Engine lift for outboard motor

Information

  • Patent Grant
  • 6168482
  • Patent Number
    6,168,482
  • Date Filed
    Monday, May 17, 1999
    25 years ago
  • Date Issued
    Tuesday, January 2, 2001
    23 years ago
Abstract
An outboard motor generally comprises a power head. An engine is mountable within an engine compartment defined within the power head. The engine is lifting into and out of the engine compartment in part through the use of lifting lugs. The engine may have one or more lifting lugs positioned in various locations for use in suspending the engine from ropes or chains during installation. The lifting lugs may attach to an upper surface of the engine, a portion of the flywheel or a drive unit of a high pressure fuel pump. The lifting lugs may also be positioned in dead space such as that between cylinder banks of a v-type engine. Moreover, the lifting lugs may be removable or pivotable to reduce the protrusion of the lifting jugs from the engine when the outboard motor is in use.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention generally relates to lift arrangements for engines of outboard motors. More particularly, the present invention relates to lift arrangements for engines for use during installation and maintenance of outboard motor engines.




2. Description of Related Art




Watercraft powered by outboard motors use internal combustion engines mounted within the outboard motor for providing power output to a propulsion device such as a propeller. In assembling the outboard motor, the engine must be positioned within an engine compartment located within a cowling portion of the outboard motor. To lift the engine and to orient the engine properly, the engine may be provided with at least one lifting hook. Typically, the lifting hook is attached to the engine proximate the cylinder block, the crankcase and the cylinder head. In such embodiments, a rope, chain or the like is attached to the lifting hook such that the engine may be raised from, or positioned within, the cowling area of the outboard motor. Lifting the engine may be necessary for routine maintenance, assembly and the like.




As the size and complexity of outboard motors has increased, the difficulties associated with mounting such engines into the outboard motors has also increased. For example, with the recent introduction of two-cycle V-type six-cylinder direct-injection engines into outboard motors, the number of components attached to the engine block has exploded. The engines feature a high-pressure fuel system that is attached to the engine and that protrudes significantly from the contours of previous engine structures. Due to both this increase in parts and the complexity of the assembly procedures associated with the engines, the space allocated to the lifting hook in such engines has decreased. Moreover, the ropes and/or chains used to raise and lower the engine may impact the engine and peripheral components and damage sensitive connections and couplings as a result of the inadvertent contact. Furthermore, as the weight and size of the engines has increased, the size of the hanger has also had to increase. Accordingly, the hanger now protrudes to a large degree from the side of the engine in some embodiments. This large protrusion requires an enlarged cowling region and an overall increase in outboard motor size and weight.




SUMMARY OF THE INVENTION




Accordingly, it is desired to have an outboard motor engine lift apparatus that may reduce the protrusion of the apparatus from the engine, as well as one that may be accommodated by engines having varying peripheral components. Moreover, the apparatus should be located in a region of the engine which allows ease of assembly and manufacture of the engine while also facilitating ease of insertion and orientation of the engine within the outboard motor.




One aspect of the present invention involves an engine for an outboard motor. The engine comprises a generally vertically oriented crankshaft and a flywheel connected to the crankshaft. A peripheral component is attached to a portion of the engine. A driven sprocket is connected to the peripheral component and arranged to power the peripheral component. A drive sprocket is attached to the flywheel with a flexible drive loop extending between and rotatably coupling the drive sprocket to the driven sprocket. A lifting lug is removably connected to one of the flywheel or the drive sprocket.




Another aspect of the present invention involves an engine for an outboard motor. The engine comprises a crankshaft, a flywheel attached to the crankshaft, and a peripheral component attached to a portion of the engine. A driven sprocket is connected to the peripheral component and is arranged to power the peripheral component. A drive sprocket is attached to the flywheel with a flexible drive member coupling the drive sprocket to the driven sprocket. A lifting lug is positioned generally between the drive sprocket and the driven sprocket.




