MODULAR VEHICULAR ENGINE CONSTRUCTION

Abstract
A vehicular engine comprises a crankcase in which a crankshaft is operably disposed and by which a plurality of pistons translate within cylinder blocks operatively coupled to the crankcase. This vehicular engine may have interchangeable cylinder blocks and exhaust manifolds, a balancer shaft disposed below the crankshaft, a balancer gear separably coupled to the crankshaft to engage a front gear of the balancer shaft and supply lubricant to the crank shaft, a separable insert disposed within the crankcase proximal to a con rod of one of the plurality of pistons to supply lubricant thereto, or combinations thereof.
Description
FIELD OF THE INVENTION

The present invention relates to the field of vehicular engines, and in particular, the location of components used in the construction and operation of the same to enable increased positioning of the engine within and/or on the vehicle(s) for which they may be intended.


BACKGROUND

As disclosed in U.S. Pat. No. 7,607,958, an exemplary engine may be illustrated with a balancer shaft located above the crankshaft of the exemplary engine. For example, as shown in FIG. 41 of U.S. Pat. No. 7,607,958, a balancer shaft 802 is located above crank shaft 66 and between cylinders 60 of the exemplary engine 10 gearing system 800.


In the position illustrated in U.S. Pat. No. 7,607,958, the balancer shaft 802 and its case 80 result in means to move lubricant to and from the case 80 between cylinder blocks and crank shaft, a configuration to space the engine cylinders further from one another in terms of angular alignment with respect to the crank shaft axis (so as to avoid the balancer shaft and its case), and limitations on placement of the exhaust and air manifold(s) for the engine.


Other engines, such as those disclosed in U.S. Pat. No. 5,960,761, utilize a plurality of balancer shafts disposed about the crank shaft, i.e., balancer shafts 9 and 10 about crank shaft 3 in in FIG. 4 of the aforementioned U.S. patent. In addition to the above-noted issues caused by a balancer shaft located above the crank shaft, the increased number of parts, such as gears and gear trains to allow for proper operation of all the shafts in the gear system unnecessarily increases the number of parts and the need for lubrication and timed engagement of the same.


As a consequence of the above-mentioned issues, there remains an unmet need for oil supply to crankshafts via the balancer shaft. In other words, while others have sought to move the balancer shaft more proximal to the crankshaft, and yet fail to reduce the engine size in the process, they have similarly failed to utilize the balancer shaft for anything other than its previously understood purpose. As such, the art has failed to utilize an engine balancer shaft in a meaningful way, including, supplying lubrication to the crankshaft while it is in operation.


Additionally, in prior engine systems, including multi-cylinder 2-stroke engines, piston rods or con rods do not receive direct oil supply. In state-of-the art systems, lubrication via oil nozzles from outside the crank case is avoided because the oil is fed against centrifugal forces. Further, the bearings of the con rod are only capable of receiving oil when they come into proximity of the external nozzle (e.g., no more than 20° per revolution), limiting the overall lubrication capability of the oil nozzle.


Further additionally, prior engine systems, due to one or more of the above-stated concerns, and others, require mirrored, although not identical, cylinder blocks and cylinder heads. Furthermore, in these prior engine systems, the cylinder block may be integrally formed with the upper portion of the crankcase, requiring more expense in fabrication, repair, and replacement in the event of operation interruptions. Still furthermore, there is heretofore non-existent an engine system comprised of cylinder blocks and cylinder heads that are interchangeable between V-style engine system configurations and those that are inline, e.g., interchangeable cylinder blocks and cylinder heads for use in both a V-6 and an inline-3 engine system.


