US20050266744A1 - Personal watercraft engine fluid cooling system - Google Patents
Personal watercraft engine fluid cooling system Download PDFInfo
- Publication number
- US20050266744A1 US20050266744A1 US10/854,625 US85462504A US2005266744A1 US 20050266744 A1 US20050266744 A1 US 20050266744A1 US 85462504 A US85462504 A US 85462504A US 2005266744 A1 US2005266744 A1 US 2005266744A1
- Authority
- US
- United States
- Prior art keywords
- engine
- propulsion unit
- jet propulsion
- engine fluid
- fluid
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H11/00—Marine propulsion by water jets
- B63H11/02—Marine propulsion by water jets the propulsive medium being ambient water
- B63H11/04—Marine propulsion by water jets the propulsive medium being ambient water by means of pumps
- B63H11/08—Marine propulsion by water jets the propulsive medium being ambient water by means of pumps of rotary type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B34/00—Vessels specially adapted for water sports or leisure; Body-supporting devices specially adapted for water sports or leisure
- B63B34/10—Power-driven personal watercraft, e.g. water scooters; Accessories therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H21/00—Use of propulsion power plant or units on vessels
- B63H21/12—Use of propulsion power plant or units on vessels the vessels being motor-driven
- B63H21/14—Use of propulsion power plant or units on vessels the vessels being motor-driven relating to internal-combustion engines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H11/00—Marine propulsion by water jets
- B63H11/02—Marine propulsion by water jets the propulsive medium being ambient water
- B63H11/04—Marine propulsion by water jets the propulsive medium being ambient water by means of pumps
- B63H11/08—Marine propulsion by water jets the propulsive medium being ambient water by means of pumps of rotary type
- B63H2011/081—Marine propulsion by water jets the propulsive medium being ambient water by means of pumps of rotary type with axial flow, i.e. the axis of rotation being parallel to the flow direction
Definitions
- This disclosure relates to a system for cooling engine fluids in a personal watercraft. More particularly, this disclosure relates to a cooling system utilizing the watercraft's jet propulsion unit to cool engine fluids.
- Personal watercrafts have an internal combustion engine contained within an engine compartment that is typically positioned forward of the tunnel.
- the engine powers a jet propulsion unit that propels the watercraft through the water.
- the output shaft of the engine drives an impeller on the jet propulsion unit.
- the impeller which is conventionally contained within a housing, pulls in water from a water inlet located on the underside of the boat, and discharges the water at high velocity through a steerable nozzle at the rear of the boat.
- An oil tank typically provided adjacent to or within the engine contains a lubricating fluid for lubricating the moving parts of the engine.
- the lubricating fluid typically oil, is cycled through the engine and returns to the oil tank where it is reused until the lubricating fluid is drained and replaced during routine maintenance.
- the lubricating fluid absorbs heat and must be cooled to function effectively.
- Known systems for cooling oil involve pumping oil from the engine to a tubular member located proximate to the water inlet. The water drawn up the water inlet by the jet propulsion pump passes over the tubular member and cools the engine oil contained therein.
- Other systems employ heat exchangers mounted to the internal combustion engine that draw heat from the lubricating oil and absorb it into a cooling fluid.
- Engine fluids can be efficiently cooled by utilizing the flow of cool water through the jet propulsion unit.
- a personal watercraft that includes a hull and an overlying deck that includes a cavity defining an engine compartment.
- the watercraft further includes an engine located in the engine compartment, coupled to a jet propulsion unit for powering the watercraft.
- a cooling system for cooling a lubricating fluid of the engine is also included.
- the cooling system includes a lubricating fluid channel surrounding a component of the jet propulsion unit for flowing the lubricating liquid through the liquid passage to exchange heat of the lubricating fluid with water taken up by the jet propulsion unit.
- a cooling system for engine lubricating fluid for a jet-propelled watercraft includes a jet propulsion unit and a channel formed about a component of the jet propulsion unit for circulating engine lubricating fluid thereabout.
- the cooling system further includes a fluid passageway coupled to an engine lubricating fluid reservoir for delivering heated lubricating fluid to the channel where it is cooled and then returning the lubricating fluid to the reservoir.
- a jet propulsion unit for a jet-propelled watercraft.
- the jet propulsion unit includes an outer housing, an impeller journalled within the outer housing, a discharge nozzle positioned rearward of the impeller, and an engine lubricating fluid channel formed about an exterior of the outer housing so that heat from the engine lubricating fluid is transferred to water pumped by the jet pump.
- FIG. 1 is a perspective view of a typical personal watercraft with the engine fluid cooling system.
- FIG. 2 is a perspective exploded view of a prior art jet propulsion unit from a typical personal watercraft.
- FIG. 3 is a schematic of an embodiment of an engine fluid cooling system.
- FIG. 4 is a perspective view of an embodiment of an engine fluid cooling system shown coupled to a personal watercraft engine.
- FIG. 5 is a perspective view of an embodiment of an engine fluid cooling system shown coupled to a personal watercraft engine.
- FIG. 6 is a perspective view of an embodiment of an engine fluid cooling system provided on a jet pump housing of a jet propulsion unit.
- FIG. 7 is a front perspective view of an embodiment of an engine fluid cooling system shown provided on a jet pump housing of a jet propulsion.
- FIG. 8 is flowchart illustrating the operation of an embodiment of an engine fluid cooling system.
- FIG. 1 illustrates generally a watercraft 10 that can include the embodiments of the engine fluid cooling system, as will be described hereinafter.
- Watercraft 10 has generally a front or bow 12 and a rear or stern 14 and includes an upper portion 16 that includes a top deck 18 and shroud 20 .
- the top deck 18 is secured to a bottom hull 22 along an overlapping portion covered with a rub rail 24 , thereby forming a hull.
