US20010008820A1 - Fuel cooling system for small watercraft engine - Google Patents
Fuel cooling system for small watercraft engine Download PDFInfo
- Publication number
- US20010008820A1 US20010008820A1 US09/759,147 US75914701A US2001008820A1 US 20010008820 A1 US20010008820 A1 US 20010008820A1 US 75914701 A US75914701 A US 75914701A US 2001008820 A1 US2001008820 A1 US 2001008820A1
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- United States
- Prior art keywords
- fuel
- coolant
- heat exchanger
- injector
- cooling water
- Prior art date
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- 239000000446 fuel Substances 0.000 title claims abstract description 154
- 238000001816 cooling Methods 0.000 title claims abstract description 20
- 239000000498 cooling water Substances 0.000 claims abstract description 40
- 239000002828 fuel tank Substances 0.000 claims abstract description 30
- 238000002347 injection Methods 0.000 claims abstract description 7
- 239000007924 injection Substances 0.000 claims abstract description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 10
- 239000002826 coolant Substances 0.000 claims 20
- 230000000694 effects Effects 0.000 description 5
- 241000005139 Lycium andersonii Species 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M31/00—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture
- F02M31/20—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for cooling
-
- 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
- B63H21/24—Use of propulsion power plant or units on vessels the vessels being small craft, e.g. racing boats
-
- 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
- B63H21/38—Apparatus or methods specially adapted for use on marine vessels, for handling power plant or unit liquids, e.g. lubricants, coolants, fuels or the like
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B61/00—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing
- F02B61/04—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing for driving propellers
- F02B61/045—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing for driving propellers for marine engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P2050/00—Applications
- F01P2050/02—Marine engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P2050/00—Applications
- F01P2050/02—Marine engines
- F01P2050/04—Marine engines using direct cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P2050/00—Applications
- F01P2050/02—Marine engines
- F01P2050/06—Marine engines using liquid-to-liquid heat exchangers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P2050/00—Applications
- F01P2050/02—Marine engines
- F01P2050/10—Z-type engine
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P2060/00—Cooling circuits using auxiliaries
- F01P2060/10—Fuel manifold
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the invention relates to a fuel cooling system for a circulating fuel supply apparatus of an engine for a small watercraft, adapted to be supplied fuel into an injector from a fuel tank through a fuel supply pipe by a fuel supply pump, and to return excess fuel in the injector to a fuel tank through a fuel return pipe.
- FIG. 6 shows a basic configuration of a circulating fuel supply apparatus. It is provided in an outboard engine, in which a fuel inlet port 14 a of each injector 14 is connected to a fuel tank 6 via a fuel supply pipe 17 and a fuel pump 18 , and an excess fuel return port 14 b of each injector 14 is connected to the fuel tank 6 via a return pipe 19 and a vapor separator 50 .
- the vapor separator 50 is provided in the return pipe 19 of an outboard engine for cooling the fuel, whereby the vapor separator 50 works to remove a vaporized component of a return fuel and to cool the fuel.
- the vapor separator 50 can be provided only in the return pipe 19 which is low pressure due to the structure thereof.
- the related art is disclosed in Japanese KOUKAI Patent No. SHO60-104760.
- the invention has been made in view of the above circumstances, and provides a circulating fuel supply apparatus for a engine of a small watercraft, having a cooling device with a simple structure, and adapted to cool the fuel in the apparatus efficiently and supply the resultant fuel to an injector so as to repress, or minimize, vaporization of the fuel.
- cooling of the injector is done with a high reliability, and injection of the fuel by the injector is done properly.
- the invention provides a circulating fuel supply apparatus for an engine of a small watercraft, which is adapted to supply a fuel in a fuel tank to an injector via a fuel supply pipe by means of a fuel pump.
- the fuel supply apparatus returns excess fuel from the injector to the fuel tank via a fuel return pipe and has a fuel cooling device in the portion of the fuel supply pipe which is between the fuel pump and the injector.
- the fuel drawn from the fuel tank and about to enter the injectors is cooled by the fuel cooling device.