SUMMARY

An exemplary vehicular engine may comprise a crankshaft configured to rotate about a longitudinal crankshaft axis while being operably mounted in a crankcase, a balancer shaft having an axis of rotation and being operably coupled to the crankshaft and disposed below the crankshaft, and each of a plurality of pistons coupled to the crankshaft via its own con rod whereby each piston is configured to translate along a radial axis extending perpendicularly from the longitudinal crankshaft axis to enable the vehicular engine to generate power. According to this exemplary embodiment of the aforementioned vehicular engine, the radial axis for a first piston of the plurality of pistons defines a first path and the radial axis for a second piston of the plurality of pistons defines a second path, such that the first path and the second path are spaced apart from one another about the longitudinal crankshaft by an angle less than 90°.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the vehicular engine may be configured such that the axis of rotation of the balancer shaft is in a plane that intersects the longitudinal crankshaft axis and substantially bisects the angle α.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the angle α may be less than 75°.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the angle α may be about 67°.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the angle α may be less than 75°.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the angle α may be about 67.5°.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the vehicular engine may further comprise at least one cylinder block for translation of at least one of the plurality of pistons along the first path and at least one cylinder block for translation of at least one of the plurality of pistons along the second path, wherein each at least one cylinder block is coupled to an upper portion of the crankcase above the longitudinal crankshaft axis.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the vehicular engine may further comprise an exhaust manifold coupled to the at least one cylinder block.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the exhaust manifold may be disposed at an angle substantially the same as the angle α.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the vehicular engine may further comprise an air plenum coupled to the crankcase.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the vehicular engine may be configured such that each of the air plenum and the exhaust manifold extends outwardly from the longitudinal crankshaft axis to a substantially same extent.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the vehicular engine may further comprise a second exhaust manifold disposed in the space in which the angle α is formed between the first path and the second path and operatively coupled to the vehicular engine.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the vehicular engine may be configured such that a center of gravity for the vehicular engine is proximal to a plane that intersects the axis of rotation of the balancer shaft and the longitudinal crankshaft axis and/or a plane that intersects the longitudinal crankshaft axis and substantially bisects the angle α.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the vehicular engine may further comprise a balancer cover disposed below a lower portion of the crankcase and operably coupled thereto.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the vehicular engine may further comprise a balancer gear separable from and operably coupled to the crankshaft and a front gear coupled to the balancer shaft, wherein the balancer gear and the front gear engage one another.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the vehicular engine may be configured such that a lubricant is supplied to a portion of the crankshaft most proximal to the balancer gear via a groove in and a passage through the balancer gear.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the vehicular engine may be configured such that a lubricant is supplied to a portion of the crankshaft distal to the balancer gear and proximal to a con rod via a separable insert operably coupled to the lower portion of the crankcase.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the separable insert for the vehicular engine may receive lubricant from within the crankcase in one direction and transmits it in a substantially orthogonal direction.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the separable insert for the vehicular engine may comprise an insert passage for receiving lubricant from within the crankcase and a nozzle for communicating the lubricant to another portion of the crankshaft, wherein the nozzle communicates the lubricant in a direction that is substantially orthogonal to the passage.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the separable insert for the vehicular engine may consist of a plastic, a rubber, or a combination thereof.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the vehicular engine may be configured such that each cylinder block is identical in construction.


An exemplary vehicular engine may comprise an upper half of a crankcase configured to operatively hold a crankshaft and a plurality of pistons, at least one cylinder block configured to house at least one of the plurality of pistons, and at least one cylinder head configured to operatively couple to the at least one cylinder block, wherein the upper half of the crankcase operates with the at least one cylinder block and the at least one cylinder head as either an inline engine configuration or a V-style engine configuration.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, the vehicular engine is configured to be in a V-style engine configuration while each of the at least one cylinder block is identical to the other.


An exemplary vehicular engine balancer gear may be configured to operably couple to a crankshaft of a vehicular engine such that the balancer gear comprises a front surface most distal from a center of the crankshaft, a rear surface most proximal to the center of the crankshaft, and a thickness connecting the front surface to the rear surface. The exemplary vehicular engine balancer gear may also comprise a catch groove in the front surface and a passage from the groove and through the thickness of the balancer gear, wherein the passage opens toward a surface on a web of the crankshaft.


An exemplary vehicular engine insert may comprise a body having a passage for a fluid, a nozzle fluidly coupled to the passage, and a channel through a thickness of the insert, wherein the channel fluidly interconnects the passage to the nozzle so that the nozzle and the passage are substantially orthogonal to one another.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, an exemplary vehicular insert may comprise two legs interconnected to a torso, wherein each of the two legs is substantially perpendicular to the nozzle and the two legs interconnect with the torso to form an arched configuration.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, an exemplary vehicular engine may comprise therein any of the aforementioned and otherwise disclosed exemplary vehicular inserts.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, an exemplary vehicular engine may comprise therein any of the aforementioned and otherwise disclosed exemplary vehicular inserts and dispose the same in a portion of a crankcase and adjacent a con rod coupled to a crankshaft operable coupled there within.


In addition to the previously described embodiment and/or as an alternative to any other described exemplary embodiment, an exemplary vehicular engine may communicate lubricant from within the crankcase to a con rod via an exemplary vehicular engine insert.





DESCRIPTION OF THE DRAWINGS


FIG. 1 illustrates an exemplary first face of an engine according to one exemplary embodiment of the inventions disclosed herein.



FIG. 2 illustrates an exemplary second face opposite the first face of the engine of FIG. 1 according to one exemplary embodiment of the inventions disclosed herein.



FIG. 3 illustrates a sectioned view of the profile of the exemplary engine of FIGS. 1-2 providing an exemplary embodiment of other aspects of the inventions disclosed herein.



FIG. 4 illustrates an exemplary embodiment of a profile view of the crankshaft, pistons, con-rods, and balancer shaft according to aspects of the inventions disclosed herein.



FIG. 4A illustrates an exemplary embodiment of a sectioned view of FIG. 4 along the crankshaft axis and providing further aspects of the inventions disclosed herein.



FIG. 4B illustrates an exemplary embodiment of a sectioned view of FIG. 4A along the dashed line marked “B-B” and providing further aspects of the inventions disclosed herein.



