pistons


124


are driven toward the crankcase chamber


128


in the cylinder bores


122


until the pistons


124


reach the lower most position (i.e., bottom dead center). Through this movement, an exhaust port (not shown) is opened to communicate with an exhaust passage


177


formed in the cylinder block


118


. The exhaust gases flow through the exhaust passages


177


to collector sections of respective exhaust manifolds that are formed within the cylinder block


118


. These exhaust manifold collector sections communicate with exhaust passages formed in an exhaust guide plate on which the engine


106


is mounted.




The ECU


148


controls the timing and duration of fuel injection. The ECU


148


thus controls the opening and closing of the solenoid valves of the fuel injectors


156


and in particular controls the selective supply of current to the solenoids of the fuel injectors


156


.




A pair of exhaust pipes


178


extend the exhaust passages


177


into an expansion chamber


179


formed in the driveshaft housing


102


. From this expansion chamber


179


, the exhaust gases are discharged to the atmosphere through a suitable exhaust system. The length of the exhaust pipes


178


from the cylinder


122


to the head of the exhaust pipe


178


differs between some or all of the cylinders


122


. As is well-known in outboard motor practice, this may include an underwater, high-speed, exhaust gas discharge and an above-water low speed exhaust gas discharge. Since these types of systems are well-known in the art, further description is not necessary to permit those skilled in the art to practice the invention.




Any type of desired controlled strategy can be employed for controlling the time and duration of fuel injection from the injectors


154


and timing of firing of the sparkplug


152


. However, a general discussion of some engine conditions and other ambient conditions that can be sensed for engine control will follow. It is to be understood, however, that those skilled in the art will readily understand how various control strategies can be employed in conjunction with the components of the invention.




The control for the fuel air ratio preferably includes a feedback control system. Thus, a combustion condition or oxygen sensor


180


is provided and determines the in-cylinder combustion conditions by sensing the residual amount of oxygen in the combustion products at about a time when the exhaust port is opened. This output signal is carried by a line to the ECU


148


as schematically illustrated in FIG.


1


.




As shown in Section B of

FIG. 1

, a crank angle position sensor


181


measures the crank angle and transmits it to the ECU


148


as schematically indicated. Engine load as determined by throttle angle of the throttle valve


142


is sensed by a throttle position sensor


182


which outputs a throttle position or load signal to the ECU


148


.




There is also provided a pressure sensor


183


communicating with the fuel line connected to the pressure regulator


174


. This pressure sensor


183


outputs the high-pressure fuel signal to the ECU


148


. Further, an intake air temperature sensor


185


may be provided when this sensor


185


outputs an intake air temperature signal to the ECU


148


.




The sense conditions are merely some of those conditions which may be sensed for engine control and it is, of course, practicable to provide other sensors such as, for example, but without limitation, an engine height sensor, a knock sensor, a neutral sensor, a watercraft pitch sensor and an atmospheric temperature sensor in accordance with various control strategies.




The ECU


148


computes and processes the detection signals of each sensor based on a control strategy. The ECU


148


forwards control signals to the fuel injector


156


, sparkplug


152


, the electromagnetic solenoid valve unit


150


and the high-pressure electric fuel pump


170


for their respective control. These control signals are carried by respective control lines that are indicated schematically in FIG.


1


.




With reference to Section C of

FIG. 1

, an oil subtank


187


located in the hull of the watercraft serves as a reservoir of lubrication oil for the engine


106


. A suitable delivery pump supplies oil from the oil subtank


187


through the oil supply pipe


187


A to a main oil tank


188


mounted to the side of the cylinder block


118


. The delivery pump can, for example, be located within the oil subtank


187


or can be positioned within the supply pipe


187


A and can be either electrically or mechanically driven. An oil feedpipe


189


supplies oil from the bottom of the main oil tank


188


to the oil pump


146


. The oil pump


146


in turn supplies oil to the solenoid valve unit


150


which regulates the flow of oil to the cylinders. The solenoid valve unit


150


is preferably controlled via control signals from the ECU


148


.




In one preferred embodiment, oil is also delivered directly to the vapor separator chamber


168


. A premixing oil pump


193


draws oil from the oil feedpipe


189


and through a premixing oil filter


195


. The oil also passes through a reed-type check valve


197


and is then delivered to the vapor separator chamber


168


through oil conduit


190


. The addition of a small amount of oil to the fuel of a fuel-injected engine has been found to inhibit the formation of deposits on fuel injectors


154


and to extend their useful life. The addition of oil may also help prevent corrosion when water is present in the system. The oil delivered directly to the combustion chamber with the fuel charge can also help to lubricate the components of the fuel system.