- the hull formed by the bottom hull 22 and top deck 18 defines a compartment sized to house an internal combustion engine 28 for powering the watercraft 10 and may also include one or more storage compartments (not shown), depending on the size and configuration of the watercraft.
- the deck portion 18 also has a raised, longitudinally extending seat 30 adapted to accommodate one or more riders seated in straddle fashion.
- a grab handle 31 may be disposed transversely across the rear of the seat 30 .
- Jet propulsion unit 32 powers a jet propulsion unit 32 (described with more detail with respect to FIG. 2 ), typically mounted in a tunnel at the bottom rear portion of the watercraft, all shown in phantom in FIG. 1 .
- An oil reservoir 33 is provided adjacent to the engine for providing lubrication to the moving parts of the engine.
- Jet propulsion unit 32 includes a steerable water discharge nozzle 34 that is operatively coupled to a set of handlebars 36 to facilitate steering of the watercraft by the operator.
- the connection between handlebars 36 and discharge nozzle 34 may be of any suitable type, and typically includes mechanical linkages including a control cable (not shown). If desired, an electronic connection could also be utilized.
- the engine may be a two-stroke or four-stroke type engine.
- a cooling system that circulates a cooling fluid, typically, a glycol/water mixture, is employed.
- Closed loop cooling systems (not shown) are well known in the art and include generally, a coolant reservoir, which includes inlet and outlet conduits for directing coolant to and from the engine.
- a pump is included for continually circulating the fluid.
- coolant is circulated through various components of the engine where heat from the engine is transferred to the coolant. Thereafter, the coolant is returned to the coolant reservoir.
- FIG. 2 is an exploded perspective view of a typical prior art jet propulsion unit 40 for a personal watercraft.
- Jet propulsion unit 40 is usually positioned towards the rear of the watercraft near a water inlet.
- a water inlet is generally provided at the rear of the watercraft.
- the jet propulsion unit 40 typically includes a water jet housing 42 , a pump stator 44 and impeller 48 .
- the pump stator 44 includes a plurality of stator blades 46 and impeller 48 includes a plurality of blades 50 .
- Jet propulsion unit 40 may also include a pump extension 52 and a first stationary nozzle 54 and second rotatable nozzle 56 .
- the impeller 48 is coupled to the engine (shown in FIG. 1 ) via a drive shaft (shown in FIG. 4 ) to pull water from the body of water in which the watercraft is operated.
- the moving parts of 4-stroke engines are typically lubricated with oil.
- heat generated by the moving parts of the engine is transferred to the lubricating fluid as it circulates, undesirably increasing the temperature of the lubricating fluid, which, in turn, decreases its efficiency as a lubricant.
- the heat absorbed by the lubricating fluid must be transferred to another source to maintain functionality of the lubricating fluid, as well as, so that the lubricating fluid has capacity to absorb more heat on its subsequent pass through the engine.
- FIG. 3 illustrates, diagrammatically, the cooling system of the disclosure.
- engines include a closed loop system 57 for circulating engine fluids, including, without limitation, engine lubricant and engine coolant.
- the closed loop system 57 continually recycles a volume of fluid until the fluid is replaced.
- engine fluids absorb heat produced by the moving parts of the engine so that the engine can operate efficiently.
- heat absorbed by the engine fluids must be removed.
- An embodiment of the engine fluid cooling system includes an open loop cooling system 59 that works in cooperation with the closed loop system 57 to remove heat retained in the engine fluid circulating therein.
- a heat transfer depicted at 61 , occurs between the closed loop system 57 and the open loop system 59 .
- FIG. 4 depicts an embodiment of the engine lubricating fluid cooling system.
- FIG. 4 illustrates a typical 4-stroke engine 58 for a personal watercraft coupled to a typical jet propulsion unit 40 via a drive shaft 60 for driving the impeller (shown in FIG. 2 ).
- the engine 58 includes an oil reservoir 33 for holding oil after it circulates through various parts of the engine 58 .
- Oil passage lines 64 and 66 are coupled to openings (not shown) in the oil reservoir 33 .
- the oil passage lines 64 and 66 may be made of rubber, plastic, metal, or any other suitable material.
- Oil passage line 64 transports warmed engine oil to the jet propulsion unit 40 , where it is cooled.
- Return line 66 extends from a cooling channel 68 of the jet propulsion unit 40 to the reservoir 33 for returning cooled oil to the reservoir 33 so that it may circulate through the engine 58 .
- the engine fluid being cooled is engine lubricating oil.
- Oil passage line 64 is coupled to a channel 68 , which is a hollow conduit 70 that is coiled about a component of the jet propulsion unit 40 .
- the conduit 70 is shown coiled about the jet pump housing of the jet propulsion unit 40 .
- the conduit 70 is made of a material that allows for heat transfer, such as, without limitation, plastic, rubber, or metal.
- the diameter of the conduit 70 will vary depending upon the geometry of the component on which it is installed. It is preferable to maximize the surface area over which heat transfer will occur. Therefore, the diameter and geometry of the conduit 70 may be varied so that efficient cooling can occur.
- the conduit 70 is coupled to the oil passage line 64 for delivering heated oil to the channel 68 and oil return line 66 for returning cooled oil to the reservoir 33 .
- heat contained in the oil is transferred to the cool water streaming through the jet propulsion unit 40 .
- the system is pressurized and a small pump may be provided to continuously circulate the oil between the reservoir, engine and cooling system.
- FIG. 5 illustrates an alternate embodiment where engine fluid, for example, engine coolant, is circulated to the cooling system at the jet propulsion unit 40 .
- engine fluid for example, engine coolant
- an outlet 66 and inlet 64 line are coupled to the engine coolant reservoir 69 and the cooling system is provided at the jet propulsion unit 40 .
- This embodiment operates similarly to the embodiment depicted in FIG. 4 .