- This enables the fuel to be cooled and then supplied to the injectors efficiently as compared with a case where the return fuel is cooled.
- injection of the fuel is done properly by the injectors.
- the circulating fuel supply apparatus for the engine of the small watercraft has a heat exchanger that uses a cooling water as the fuel cooling device. This enables the fuel cooling device to be simplified, and the manufacturing costs to be reduced.
- the heat exchanger uses, as cooling water, an exchanger external cooling water taken in from the outside by a water jet propulsion unit of the watercraft, and the external cooling water which has been used to cool the fuel is discharged to the outside of the watercraft.
- Such enables maintenance of the cooling water to be done simply, the running costs to be reduced, and the fuel cooling effect to be increased as compared with a similar apparatus in which the internal cooling water is circulated in a closed circuit.
- FIG. 1 is a side view of a small watercraft to which the invention is applied;
- FIG. 2 is a schematic piping diagram of a circulating fuel supply apparatus shown in FIG. 1;
- FIG. 3 is an enlarged longitudinal section of a heat exchanger shown in FIG. 2;
- FIG. 4 is a longitudinal sectional view showing a modified example of the heat exchanger
- FIG. 5 is a longitudinal sectional view showing another modified example of the heat exchanger.
- FIG. 6 is a schematic piping diagram showing an example of a related art circulating fuel supply apparatus.
- FIG. 1 is a schematic side view showing the interior of a small watercraft to which the invention is applied.
- the body of the small watercraft is formed of a hull 1 and a deck 2 is disposed thereon.
- a straddle type seat 3 and a handle 4 are provided on an upper side of the deck 2 .
- a water jet propulsion unit 8 including a duct 9 , guide blades (flow setting plates) 40 , an ejection, or jet, nozzle 5 , and an impeller 7 are provided in a rear portion of the hull 1 .
- a water jet propulsion unit 8 including a duct 9 , guide blades (flow setting plates) 40 , an ejection, or jet, nozzle 5 , and an impeller 7 are provided.
- Fixed to the rear of the ejection nozzle 5 is a laterally controllable steering nozzle 13 .
- the impeller 7 is housed in the duct 9 and connected to an output shaft of an engine 11 via an impeller (driving) shaft 10 .
- a rear end portion of the impeller shaft 10 is supported rotatably in a bearing case 40 a retained by the guide blades 40 .
- water is sucked from a water intake port 12 in a bottom wall of the hull 1 into the duct 9 , and ejected from a rear end discharge port 13 a of the steering nozzle 13 via the guide blades 40 , and a jet nozzle 5 .
- An engine 11 is a direct injection type 3-cylinder 2-cycle engine, disposed in the engine compartment provided below the seat 3 , and having an injector 14 in each cylinder head 20 .
- a fuel tank 6 is provided ahead of the engine in the hull.
- a circulating fuel supply apparatus will now be described.
- a basic structure of the apparatus is similar to that of the above described related art shown in FIG. 6.
- an inlet port 14 a of each injector 14 is connected to the fuel tank 6 via a fuel supply pipe 17 and a fuel pump 18
- an excess fuel return port 14 b of the injector 14 is connected to the fuel tank 6 via a return pipe 19 .
- the fuel is sucked from the fuel tank 6 by the fuel pump 18 , then pressurized, and supplied to each injector 14 via the fuel supply pipe 17 by the fuel pump 18 .
- Excess fuel in the injectors 14 is returned to the fuel tank 6 via the return pipe 19 .
- FIG. 2 shows three injectors 14 in a left portion thereof, in addition to the three injectors 14 drawn on the upper side of the engine 11 , they are one and the same three injectors 14 .
- the injectors 14 shown in the left portion of the drawing, are drawn between the fuel supply pipe 17 and return pipe 19 for the purpose of more clearly showing the fuel circulating path.
- the above described circulating fuel supply apparatus has a heat exchanger 21 for cooling the fuel.
- the heat exchanger 21 is provided in the portion of the fuel supply pipe 17 which is between the fuel pump 18 and the injectors 14 .