A further aspect of the present invention involves an outboard motor. The outboard motor comprises a power head, an engine compartment defined within the power head and an engine mounted within the engine compartment. The engine comprises a crankshaft, a crankcase encasing the crankshaft and a flywheel attached to the crankshaft. The crankcase is attached to a cylinder block with a pair of cylinder banks positioned within the cylinder block. A removable lifting lug and a pivotable lifting lug are also attached to the engine. One of the removable lifting lug and the pivotable lifting lug is positioned generally above the crankshaft and the other of the removable lifting lug and the pivotable lifting lug is positioned generally rearward of the crankshaft.











BRIEF DESCRIPTION OF THE DRAWINGS




These and other features, aspects and advantages of the present invention will now be described with reference to the drawings of several preferred embodiments, which embodiments are intended to illustrate and not to limit the invention, and in which drawings:





FIG. 1

is a side view of an outboard motor attached to a transom of a watercraft, which is shown in partial section, having certain internal components illustrated with hidden lines;





FIG. 2

is a top view of the outboard motor of

FIG. 1

having certain internal components illustrated with hidden lines;





FIG. 3A

is a top view of a high pressure fuel pump drive arrangement including a lifting lug support assembly;





FIG. 3B

is a side view of the arrangement of

FIG. 3A

;





FIG. 4A

is a top view of the embodiment of

FIG. 3A

with a removable lifting lug installed within the lifting lug support assembly;





FIG. 4B

is a side view in partial section taken along the line


4


B—


4


B in

FIG. 4A

;





FIG. 5A

is an exploded side view of a secondary pivoting lifting lug having features, aspects and advantages in accordance with the present invention;





FIG. 5B

is a side view of the pivoting lifting lug of

FIG. 5A

;





FIG. 6A

is a partially sectioned side view of the pivoting lifting lug shown in

FIG. 5A

assembled and affixed to an engine block;





FIG. 6B

is a partially sectioned side view of the pivoting lifting lug shown in

FIG. 5A

in a stowed configuration;





FIG. 7A

is an exploded side view of another lifting lug support assembly illustrated with a removable lifting lug removed from the assembly;





FIG. 7B

is a partially sectioned side view of the arrangement of

FIG. 7A

;





FIG. 7C

is a partially sectioned side view of the lifting lug support assembly of

FIG. 7A

with a removable lifting lug installed in the lifting lug support assembly of

FIG. 7A

;





FIG. 8A

is a top view of another removable lifting lug installed within a lifting lug support assembly;





FIG. 8B

is a side view of the removable lifting lug and lifting lug support assembly shown in

FIG. 8A

;





FIG. 8C

is a top view of a high pressure fuel pump drive arrangement including a lifting lug support assembly similar to that illustrated in

FIG. 8A

;





FIG. 8D

is a side view of the arrangement of

FIG. 8C

;





FIG. 8E

is a top view of yet another removable lifting lug installed within a lifting lug support assembly similar to that illustrated in

FIG. 8A

; and,





FIG. 8F

is a side view of the removable lifting lug and lifting lug support assembly shown in FIG.


8


E.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS OF THE INVENTION




With initial reference to

FIG. 1

, an outboard motor for powering watercraft is illustrated therein. The outboard motor, indicated generally by the reference numeral


10


, advantageously features a lift arrangement having certain features, aspects and advantages of the present invention. The outboard motor


10


provides an exemplary environment in which the present lift arrangement has particular utility. Other environments of use may readily present themselves to individuals having ordinary skill in the relevant arts. The lift assembly includes one or more lifting lug. The term lifting lug as used herein shall refer to any of a number of mechanical arrangements providing a specific component or structure sized and configured specifically for being gripped for lifting. Accordingly, lifting lugs should be construed to include, but not be limited to, curved clutches, dogs, hooks, claws, clasps, curved members, stays, eyelets, eyebolts, rings, t-bolts, and the like.




With continued reference to

FIG. 1

, the illustrated outboard motor


10


generally comprises a power head


12


having a lower tray portion


14


and an upper cowling portion


16


. The power head components may be manufactured of any suitable material, including, without limitation, reinforced plastics, fiberglass and metals, in any known manner. The lower tray portion


14


and the upper cowling portion


16


preferably are joined together to form a power head area


12


that is substantially weatherproof and water spray resistant. For instance, a rubber seal (not shown) may be positioned in the joining region. Additionally, the lower tray portion


14


and the upper cowling portion generally form an engine compartment


17


in which an engine is positioned and somewhat protected.