- a pump is provided to maintain constant circulation. In general, the pressure created by this pump is adequate to continue the flow of coolant throughout the engine and to and from the open loop cooling system 59 provided at the jet propulsion unit 40 .
- coolant has circulated through the engine and absorbed heat therefrom, it circulates to the cooling system and the heat is transferred to the ambient water flowing through the jet propulsion unit 40 .
- FIG. 6 is a more detailed perspective view of an embodiment of the cooling channel.
- a length of hollow conduit 70 is coiled a number of times about the exterior of the jet propulsion unit 40 .
- the hollow conduit 70 is coiled about the exterior surface of the jet pump housing 72 in a linear fashion.
- the conduit may be coiled about the component in any pattern, such as, for example, a helical pattern.
- the adjacent coils are shown touching each other. The coils may or may not be welded together, however, it should be understood that the conduit may be coiled such that a gap is left between adjacent coils.
- the number of times that the conduit is coiled about a component is dependent on factors such as the length and diameter of the conduit as well as the geometry of the particular jet propulsion component about which the conduit is coiled. As mentioned above, it is desirable to maximize the surface area to maximize heat transfer.
- the engine fluid cooling system de allows for cooling at any engine speed including idle.
- the impeller rotates at approximately 1,500 RPM at idle.
- water continues to travel through the jet pump system even when the watercraft is at idle, thus providing continuous cooling capacity of engine fluids even when the watercraft is not in motion.
- FIG. 7 depicts an embodiment of a cooling channel.
- the oil is directed from the engine to a cooling channel 68 that is formed between the outer surface 74 of a component of the jet propulsion unit 40 and an internal surface 76 of ajacket 78 .
- the jacket 78 is comprised of a solid enclosure that encases any qualifying component of the jet propulsion unit (described above).
- the channel 68 is shown formed on the jet pump housing 79 .
- An empty space, or channel 80 is created between the jet propulsion unit component and the jacket through which heated oil delivered from the oil reservoir may flow and transfer heat to the water traveling through the jet propulsion unit 40 .
- the cooling channel jacket 78 may be formed of a single piece that includes an internal channel with walls defined solely by the internal surfaces of the jacket.
- the oil does not directly contact a surface of the jet propulsion unit.
- an internal surface contacts the outer surface of the jet propulsion unit and heat transfer from the oil to the water flowing through the jet propulsion unit occurs through the surface of the jacket and the surface of the jet propulsion unit.
- the jacket may be fabricated from metal, plastic, rubber, or any other suitable material that is impermeable yet capable of transferring heat efficiently.
- a separate water jacket piece as described above may be used to retrofit an existing jet propulsion unit.
- the water jacket and jet propulsion unit are formed as one integral piece as is well known in the art.
- a channel is formed between the jet propulsion component and water jacket, as in the embodiment already described, by providing a mold that produces such a channel.
- the jacket formed according to any of the embodiments, includes an inlet (not shown) for coupling the oil reservoir to the cooling jacket to deliver heated oil to the cooling jacket and an outlet (not shown) for returning the cooled oil to the oil reservoir 33 .
- the inlet and outlet may be formed as orifices for receiving oil passage lines as shown in FIG. 3 in a sealed manner so that no oil is lost in the cooling process.
- the cooling channel is sized and shaped so that it interfaces with the component of the jet propulsion unit without interfering with the operation of the jet propulsion unit.
- the cooling channel is provided on the second nozzle (shown in FIG. 2 ), it should be of a size and configuration so as to not interfere with the pivotal rotation of the rotatable nozzle (shown in FIG. 2 ).
- the channel may be provided on any component of the jet propulsion unit that is between the inlet and outlet of the jet pump.
- the channel may be provided on the pump extension, the jet pump housing, the stator, the first stationary nozzle or the second rotatable nozzle (all shown in FIG. 2 ).
- the only requirements for the placement of the cooling channel is that it lie adjacent to the flow of water through the jet propulsion unit and the component is of a size so that a sufficient surface is exposed to the water flowing through the jet propulsion unit to accomplish adequate cooling of the oil.
- the cooling system can be used to cool any number of engine fluids. As FIG. 3 illustrates diagrammatically, the cooling system may be used to cool the engine cooling fluid. As depicted, coolant from the closed loop cooling system 57 may be directed to the open loop cooling system 59 and heat contained within the engine fluid is transferred to the water flowing through the jet propulsion unit 40 as described above.
- the engine fluid cooling process is illustrated diagrammatically in FIG. 8 .
- various engine fluids including lubricating oil and coolant, are circulated through various engine parts.
- the temperature of the engine fluids increases.
- these fluids must be cooled before subsequent cycling through system.
- the engine drives a drive shaft that rotates an impeller.
- the impeller rotates, water is drawn inward and flows through the jet propulsion unit.
- Heated engine fluids are transferred to the jet propulsion unit where a heat transfer between the engine fluid and the ambient water entering the jet propulsion unit occurs.
- the cooled engine fluid is routed back to the engine where it can be cycled again.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Lubrication Of Internal Combustion Engines (AREA)
Abstract
An engine fluid cooling system that utilizes the jet propulsion unit of a personal watercraft to cool the engine fluid. The cooling system includes passages for transporting engine fluid to and from a cooling system that includes a cooling channel formed about a component of the jet propulsion unit so that as the engine fluid travels through the cooling channel, heat, contained in the engine fluid, is transferred to the water flowing through the jet propulsion unit.
Description
- This disclosure relates to a system for cooling engine fluids in a personal watercraft. More particularly, this disclosure relates to a cooling system utilizing the watercraft's jet propulsion unit to cool engine fluids.