FIG. 5 illustrates an exemplary embodiment of a front-facing view of the crankshaft, pistons, con-rods, and balancer shaft of FIG. 4 according to aspects of the inventions disclosed herein.



FIG. 6 illustrates an exemplary embodiment of a front-facing view of a section view of an exemplary crankcase upper portion, a crankshaft web, and a balancer shaft gear according to aspects of the inventions disclosed herein.



FIGS. 7A-B each illustrates an exemplary embodiment of a sectioned profile view of a crankcase lower portion, a portion of the crankshaft and crankshaft web, and a con rod lubrication insert according to aspects of the inventions disclosed herein.



FIG. 8 illustrates an exemplary embodiment of another sectioned view of a crankcase lower portion, a portion of the crankshaft and crankshaft web, and a con rod lubrication insert according to other aspects of the inventions disclosed herein.



FIGS. 9A-B illustrates an exemplary embodiment of sectioned views of portions of the crankshaft, crankshaft web, and a con rod sections according to aspects of the inventions disclosed herein.



FIGS. 10A-B illustrate exemplary embodiments of a con rod lubrication insert and a con rod lubrication insert as it would be used in operation within an exemplary crankcase lower portion according to aspects of the inventions disclosed herein.



FIG. 11 illustrates an exemplary embodiment of an exploded view of an exemplary engine system according to still further aspects of the inventions disclosed herein.





In the drawings like characters of reference indicate corresponding parts in the different and interchangeable and interrelated figures. Parts and components of each figure may be substitutes for other components in other figures to achieve the various methods and embodiments disclosed herein. Methods and protocols disclosed in any embodiment may be run in any order so as to affect their disclosed goals and/or enable performance of the systems as described. Additionally, any one embodiment may utilize any method or protocol described and in any portions, sequences, and combinations thereof.


DETAILED DESCRIPTION

With reference to the illustrative embodiments described herein and illustrated in FIGS. 1-2, an exemplary engine 10 may comprise a crankcase upper portion 1a and a crankcase lower portion 1b separatable along plane 9b, but otherwise coupled to one another using attachments means and mechanisms known to those skilled in the art. Each of crankcase upper portion 1a and crankcase lower portion 1b may be designed and configured using known methods to permit the disclosed features of the various inventions of this application, including among them, the operable holding of crankshaft 5 therein. In an exemplary embodiment, the portions of crankcase 1a and 1b that circumscribe crankshaft 5 may be designed so that a longitudinal axis of crankshaft 5 (that is, the major axis along the length of crankshaft 5 as opposed to the radial axes that may extend perpendicularly therefrom in the direction of the one or more con rods of the pistons operably connected to the same) may be found in a plane 9b. Distal from the plane 9b may be plane 9a, which is angularly oriented with respect to the longitudinal axis of crankshaft 5. Like plane 9b, plane 9a may delineate the plane separating the crankcase upper portion 1a from each of the cylinder blocks 2a and/or 2b, which are coupled with their corresponding cylinder heads 3a and 3b, respectively. Likewise, plane 9d may be angularly oriented with respect to the longitudinal axis of crankshaft 5 in substantially the same arrangement as plane 9a and 9b or at any other angle so as to provide coupling between an exhaust manifold 4a and 4b to each of cylinder blocks 2a and 2b, respectively. In an exemplary embodiment, exhaust manifolds 4a and 4b couple to cylinder blocks 2a and 2b, respectively, at an angle that is substantially the same as the angle of the cylinder blocks 2a and 2b with respect to the longitudinal axis of crankshaft 5. In yet another exemplary embodiment, exhaust manifolds 4a and 4b may be coupled to cylinder blocks 2a and 2b, respectively, so that the downstream exhaust opening of one manifold (e.g., manifold exhaust 4bx as shown in FIG. 2) lies in a plane perpendicular to the longitudinal axis of the crankshaft 5 and such plane is also intercepted by the downstream exhaust opening of the other manifold (e.g., manifold exhaust 4ax as shown in FIG. 2), although at a different position (e.g., an angularly off-set position from one another about the longitudinal axis of the crankshaft 5). The crankcase lower portion 1b may be separably coupled to a balancer cover 8 along a plane 9c, which plane 9c may be substantially parallel with plane 9b. In similar fashion to upper crankcase portion 1a and lower crankcase portion 1b vis-à-vis crankshaft 5 longitudinal axis and plane 9b, a longitudinal axis of a balancer shaft 7 may be substantially parallel to the longitudinal axis of crankshaft 5, be circumscribed by surfaces in lower crankcase portion 1b and balancer cover 8, and be situated so that its longitudinal axis lay in plane 9c in substantially vertical alignment with that of the crankshaft 5.