An air vent or air inlet area


18


, which may be rearward facing, is provided in the illustrated upper cowling portion


16


. Air may enter through the vent


18


for induction into an internal combustion engine


20


that is preferably arranged and encased within the power head


12


. The air vent


18


may also allow heated air to be exhausted from within the power head


12


after circulation within the power head


12


.




With continued reference to

FIG. 1

, the illustrated outboard motor


10


also includes a lower unit


22


extending downwardly from the lower tray portion


14


of the power head area


12


. The illustrated lower unit


22


generally comprises an enlarged upper casing


24


and a narrower lower casing


26


. Generally, the illustrated upper casing


24


is connected to the lower tray portion


14


through an apron


28


, which encases the lower unit


22


and supports the lower tray portion


14


.




The illustrated outboard motor is generally attached to a transom


30


of a watercraft


31


using a mount


32


and a bracket


34


as is well known in the art. The bracket


34


preferably enables both steering and tilt and trim such that the outboard motor


10


may be steered about a substantially vertical axis and tilted or trimmed about a substantially horizontal axis in manners well known to those skilled in the art.




With continued reference to

FIG. 1

, the engine


20


may be of any configuration. In the illustrated embodiment, the engine


20


is substantially vertically oriented such that an axis of a crankshaft


38


has an inclined or substantially vertical axis. As is known, the illustrated engine


20


generally comprises a cylinder block


36


having a plurality of cylinder bores


37


. In some embodiments, the engine


20


may contain as few as one cylinder or more than two cylinders. In the illustrated embodiment, the engine


20


comprises two banks of three cylinders arranged in a V-type engine. As such, two planes are defined along the cylinder banks that are inclined to intersect such that a generally v-shape configuration results.




The engine


20


may also operate on any known operating principle. The illustrated engine


20


preferably operates on a four-cycle principle. It should be understood, however, that the engine may also operate on a two-stroke or rotary principle as well.




A crankshaft is rotatably driven by the engine


20


in any manner well known to those of ordinary skill in the art. Specifically, with reference to

FIG. 2

, the illustrated engine


20


contains a plurality of pistons


40


, which are mounted for reciprocation within the cylinder block


36


. The pistons, in turn, are connected to the crankshaft


38


via connecting rods


42


in any suitable manner. Thus, as the pistons are driven by the expansion of gases following combustion, the translating motion is transferred to the crankshaft through the connecting rods. As a result of the movement of the connecting rods, the crankshaft is driven for rotation about its axis.




The illustrated crankshaft


38


is preferably coupled to a downwardly extending driveshaft


44


in any suitable manner. Accordingly, the driveshaft


44


is powered for rotation by the engine


20


through the crankshaft


38


. The rotation of the driveshaft


44


, in turn, drives a propeller


46


in the illustrated embodiment. The illustrated propeller


46


is driven in both a forward direction and a reverse direction through the shiftable transmission


48


. In the illustrated embodiment, this shiftable transmission generally comprises a selectable bevel gear arrangement. The selectable bevel gear arrangement preferably couples the drive shaft


44


to a propeller shaft


50


and the propeller


46


. These components are journaled for rotation in any suitable manner, such arrangements being well known to those of ordinary skill in the art.




With reference again to

FIG. 1

, the illustrated engine


20


is preferably a directly injected engine having at least one fuel injector


60


positioned and arranged to directly inject a charge of fuel into a combustion chamber


62


. It is anticipated, however, that the present invention may also be utilized with indirectly injected engines as well. Moreover, in some embodiments, the engine may be of the carbureted type and an air fuel charge may be provided to a combustion chamber through an induction system including a carburetor. The fuel injectors


60


may be positioned to inject fuel into the combustion chambers


62


in any suitable manner.




With reference to

FIG. 1

, the illustrated engine has a belt-driven high pressure fuel pump


64


mounted to the top and rear of the illustrated engine


20


. The fuel pump supplies fuel to the fuel injectors in the illustrated embodiment.