- a cooling water intake port 23 is opened in the portion of the interior of the water jet propulsion unit 8 which corresponds to the guide blades 40 .
- the cooling water intake port 23 is connected to a cooling water inlet port 31 of the heat exchanger 21 via a cooling water pipe 24 .
- a cooling water outlet port 32 of the heat exchanger 21 is connected to a cooling water jacket inlet port 15 a of a inlet manifold 15 of the engine 11 via a cooling water pipe 25 , and a cooling water jacket in the inlet manifold 15 communicates with water jackets in cylinders 16 and cylinder heads 20 of the engine 11 .
- a cooling water discharge pipe 26 is connected to a cooling waterjacket outlet port 20 a of the cylinder heads 20 .
- the cooling water discharge pipe 26 is adapted to discharge used cooling water to the outside of the small watercraft.
- FIG. 3 shows a preferred embodiment of the heat exchanger 21 .
- the heat exchanger 21 is formed of an outer case 30 of aluminum for the cooling water, and an inner pipe 27 of stainless steel for the fuel which is disposed coaxially in and extends through the outer case 30 .
- the inner pipe 27 for the fuel is connected at both ends of the case to the fuel supply pipe 17 .
- the cooling water inlet port 31 is provided at a lower end of a fuel downstream side portion of the outer case 30 with respect to a flow of the fuel (direction of an arrow A), and the cooling water outlet port 32 is provided at an upper end of a fuel upstream side portion of the outer case 30 .
- the fuel in the fuel tank 6 is sucked, pressurized, and sent under pressure into the fuel supply pipe 17 by the fuel pump 18 , passed through the heat exchanger 21 in which the fuel is cooled with the cooling water, and then sent under pressure into the injectors 14 from which a part of fuel is injected into combustion chambers of the engine (not shown).
- the fuel in the heat exchanger 21 hardly includes vaporized fuel. Therefore, the fuel cooling effect is higher than as compared with that in a case where the return fuel is cooled.
- the quantity of the fuel injected by the injectors 14 into the combustion chambers in this embodiment is substantially not larger than a half of that discharged from the fuel pump 18 .
- the excess fuel is returned to the fuel tank 6 through the return pipe 19 .
- the cooling water (external cooling water) is taken in from the outside through the cooling water intake port 23 by the water jet propulsion unit 8 , enters the outer case 30 of the heat exchanger 21 , of FIG. 3, via the cooling water pipe 24 , and cools the fuel from an outer circumference of the inner pipe 27 .
- the cooling water is used for the fuel cooling operation, it is supplied from the cooling water outlet port 32 of the outer case to the inlet manifold 15 , shown in FIG. 2, through the cooling water pipe 25 , and then to the interior of the engine 11 , whereby the inlet manifold 15 , cylinder heads 20 and cylinder 16 of the engine 11 are cooled.
- the cooling water with which the engine 11 has been cooled is discharged to the exterior of the boat through the discharge pipe 26 .
- FIG. 4 shows a modified embodiment of the heat exchanger 21 , in which an inner pipe 27 for fuel is formed spirally.
- the contact area (length) of the inner pipe 27 with respect to the cooling water is increased.
- the structure of the other parts is identical with that of the corresponding parts of the heat exchanger of FIG. 3.
- FIG. 5 also shows a modified embodiment of the heat exchanger 21 , in which an inner pipe 27 for the fuel is formed in the shape of the letter “U” (the inner pipe U-type so as to have forwardly and backwardly extending portions), whereby the cooling water contact area of the inner pipe 27 is increased.
- the inlet and outlet side portions of the inner pipe 27 extend through the same side end wall of the outer case 30 .
- the structure of the remaining parts is identical with that of the corresponding parts of the heat exchanger of FIG. 3.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
A circulating fuel supply apparatus for an engine of a small watercraft, formed so as to supply fuel in a fuel tank to at least one injector via a fuel supply pipe using a fuel pump. The apparatus returns excess fuel in at least one injector to the fuel tank via a fuel return pipe. A heat exchanger uses externally obtained cooling water as a fuel cooling device in the portion of the fuel supply pipe which is between the fuel pump and the injector. As the fuel which is about to enter the injector is cooled, a sufficiently cooled fuel can be supplied to at least one injector as compared with a case where return fuel is cooled, thus enabling the injector to carry out proper fuel injection operation.
