Engine assembly for a watercraft
US-2020198732-A1 · Jun 25, 2020 · US
US11279444B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11279444-B2 |
| Application number | US-201916549322-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 23, 2019 |
| Priority date | Dec 20, 2018 |
| Publication date | Mar 22, 2022 |
| Grant date | Mar 22, 2022 |
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A watercraft includes a hull, an engine compartment defined at least in part by the hull, an engine disposed in the engine compartment, an air intake conduit fluidly connected to the engine, an air filter fluidly connected to the air intake conduit, and a shroud connected to an inlet end of the air intake conduit located in the engine compartment. The shroud has an open end and a closed end. The open end is open to flow of air therethrough and the closed end is closed to flow of air therethrough. The shroud has a sidewall extending between the closed and open ends. The shroud is oriented such that the open end is disposed rearward of the closed end. Noise exiting the inlet end of the air intake conduit and the air filter is reflected generally rearward by the shroud. An engine assembly for a watercraft is also disclosed.
Opening claim text (preview).
What is claimed is: 1. A watercraft comprising: a hull having a bow and a stern opposite the bow; an engine compartment defined at least in part by the hull; an internal combustion engine disposed in the engine compartment; an air intake conduit fluidly connected to the engine, the air intake conduit having an inlet end and an outlet end, the inlet end being located in the engine compartment; an air filter fluidly connected to the air intake conduit for filtering air flowing into the air intake conduit; and a shroud connected to the inlet end of the air intake conduit, the shroud having an open end and a closed end, the open end being open to flow of air therethrough, the closed end being closed to flow of air therethrough, the shroud having a sidewall extending between the closed and open ends, the shroud being oriented such that the open end is disposed rearward of the closed end, wherein noise exiting the inlet end of the air intake conduit and the air filter is reflected generally rearward by the shroud. 2. The watercraft of claim 1 , wherein: the open end has a rear peripheral edge; the closed end has a front peripheral edge; and a perimeter of the rear peripheral edge is greater than a perimeter of the front peripheral edge. 3. The watercraft of claim 2 , wherein: the rear and front peripheral edges are circular; and a diameter of the rear peripheral edge is greater than a diameter of the front peripheral edge. 4. The watercraft of claim 1 , wherein: the shroud is generally frustoconical; and the open end has a diameter that is greater than a diameter of the closed end. 5. The watercraft of claim 1 , wherein the inlet end of the air intake conduit is located in a front portion of the engine compartment. 6. The watercraft of claim 5 , wherein the engine comprises: a crankcase; a crankshaft disposed at least in part in the crankcase; a cylinder block connected to the crankcase; at least one cylinder defined in the cylinder block; and at least one piston movably disposed within a corresponding one of the at least one cylinder, each of the at least one piston being operatively connected to the crankshaft, the shroud being disposed forward of each of the at least one cylinder. 7. The watercraft of claim 1 , wherein the engine comprises: a crankcase; a crankshaft disposed at least in part in the crankcase, the crankshaft extending longitudinally; a cylinder block connected to the crankcase; at least one cylinder defined in the cylinder block; and at least one piston movably disposed within a corresponding one of the at least one cylinder, each of the at least one piston being operatively connected to the crankshaft, wherein the air intake conduit extends parallel to the crankshaft. 8. The watercraft of claim 1 , further comprising: a supercharger fluidly connected between the outlet end of the air intake conduit and the engine to compress and feed air to the engine. 9. The watercraft of claim 8 , wherein the supercharger is disposed rearward of the engine. 10. The watercraft of claim 1 , wherein the air filter covers the inlet end of the air intake conduit. 11. The watercraft of claim 1 , wherein the shroud is connected to the air filter. 12. The watercraft of claim 1 , wherein the inlet end of the air intake conduit faces forwardly. 13. The watercraft of claim 1 , wherein the air intake conduit extends longitudinally. 14. The watercraft of claim 1 , wherein the inlet end and the outlet end of the air intake conduit are disposed on opposite longitudinal sides of the engine. 15. The watercraft of claim 1 , wherein the inlet end faces rearward. 16. The watercraft of claim 1 , wherein the air filter is generally tubular. 17. The watercraft of claim 1 , wherein the engine compartment is located at a rear portion of the watercraft. 18. The watercraft of claim 1 , further comprising: a driver seat; and at least one passenger seat disposed behind the driver seat, the at least one passenger seat being proximate a front portion of the engine compartment. 19. The watercraft of claim 1 , further comprising a jet propulsion system driven by the engine. 20. The watercraft of claim 1 , wherein the air filter is disposed inside the shroud. 21. The watercraft of claim 1 , wherein the air filter comprises a pleated paper filtering member. 22. The watercraft of claim 1 , wherein the air intake conduit has a secondary inlet near the outlet end for ingress of blow-by gas into the air intake conduit. 23. The watercraft of claim 1 , further comprising an air intake manifold, the air intake manifold and the air intake conduit being disposed on opposite lateral sides of the engine. 24. The watercraft of claim 23 , further comprising: a supercharger fluidly connected between the outlet end of the air intake conduit and the engine to compress and feed air to the engine, the supercharger being disposed laterally between the air intake manifold and the air intake conduit. 25. The watercraft of claim 1 , wherein: the air intake conduit, the air filter and the shroud define in part an air intake system of the watercraft; and the shroud is a front-most element of the air intake system. 26. The watercraft of claim 1 , further comprising a deck disposed on top of and connected to the hull, the deck also defining the engine compartment. 27. The watercraft of claim 1 , wherein the air intake conduit is a straight pipe. 28. The watercraft of claim 1 , further comprising: a supercharger fluidly connected between the outlet end of the air intake conduit and the engine to compress and feed air to the engine, the air intake conduit being vertically higher than the supercharger. 29. The watercraft of claim 1 , wherein the air intake conduit, the shroud, and the air filter are coaxial with one another. 30. The watercraft of claim 1 , wherein the sidewall of the shroud extends at an angle between 5° and 15° relative to a longitudinal axis of the shroud. 31. An engine assembly for a watercraft, comprising: an internal combustion engine comprising: a crankcase; a crankshaft disposed at least in part in the crankcase; a cylinder block connected to the crankcase; at least one cylinder defined in the cylinder block; and at least one piston movably disposed within a corresponding one of the at least one cylinder, each of the at least one piston being operatively connected to the crankshaft; an air intake conduit fluidly connected to the engine, the air intake conduit having an inlet end and an outlet end, the inlet end being disposed on a first side of the engine, the outlet end of the air intake conduit being disposed on a second side of the engine, the first side being opposite the second side; an air filter fluidly connected to the air intake conduit for filtering air flowing into the air intake conduit; and a shroud connected to the inlet end of the air intake conduit, the shroud having an open end and a closed end, the open end being open to flow of air therethrough, the closed end being closed to flow of air therethrough, the shroud having a sidewall extending between the closed and open ends, the shroud being oriented such that a distance between the open end and the second side of the engine is less than a distance between the closed end and the second
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