The fuel pump


64


comprises an input shaft


66


mounted on an uppermost surface of the fuel pump


64


in the illustrated embodiment. The illustrated input shaft


66


desirably carries a driven sprocket


68


. As used herein, sprocket may refer to a gear, sprocket, pulley, sheave or the like. The driven sprocket


68


may be of any size or configuration known to those of skill in the art. Preferably, the driven sprocket


68


is splined or keyed to the input shaft


66


such that rotation of the driven sprocket


68


is transferred to the input shaft


66


.




The driven sprocket


68


is driven by a drive sprocket


70


through the use of a drive belt


72


. The drive belt


72


may be a chain, a belt, or any other flexible member coupling the two sprockets


68


,


70


together for rotation. Additionally, the two sprockets


68


,


70


may be sized to effect either an increase or decrease in revolution speed between the input shaft


66


and the crankshaft


38


. The coupling of the sprockets forms, in part, a drive unit for powering the high pressure fuel pump. The drive unit is indicated generally by the reference numeral


74


.




With continued reference to

FIGS. 1 and 2

, the illustrated engine


20


further comprises a flywheel magneto arrangement


76


that is mounted to an upper end of the illustrated crankshaft


38


. The flywheel arrangement


76


generally comprises a flywheel


78


that is mounted to an upper end of the illustrated crankshaft


38


for rotation about the same axis in the illustrated embodiment. In the illustrated embodiment, the flywheel carries magnets and forms a rotor of a electrical generator. An armature (not shown) is joined to the engine and is attached proximate a bearing carrier of the crankshaft or other output shaft.




With continued reference to

FIG. 2

, the illustrated flywheel


78


also carries a geared outer periphery


80


that meshes with a geared surface


82


of a starter motor


84


to enable the starter motor


84


to provide an initial turning to the crankshaft


38


through the flywheel


78


in order to assist in starting the engine


20


. It is anticipated that the present lifting arrangement may also find utility in engines having pull-start, other manual starting arrangements or other electric starting arrangements as well.




With reference now to

FIGS. 1 and 2

, a hanging arrangement for the engine


20


will be described in detail. As illustrated in

FIG. 2

, the engine comprises a sprocket support


90


that is attached to an upper surface of the flywheel


78


in the illustrated embodiment. The sprocket support


90


is preferably splined or keyed to the sprocket


70


of the drive unit


74


such that the sprocket support


90


and sprocket


70


turn together. It is envisioned, however, that the sprocket


70


may be capable of movement relative to the sprocket support


90


in some embodiments. For instance, the sprocket may be carried by a bearing or bushing such that the sprocket


70


may turn with a large degree of freedom relative to the sprocket support


90


. Moreover, the sprocket may be directly attached to the flywheel in some embodiments without the use of a sprocket support


90


.




With reference now to

FIGS. 3A and 3B

, the illustrated sprocket support


90


will be described in greater detail. As introduced above, the sprocket support


90


is desirabley affixed to the flywheel


78


. In the illustrated embodiment, the sprocket support


90


is advantageously attached through the use of threaded fasteners


92


. The use of the threaded fasteners enables ease of removal and replacement of the sprocket support during routine maintenance. Of course, the sprocket support may also be attached in other manners, such as, for example but without limitation, welding, clamping or the use of interlocking features.




The fasteners


92


of the illustrated embodiment extend through a plurality of apertures


94


in the stay


90


. The apertures


94


are preferably slightly countersunk. The countersink may allow the fasteners


92


to protrude upwardly from the sprocket support


90


to lesser degree than using the fasteners


92


without the countersinks. In the embodiment of FIGS.


3


A-


3


B, three apertures


94


are used. It is anticipated, however, that as few as one or more than two apertures may also serve to secure the sprocket support


90


to the upper surface of the flywheel


78


. With reference to

FIG. 4B

, the support in the illustrated embodiment is preferably affixed directly to the flywheel; however, as will be described below, the support


90


may also be spaced apart from the flywheel or other engine surface in some embodiments.