Description
- 1. Field of Invention
- The invention relates to a fuel cooling system for a circulating fuel supply apparatus of an engine for a small watercraft, adapted to be supplied fuel into an injector from a fuel tank through a fuel supply pipe by a fuel supply pump, and to return excess fuel in the injector to a fuel tank through a fuel return pipe.
- 2. Description of Related Art
- FIG. 6 shows a basic configuration of a circulating fuel supply apparatus. It is provided in an outboard engine, in which a
fuel inlet port 14a of eachinjector 14 is connected to afuel tank 6 via afuel supply pipe 17 and afuel pump 18, and an excessfuel return port 14 b of eachinjector 14 is connected to thefuel tank 6 via areturn pipe 19 and avapor separator 50. - When such a circulating fuel supply apparatus, as shown in FIG. 6, is applied to the engine of a small watercraft, fuel temperature increases for the following reasons:
- (1) When the fuel supply apparatus is operated in midsummer, the fuel tank itself is heated by the sunlight to cause the fuel temperature to increase in the interior of the fuel tank. Especially, a small watercraft that is used primarily in summer, has an engine compartment in the hull that has small dimensions as compared with those of an automobile or larger boat. The fuel tank is provided in a small space in the engine compartment with the engine, so that the temperature in the interior of the
fuel tank 6 increases even more. - (2) In the circulating fuel supply apparatus, a part of fuel supplied by the fuel pump is used for the injection by the injector, and the remaining fuel in the injector is returned as an excess fuel to the fuel tank, so that the fuel, the temperature of which has been increased in the interior of the injector, returns with the increased temperature to the fuel tank. Therefore, the temperature in the interior of the fuel tank increases gradually as the operation of the circulating fuel supply apparatus continues.
- In the case where an electromagnetic solenoid, for opening and closing a valve of the injector, is contained in the injector, the temperature of the injector itself increases, and this also constitutes one of the reasons for the rise in temperature of the fuel.
- When fuel temperature increases excessively, variation occurs in the movements of the electromagnetic valve in the injector, and it is conceivable that proper fuel injection by the injector becomes difficult.
- In order to prevent the fuel temperature rise in the circulating fuel supply apparatus in the prior art, as shown in FIG. 6, the
vapor separator 50 is provided in thereturn pipe 19 of an outboard engine for cooling the fuel, whereby thevapor separator 50 works to remove a vaporized component of a return fuel and to cool the fuel. Thevapor separator 50 can be provided only in thereturn pipe 19 which is low pressure due to the structure thereof. The related art is disclosed in Japanese KOUKAI Patent No. SHO60-104760. - In a circulating fuel supply apparatus in which the
vapor separator 50 is provided in thereturn pipe 19, as shown in FIG. 6, the cooling effect for the fuel supplied to theinjectors 14 is low, as will be described in the following: - (1) The quantity of the fuel returning from the
return pipe 19 to thefuel tank 6 is small as compared with an absolute quantity of the fuel in thefuel tank 6. Therefore, even when the small quantity of the return fuel is cooled by thevapor separator 50, it can not sufficiently reduce the temperature of the fuel in the fuel tank. Consequently, it is difficult to sufficiently cool the fuel supplied to theinjectors 14. - (2) A vaporized component is mixed in large quantities in the return fuel. Therefore, even when the fuel is cooled as a gas-liquid separation operation is carried out in the
vapor separator 50, the cooling of the fuel is difficult as compared with that of the liquid component alone. - The invention has been made in view of the above circumstances, and provides a circulating fuel supply apparatus for a engine of a small watercraft, having a cooling device with a simple structure, and adapted to cool the fuel in the apparatus efficiently and supply the resultant fuel to an injector so as to repress, or minimize, vaporization of the fuel. Thus, cooling of the injector is done with a high reliability, and injection of the fuel by the injector is done properly.
- The invention provides a circulating fuel supply apparatus for an engine of a small watercraft, which is adapted to supply a fuel in a fuel tank to an injector via a fuel supply pipe by means of a fuel pump. The fuel supply apparatus returns excess fuel from the injector to the fuel tank via a fuel return pipe and has a fuel cooling device in the portion of the fuel supply pipe which is between the fuel pump and the injector.
- With such an apparatus, the fuel drawn from the fuel tank and about to enter the injectors is cooled by the fuel cooling device. This enables the fuel to be cooled and then supplied to the injectors efficiently as compared with a case where the return fuel is cooled. As a result, injection of the fuel is done properly by the injectors.
- Preferably, the circulating fuel supply apparatus for the engine of the small watercraft has a heat exchanger that uses a cooling water as the fuel cooling device. This enables the fuel cooling device to be simplified, and the manufacturing costs to be reduced.
- Preferably, the heat exchanger uses, as cooling water, an exchanger external cooling water taken in from the outside by a water jet propulsion unit of the watercraft, and the external cooling water which has been used to cool the fuel is discharged to the outside of the watercraft. Such enables maintenance of the cooling water to be done simply, the running costs to be reduced, and the fuel cooling effect to be increased as compared with a similar apparatus in which the internal cooling water is circulated in a closed circuit.
- These objectives as well as other features and advantages of the invention will become more apparent to those skilled in the art from the following description with reference to the accompanying drawings.
- FIG. 1 is a side view of a small watercraft to which the invention is applied;
- FIG. 2 is a schematic piping diagram of a circulating fuel supply apparatus shown in FIG. 1;
- FIG. 3 is an enlarged longitudinal section of a heat exchanger shown in FIG. 2;
- FIG. 4 is a longitudinal sectional view showing a modified example of the heat exchanger;
- FIG. 5 is a longitudinal sectional view showing another modified example of the heat exchanger; and
- FIG. 6 is a schematic piping diagram showing an example of a related art circulating fuel supply apparatus.
- FIG. 1 is a schematic side view showing the interior of a small watercraft to which the invention is applied. First, the general structure of the small watercraft will be described. The body of the small watercraft is formed of a hull1 and a deck 2 is disposed thereon. A
straddle type seat 3 and ahandle 4 are provided on an upper side of the deck 2. In a rear portion of the hull 1, a waterjet propulsion unit 8, including a duct 9, guide blades (flow setting plates) 40, an ejection, or jet, nozzle 5, and an impeller 7 are provided. Fixed to the rear of the ejection nozzle 5 is a laterallycontrollable steering nozzle 13. The impeller 7 is housed in the duct 9 and connected to an output shaft of anengine 11 via an impeller (driving)shaft 10. A rear end portion of theimpeller shaft 10 is supported rotatably in abearing case 40 a retained by theguide blades 40. In accordance with a rotation of the impeller 7, water is sucked from awater intake port 12 in a bottom wall of the hull 1 into the duct 9, and ejected from a rearend discharge port 13 a of thesteering nozzle 13 via theguide blades 40, and a jet nozzle 5. Anengine 11 is a direct injection type 3-cylinder 2-cycle engine, disposed in the engine compartment provided below theseat 3, and having aninjector 14 in eachcylinder head 20. Afuel tank 6 is provided ahead of the engine in the hull. - A circulating fuel supply apparatus will now be described. A basic structure of the apparatus is similar to that of the above described related art shown in FIG. 6. As shown in FIG. 2, an
inlet port 14 a of eachinjector 14 is connected to thefuel tank 6 via afuel supply pipe 17 and afuel pump 18, and an excessfuel return port 14 b of theinjector 14 is connected to thefuel tank 6 via areturn pipe 19. Namely, the fuel is sucked from thefuel tank 6 by thefuel pump 18, then pressurized, and supplied to eachinjector 14 via thefuel supply pipe 17 by thefuel pump 18. Excess fuel in theinjectors 14 is returned to thefuel tank 6 via thereturn pipe 19. Although FIG. 2 shows threeinjectors 14 in a left portion thereof, in addition to the threeinjectors 14 drawn on the upper side of theengine 11, they are one and the same threeinjectors 14. Theinjectors 14, shown in the left portion of the drawing, are drawn between thefuel supply pipe 17 andreturn pipe 19 for the purpose of more clearly showing the fuel circulating path. - The above described circulating fuel supply apparatus has a
heat exchanger 21 for cooling the fuel. Theheat exchanger 21 is provided in the portion of thefuel supply pipe 17 which is between thefuel pump 18 and theinjectors 14. - The path of the cooling water used for the
heat exchanger 21 will now be described. As shown in FIG. 1, a coolingwater intake port 23 is opened in the portion of the interior of the waterjet propulsion unit 8 which corresponds to theguide blades 40. The coolingwater intake port 23 is connected to a coolingwater inlet port 31 of theheat exchanger 21 via a coolingwater pipe 24. A coolingwater outlet port 32 of theheat exchanger 21 is connected to a cooling water jacket inlet port 15 a of ainlet manifold 15 of theengine 11 via a coolingwater pipe 25, and a cooling water jacket in theinlet manifold 15 communicates with water jackets incylinders 16 andcylinder heads 20 of theengine 11. A coolingwater discharge pipe 26 is connected to a coolingwaterjacket outlet port 20 a of the cylinder heads 20. The coolingwater discharge pipe 26 is adapted to discharge used cooling water to the outside of the small watercraft. - FIG. 3 shows a preferred embodiment of the
heat exchanger 21. Theheat exchanger 21 is formed of anouter case 30 of aluminum for the cooling water, and aninner pipe 27 of stainless steel for the fuel which is disposed coaxially in and extends through theouter case 30. Theinner pipe 27 for the fuel is connected at both ends of the case to thefuel supply pipe 17. The coolingwater inlet port 31 is provided at a lower end of a fuel downstream side portion of theouter case 30 with respect to a flow of the fuel (direction of an arrow A), and the coolingwater outlet port 32 is provided at an upper end of a fuel upstream side portion of theouter case 30. - As shown in FIG. 2, the fuel in the
fuel tank 6 is sucked, pressurized, and sent under pressure into thefuel supply pipe 17 by thefuel pump 18, passed through theheat exchanger 21 in which the fuel is cooled with the cooling water, and then sent under pressure into theinjectors 14 from which a part of fuel is injected into combustion chambers of the engine (not shown). In this structure, the fuel in theheat exchanger 21 hardly includes vaporized fuel. Therefore, the fuel cooling effect is higher than as compared with that in a case where the return fuel is cooled. - The quantity of the fuel injected by the
injectors 14 into the combustion chambers in this embodiment is substantially not larger than a half of that discharged from thefuel pump 18. The excess fuel is returned to thefuel tank 6 through thereturn pipe 19. - The cooling water (external cooling water) is taken in from the outside through the cooling
water intake port 23 by the waterjet propulsion unit 8, enters theouter case 30 of theheat exchanger 21, of FIG. 3, via the coolingwater pipe 24, and cools the fuel from an outer circumference of theinner pipe 27. After the cooling water is used for the fuel cooling operation, it is supplied from the coolingwater outlet port 32 of the outer case to theinlet manifold 15, shown in FIG. 2, through the coolingwater pipe 25, and then to the interior of theengine 11, whereby theinlet manifold 15,cylinder heads 20 andcylinder 16 of theengine 11 are cooled. The cooling water with which theengine 11 has been cooled is discharged to the exterior of the boat through thedischarge pipe 26. - Because a one-way system that always uses fresh external cooling water is employed, the fuel cooling effect is large and the apparatus can be formed simply as compared with the effects obtained in a system in which an internal cooling water is circulated in a closed circuit.