- Personal watercrafts have an internal combustion engine contained within an engine compartment that is typically positioned forward of the tunnel. The engine powers a jet propulsion unit that propels the watercraft through the water. The output shaft of the engine drives an impeller on the jet propulsion unit. The impeller, which is conventionally contained within a housing, pulls in water from a water inlet located on the underside of the boat, and discharges the water at high velocity through a steerable nozzle at the rear of the boat. An oil tank, typically provided adjacent to or within the engine contains a lubricating fluid for lubricating the moving parts of the engine. The lubricating fluid, typically oil, is cycled through the engine and returns to the oil tank where it is reused until the lubricating fluid is drained and replaced during routine maintenance.
- During operation, the lubricating fluid absorbs heat and must be cooled to function effectively. Known systems for cooling oil involve pumping oil from the engine to a tubular member located proximate to the water inlet. The water drawn up the water inlet by the jet propulsion pump passes over the tubular member and cools the engine oil contained therein. Other systems employ heat exchangers mounted to the internal combustion engine that draw heat from the lubricating oil and absorb it into a cooling fluid.
- Engine fluids can be efficiently cooled by utilizing the flow of cool water through the jet propulsion unit.
- In various embodiments there is provided a personal watercraft that includes a hull and an overlying deck that includes a cavity defining an engine compartment. The watercraft further includes an engine located in the engine compartment, coupled to a jet propulsion unit for powering the watercraft. A cooling system for cooling a lubricating fluid of the engine is also included. The cooling system includes a lubricating fluid channel surrounding a component of the jet propulsion unit for flowing the lubricating liquid through the liquid passage to exchange heat of the lubricating fluid with water taken up by the jet propulsion unit.
- In various embodiments there is provided a cooling system for engine lubricating fluid for a jet-propelled watercraft. The cooling system includes a jet propulsion unit and a channel formed about a component of the jet propulsion unit for circulating engine lubricating fluid thereabout. The cooling system further includes a fluid passageway coupled to an engine lubricating fluid reservoir for delivering heated lubricating fluid to the channel where it is cooled and then returning the lubricating fluid to the reservoir.
- In various embodiments there is provided a jet propulsion unit for a jet-propelled watercraft. The jet propulsion unit includes an outer housing, an impeller journalled within the outer housing, a discharge nozzle positioned rearward of the impeller, and an engine lubricating fluid channel formed about an exterior of the outer housing so that heat from the engine lubricating fluid is transferred to water pumped by the jet pump.
-
FIG. 1 is a perspective view of a typical personal watercraft with the engine fluid cooling system. -
FIG. 2 is a perspective exploded view of a prior art jet propulsion unit from a typical personal watercraft. -
FIG. 3 is a schematic of an embodiment of an engine fluid cooling system. -
FIG. 4 is a perspective view of an embodiment of an engine fluid cooling system shown coupled to a personal watercraft engine. -
FIG. 5 is a perspective view of an embodiment of an engine fluid cooling system shown coupled to a personal watercraft engine. -
FIG. 6 is a perspective view of an embodiment of an engine fluid cooling system provided on a jet pump housing of a jet propulsion unit. -
FIG. 7 is a front perspective view of an embodiment of an engine fluid cooling system shown provided on a jet pump housing of a jet propulsion. -
FIG. 8 is flowchart illustrating the operation of an embodiment of an engine fluid cooling system. - The following detailed description should be read with reference to the drawings, in which like elements in different drawings are numbered identically. The drawings, which are not necessarily drawn to scale, depict selected embodiments and are not intended to limit the scope of the embodiments. Several forms of the embodiments will be shown and described, and other forms will be apparent to those skilled in the art. It will be understood that embodiments shown in drawings and described are merely for illustrative purposes and are not intended to limit the scope of the embodiments as defined in the claims that follow. Although the engine fluid cooling system is shown with respect to a sit-down type jet ski it should be understood that the embodiments of the engine fluid cooling system can be practiced with any marine vehicle that utilizes a jet propulsion unit.
-
FIG. 1 illustrates generally a watercraft 10 that can include the embodiments of the engine fluid cooling system, as will be described hereinafter. Watercraft 10 has generally a front or bow 12 and a rear orstern 14 and includes an upper portion 16 that includes atop deck 18 andshroud 20. Thetop deck 18 is secured to abottom hull 22 along an overlapping portion covered with arub rail 24, thereby forming a hull. The hull formed by thebottom hull 22 andtop deck 18 defines a compartment sized to house aninternal combustion engine 28 for powering the watercraft 10 and may also include one or more storage compartments (not shown), depending on the size and configuration of the watercraft. - The
deck portion 18 also has a raised, longitudinally extendingseat 30 adapted to accommodate one or more riders seated in straddle fashion. Agrab handle 31 may be disposed transversely across the rear of theseat 30. -
Engine 28 powers a jet propulsion unit 32 (described with more detail with respect toFIG. 2 ), typically mounted in a tunnel at the bottom rear portion of the watercraft, all shown in phantom inFIG. 1 . Anoil reservoir 33 is provided adjacent to the engine for providing lubrication to the moving parts of the engine.Jet propulsion unit 32 includes a steerablewater discharge nozzle 34 that is operatively coupled to a set ofhandlebars 36 to facilitate steering of the watercraft by the operator. The connection betweenhandlebars 36 anddischarge nozzle 34 may be of any suitable type, and typically includes mechanical linkages including a control cable (not shown). If desired, an electronic connection could also be utilized. - The engine may be a two-stroke or four-stroke type engine. Typically, in four-stroke engine watercrafts, a cooling system that circulates a cooling fluid, typically, a glycol/water mixture, is employed. Closed loop cooling systems, (not shown) are well known in the art and include generally, a coolant reservoir, which includes inlet and outlet conduits for directing coolant to and from the engine. Typically, a pump is included for continually circulating the fluid. In operation, as the engine cycles, coolant is circulated through various components of the engine where heat from the engine is transferred to the coolant. Thereafter, the coolant is returned to the coolant reservoir.