Additionally, an exemplary crankcase lower portion 1b may be coupled to an air intake plenum 6 along plane 9e. In an exemplary embodiment, an exemplary air intake plenum 6 may occupy substantially the same space bounded by cylinder block 2a, crankcase upper portion 1a, crankcase lower portion 1b, and balancer cover 8 as exhaust manifold 4b on the opposite side of engine 10. In an exemplary embodiment, the engine 10 according to the disclosures herein may have radial extents 10a and 10b extending in opposite radial directions from the longitudinal crankshaft axis and lie along plane 9b. An exemplary radial extent 10a may be a plane that is perpendicular to plane 9b and intersects a distal-most edge of one of cylinder block cover 3a/3b, cylinder block 2a/2b, manifold 4b (or whichever manifold is located outside of the “v” formed by the cylinder blocks), and/or plenum 6. In a preferred embodiment, radial extent 10a may be substantially the same length as radial extent 10b when measured from the center (e.g., longitudinal axis) of crankshaft 5 along plane 9b (e.g., the plane about which the upper crankcase portion 1a and lower crankcase portion 1b couple) when plane 9b is positioned parallel with the surface of measurement (e.g., the floor or table). Using the same measurement protocol as stated, an exemplary engine 10 may have ratios of radial extent 10a to radial extent 10b between about 95% and about 105%, between about 98% and about 102%, and most preferably about 100%.


Each of the aforementioned components (1a, 1b, 2a, 2b, 3a, 3b, 4a, 4b, 5, 6, and 7) and any others required for engine 10 operation in a particular vehicle may be coupled to one another (e.g., along one or more of planes 9a-e, or any other portions of the aforementioned components) using attachment mechanisms and techniques known to those skilled in the art (e.g. bolts, brackets, gasket-type connections).


In accordance with one or more of the teachings herein, the illustrative embodiment provided in FIG. 3 may disclose a profile arrangement of the components identified in FIGS. 1-2. According to FIG. 3, an exemplary longitudinal axis 5a may be located along the plane 9b illustrated. As further provided for in FIG. 3, an exemplary balancer shaft 7 may have a non-linear arrangement so that it has both a first axis 7a arranged along plane 9c and a second axis 7b offset from the first axis 7a by a certain offset 7c. Despite the different axes 7a/7b, balancer shaft 7 has only one axis of rotation in plane 9c, which in the illustrative embodiments of FIGS. 3-4 is first axis 7a. In a preferred embodiment, an exemplary offset 7c between the first axis 7a and the second axis 7b of the balancer shaft 7 may be between 1% and 8%, more preferably between 3% and 6%, and even more preferably about 4.5% of the distance measured between each axis 7a and 7b from the longitudinal axis 5a of the crankshaft 5 when axis 7b is at its closest position to longitudinal axis 5a. For example, referencing the illustrative embodiment of FIG. 4, an exemplary axis 7a that may be located about 200 mm from the longitudinal axis 5a of crankshaft 5 in an exemplary engine may have an exemplary axis 7b that is located an exemplary distance 7c of 5% may result in axis 7b being located a distance that is 190 mm from the longitudinal axis 5a of crankshaft 5 when axis 7b of balancer shaft 7 is at its most proximal point to longitudinal axis 5a. An illustrative example of the degree of offset 7c between axes 7a and 7b of an exemplary balancer shaft 7 as compared to the longitudinal axis 5a of an exemplary crank shaft 5 may be further illustrated with reference to FIG. 4. As illustrated, an exemplary axis 7a may be shown in (— — —) dashed lines while exemplary axis 7b may be shown in (— ⋅ — ⋅) dashed lines. Although



FIGS. 3-4 may illustrate balancer shaft 7 with offset axes, those skilled in the art may instead use a balancer shaft 7 with no offset, but possess other characteristics and configurations to achieve the engine balancing and other goals thereof.


With continued reference to FIG. 4, an exemplary crankshaft 5 may have a balancer gear 13 configured to mesh with balancer shaft 7 via front gear 14. However, an exemplary balancer shaft 7 may have a front bearing 14a and a rear bearing 14b. Front and rear bearings 14a-b support rotation of balancer shaft 7 within crank case lower 1b and balancer cover 8 during operation of engine 10.


In an exemplary embodiment, an exemplary balancer shaft 7 may be located with respect to the crankshaft 5 as described herein to effect a more centralized location for the center of gravity of the vehicular engine 10, which may be located at a point between the top of the crankcase upper 1a and the longitudinal crankshaft axis 5a from the front to the rear of the vehicular engine 10. Alternatively, the center of gravity may be at any other location about engine 10 to enable stable and symmetrical placement of two such engines 10 on a portion of a frame or body of a vehicle. For example, the center of gravity of an exemplary engine 10 may be such that two such engine 10 may be placed equidistant from the centerline of a watercraft frame such that, when considering the frame and the engines, the moment about the watercraft centerline due to either engine 10 would be substantially the same. Accordingly, designers of vehicles may take advantage of the centralized mass enhancements resulting from the disclosures herein to better design and increase performance of vehicles that incorporate the same.


