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.
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 rod pins 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 con rod pins may be 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.
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 pin 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 pin 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 at least one L-shaped body or may be a combination of 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 pin coupled to a crankshaft and operably 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 pin via an exemplary vehicular engine insert.
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.
With reference to the illustrative embodiments described herein and illustrated in
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
With continued reference to
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
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
Referring to the illustrative embodiment of
Referring now to the exemplary embodiment illustrated in
In typical crankshaft housings, internal conduits for lubricants to con rod pins 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
Referring back to the illustrative embodiments of
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
Referring to both
An exemplary insert 30, as may be viewed in
In the alternative embodiments illustratively provided for in
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
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
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.
This application claims priority to U.S. Provisional Patent Application No. 63/483,649, filed Feb. 7, 2023, the disclosures of which are incorporated herein in their entirety.
Number | Date | Country | |
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63483649 | Feb 2023 | US |