- FIG. 4 shows a modified embodiment of the
heat exchanger 21, in which aninner pipe 27 for fuel is formed spirally. Thus, the contact area (length) of theinner pipe 27 with respect to the cooling water is increased. The structure of the other parts is identical with that of the corresponding parts of the heat exchanger of FIG. 3. - FIG. 5 also shows a modified embodiment of the
heat exchanger 21, in which aninner pipe 27 for the fuel is formed in the shape of the letter “U” (the inner pipe U-type so as to have forwardly and backwardly extending portions), whereby the cooling water contact area of theinner pipe 27 is increased. In this case, the inlet and outlet side portions of theinner pipe 27 extend through the same side end wall of theouter case 30. The structure of the remaining parts is identical with that of the corresponding parts of the heat exchanger of FIG. 3. - Numerous modifications and alternative embodiments of the invention will be apparent to those skilled in the art in view of the foregoing description. Accordingly, the description is to be construed as illustrative only, and is provided for the purpose of teaching those skilled in the art the best mode for carrying out the invention. The details of the structure and/or function may be varied substantially without departing from the spirit of the invention and all modifications which come within the scope of the appended claims are reserved.
Claims (11)
1. A circulating fuel supply apparatus for an engine of a small watercraft, adapted to supply a fuel in a fuel tank to an injector through a fuel supply pipe using a fuel pump, and returning excess fuel in the injector to the fuel tank through a fuel return pipe, comprising a fuel cooling device provided in the portion of the fuel supply pipe which is between the fuel pump and the injector.
2. The circulating fuel supply apparatus for the engine of the small watercraft according to , wherein a heat exchanger using a cooling water is provided as the fuel cooling device.
claim 1
3. The circulating fuel supply apparatus for the engine of the small watercraft according to , wherein an external cooling water, taken in from outside by a water jet propulsion unit provided in a hull of the small watercraft, is used as a cooling water for the heat exchanger and the cooling water which has been used to cool the fuel is discharged to the outside of the small watercraft.
claim 2
4. A fuel coolant system used with a circulating fuel supply for a fuel injection engine having a fuel tank, a fuel supply pipe with a fuel pump, a plurality of fuel injectors and a return pipe to the fuel tank, the fuel coolant system comprising:
a coolant intake;
a heat exchanger surrounding the fuel supply pipe and receiving coolant from the coolant intake; and
a coolant exhaust for exhausting coolant that has passed through the heat exchanger, the heat exchanger positioned on the fuel supply pipe between the fuel pump and the plurality of fuel injectors.
5. The fuel coolant system according to , wherein the fuel coolant system is used in a personal water craft (PWC) and the coolant is water taken from a body of water on which the PWC is operating.
claim 4
6. The fuel coolant system according to , wherein the coolant intake is a through hull intake in the PWC.
claim 5
7. The fuel coolant system according to , wherein the coolant exhaust is an exhaust port from the PWC.
claim 5
8. The fuel coolant system according to , wherein the coolant intake is a shared intake with a propulsion system of the PWC.
claim 6
9. The fuel coolant system according to , wherein coolant exiting the heat exchanger is passed through a cooling water jacket of an engine of the PWC before exiting the exhaust port.
claim 7
10. The fuel coolant system according to , wherein a portion of the fuel supply pipe passing through the heat exchanger has a coil shape.
claim 4
11. The fuel coolant system according to , wherein a portion of the fuel supply pipe passing through the heat exchanger has a U-shape.