With reference to the exemplary sectional views provided for in FIGS. 4A-B, an exemplary crankshaft 5 may be frictionally coupled to balancer gear 13 at a position 5b that may separate the cylindrical portions of crankshaft 5 from the remainder making up the crankshaft web 5W. An exemplary position 5b may be the position at which the balancer gear 13 may be most proximal to an oil groove 17 in the crank web 5W, which may include direct abutment or other spaced arrangements that facilitate passage of oil through balancer gear 13 to crankshaft web 5W. In an exemplary embodiment, balancer gear 13 may comprise an oil catch groove 15 that may be configured to meter oil received therein to an oil passage 16 that may act as a conduit of oil from one or more sources within the crankcase portions 1a and/or 1b to the crankshaft web 5W. Thus, an exemplary crankshaft 5 may enable the promotion of lubricants, such as oil, to the immediately most proximal web section 5W via an exemplary balancer gear 13, e.g., crankshaft web portions 5W most proximal to the generator end of crankshaft 5. In alternative embodiments, an exemplary balancer gear 13 located on the power take-off side of crankshaft 5 (e.g., more proximal to the end cylinder 14b of balancer shaft 7 illustrated in FIG. 3), may provide the same or similar lubrication capabilities to an opposite extremity of the crankshaft 5. Thus, an exemplary engine 10 gear system may not only provide the motive conduction through its geared engagements, such as between crankshaft 5 and balancer shaft 7, but may simultaneously enable the passage of lubricants to certain parts, such as the generator end or power take-off end, of an exemplary crankshaft 5 and/or proximal sections of crankshaft web 5W thereto with appropriately configured oil grooves 17 machined therein. In other disclosures, use of other features may provide lubricant to portions of the crankshaft web 5W that are more distal to the crankshaft portions depicted in FIGS. 4A-B.


An exemplary balancer gear 13 may provide oil conduction to terminal parts of the crankshaft 5 (generator or power take off ends) without having to machine oil conduits in the crankshaft 5 itself, and may only require the crankshaft 5 and/or the web 5W be designed to receive oil through the balancer gear 13. Accordingly, an exemplary balancer gear 13 may be machined separately to provide an exemplary groove 15 and oil conduit 16 therein, while being designed to fit about crankshaft 5, to collectively create a more easily manufacturable system that allows for modularity and ease of replacement, if necessary. Furthermore, clogged grooves 15 and/or conduits 16 in such exemplary balancer gears 13 may allow for ease of servicing as only the gear 13 may be subjected to maintenance without full deconstruction and remediation of the crankshaft 5, which saves time and cost of such maintenance of the engine 10. An exemplary operative depiction of the provision of oil from a source 19 (e.g., an injector) through a crankcase conduit 18, which may be located in one or more of crankcase upper portion 1a and/or crankcase lower potion 1b about crankshaft 5, into a groove 15 in an exemplary balancer gear 13 for metered delivery of lubricant, e.g., oil, through conduit 16 to the most proximal crankshaft web 5W may be shown with reference to FIG. 6.


Referring to the illustrative embodiment of FIG. 5, an illustrative engine 10 may contain within banks within cylinder blocks 2a and 2b (not shown) one or more pistons 11 and 12, respectively, each of which being configured to translate about paths 11a and 12a, respectively. Paths 11a and 12a may be similar to a line passing through the center of cylinders 11 and 12, respectively, and intercepting the longitudinal axis 5a of an exemplary crankshaft 5. In an exemplary embodiment, an angle α may represent the angular disposition of each cylinder 11 and 12 with respect to the other about longitudinal axis 5a of the crankshaft 5. In a preferred embodiment, angle α may be less than 90°, and in an even more preferred embodiment may be between 60° and 75°, and in still more preferred embodiment, may be about 67°.


Referring now to the exemplary embodiment illustrated in FIGS. 7A-B, an exemplary generator side of an exemplary crankshaft 5 may be shown within crankcase lower portion 1b. As illustrated, a crankshaft journal 20 may be operatively disposed about crankshaft web 5W at a location proximal to con rod coupling portions 5C. As may be understood with reference to the crankshaft and bore systems disclosed in U.S. Pat. No. 8,757,028, which disclosures are incorporated herein by reference in their entirety, an exemplary crankshaft 5 may likewise contain pathways through the crankshaft web 5W for metering lubricant to the portions inward of the generator end, e.g., the con rod portions 5C and/or those portions of web 5W that are distal from balancer gear 13 and/or balancer shaft 7 rear bearing 14b, such as, for example, the journaled sections of the crankshaft 5 that allow for the adjacent rotary movement of the con rods of the pistons (e.g., pistons 11 and/or 12) within cylinder blocks 2a and/or 2b. It may also be contemplated that the disclosures herein may apply to unitary or forged crankshafts 5 and/or built crankshafts 5, that is crankshafts whose portions are assembled to one another as opposed to being integrally formed/forged.


In typical crankshaft housings, internal conduits for lubricants to con rods may require expensive machining and, in the event of failure or other issues, result in time-intensive and costly remediation. Thus, in an exemplary embodiment, as illustrated in FIGS. 7A-B, an insert 30 may be used as a lubricant redirection bridge to communicate lubricant, such as oil, supplied radially into the crankshaft web 5W within its repository in crankcase portions (1a and/or 1b) from a lubrication inlet 21 via a channel 22 bored into the crankcase (e.g., in the illustrative embodiment of FIG. 8, channel 22 may be bored into crank case lower 1b). An exemplary insert 30 may communicate the lubrication it receives and induce it, using a nozzle effect in combination with other forces experienced within the engine 10 during operation, to pass the lubrication from its radially originating source within the crankcase portion in which it may be found 1a/1b (e.g., groove 5G from inlet 21 via channel 22) and urge it into a plane substantially parallel to longitudinal axis 5a of the crankshaft 5 so that it may travel through crankshaft 5 borings (such as those depicted by items 106(a), 106(b), 250, 316, 316(a), 316(b), 318, 320, 324(a), 324(b), 326, 328, and FIGS. 7(a)-(b) and 8(a)-(b) in U.S. Pat. No. 8,757,028, the disclosures of which are incorporated herein by reference in their entirety) to pass lubricant to the con rod retaining portions of crankshaft 5, namely sections 5C via outlet 5P (as illustrated in FIGS. 8A-B). While such crankshaft bores may be parallel with the crankshaft 5 axis through the web 5W and con rod sections 5C, as may be illustrated in U.S. Pat. No. 8,757,028, which such disclosures are incorporated herein, these bores may also be in planes that are at an angle to both the vertical plane and the horizontal plane that intersect about crankshaft 5 longitudinal axis 5a. In other words, an exemplary bore, e.g., a bore 18 may be at an angle that is at an angle to longitudinal axis 5A in a plurality of planes.


Referring back to the illustrative embodiments of FIGS. 7A-B, an exemplary insert 30 may be shown in an exploded view from within crankcase lower 1b and crankshaft 5. An exemplary insert 30 may be configured as an inverted arch-shaped structure having legs 30a and 30b interconnected by a torso 30c and disposed adjacent to the bearing 23 of the journaled section 5J of an exemplary crankshaft 5. In an exemplary embodiment, a pair of opposing nozzles 31 may extend outwardly from torso 30c in a direction substantially perpendicular to the extent of legs 30a and/or 30b. An exemplary insert 30 may also have a gasket 33 with portions extending around and through the thickness of insert 30, as may be illustrated with reference to the exploded view shown in FIGS. 7B-C and 10A. In an exemplary embodiment, an exemplary insert 30 may be disposed on a mechanical attachment feature X formed in or otherwise fabricated for the crankcase lower portion 1b (and/or crankcase portion 1a or other portions as the case may be). In a preferred embodiment, feature X is a part of lower portion 1b designed for coupling with other parts of vehicular engine 10. In other words, crankcase lower portion 1b may be coupled to the crankcase upper portion 1a in such a manner that may cause an exemplary insert 30 to be rigidly and/or frictionally contained therebetween to reduce and/or alleviate potential for movement during engine 10 use.


Referring to both FIGS. 7A-B, 8, and 9A-B, an exemplary insert 30 may operate within an exemplary engine 10 by channeling lubricant pumped through nozzles upstream of inlet 21 in crankcase portion 1b via a crankcase channel 22 into the passage 32 of insert 30. An exemplary passage 32 may be designed to reduce turbulence of the incoming lubricant and/or reduce the effects of its viscosity on the inside of insert 30. An exemplary passage 32 may be fluidly connected to nozzles 31 to allow for a substantial change in direction (e.g., about) 90° of the incoming lubricant from channel 22 toward its destination, e.g., groove 5G in crankshaft webbing 5W, and thereafter, via conduit 5P on web 5W and through bore 18, said lubricant may be passed through to the con rod pins 5C. In an exemplary embodiment, nozzles 31 may be configured to emit lubricant from inlet 21 in a metered fashion through catch groove 5G found along the intermediate crankshaft web portions 5W. Via an exemplary catch groove 5G, a conduit 5P through the crankshaft web 5W may permit lubricant to then engage the con rod section 5C disposed distally from an exemplary insert 30 location. In another exemplary embodiment, exemplary nozzles 31 may be disposed toward an acute corner of catch groove 5G to allow for expedited delivery through conduit 5P located in the crankshaft webbing 5W in which it may be found. Due to exemplary rotational velocities involved for an exemplary crankshaft 5, delivery of lubricant along the arc shown in dashed lines in FIG. 7B and into the acute radially distant corners of catch groove 5G as depicted in FIGS. 7A and 7B may allow the lubricant received therein to be pushed radially-outwardly by centrifugal forces and find its way to the conduit 5P and the bore 18 through the webbing 5G to ultimately reach the corresponding opening for bore 18 in the con rod section 5C. The disclosures herein may allow for lubricant provision in an exemplary engine 10 using a combination of pumps (e.g., through and to inlets 21) and the fluid dynamics induced by the configuration of the crankshaft 5 in collaboration with the flow redirection features of an exemplary insert 30 when disposed in the crankcase 1a/1b.


An exemplary insert 30, as may be viewed in FIGS. 7A and 10A-B, may also contain alignment feet 34 and adjustment pins 35 disposed outwardly from the plane in which nozzle 31 may be found. Exemplary alignment feet 34 may be used to more easily procure and replace an exemplary insert 30 for servicing of the same. Additionally, exemplary adjustment pins 35 may be used to accurately place an exemplary insert 30 within a particular portion of the crankcase lower 1b and/or upper 1a, as the case may be. While alignment feet 34 and adjustment pins 35 may be illustrated with particular geometries, those skilled in the art could design these fee 34 and pins 35 in any manner that accomplishes the purposes set forth above.


In an exemplary embodiment, an exemplary insert 30 may be made out of plastic, in particular, any heat-resistant and load-bearing plastic known to those skilled in the art. In a preferred embodiment, insert 30 may be made from a polyacrylic acid (“PA”) or a polycarbonate (“PC”). Additionally, an exemplary gasket 33 may be made from any type of rubber or other elastomers that may be used to reduce shock, increase operation capacity, and/or resist high temperatures. In a preferred embodiment, gasket 33 may be made from a hydrogenated nitrile rubber (“HNBR”). While insert 30 may be made to snap-fit or frictionally couple with gasket 33, it may be contemplated that the two are integrally molded with one another, such as through over-molding, or that one is mechanically fastened to the other. In the former exemplary embodiment, an over-molded insert 30 and gasket 33 may have increased rigidity and resistance to vibratory loads caused by the operation of engine 10. An exemplary insert 30 may be manufactured in two halves and vibration welded together or otherwise adhered to one another using techniques known to those skilled in the art. Additionally, so long as an exemplary engine 10 provides an appropriately configured repository for an exemplary insert 30, a replacement exemplary insert 30 may be created using additive manufacturing techniques using known materials available to those skilled in the art.


Referring now to the exemplary embodiment illustrated by FIG. 11, an exemplary engine 10 may be shown with each of its constituent components, crankcase upper portion 1a, cylinder blocks 2a and 2b, cylinder heads 3a and 3b, and exhaust manifolds 4a and 4b, in exploded view. According to the exemplary embodiment of FIG. 11, and alternatively applicable to all other embodiments and illustrations provided herein, each of cylinder blocks 2a and 2b may be identical in construction such that either one can represent the same constructed part. In a preferred embodiment, cylinder blocks 2a and 2b may be machined in the same fashion without mirroring, and yet each would still allow for appropriate coupling between each cylinder head 3a/3b and/or exhaust manifold 4a/4b. In another preferred embodiment, exhaust manifolds 4a and 4b may be machined in the same fashion without mirroring. Thus, an exemplary engine 10 according to the embodiment illustrated in FIG. 11 may utilize a single crankcase upper portion 1a but place any of cylinder blocks 2a/2b, cylinder heads 3a/3b, and/or exhaust manifolds 4a/4b along planes 9aand 9d of upper portion 1a provided at least one of the exhaust manifolds 4a/4b may be disposed between the “V” formation of the cylinder blocks 2a and 2b.


Accordingly, an engine 10 of the type described may be used for a V-style engine such that only one mold of each component 2a/2b, 3a/3b, and 4a/4b need be made thereby reducing the manufacturing molds necessary to form a complete engine 10. Furthermore, an exemplary engine 10 that is made in a V-style configuration may also be rendered in an in-line 3 configuration using the same crankcase upper portion 1a, cylinder blocks 2a, cylinder head 3a, and exhaust manifold 4a. In this manner, the modularity illustrated and described with respect to FIG. 11 and its applicable disclosures to all other embodiments, increases efficiency of engine 10 creation and reduces the number of components involved in manufacturing a V-style engine and an inline style engine on assembly lines.


The vehicular engine 10 may be used in a variety of different types of vehicles, including, but not limited to, marine vehicles (e.g., boats) as one of an inboard or one of an outboard engine (including multiple engines aligned side-to-side), recreational vehicles (snowmobiles, all-terrain vehicles, side-by-side, personal watercraft), and other on-road vehicles such as motorcycles, scooters, and automobiles. Compliance with the disclosures contained herein may provide additional advantages for marine vehicle engine arrangements where such vehicular engines may be placed side-by-side and space is limited. Therefore, compliance with such disclosures may enable a more efficient arrangement of the vehicular engines used on a marine vehicle and optimize both power, frame size, and overall marine vehicle balance. While such disclosures provide the aforementioned benefits on a marine vehicle, it is contemplated that any other vehicles would obtain the same and/or selective combinations of such benefits and others from following these disclosures.


Many further variations and modifications may suggest themselves to those skilled in art upon making reference to above disclosure and foregoing interrelated and interchangeable illustrative embodiments, which are given by way of example only, and are not intended to limit the scope and spirit of the interrelated embodiments of the invention described herein.

Claims
  • 1. A vehicular engine, comprising: a crankshaft operably mounted in a crankcase, the crankshaft being configured to rotate about a longitudinal crankshaft axis;a balancer shaft operably coupled to the crankshaft and disposed below the crankshaft, the balancer shaft having an axis of rotation; anda plurality of pistons coupled to the crankshaft, wherein each piston is coupled to the crankshaft via a con rod and each piston is configured to translate along a radial axis extending perpendicularly from the longitudinal crankshaft axis to enable the vehicular engine to generate power, wherein the radial axis for a first piston of the plurality of pistons defines a first path and the radial axis for a second piston of the plurality of pistons defines a second path,wherein the first path and the second path are disposed at positions spaced from one another along the longitudinal crankshaft axis,wherein an angle α formed between the first path and the second path is less than 90°.
  • 2. The vehicular engine of claim 1, wherein the axis of rotation of the balancer shaft is in a plane that intersects the longitudinal crankshaft axis and substantially bisects the angle α.
  • 3. The vehicular engine of claim 1, wherein the angle α is less than 75°.
  • 4. The vehicular engine of claim 3, wherein the angle α is about 67°.
  • 5. The vehicular engine of claim 2, wherein the angle α is less than 75°.
  • 6. The vehicular engine of claim 5, wherein the angle α is about 67°.
  • 7. The vehicular engine of claim 1, further comprising at least one cylinder block for translation of at least one of the plurality of pistons along the first path and at least one cylinder block for translation of at least one of the plurality of pistons along the second path, wherein each at least one cylinder block is coupled to an upper portion of the crankcase above the longitudinal crankshaft axis.
  • 8. The vehicular engine of claim 7, further comprising an exhaust manifold coupled to the at least one cylinder block.
  • 9. The vehicular engine of claim 8, wherein the exhaust manifold is disposed at an angle substantially the same as the angle α.
  • 10. The vehicular engine of claim 9, further comprising an air plenum coupled to the crankcase.
  • 11. The vehicular engine of claim 10, wherein each of the air plenum and the exhaust manifold extends outwardly from the longitudinal crankshaft axis to a substantially same extent.
  • 12. The vehicular engine of claim 11, further comprising a second exhaust manifold disposed in the space in which the angle α is formed between the first path and the second path and operatively coupled to the vehicular engine.
  • 13. The vehicular engine of claim 12, wherein a center of gravity for the vehicular engine is proximal to a plane that intersects the longitudinal crankshaft axis and substantially bisects the angle α.
  • 14. The vehicular engine of claim 8, further comprising an air plenum coupled to the crankcase.
  • 15. The vehicular engine of claim 14, wherein each of the air plenum and the exhaust manifold extends outwardly from the longitudinal crankshaft axis to a substantially same extent.
  • 16. The vehicular engine of claim 2, further comprising a balancer cover disposed below a lower portion of the crankcase and operably coupled thereto.
  • 17. The vehicular engine of claim 16, further comprising a balancer gear separable from and operably coupled to the crankshaft and a front gear coupled to the balancer shaft, wherein the balancer gear and the front gear engage one another.
  • 18. The vehicular engine of claim 18, wherein a lubricant is supplied to a portion of the crankshaft most proximal to the balancer gear via a groove in and a passage through the balancer gear.
  • 19. The vehicular engine of claim 8, wherein each cylinder block and corresponding cylinder head is identical in construction.
  • 20. A vehicular engine balancer gear configured to operably couple to a crankshaft
  • 1. vehicular engine of claim 1, wherein the balancer gear comprises: a front surface most distal from a center of the crankshaft, a rear surface most proximal to the center of the crankshaft, and a thickness connecting the front surface to the rear surface;a catch groove in the front surface; anda passage from the groove and through the thickness of the balancer gear, wherein the passage opens toward a surface on a web of the crankshaft.
  • 21. A vehicular engine, comprising: an upper half of a crankcase configured to operatively hold a crankshaft and a plurality of pistons;at least one cylinder block configured to house at least one of the plurality of pistons; andat least one cylinder head configured to operatively couple to the at least one cylinder block, wherein the upper half of the crankcase operates with the at least one cylinder block and the at least one cylinder head to enable formation of an inline engine configuration and a V-style engine configuration.
  • 22. The vehicular engine of claim 21, wherein when the vehicular engine is in a V-style engine configuration, each of the at least one cylinder block is identical to the other.
  • 23. The vehicular engine of claim 22, wherein one of the at least one cylinder block is used to form the inline engine configuration.
RELATED APPLICATION

This application claims priority to U.S. Provisional Patent Application No. 63/483,640, filed Feb. 7, 2023, the disclosures of which are incorporated herein in their entirety.

Provisional Applications (1)
Number Date Country
63483640 Feb 2023 US