In the illustrated embodiment, the support


90


is preferably triangular in shape having one aperture


94


positioned in each apex of the triangle. While it is not critical that the support


90


be triangular in configuration, it is desirable that the support have a generally symmetrical appearance. A symmetrical appearance may result in a more balanced rotation than otherwise possible. It is anticipated, however, that other shapes may be utilized. In such instances, it is desirable to locate an axis of rotation of the support to be aligned with the center of mass of the support unless an appropriately positioned counterbalance is utilized. Moreover, the off-center center of mass may be used to off-set other component motion if desired or advantageous.




The illustrated support


90


further comprises a centrally located threaded hole


96


into which a lifting lug, described in more detail below, may be inserted. The hole


96


may also extend through the sprocket


70


in embodiments in which the sprocket is directly mounted to the flywheel. Such an embodiment would eliminate the support and simplify the construction. The lifting lug, when coupled to the support


90


, or sprocket, is used to raise and lower the engine


20


into and out of the outboard motor power head


12


. Notably, the threaded hole


96


may also be located in other regions of the support


90


or sprocket


70


; however, the central location of the illustrated support is presently preferred as it reduces bending forces created in the connection to the crankshaft of the illustrated embodiment.




With reference now to

FIG. 4A

, a lifting lug


98


is illustrated in a presently preferred lifting arrangement. The lifting lug


98


is shown assembled to the flywheel


78


through the support


90


. As discussed above, the lifting lug


98


may also be attached directly to the sprocket or pulley


70


, the flywheel


78


, or the crankshaft


36


. With reference now to

FIG. 4B

, the lifting lug


98


generally comprises a grappling portion


100


and a support engaging portion


102


. The lifting lug


98


may also be formed as an integral component of the support or other element that is removably attached to the engine. The grappling portion may comprise a hook, a threaded eyebolt, a T-bar, or any other suitable member featuring a graspable component such that a chain, a rope or the like may be fastened to the engine through grappling portion


100


. In a presently preferred structure, the grappling portion


100


is an eyebolt. The support engaging portion


102


may assume any of number of suitable configurations. In some embodiments, the support engaging portion may feature multiple threads. In other embodiments, a quick-release arrangement may be employed such that the support engaging portion may be engaged and disengaged with less than a full revolution. In one presently preferred embodiment, the support engaging portion features a single standard thread that begins at one end of the support engaging portion


102


and terminates proximate an enlarged portion


103


that forms a stop.




With reference now to FIGS.


5


A-


6


B, another lift assembly will be described in detail. As shown in

FIGS. 1 and 2

, a pivotable lifting lug


104


is preferably nestled within a valley defined between the banks of cylinders. Positioning the lifting lug


104


in the valley takes advantage of space not utilized by engine accessories or peripheral components. Further, as illustrated in

FIG. 2

, the positioning allows the lifting lug


104


to lie within the loop of the drive belt


72


of the drive unit


74


. Such positioning again takes advantage of dead space within the engine profile.




With reference to

FIGS. 5A and 5B

, the pivotable lifting lug


104


generally comprises a pedestal portion


106


and a grappling portion


108


. The grappling portion


108


is desirably pivotably attached to the pedestal portion


106


with a pin


110


in the illustrated embodiment. Accordingly, the illustrated grappling portion


108


may be pivoted into an upright position for use and pivoted downward into a stowed position when not in use.




The illustrated pedestal portion, as depicted in

FIGS. 5A and 5B

, generally comprises a supporting yoke


112


at one end and a foundational mounting boss


114


at the other. The supporting yoke


112


generally comprises a u-shaped channel


116


defined between two legs


118


. A pair of generally aligned apertures


119


extend through the legs


118


such that one aperture


119


extends through each leg


118


. The apertures


119


are preferably sized and configured to receive the pin


110


. The pin may be force fit, may be a threaded member held in position with a nut, may be a grooved pin, may be a roll pin, may be a spiral pin, may be a cotter pin, may be a rivet or may be any other mechanical element, for example, capable of securing the grappling portion


108


to the pedestal portion


106


such that one may rotate relative to the other. The apertures


119


may or may not extend all the way through the legs


118


. The presently preferred embodiment, however, features two holes that extend through the legs such that the supporting yoke may be easily and inexpensively manufactured.