-
FIG. 2 is an exploded perspective view of a typical prior artjet propulsion unit 40 for a personal watercraft.Jet propulsion unit 40 is usually positioned towards the rear of the watercraft near a water inlet. A water inlet is generally provided at the rear of the watercraft. Thejet propulsion unit 40 typically includes a water jet housing 42, a pump stator 44 andimpeller 48. The pump stator 44 includes a plurality of stator blades 46 andimpeller 48 includes a plurality ofblades 50.Jet propulsion unit 40 may also include a pump extension 52 and a firststationary nozzle 54 and second rotatable nozzle 56. Theimpeller 48 is coupled to the engine (shown inFIG. 1 ) via a drive shaft (shown inFIG. 4 ) to pull water from the body of water in which the watercraft is operated. - The moving parts of 4-stroke engines are typically lubricated with oil. In the course of lubrication, heat generated by the moving parts of the engine is transferred to the lubricating fluid as it circulates, undesirably increasing the temperature of the lubricating fluid, which, in turn, decreases its efficiency as a lubricant. Obviously, the heat absorbed by the lubricating fluid must be transferred to another source to maintain functionality of the lubricating fluid, as well as, so that the lubricating fluid has capacity to absorb more heat on its subsequent pass through the engine.
-
FIG. 3 illustrates, diagrammatically, the cooling system of the disclosure. Typically, engines include aclosed loop system 57 for circulating engine fluids, including, without limitation, engine lubricant and engine coolant. Theclosed loop system 57 continually recycles a volume of fluid until the fluid is replaced. Generally, engine fluids absorb heat produced by the moving parts of the engine so that the engine can operate efficiently. In order for the engine fluids to function efficiently, heat absorbed by the engine fluids must be removed. An embodiment of the engine fluid cooling system includes an openloop cooling system 59 that works in cooperation with theclosed loop system 57 to remove heat retained in the engine fluid circulating therein. In operation, a heat transfer, depicted at 61, occurs between theclosed loop system 57 and theopen loop system 59. -
FIG. 4 depicts an embodiment of the engine lubricating fluid cooling system.FIG. 4 illustrates a typical 4-stroke engine 58 for a personal watercraft coupled to a typicaljet propulsion unit 40 via a drive shaft 60 for driving the impeller (shown inFIG. 2 ). Theengine 58 includes anoil reservoir 33 for holding oil after it circulates through various parts of theengine 58. Oil passage lines 64 and 66 are coupled to openings (not shown) in theoil reservoir 33. The oil passage lines 64 and 66 may be made of rubber, plastic, metal, or any other suitable material.Oil passage line 64 transports warmed engine oil to thejet propulsion unit 40, where it is cooled. Return line 66 extends from a coolingchannel 68 of thejet propulsion unit 40 to thereservoir 33 for returning cooled oil to thereservoir 33 so that it may circulate through theengine 58. - In the embodiment depicted in
FIG. 4 , the engine fluid being cooled is engine lubricating oil.Oil passage line 64 is coupled to achannel 68, which is ahollow conduit 70 that is coiled about a component of thejet propulsion unit 40. Theconduit 70 is shown coiled about the jet pump housing of thejet propulsion unit 40. Theconduit 70 is made of a material that allows for heat transfer, such as, without limitation, plastic, rubber, or metal. The diameter of theconduit 70 will vary depending upon the geometry of the component on which it is installed. It is preferable to maximize the surface area over which heat transfer will occur. Therefore, the diameter and geometry of theconduit 70 may be varied so that efficient cooling can occur. - The
conduit 70 is coupled to theoil passage line 64 for delivering heated oil to thechannel 68 and oil return line 66 for returning cooled oil to thereservoir 33. As the heated oil travels the length of the conduit, heat contained in the oil is transferred to the cool water streaming through thejet propulsion unit 40. Typically, as is known in the art, in closed loop systems, the system is pressurized and a small pump may be provided to continuously circulate the oil between the reservoir, engine and cooling system. -
FIG. 5 illustrates an alternate embodiment where engine fluid, for example, engine coolant, is circulated to the cooling system at thejet propulsion unit 40. Similar to the embodiment depicted inFIG. 4 , an outlet 66 andinlet 64 line are coupled to the engine coolant reservoir 69 and the cooling system is provided at thejet propulsion unit 40. This embodiment operates similarly to the embodiment depicted inFIG. 4 . Typically, in closed loop systems, a pump is provided to maintain constant circulation. In general, the pressure created by this pump is adequate to continue the flow of coolant throughout the engine and to and from the openloop cooling system 59 provided at thejet propulsion unit 40. Thus, after coolant has circulated through the engine and absorbed heat therefrom, it circulates to the cooling system and the heat is transferred to the ambient water flowing through thejet propulsion unit 40. -
FIG. 6 is a more detailed perspective view of an embodiment of the cooling channel. As can be seen, a length ofhollow conduit 70 is coiled a number of times about the exterior of thejet propulsion unit 40. In the embodiment depicted, thehollow conduit 70 is coiled about the exterior surface of the jet pump housing 72 in a linear fashion. Those skilled in the art will appreciate that the conduit may be coiled about the component in any pattern, such as, for example, a helical pattern. In the embodiment depicted inFIG. 4 , the adjacent coils are shown touching each other. The coils may or may not be welded together, however, it should be understood that the conduit may be coiled such that a gap is left between adjacent coils. The number of times that the conduit is coiled about a component is dependent on factors such as the length and diameter of the conduit as well as the geometry of the particular jet propulsion component about which the conduit is coiled. As mentioned above, it is desirable to maximize the surface area to maximize heat transfer. - As water is drawn through the jet pump housing 72, heat from the oil flowing through the
hollow conduit 70 is transferred to the water that is at a lower temperature and thus cools the oil. The engine fluid cooling system de allows for cooling at any engine speed including idle. In a typical watercraft, the impeller rotates at approximately 1,500 RPM at idle. Thus, water continues to travel through the jet pump system even when the watercraft is at idle, thus providing continuous cooling capacity of engine fluids even when the watercraft is not in motion. -