claim 4
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2000-008853 | 2000-01-18 | ||
JP2000008853A JP2001200772A (en) | 2000-01-18 | 2000-01-18 | Circulating type fuel supplying device of engine for small planing boat |
Publications (2)
Publication Number | Publication Date |
---|---|
US20010008820A1 true US20010008820A1 (en) | 2001-07-19 |
US6454621B2 US6454621B2 (en) | 2002-09-24 |
Family
ID=18537071
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/759,147 Expired - Lifetime US6454621B2 (en) | 2000-01-18 | 2001-01-16 | Fuel cooling system for small watercraft engine |
Country Status (2)
Country | Link |
---|---|
US (1) | US6454621B2 (en) |
JP (1) | JP2001200772A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2863315A1 (en) * | 2003-12-05 | 2005-06-10 | Renault Sas | Fuel injection device for use in internal combustion engine of motor vehicle, has chiller heat exchanger inserted between fuel tank and injectors in direction of circulation of fuel from injectors |
US20060105645A1 (en) * | 2004-10-25 | 2006-05-18 | Sword Marine Technology Llc | Outboard jet drive marine propulsion system with increased horsepower |
DK201670613A1 (en) * | 2016-08-11 | 2018-02-26 | Maersk As | A fuel system for a marine engine |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6840829B2 (en) * | 2002-08-30 | 2005-01-11 | Kawasaki Jukogyo Kabushiki Kaisha | Jet-propulsion watercraft |
JP2004197692A (en) * | 2002-12-20 | 2004-07-15 | Kawasaki Heavy Ind Ltd | Small planing boat |
US7220154B2 (en) * | 2003-11-13 | 2007-05-22 | Sword Marine Technology, Inc. | Outboard jet drive marine propulsion system |
KR20070073603A (en) * | 2004-05-25 | 2007-07-10 | 스워드 마린 테크놀로지, 인코포레이티드 | Outboard jet drive marine propulsion system and control lever therefor |
US20090318039A1 (en) * | 2008-06-23 | 2009-12-24 | Hays Kevin P | Boat engine cooling system |
US8869756B2 (en) * | 2008-12-10 | 2014-10-28 | Ford Global Technologies, Llc | Cooling system and method for a vehicle engine |
DE102010031486A1 (en) * | 2010-07-16 | 2012-01-19 | Robert Bosch Gmbh | Test bench for fluid pumps and fluid injectors |
US8725328B1 (en) * | 2012-10-18 | 2014-05-13 | Brunswick Corporation | Methods and systems for monitoring marine engine cooling water pumps |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS60104760A (en) | 1983-11-10 | 1985-06-10 | Nissan Motor Co Ltd | Fuel circulation device for diesel engine car |
US4768492A (en) * | 1987-01-09 | 1988-09-06 | Brunswick Corporation | Marine propulsion system with fuel line cooler |
US4768983A (en) * | 1987-03-03 | 1988-09-06 | Smith Allen J | Power drive assembly for outboard engines |
JPH10246162A (en) * | 1997-03-03 | 1998-09-14 | Sanshin Ind Co Ltd | Fuel supply device for cylinder fuel injection engine |
-
2000
- 2000-01-18 JP JP2000008853A patent/JP2001200772A/en active Pending
-
2001
- 2001-01-16 US US09/759,147 patent/US6454621B2/en not_active Expired - Lifetime
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2863315A1 (en) * | 2003-12-05 | 2005-06-10 | Renault Sas | Fuel injection device for use in internal combustion engine of motor vehicle, has chiller heat exchanger inserted between fuel tank and injectors in direction of circulation of fuel from injectors |
US20060105645A1 (en) * | 2004-10-25 | 2006-05-18 | Sword Marine Technology Llc | Outboard jet drive marine propulsion system with increased horsepower |
WO2006047585A3 (en) * | 2004-10-25 | 2007-02-08 | Sword Marine Technology Llc | Outboard jet drive marine propulsion system with increased horsepower |
EP1814781A2 (en) * | 2004-10-25 | 2007-08-08 | Sword Marine Technology, LLC | Outboard jet drive marine propulsion system with increased horsepower |
EP1814781A4 (en) * | 2004-10-25 | 2009-03-25 | Sword Marine Technology Llc | Outboard jet drive marine propulsion system with increased horsepower |
DK201670613A1 (en) * | 2016-08-11 | 2018-02-26 | Maersk As | A fuel system for a marine engine |
DK179250B1 (en) * | 2016-08-11 | 2018-03-05 | Maersk As | A fuel system for a marine engine |
Also Published As
Publication number | Publication date |
---|---|
JP2001200772A (en) | 2001-07-27 |
US6454621B2 (en) | 2002-09-24 |
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