Moreover, a stepped ledge


120


is positioned within the channel


116


. In the illustrated embodiment, the ledge


120


extends between both legs


118


. It is anticipated, however, that the ledge may extend only partially between the legs


118


or that the ledge may be constituted of several portions, such as, for example but without limitation, a series of serrated teeth. The ledge


120


, as will be described below, advantageously limits the travel of the upper grappling portion


108


as it pivots within the channel


116


.




The mounting boss portion


114


of the pedestal


106


is the location at which the illustrated pivotable lifting lug


104


is attached to the engine


20


. The illustrated mounting boss portion


114


is configured as a t-shape; however, many other configuration are also possible and may be readily interchanged to securely mount the lifting lug


104


to the engine


20


. Moreover, apertures are formed within each of the bars of the T-configuration through which threaded fasteners extend when connecting the lifting lug


104


to the engine or any other suitable mounting surface.




With continued reference to

FIGS. 5A and 5B

, the illustrated grappling portion


108


is pivotably connected to the pedestal portion


106


. The grappling portion, as in the lifting lug of FIG.


3


A-


3


B, may assume any of a number of shapes and configurations. The illustrated grappling portion


108


comprises a ring


122


and a body


124


. The ring


122


and the body


124


are preferably welded together to form a contiguous member; however, the two portions may also be formed as a unitary body using any suitable method, such as forging.




The illustrated body


124


has a through hole


126


, for accommodating the pin


110


, and a stopper edge


128


. The through hole


126


should be sized to allow relative movement between the pin


110


and the body


124


. In configurations in which the pin


110


does not rotate relative to the body


124


, the pin


110


should rotate relative to the yoke


112


. Of course, the pin


110


and apertures


119


could be replaced by a shaft extending from either end of the grappling portion to be secured within the pedestal portion in any suitable manner. In such instances, the shaft may be integrally formed with the grappling portion


108


and the pedestal portion


106


may contain slots or apertures to allow the shaft to be inserted and secured held by the pedestal portion


106


.




The stopper edge


126


, similar to the ledge


120


, may extend the entire width of the body


124


. The edge


126


may also have may other configuration, such as those described above in reference to the ledge


120


. Generally, the edge


126


contacts the ledge


120


and limits the rotation of the grappling portion


108


within the yoke


112


of the pedestal portion


106


. This allows the pivotable lifting lug to be raised for use without excessive pivoting of the two portions while being used. The edge


126


and ledge


120


should be sized and configured to have adequate strength and contact surface area to resist undesired motion when in contact and to avoid undesired deformation while being used. Such sizing and configuring may vary from application to application.




With reference now to

FIGS. 6A and 6B

, the pivotable lifting lug of

FIGS. 5A and 5B

is illustrated as attached to an upper surface of a flywheel magneto therein. As described above, a set of threaded fasteners


130


are used to attach the pedestal portion


106


of the lifting lug to the flywheel


78


. Of course, the threaded fasteners may be of any suitable type, including but not limited to, bolts, threaded rods and threaded studs welded to the flywheel.

FIGS. 6A and 6B

also illustrate a desired range of motion for the illustrated embodiment. In one embodiment, the range of motion is approximately 90 degrees. In another embodiment, the range of motion is between approximately 70 degrees and 115 degrees. As illustrated, the range of motion may be limited by the sizing of the body


124


and the yoke


112


as well as the sizing and configuration of the edge


128


and ledge


120


.




With reference to

FIG. 1

, the pivotable lifting lug is positioned in a valley defined between the two banks of cylinders. It should be appreciated that any number of positions are position. The illustrated positioning advantageously reduces the likelihood of inadvertent contact of lifting apparatus with components of the engine. Moreover, it is desired that the positioning results in a fairly balanced engine when suspended by the lifting apparatus. Accordingly, in some embodiments, the lifting lug is positioned proximate a axis that extends in a generally vertical direction through approximately a center of mass of the assembled engine. In other embodiments, the lifting lug is positioned along a plane that extends approximately through the center of mass. In one presently preferred embodiment, the lifting lug is positioned along a longitudinally extending generally vertical plane that extends through approximately the center of mass.




With reference now to FIGS.


7


A-


7


C, another lift arrangement is illustrated therein. Because many of the elements are similar to the above described embodiments, the description above should be considered to apply to the embodiments disclosed in FIGS.


7


A-


8


F unless otherwise indicated. Moreover, like reference numerals will refer to like elements in each embodiment. As illustrated in

FIG. 7A

, the sprocket


70


contains a through hole


132


that is sized and configured to be positioned over a seat


134


of the sprocket support


90


. The seat


134


in the illustrated embodiment is sized such that the sprocket


70


may rotate relative to the seat


134


and the support


90


; however, it is anticipated that the seat


134


and the sprocket


70


may sized and/or configured (press fit, keyed, splined, or otherwise coupled) such that the two rotate together as a unit. In the illustrated embodiment, a lubricous surface


136


may be positioned to encourage movement of the sprocket


70


relative to the support


90


by reducing surface friction between the two components. For instance, but without limitation, the surface may be coated or formed of brass.




With continued reference to

FIG. 7A

, the sprocket


70


is secured on the seat


134


with the use of a locking plate


138


. The locking plate


138


may be a simple pan washer or may be any other shape or configuration which helps to secure the sprocket from working off of the seat


134


. In the illustrated embodiment, a ring plate


138


having an upturned periphery is secured to the seat


134


over the sprocket


70


with a fastener


140


that threads into the threaded aperture


96


of the support


90


. The support may also have a threaded portion such that a nut holds the plate


138


in position. Moreover, any other suitable fastening method may be used to limit the axial travel of the sprocket


70


relative to the seat


134


.




With reference now to

FIGS. 7B and 7C

, the lift arrangement of

FIG. 7A

is illustrated with assembled to the upper surface of the flywheel


78


in FIG.


7


B and with a removable lifting lug in FIG.


7


C. As each of the features has been described above in detail, further description of the illustrated embodiment is deemed unnecessary.




With reference now to

FIG. 8A through 8F

, more lift arrangements are illustrated therein. The arrangement of

FIGS. 8A and 8B

is very similar to that of

FIG. 7A through 7C

, with the exception that no sprocket is positioned on the seat


134


. In fact, two mounting assemblies of the arrangement of

FIGS. 8A and 8B

are illustrated in

FIGS. 8C and 8D

and

FIGS. 8E and 8F

respectively.




With reference to

FIGS. 8C and 8D

, the support of

FIGS. 8A and 8B

is shown attached to a sprocket carrier


142


. In the illustrated embodiment, the sprocket carrier is configured with apertures


144


through which threaded fasteners


146


extend. Such an embodiment does not compromise the sprocket


70


or other components through positioning a hole in the component. The threaded fasteners


146


affix the sprocket carrier to the flywheel


78


in the illustrated embodiment. Of course, other mounting methods, such as those discussed above in relation to the sprocket support


90


, may also be used. Further, the sprocket support


90


is preferably spaced from and suspended above at least a portion of the sprocket carrier


142


through the use of an additional threaded fastener


148


. According to the illustrated assembly, the fastener


148


may extend through any of the apertures


94


. Preferably the aperture is threaded such that the position of the support


90


may be fixed along the fastener


148


. It is anticipated that a nut may hold the support


90


in a desired position along the fastener in some embodiments. Moreover, other suitable spacing techniques may also be used. While the fastener


148


extends into a hole in the carrier


142


in the illustrated arrangement, the fastener may also extend into a surface of the engine or the flywheel in other arrangements. Such an embodiment is illustrated in

FIGS. 8E and 8F

. Moreover, the support may be removed or, in one embodiment, the lifting lug may be removed without removing the support if no lifting lug is needed (i.e., during standard operating conditions).




It is to be understood that the present lifting arrangement may use one or more lifting lug, either pivotable or otherwise. Moreover, the lifting lugs may be permanently attached to the engine or a peripheral component or may be removably attached to the same. The lifting lugs may be directly attached to a sprocket carrier or may be positioned elsewhere on the engine or the peripheral components. Although the present invention has been described in terms of certain embodiments and arrangments, other embodiments and arrangements apparent to those of ordinary skill in the art also are within the scope of this invention. Thus, various changes and modifications may be made without departing from the spirit and scope of the invention. Moreover, not all of the features, aspects and advantages are necessarily required to practice the present invention. Accordingly, the scope of the present invention is intended to be defined only by the claims that follow.



Claims
  • 1. An engine for an outboard motor, the engine comprising a generally vertically oriented crankshaft, a flywheel connected to the crankshaft, a peripheral component attached to a portion of the engine, a driven sprocket connected to the peripheral component and arranged to power the peripheral component, a drive sprocket attached to the flywheel, a flexible drive loop extending between and rotatably coupling the drive sprocket to the driven sprocket, a lifting lug is removably connected one of the flywheel or the drive sprocket.
  • 2. The engine of claim 1, wherein a sprocket support attaches the drive sprocket to the flywheel.
  • 3. The engine of claim 1, wherein the lifting lug is connected solely to the drive sprocket though at least one intermediate member.
  • 4. The engine of claim 3, wherein the intermediate member is a sprocket carrier.
  • 5. The engine of claim 1, wherein the lifting lug is directly connected solely to the drive sprocket.
  • 6. The engine of claim 2, wherein the sprocket support is spaced from the flywheel through an intermediate member.
  • 7. An engine for an outboard motor, the engine comprising a crankshaft, a flywheel attached to the crankshaft, a peripheral component attached to a portion of the engine, a driven sprocket connected to the peripheral component and arranged to power the peripheral component, a drive sprocket attached to the flywheel, a flexible drive member coupling the drive sprocket to the driven sprocket, and a lifting lug positioned between the drive sprocket and the driven sprocket.
  • 8. The engine of claim 7, wherein the lifting lug has a grappling portion that is pivotably attached to a mounting portion, the grappling portion being pivotable between a useable position and a stowed position.
  • 9. The engine of claim 8, wherein the lifting lug is capable of pivoting through a complete range of motion of approximately 90 degrees.
  • 10. The engine of claim 8, wherein the grappling portion extends up above an upper surface of the engine when positioned in the useable position and folds into a stowed position such that the grappling portion overlaps a portion of the flywheel.
  • 11. An outboard motor comprising a power head, an engine compartment defined within the powerhead, an engine mounted within the engine compartment, the engine comprising a crankshaft, a crankcase encasing the crankshaft, a flywheel attached to the crankshaft, the crankcase attached to a cylinder block, a pair of cylinder banks positioned within the cylinder block, a removable lifting lug and a pivotable lifting lug, one of the removable lifting lug and the pivotable lifting lug positioned generally above the crankshaft, the other of the removable lifting lug and the pivotable lifting lug positioned generally rearward of the crankshaft.
  • 12. The outboard motor of claim 11, wherein the rearmost of the lifting lugs is positioned generally between the two banks of cylinders.
  • 13. The outboard motor of claim 12 further comprising a generally vertical plane extending through the removable lifting lug and the pivotable lifting lug, the vertical plane also extending through a position proximate a center of mass of the assembled engine.
  • 14. The outboard motor of claim 12, wherein the removable lifting lug is connected to the flywheel.
  • 15. The outboard motor of claim 14 further comprising a pulley affixed to the flywheel, wherein the removable lifting lug is connected to the flywheel through the pulley.
  • 16. The outboard motor of claim 15 further comprising a pulley support, wherein the pulley is attached to the crankshaft through at least one of the pulley support and the flywheel.
  • 17. The outboard motor of claim 16, wherein the pulley is configured to rotate relative to the pulley support.
Priority Claims (1)
Number Date Country Kind
10-132790 May 1998 JP
US Referenced Citations (1)
Number Name Date Kind
5616058 Nakai Apr 1997
Foreign Referenced Citations (1)
Number Date Country
47796 Mar 1985 JP