FIG. 7 depicts an embodiment of a cooling channel. In this embodiment, the oil is directed from the engine to a coolingchannel 68 that is formed between the outer surface 74 of a component of thejet propulsion unit 40 and aninternal surface 76 of ajacket 78. The jacket 78 is comprised of a solid enclosure that encases any qualifying component of the jet propulsion unit (described above). In the embodiment depicted inFIG. 7 , thechannel 68 is shown formed on thejet pump housing 79. An empty space, orchannel 80 is created between the jet propulsion unit component and the jacket through which heated oil delivered from the oil reservoir may flow and transfer heat to the water traveling through thejet propulsion unit 40. Alternately, the cooling channel jacket 78 may be formed of a single piece that includes an internal channel with walls defined solely by the internal surfaces of the jacket. In this embodiment, the oil does not directly contact a surface of the jet propulsion unit. However, an internal surface contacts the outer surface of the jet propulsion unit and heat transfer from the oil to the water flowing through the jet propulsion unit occurs through the surface of the jacket and the surface of the jet propulsion unit. The jacket may be fabricated from metal, plastic, rubber, or any other suitable material that is impermeable yet capable of transferring heat efficiently. A separate water jacket piece as described above may be used to retrofit an existing jet propulsion unit. - In an alternate embodiment, the water jacket and jet propulsion unit are formed as one integral piece as is well known in the art. In this embodiment, a channel is formed between the jet propulsion component and water jacket, as in the embodiment already described, by providing a mold that produces such a channel.
- The jacket, formed according to any of the embodiments, includes an inlet (not shown) for coupling the oil reservoir to the cooling jacket to deliver heated oil to the cooling jacket and an outlet (not shown) for returning the cooled oil to the
oil reservoir 33. The inlet and outlet may be formed as orifices for receiving oil passage lines as shown inFIG. 3 in a sealed manner so that no oil is lost in the cooling process. - The cooling channel, according to any embodiment, is sized and shaped so that it interfaces with the component of the jet propulsion unit without interfering with the operation of the jet propulsion unit. For example, if the cooling channel is provided on the second nozzle (shown in
FIG. 2 ), it should be of a size and configuration so as to not interfere with the pivotal rotation of the rotatable nozzle (shown inFIG. 2 ). - The channel may be provided on any component of the jet propulsion unit that is between the inlet and outlet of the jet pump. For example, without limitation, the channel may be provided on the pump extension, the jet pump housing, the stator, the first stationary nozzle or the second rotatable nozzle (all shown in
FIG. 2 ). The only requirements for the placement of the cooling channel is that it lie adjacent to the flow of water through the jet propulsion unit and the component is of a size so that a sufficient surface is exposed to the water flowing through the jet propulsion unit to accomplish adequate cooling of the oil. - The cooling system can be used to cool any number of engine fluids. As
FIG. 3 illustrates diagrammatically, the cooling system may be used to cool the engine cooling fluid. As depicted, coolant from the closedloop cooling system 57 may be directed to the openloop cooling system 59 and heat contained within the engine fluid is transferred to the water flowing through thejet propulsion unit 40 as described above. - The engine fluid cooling process is illustrated diagrammatically in
FIG. 8 . As the engine operates, various engine fluids, including lubricating oil and coolant, are circulated through various engine parts. During circulation, the temperature of the engine fluids increases. To function effectively, these fluids must be cooled before subsequent cycling through system. Contemporaneously with fluid cycling, the engine drives a drive shaft that rotates an impeller. As the impeller rotates, water is drawn inward and flows through the jet propulsion unit. Heated engine fluids are transferred to the jet propulsion unit where a heat transfer between the engine fluid and the ambient water entering the jet propulsion unit occurs. Finally, the cooled engine fluid is routed back to the engine where it can be cycled again. - Thus, embodiments of the Personal Watercraft Engine Fluid Cooling System are disclosed. One skilled in the art will appreciate that these embodiments can be practiced with embodiments other than those disclosed. The disclosed embodiments are presented for purposes of illustration and not limitation, and the embodiments are limited only by the claims that follow.
Claims (24)
1. A system for a personal watercraft having an engine fluid cooling apparatus, the system comprising:
a hull and an overlying deck, forming a cavity that defines an engine compartment;
an engine, located in the engine compartment, coupled to a jet propulsion unit for powering the watercraft; and
an engine fluid passage surrounding a component of the jet propulsion unit for directing the engine fluid through the engine fluid passage so that heat in the engine fluid is transferred to water taken up by the jet propulsion unit.
2. The personal watercraft of claim 1 , further including an engine fluid channel line coupling an engine fluid reservoir to the engine fluid passage for delivering heated lubricating fluid to the passage for cooling.
3. The personal watercraft of claim 1 , wherein the engine fluid passage is a conduit coiled about the component of the jet propulsion unit.
4. The personal watercraft of claim 1 , wherein the engine fluid passage is a coil formed about a jet pump housing of the jet propulsion unit.
5. The personal watercraft of claim 1 , wherein the engine fluid passage is a channel formed between an exterior of the component of the jet propulsion unit and a jacket formed about the component of the jet propulsion unit.
6. The personal watercraft of claim 5 , wherein the jacket is integral with the component of the jet propulsion unit.
7. The personal watercraft of claim 1 , wherein the engine fluid passage is a channel formed between an exterior of a jet pump housing of the jet propulsion unit and a jacket formed thereabout.