In at least one embodiment, a plurality of oil conduits


151


are provided for delivering oil to a plurality of solenoid valve units


150


which correspond to the number of cylinders


122


in the engine


106


. The oil supply pipes


151


are preferably configured so that their lengths are as short as possible to minimize the distance the oil must travel to the air induction system


132


for each cylinder


122


.




In one preferred embodiment, the oil pump


146


is a positive displacement-type oil pump that is driven by the crankshaft


116


. A positive displacement type oil pump delivers a volume of oil for each crankshaft revolution as opposed to, for example, an impeller-type pump that supplies an approximate pressure of oil based upon engine speed.




The oil delivered through the oil supply pipe


151


is regulated by the solenoid valve unit


150


for delivery into the air intake passage


135


. Preferably, the oil is sprayed into the air intake passage


135


as a mist, such that the oil is carried by the intake air passing through the air intake passage


135


. The air thus carries misted oil into the crankcase chamber


128


and subsequently into the combustion chamber


206


.




With reference to

FIGS. 2 and 3

, the intake silencer


136


includes an opening for allowing intake air to enter therein. The air flows through the intake silencer


136


and is regulated by throttle valves


142


within the throttle body


140


. The air intake passageway


135


is partially defined by a left side part


220


and a right side part


222


that each hold one or more oil delivery pipes


151


. The oil delivery pipes


151


regulate the delivery of oil into the intake air as previously described.




A reed-valve unit


143


comprises a reed valve holder


145


which carries a number of reed valves


144


, which typically correspond in number to the number of engine cylinders. The intake air is drawn through the reed valves


144


and into the crankcase chamber


128


as the piston


124


reciprocates upwardly thereby causing a negative pressure within the crankcase chamber


128


.




The crankshaft


116


is journaled for rotation within the crankcase chamber


118


and has a number of throws


224


each of which are connected to a connecting rod


126


. The connecting rod


126


typically terminates in a semi-circular concave inner peripheral surface that corresponds to a portion of the crankshaft throw


224


. An endcap


226


cooperates with the connecting rod


126


to circumscribe the crankshaft throw


224


.




A plurality of roller bearings


228


are interposed between the interior peripheral surface


230


of the connecting rod


126


and the crankshaft


116


. Alternatively, the connecting rod


126


may engage the crankshaft throw


225


through other means, as are known in the art. The connecting rod


126


opposing end, or small end


230


, is rotatably connected to a piston


124


as previously described.




Referring to

FIGS. 4 and 7

, the crankshaft


116


includes a plurality of webs


234


that cooperate with the cylinder block


121


and crankcase member


130


to separate and substantially seal each crankshaft throw


224


and associated connecting rod


126


within individual portions of the crankcase chamber


128


. The air induction system delivers intake air to each of these individual portions of the crankcase chamber


128






As shown in

FIG. 5

, the reed-type check valve


144


comprises a reed valve unit


143


having a reed valve holder


145


configured to carry a reed


236


. The reeds


236


are biased in a closed position against a frame


238


. In this orientation, the crankcase chamber


128


is closed such that air within the crankcase chamber


128


can be compressed. As the piston


124


moves away from the crankshaft


116


toward its uppermost limit (i.e., top dead center), the volume within the crankcase chamber


128


increases, thereby creating a negative pressure and drawing air into the crankcase chamber


128


from the intake passageway


125


. This air pressure causes the reeds


236


to open away from the frame


238


to thereby allow air to enter the crankcase chamber


128


. The reed's


236


travel limit is defined by a stopper plate


240


attached to the reed-valve holder


145


such as by mounting screws


242


.




Referencing

FIGS. 4-6

, the crankcase bottom wall


244


preferably includes a lubricant guide groove


246


formed therein leading to a lubricant recess


250


. As shown additionally in

FIGS. 2 and 3

, the lubricant recess


250


is semi-circular, and extends around a portion of the perimeter of the crankshaft


116


. The sides of the lubricant recess


250


are defined by an outer sidewall


252


which, in one embodiment, is a substantially vertical portion of the crankcase bottom wall


244


, and by an outer peripheral surface


254


of the crankshaft web


234


forming the inner boundary. In at least one embodiment, the outer peripheral surface


254


of the crankshaft web


234


has a draft angle that inclines away from the center of the lubricant recess


250


, discussed below in greater detail.




The lubricant guide groove


246


extends from approximately below the inner extremity of the reed valve


144


to the lubricant recess


250


and is configured so as to urge lubricant to flow toward the crankshaft


116


. During engine operation, a quantity of oil discharged by the oil delivery pipe


151


deposits on the components within the intake passageway


135


. Such oil deposition occurs more quickly when the mist moves more slowly, such as when the engine is operating at lower speeds, including idling speed. The oil, under gravitational force, will tend to collect at the lower crankcase bottom wall


244


.




Accordingly, the lubricant guide groove


246


is configured to direct this collecting oil to flow toward the lubricant recess


250


. In one embodiment, the lubricant guide groove


246


slopes downwardly toward the lubricant recess


250


to urge the oil to flow in that direction. The oil is further urged through the lubricant guide groove


246


by the intake air. For example, as the piston


124


moves toward the combustion chamber


206


, the intake air is drawn in through the intake passageway


135


and through the reed valve


144


which tends to push the deposited oil along the lubricant groove


246


toward the lubricant recess


250


. Further, as the deposited oil collects in the lubricant recess


250


, it is urged toward the outer peripheral surface


254


of the crankshaft web


234


.




The connecting rod endcap


226


, during a range of its rotational movement, is disposed above, and in close proximity to, the lubricant recess


250


. As such, the connecting rod endcap


226


contacts the collected oil in the lubricant recess


250


. As the crankshaft


116


rotates, a centrifugal force causes the oil deposited on the connecting rod endcap


226


to be thrown around the interior of the crankcase chamber


128


.




Referencing

FIGS. 5 and 8

, the connecting rod


126


has a small end


230


configured for rotatable attachment to a piston


124


. The opposing end includes an endcap


226


formed with one or more oil holes


232


therethrough. The oil holes extend from an inner peripheral surface


256


to an outer peripheral surface


258


of the endcap


226


and permit fluid communication therebetween. In at least one embodiment, the inner peripheral surface


256


of the endcap


226


is directly above the lubricant recess


250


during a range as the crankshaft rotates. This location of the inner oil hole


232


opening facilitates oil draw upwardly into the roller bearing space


262


.




Thus, as the crankshaft


116


rotates, oil that is deposited onto the inner peripheral surface


256


of the endcap


226


flows upwardly into the roller bearing space


262


and is exits the oil hole


232


as shown by the arrows of FIG.


5


. The rotation of the crankshaft


116


causes air turbulence above the lubricant recess


250


and causes the oil deposited within the lubricant recess to flow within the lubricant recess


250


in a direction corresponding to the direction of rotation of the crankshaft.




For example, if the crankshaft


116


rotates in a clockwise direction, the oil within the lubricant recess


250


will tend to flow within the lubricant recess


250


in a clockwise direction and will thus collect toward a clockwise end


260


(

FIG. 3

) of the lubricant recess


250


. Accordingly, there may be a greater volume of oil collecting in this portion of the lubricant recess


250


. As the endcap


226


approaches the clockwise end


260


of the lubricant recess


250


, the available volume for the oil to occupy will be reduced and will thus cause the oil to flow rather than be subjected to compressive forces. The oil will therefore be forced to flow in a counter-clockwise direction within the lubricant recess


250


, or upwardly into the roller bearing space


262


between the endcap


226


and the crankshaft throw


224


. Typically, oil will flow both upwardly into the roller bearing space


262


and within the lubricant recess


250


. The outer peripheral surface


254


of the crankshaft throw


224


further aids the upward flowing of oil into the roller bearing space


262


.




As the oil flows into the roller bearing space


262


, it not only provides a direct lubrication to the roller bearings


228


contained therein, but is also thrown outwardly through the oil holes


232


as the crankshaft


116


rotates and becomes deposited onto the various components within the crankcase chamber


128


, thus providing additional lubrication to the engine components, even during periods of relatively slow operation. Moreover, oil is free to enter the roller bearing space


262


from above the endcap


256


and flow downward to provide further lubrication to roller bearings


228


and be thrown through the oil holes


232


.




In addition to the contact of the endcap


256


directly with the oil in the lubricant recess


250


that causes the oil to flow into the roller bearing space


262


, air pressure also urges the oil to flow upwardly into the roller bearing space


262


. As the crankshaft


116


rotates, even at a slow rpm, such as, for example, 1000 rpm, a pressure differential is created between the inner peripheral surface


256


and the outer peripheral surface


258


of the endcap since a point on the outer peripheral surface


258


is traveling at a greater tangential velocity than a corresponding point on the inner peripheral surface


256


. Thus, according to Bernoulli's principal, the air pressure differential will cause air and oil to flow from the region of relatively higher pressure at the interior peripheral surface


256


of the endcap


226


to the region of lower pressure at the outer peripheral surface


258


of the endcap


226


.




This air pressure differential can also cause air to circulate from within the roller bearing space


262


outwardly through the oil holes


232


. Consequently, the moving air will draw oil from the lubricant recess


250


up into the bearing space


262


which will then be thrown out the oil holes


232


. The drawing of liquid oil from the lubricant recess


250


is further enhanced by the draft angle of the outer peripheral surface


254


of the crankshaft web


234


. As an air flow path is established by the pressure differential, the rushing air will cause oil within the lubricant recess


250


to flow up the incline of the outer peripheral surface


254


and into the roller bearing space


262


where it will flow through the oil holes


232


and be thrown about the crankcase chamber


128


.




Once the oil is thrown throughout the crankcase chamber


128


, it may again collect at the crankcase bottom wall


244


through gravity and be recirculated throughout the crankcase chamber


128


as described herein. Additionally, especially during periods of slower operation when there may be insufficient oil entrained in the intake air, oil thrown around the crankcase chamber


128


may become entrained in the intake air and thus provide increased lubrication to the combustion chamber


206


and related components.




Thus, an improved lubrication system includes a crankcase


130


which may have a lubricant guide groove


246


and/or a lubricant recess


250


formed therein. A connecting rod


126


may include oil holes


232


formed through the connecting rod endcap


226


. At least one embodiment of the improved lubrication system is configured to redistribute oil collecting within the intake passageway


135


and crankcase chamber


128


to the roller bearings


228


and other various components disposed within the crankcase chamber


128


.




Although this invention has been disclosed in the context of certain preferred embodiments and examples, it will be understood by those skilled in the art that the present invention extends beyond the specifically disclosed embodiments to other alternative embodiments and/or uses of the invention and obvious modifications and equivalents thereof. In addition, while a number of variations of the invention have been shown and described in detail, other modifications, which are within the scope of this invention, will be readily apparent to those of skill in the art based upon this disclosure. It is also contemplated that various combinations or subcombinations of the specific features and aspects of the embodiments may be made and still fall within the scope of the invention. Accordingly, it should be understood that various features and aspects of the disclosed embodiments can be combined with or substituted for one another in order to form varying modes of the disclosed invention. Thus, it is intended that the scope of the present invention herein disclosed should not be limited by the particular disclosed embodiments described above, but should be determined only by a fair reading of the claims that follow.



Claims
  • 1. A lubrication system for a two-cycle engine comprising a vertical crankshaft and a lubrication recess disposed generally adjacent to a throw of said crankshaft which opens upwardly such that at least a portion of an endcap of a connecting rod connected to said throw of said crankshaft passes over said recess.
  • 2. The lubrication system of claim 1, wherein said lubrication recess is formed in an interior wall of a crankcase of said two-cycle engine.
  • 3. The lubrication system of claim 2, further comprising a guide groove extending generally from an air intake of said crankcase to said lubrication recess formed in said interior wall of said crankcase.
  • 4. The lubrication system of claim 1, wherein said endcap includes a hole formed therethrough thereby providing an opening in an interior surface of said endcap and an opening in an exterior surface of said endcap.
  • 5. The lubrication system of claim 4, wherein said opening in said interior surface of said endcap passes over said lubrication recess during a predetermined range of crankshaft rotation.
  • 6. The lubrication system of claim 1, wherein said two-cycle engine is a direct fuel injection engine.
  • 7. A two-stroke internal combustion engine comprising one or more cylinders wherein each cylinder has a piston for reciprocation therein, a connecting rod rotatably coupled to each piston and further including an endcap to facilitate coupling of the connecting rod to a throw of a crankshaft, wherein the crankshaft is disposed generally vertically, a lubrication recess disposed adjacent to the crankshaft and generally below a throw of the crankshaft, one or more oil holes formed through the endcap thereby providing fluid communication between an opening in an interior peripheral surface and an opening in an exterior peripheral surface of the endcap, wherein rotation of the crankshaft causes each opening in the interior peripheral surface of the endcap to pass over the lubrication recess.
  • 8. The two-stroke internal combustion engine of claim 7, wherein the rotation of the crankshaft causes a pressure differential between the interior surface of the endcap and the exterior surface of the endcap such that oil from within the recess is drawn upwardly and into the interior peripheral surface opening and is thrown through the exterior peripheral surface opening.
  • 9. An outboard motor having a powerhead, a driveshaft housing depending from the powerhead, and a lower unit connected to and disposed below the driveshaft housing, the powerhead including an internal combustion engine coupled to a propeller of the lower unit through a driveshaft extending through the driveshaft housing for propelling a watercraft, the internal combustion engine comprising a cylinder block defining a cylinder bore and a cylinder head connected to the cylinder block, the cylinder head further defining a recess in a lower surface thereof, a piston configured for reciprocation within said cylinder bore, wherein a surface of said piston cooperates with the cylinder bore and recess to define a combustion chamber, a crankshaft disposed generally vertically and coupled to the piston through a connecting rod having a large end engaging the crankshaft and a small end engaging the piston, wherein the crankshaft is configured for rotation within a crankcase chamber defined, in part, by a crankcase member, the crankcase member further defining an air intake passageway having a valve disposed therein for regulating the delivery of air and oil to the crankcase chamber, the crankcase member further defining a lubricant recess disposed generally below the large end of the connecting rod during at least a range of the crankshaft rotation and further defining a guide groove configured to urge deposited lubricant to flow toward the lubricant recess, and wherein the large end of the connecting rod draws lubricant from the lubricant recess and throws the lubricant within the crankcase chamber.
  • 10. A two-stroke internal combustion engine comprising one or more cylinders wherein each cylinder has a piston for reciprocation therein, a connecting rod rotatably coupled to each piston and further including an endcap to facilitate coupling of the connecting rod to a throw of a crankshaft, wherein the crankshaft is disposed generally vertically within a crankcase chamber, and one or more holes formed radially through the endcap thereby providing fluid communication between a first opening disposed inwardly from an outer peripheral surface and a second opening in the outer peripheral surface of the endcap.
  • 11. The two-stroke internal combustion engine of claim 10, further comprising a lubrication recess disposed adjacent the crankshaft and generally below a throw of the crankshaft during at least a range of its rotation.
  • 12. The two-stroke internal combustion engine of claim 11, wherein rotation of the crankshaft causes lubricant from within the lubrication recess to be drawn into the first opening and discharged out the second opening.
  • 13. The two-stroke internal combustion engine of claim 12, wherein lubricant drawn into the first opening lubricates the coupling between the connecting rod and the crankshaft throw.
  • 14. The two-stroke internal combustion engine of claim 12, wherein lubrication is drawn into the first opening by a pressure differential caused by the rotation of the crankshaft.
  • 15. The two-stroke internal combustion engine of claim 11, wherein rotation of the crankshaft causes the endcap to splash the lubricant within the lubrication recess thereby forcing lubricant into the first opening.
  • 16. The two-stroke internal combustion engine of claim 11, further comprising a guide groove formed in a lower surface of the crankcase and extending generally from an air intake of the crankcase to the lubrication recess.
  • 17. A two-stroke internal combustion engine comprising one or more cylinders wherein each cylinder has a piston for reciprocation therein, a connecting rod rotatably coupled to each piston and further including an endcap to facilitate coupling of the connecting rod to a throw of a crankshaft, wherein the crankshaft is disposed generally vertically within a crankcase chamber, and a lubrication recess disposed adjacent to the crankshaft and generally below a throw of the crankshaft.
  • 18. The two-stroke internal combustion engine of claim 17, wherein liquid oil within the crankcase chamber collects in the lubrication recess.
  • 19. The two-stroke internal combustion engine of claim 18, wherein the endcap and/or connecting rod throw oil from within the lubrication recess about the crankcase chamber.
  • 20. An outboard motor having an internal combustion engine with a crankshaft journaled for rotation within a crankcase and coupled to a driveshaft for rotating a propeller connected to the driveshaft, the internal combustion engine comprising means for causing oil to pool adjacent a throw of the crankshaft, and means for redistributing pooled oil around the crankcase.
Priority Claims (1)
Number Date Country Kind
2001-301620 Sep 2001 JP
US Referenced Citations (3)
Number Name Date Kind
5617822 Masuda Apr 1997 A
5806631 Yoshida et al. Sep 1998 A
5887678 Lavender Mar 1999 A