8. An engine fluid cooling apparatus for a jet-propelled watercraft, comprising:
an engine fluid passage formed about a component of a jet propulsion unit for circulating engine fluid thereabout, and
an engine fluid passageway coupling an engine fluid reservoir to the engine fluid passage, wherein heated engine fluid is delivered to the engine fluid passage where it is cooled and then returned to the engine fluid reservoir.
9. The cooling system of claim 8 , wherein the engine fluid passage is formed by coiling a hollow conduit about the component of the jet propulsion unit.
10. The cooling system of claim 8 , wherein the engine fluid passage is a hollow conduit coiled about a stator of the jet propulsion unit.
11. The cooling system of claim 8 , wherein the engine fluid passage is formed by coiling a hollow conduit coiled about a jet pump housing of the jet propulsion unit.
12. The cooling system of claim 8 , wherein the engine fluid passage is a channel formed between an exterior of the component of the jet propulsion unit and a jacket that at least partially surrounds the component of the jet propulsion unit.
13. The cooling system of claim 12 , wherein the component of the jet propulsion unit is a stator.
14. The cooling system of claim 12 , wherein the component of the jet propulsion unit is a jet pump housing.
15. A jet propulsion unit for a jet-propelled watercraft, comprising:
an outer housing;
an impeller journalled within the outer housing;
a discharge nozzle positioned rearward of the impeller; and
an engine lubricating fluid channel formed contiguously with the outer housing so that heat from an engine fluid is transferred to water flowing through the jet propulsion unit.
16. The jet propulsion unit of claim 15 , wherein the engine lubricating fluid channel is couplable to an engine lubricating fluid reservoir.
17. The jet propulsion unit of claim 15 , wherein the engine lubricating fluid channel is a hollow conduit coiled around the outer housing.
18. The jet propulsion unit of claim 17 , wherein the hollow conduit is coiled around a jet pump housing.
19. The jet propulsion unit of claim 17 , wherein the hollow conduit is coiled around a stator of the jet propulsion unit.
20. The jet propulsion unit of claim 15 , further comprising an inlet in the engine lubricating fluid channel for receiving heated lubricating fluid from an engine of the watercraft.
21. The jet propulsion unit of claim 20 , further comprising an outlet in the engine lubricating fluid channel for diverting cooled lubricating fluid back to the engine.
22. A cooling system for cooling an engine fluid of a watercraft, comprising:
cooling means formed about a component of the jet propulsion unit; and
means for transporting the engine fluid to and from the cooling means.
23. A method of cooling an engine fluid of a watercraft, the method comprising the steps of:
diverting an engine fluid from a circulatory path to an engine fluid cooling system located at a jet propulsion unit of a watercraft;
transferring heat stored in the engine fluid to ambient water traveling through the jet propulsion unit thereby cooling the engine fluid; and
returning the cooled engine fluid to its circulatory path.
24. A method of cooling an engine fluid in a watercraft, comprising the step of:
circulating a heated engine fluid adjacent to a component of a jet propulsion unit so that heat contained in the engine fluid is transferred to ambient water flowing through the jet propulsion unit.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/854,625 US20050266744A1 (en) | 2004-05-26 | 2004-05-26 | Personal watercraft engine fluid cooling system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/854,625 US20050266744A1 (en) | 2004-05-26 | 2004-05-26 | Personal watercraft engine fluid cooling system |
Publications (1)
Publication Number | Publication Date |
---|---|
US20050266744A1 true US20050266744A1 (en) | 2005-12-01 |
Family
ID=35425974
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/854,625 Abandoned US20050266744A1 (en) | 2004-05-26 | 2004-05-26 | Personal watercraft engine fluid cooling system |
Country Status (1)
Country | Link |
---|---|
US (1) | US20050266744A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2508196A (en) * | 2012-11-23 | 2014-05-28 | Bwm Ribs Ltd | Water craft jet pump heat exchanger |
Citations (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US625442A (en) * | 1899-05-23 | Herbert flanders | ||
US2970436A (en) * | 1958-06-26 | 1961-02-07 | United Aircraft Corp | Fuel control for dual heat source power plant |
US3292373A (en) * | 1963-12-10 | 1966-12-20 | Yanmar Diesel Engine Co | Marine propulsion apparatus |
US3306046A (en) * | 1965-03-19 | 1967-02-28 | Ontboard Marine Corp | Reaction jet marine engine |
US4552537A (en) * | 1979-06-20 | 1985-11-12 | Haynes Hendrick W | Marine propulsion device with engine heat recovery system and streamlining hull closures |
US5330374A (en) * | 1992-02-17 | 1994-07-19 | Sanshin Kogyo Kabushiki Kaisha | Jet propulsion system |
US5403216A (en) * | 1992-09-28 | 1995-04-04 | Kvaerner Masa-Yards Oy | Ship propulsion arrangement |
US5507673A (en) * | 1995-05-30 | 1996-04-16 | Boggia; Richard | Jet propelled watercraft |
US5885121A (en) * | 1996-03-19 | 1999-03-23 | Yamaha Hatsudoki Kabushiki Kaisha | Cooling system for watercraft engine |
US5937801A (en) * | 1998-07-31 | 1999-08-17 | Brunswick Corporation | Oil temperature moderator for an internal combustion engine |
US6029463A (en) * | 1995-12-22 | 2000-02-29 | Thermoprodukter Ab | Method and apparatus for cooling or condensing mediums |
US6062922A (en) * | 1998-10-30 | 2000-05-16 | Yamaha Hatsudoki Kabushiki Kaisha | Watercraft propulsion system |
US6431925B1 (en) * | 1999-08-04 | 2002-08-13 | Sanshin Kogyo Kabushiki Kaisha | Jet propulsion system for watercraft |
US6482055B1 (en) * | 2001-08-11 | 2002-11-19 | Bombardier Motor Corporation Of America | Water jet propulsion unit having linear weed grate clean-out system |
US6497596B1 (en) * | 1996-05-31 | 2002-12-24 | Yamaha Hatsudoki Kabushiki Kaisha | Oil cooler for watercraft |
US6500035B2 (en) * | 1999-10-01 | 2002-12-31 | Hrp Nederland B.V. | Waterjet propulsion unit |
US6524149B1 (en) * | 1998-04-13 | 2003-02-25 | Yamaha Hatsudoki Kabushiki Kaisha | Cooled oil reservoir for watercraft |
US6869324B2 (en) * | 2002-02-07 | 2005-03-22 | Kawasaki Jukogyo Kabushiki Kaisha | Small watercraft |
-
2004
- 2004-05-26 US US10/854,625 patent/US20050266744A1/en not_active Abandoned
Patent Citations (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US625442A (en) * | 1899-05-23 | Herbert flanders | ||
US2970436A (en) * | 1958-06-26 | 1961-02-07 | United Aircraft Corp | Fuel control for dual heat source power plant |
US3292373A (en) * | 1963-12-10 | 1966-12-20 | Yanmar Diesel Engine Co | Marine propulsion apparatus |
US3306046A (en) * | 1965-03-19 | 1967-02-28 | Ontboard Marine Corp | Reaction jet marine engine |
US4552537A (en) * | 1979-06-20 | 1985-11-12 | Haynes Hendrick W | Marine propulsion device with engine heat recovery system and streamlining hull closures |
US5330374A (en) * | 1992-02-17 | 1994-07-19 | Sanshin Kogyo Kabushiki Kaisha | Jet propulsion system |
US5403216A (en) * | 1992-09-28 | 1995-04-04 | Kvaerner Masa-Yards Oy | Ship propulsion arrangement |
US5507673A (en) * | 1995-05-30 | 1996-04-16 | Boggia; Richard | Jet propelled watercraft |
US6029463A (en) * | 1995-12-22 | 2000-02-29 | Thermoprodukter Ab | Method and apparatus for cooling or condensing mediums |
US5885121A (en) * | 1996-03-19 | 1999-03-23 | Yamaha Hatsudoki Kabushiki Kaisha | Cooling system for watercraft engine |
US6497596B1 (en) * | 1996-05-31 | 2002-12-24 | Yamaha Hatsudoki Kabushiki Kaisha | Oil cooler for watercraft |
US6524149B1 (en) * | 1998-04-13 | 2003-02-25 | Yamaha Hatsudoki Kabushiki Kaisha | Cooled oil reservoir for watercraft |
US5937801A (en) * | 1998-07-31 | 1999-08-17 | Brunswick Corporation | Oil temperature moderator for an internal combustion engine |
US6062922A (en) * | 1998-10-30 | 2000-05-16 | Yamaha Hatsudoki Kabushiki Kaisha | Watercraft propulsion system |
US6431925B1 (en) * | 1999-08-04 | 2002-08-13 | Sanshin Kogyo Kabushiki Kaisha | Jet propulsion system for watercraft |
US6500035B2 (en) * | 1999-10-01 | 2002-12-31 | Hrp Nederland B.V. | Waterjet propulsion unit |
US6482055B1 (en) * | 2001-08-11 | 2002-11-19 | Bombardier Motor Corporation Of America | Water jet propulsion unit having linear weed grate clean-out system |
US6869324B2 (en) * | 2002-02-07 | 2005-03-22 | Kawasaki Jukogyo Kabushiki Kaisha | Small watercraft |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2508196A (en) * | 2012-11-23 | 2014-05-28 | Bwm Ribs Ltd | Water craft jet pump heat exchanger |
GB2508196B (en) * | 2012-11-23 | 2015-08-12 | Bwm Ribs Ltd | Water craft jet pump heat exchanger |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US6497596B1 (en) | Oil cooler for watercraft | |
US6544085B1 (en) | Watercraft having a closed coolant circulating system with a heat exchanger that constitutes an exterior surface of the hull | |
US5921829A (en) | Outboard motor cooling system | |
US20070135000A1 (en) | Outboard jet drive marine propulsion system | |
US6418887B1 (en) | Lubricant cooling system for outboard motor | |
US6869324B2 (en) | Small watercraft | |
US11454158B2 (en) | Outboard motor and marine vessel | |
US6347969B1 (en) | Cooling system for outboard motor | |
US6406344B1 (en) | Marine exhaust with dual cooling | |
US20050266744A1 (en) | Personal watercraft engine fluid cooling system | |
US7597600B2 (en) | Engine for driving a watercraft propelled by a water jet | |
US7094118B1 (en) | Heat exchanger for a marine propulsion system | |
US20230211863A1 (en) | Marine drive unit comprising a closed cooling circuit | |
US6524149B1 (en) | Cooled oil reservoir for watercraft | |
JPS63170190A (en) | Lubricating device for marine propeller | |
US7137376B2 (en) | Viscoidal fluid removing arrangement for engine | |
US20220297814A1 (en) | Outboard engine | |
US6863582B1 (en) | Air ventilation system for a watercraft | |
JP4017890B2 (en) | Small planing boat | |
US7056173B1 (en) | Heater and a method for delivering heat energy from a water cooled two cycle marine engine | |
AU2020231603A1 (en) | A marine outboard motor with drive shaft and cooling system | |
US20230084989A1 (en) | Jet pump housing with cooling channels | |
US20040099194A1 (en) | Conduit-supporting structure for a small watercraft | |
WO2024052109A1 (en) | A marine drive unit with a bi-directional integrated oil channel | |
JP2006307865A (en) | Small ship |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: POLARIS INDUSTRIES INC., MINNESOTA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:GARDNER, JEFFREY L.;KNUDTSON, CORY DANE;REEL/FRAME:015728/0727 Effective date: 20040816 |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |