WO2015029390A1 - 燃料ポンプ及びその制御方法 - Google Patents
燃料ポンプ及びその制御方法 Download PDFInfo
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- WO2015029390A1 WO2015029390A1 PCT/JP2014/004291 JP2014004291W WO2015029390A1 WO 2015029390 A1 WO2015029390 A1 WO 2015029390A1 JP 2014004291 W JP2014004291 W JP 2014004291W WO 2015029390 A1 WO2015029390 A1 WO 2015029390A1
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- WIPO (PCT)
- Prior art keywords
- fuel
- flow path
- vapor
- impeller
- fuel pump
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- 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
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/04—Feeding by means of driven pumps
- F02M37/08—Feeding by means of driven pumps electrically driven
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D33/00—Controlling delivery of fuel or combustion-air, not otherwise provided for
- F02D33/003—Controlling the feeding of liquid fuel from storage containers to carburettors or fuel-injection apparatus ; Failure or leakage prevention; Diagnosis or detection of failure; Arrangement of sensors in the fuel system; Electric wiring; Electrostatic discharge
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/0025—Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/3082—Control of electrical fuel pumps
-
- 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
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/04—Feeding by means of driven pumps
- F02M37/08—Feeding by means of driven pumps electrically driven
- F02M37/10—Feeding by means of driven pumps electrically driven submerged in fuel, e.g. in reservoir
-
- 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
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/20—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines characterised by means for preventing vapour lock
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D13/00—Pumping installations or systems
- F04D13/02—Units comprising pumps and their driving means
- F04D13/06—Units comprising pumps and their driving means the pump being electrically driven
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D15/00—Control, e.g. regulation, of pumps, pumping installations or systems
- F04D15/0066—Control, e.g. regulation, of pumps, pumping installations or systems by changing the speed, e.g. of the driving engine
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/18—Rotors
- F04D29/181—Axial flow rotors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/528—Casings; Connections of working fluid for axial pumps especially adapted for liquid pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D3/00—Axial-flow pumps
- F04D3/005—Axial-flow pumps with a conventional single stage rotor
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2200/00—Input parameters for engine control
- F02D2200/02—Input parameters for engine control the parameters being related to the engine
- F02D2200/06—Fuel or fuel supply system parameters
- F02D2200/0602—Fuel pressure
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2250/00—Engine control related to specific problems or objectives
- F02D2250/02—Fuel evaporation in fuel rails, e.g. in common rails
-
- 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
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/04—Feeding by means of driven pumps
- F02M37/08—Feeding by means of driven pumps electrically driven
- F02M2037/085—Electric circuits therefor
Definitions
- the present disclosure relates to a fuel pump that supplies fuel in a fuel tank of a vehicle to an internal combustion engine and a control method thereof.
- a vehicle is used in an environment of high temperature and low pressure, and a fuel having a high vapor pressure such as an alcohol-mixed fuel is used, so that vapor is contained in the fuel supplied from the fuel tank to the internal combustion engine. It may be prone to occur. In this case, the vapor corresponds to bubbles.
- Patent Document 1 when vapor is generated in the fuel flowing through the fuel pipe connecting the fuel pump and the internal combustion engine, vapor lock occurs in the fuel pipe by setting the target fuel pressure of the fuel discharged from the fuel pump high. Techniques to prevent this are described.
- variable fuel pressure system that pumps fuel from the fuel pump to the internal combustion engine according to the fuel pressure and flow rate required by the internal combustion engine has been adopted as a control system for the fuel supply system.
- a fuel pump used in this system is required to have a stable discharge at a low flow rate.
- the fuel pump may be vapor locked and fuel may not be discharged.
- the present disclosure has been made in view of the above matters, and an object thereof is to provide a fuel pump capable of preventing vapor lock in a pump chamber that boosts fuel.
- the rotation speed of the impeller is set higher than the rotation speed of the normal control for a predetermined time. As a result, the vapor in the pump chamber is discharged into the vapor discharge hole.
- the control of the fuel pump is switched from the normal control to the control of discharging the vapor to the vapor discharge hole. Therefore, the vapor in the pump chamber is reliably discharged from the vapor discharge hole to the outside of the fuel pump. Therefore, the fuel pump can discharge the required flow rate without vapor locking.
- the rotational speed of the impeller is set higher than the rotational speed corresponding to the target fuel pressure at normal time for a predetermined time. Then, the vapor in the pump chamber and the fuel flow path is discharged to the vapor discharge hole.
- FIG. 1 is a configuration diagram of a fuel supply system in which a fuel pump according to a first embodiment of the present disclosure is used
- FIG. 2 is a cross-sectional view of the fuel pump according to the first embodiment.
- FIG. 3 is a diagram showing only the lower casing along the line III-III in FIG. 4 is a cross-sectional view taken along line IV-IV in FIG.
- FIG. 5 is an enlarged view of a portion V in FIG.
- FIG. 6 is a characteristic diagram of the shape of the first flow path of the vapor discharge hole and the vapor discharge ratio.
- FIG. 7 is a diagram showing the fuel flow in the vapor discharge hole of the comparative example
- FIG. 8 is an analysis diagram showing the fuel flow in the vapor discharge hole of the first embodiment.
- FIG. 9 is a flowchart of control of the fuel pump according to the first embodiment.
- FIG. 10 is a configuration diagram of an evaluation test of the fuel pump according to the first embodiment.
- FIG. 11 is a diagram showing test data based on the evaluation test of FIG.
- FIG. 12 is a diagram showing test data when the control of FIG. 9 is performed in the evaluation test of FIG.
- FIG. 13 is a diagram showing test data when the rate of increase of the impeller rotation speed at the time of vapor generation is changed, FIG.
- FIG. 14 is a characteristic diagram of the rate of increase of the impeller rotation speed and the rate of decrease in flow rate when vapor is generated
- FIG. 15 is a characteristic diagram of the negative pressure limit and the flow rate in the fuel pump of the first embodiment and the conventional fuel pump
- FIG. 16 is an enlarged view of the vapor discharge hole of the fuel pump according to the second embodiment
- FIG. 17 is an enlarged view of the vapor discharge hole of the fuel pump according to the third embodiment.
- FIGS. A first embodiment of the present disclosure is shown in FIGS.
- the fuel pump 1 of the present embodiment is used in a fuel supply system by a variable fuel pressure system, and pumps fuel in a fuel tank 2 to an internal combustion engine (ICE) 4 through a fuel pipe 3.
- ICE internal combustion engine
- an electronic control unit (ECU) 5 of the vehicle detects the number of revolutions of the impeller corresponding to the fuel pressure and flow rate required by the internal combustion engine 4, and the command value is detected by the fuel pump 1.
- the controller (FPC) 6 supplies a three-phase alternating current corresponding to the command value of the ECU 5 to the motor of the fuel pump 1.
- the pressure of the fuel discharged from the fuel pump 1 to the fuel pipe 3 is detected by a pressure sensor (P) 7, and the signal is transmitted to the ECU 5.
- the fuel pressure is also referred to as fuel pressure.
- the ECU 5 performs feedback control of the fuel pump 1 via the FPC 6 so that the fuel pressure detected by the pressure sensor 7 matches the target fuel pressure.
- the ECU 5 of the present embodiment performs control for discharging the vapor to the vapor discharge hole by predetermined feedforward control. Do. In this case, the vapor corresponds to bubbles.
- the fuel pump 1 includes a pump unit 10, a motor unit 30, a housing 39, a motor cover 40, and the like.
- the fuel pump 1 sucks fuel from the suction port 12 shown in the lower part of FIG. 2 by the rotation of the impeller 11 provided in the pump unit 10, boosts the fuel, and discharges it from the fuel discharge pipe 41 shown in the upper part of FIG. To do.
- the pump unit 10 includes an impeller 11, an upper casing 13, a lower casing 14, and the like.
- the upper casing 13 and the lower casing 14 correspond to casings.
- the impeller 11 is formed in a disk shape and has a plurality of blade grooves 15 arranged in the circumferential direction.
- the impeller 11 is fixed to the shaft 31 of the motor unit 30 and rotates together with the shaft 31.
- a pump chamber 16 is formed between the upper casing 13 and the lower casing 14 to accommodate the impeller 11 in a rotatable manner.
- the lower casing 14 has an inlet 12 for introducing fuel into the pump chamber 16 from the outside of the fuel pump 1.
- the lower casing 14 has the suction port 12 for introducing fuel into the pump chamber 16 from the outside of the lower casing 14.
- the upper casing 13 has a discharge port 17 through which fuel is discharged from the pump chamber 16 to the motor unit 30.
- the upper casing 13 has a discharge port 17 that discharges fuel from the pump chamber 16 to the outside of the upper casing 13.
- the lower casing 14 has a lower fuel passage 18 formed in an annular shape corresponding to the blade groove 15 of the impeller 11 from the inlet 12 to the outlet 17.
- the lower fuel flow path 18 is formed in a substantially C shape.
- the lower casing 14 also has a vapor discharge hole 20 through which the vapor contained therein can be discharged from the pump chamber 16 and the lower fuel flow path 18 to the outside of the fuel pump 1 together with fuel.
- the upper casing 13 similarly to the lower casing 14, the upper casing 13 also has an upper fuel passage 19 formed in an annular shape corresponding to the blade groove 15 of the impeller 11 from the inlet 12 to the outlet 17. Have.
- the motor unit 30 is a brushless motor and includes a stator 32, a rotor 36, a shaft 31, and the like.
- the stator 32 has a cylindrical shape and includes a stator core 33, an insulator 34, and a winding 35.
- the stator core 33 is made of a magnetic material such as iron.
- the insulator 34 resin-molds the stator core 33.
- Winding 35 is wound around insulator 34 to form a three-phase winding.
- the insulator 34 around which the winding 35 is wound is further integrally resin-molded by the motor cover 40. Therefore, the stator 32 is formed integrally with the motor cover 40.
- the rotor 36 is rotatably accommodated inside the stator 32.
- a magnet 38 is fixed around the iron core 37.
- the magnet 38 has N and S poles alternately arranged in the circumferential direction.
- the shaft 31 is press-fitted and fixed at the center of the rotor 36 and rotates together with the rotor 36.
- the shaft 31 has a first end rotatably supported by a first bearing 42 provided on the motor cover 40 and a second end rotatably supported by a second bearing 43 provided on the upper casing 13.
- the housing 39 is formed in a cylindrical shape, and the first end portion in the axial direction is caulked in the radially inward direction, and the motor cover 40 and the motor portion 30 are fixed.
- the housing 39 has two axial ends that are caulked radially inward to fix the lower casing 14 and the upper casing 13.
- the motor cover 40 has a fuel discharge pipe 41 protruding upward in FIG.
- the fuel boosted by the pump unit 10 passes through the gap between the stator 32 and the rotor 36 of the motor unit 30 and is discharged from the fuel discharge pipe 41.
- the vapor discharge hole 20 has an angle ⁇ a in the range of about 110 ° to 130 ° when the position of the suction port 12 is 0 °. Vapor may be generated in the fuel sucked into the pump chamber 16 from the suction port 12 due to the suction negative pressure. The vapor discharge hole 20 discharges vapor generated in the vicinity of the suction port 12 to the outside of the fuel pump 1.
- the fuel introduced into the lower fuel flow path 18 and the pump chamber 16 by the negative pressure from the suction port 12 is gradually increased in pressure and reaches several tens of kPa in the vicinity of the vapor discharge hole 20. Therefore, the fuel in the lower fuel flow path 18 is discharged from the vapor discharge hole 20 to the outside of the fuel pump 1.
- the lower fuel flow path 18 has an outer curved surface portion 181, a flat surface portion 182, and an inner curved surface portion 183 from the radially outer side toward the radially inner side.
- the outer curved surface portion 181 is a part of the surface portion of the lower fuel flow path 18 whose depth gradually increases from the outside diameter toward the inside diameter.
- the flat portion 182 is a part of the surface portion of the lower fuel flow path 18 having a constant depth.
- the inner curved surface portion 183 is a part of the surface portion of the lower fuel flow path 18 whose depth gradually decreases from the flat surface portion 182 toward the inside of the diameter.
- the vapor discharge hole 20 is connected to the inner curved surface portion 183 of the lower fuel flow path 18.
- the centrifugal force generated by the rotation of the impeller 11 acts on the fuel flowing through the lower fuel flow path 18, the pressure of the fuel flowing radially outside the lower fuel flow path 18 is high. Since the vapor contained in the fuel has a smaller mass than the fuel, it flows inside the lower fuel flow path 18 in the radial direction. Therefore, by connecting the vapor discharge hole 20 to the inner curved surface portion 183 of the lower fuel flow path 18, it is possible to reliably introduce the vapor flowing through the lower fuel flow path 18 into the vapor discharge hole 20.
- the vapor discharge hole 20 includes a first flow path 21, a second flow path 22, a third flow path 23, and a tapered portion 24. These are all formed coaxially.
- the first flow path 21 is connected to the inner curved surface portion 183 of the lower fuel flow path 18 and communicates with the lower fuel flow path 18.
- the first flow path 21 prevents the fuel from leaving the inner wall of the vapor discharge hole 20 when the fuel flows into the vapor discharge hole 20 from the lower fuel flow path 18.
- the second flow path 22 has a smaller inner diameter than the first flow path 21 and communicates with the anti-fuel flow path side of the first flow path 21.
- the flow rate of the fuel flowing through the vapor discharge hole 20 is adjusted by setting the inner diameter and length of the second flow path 22.
- the taper portion 24 is provided at a connection location between the first flow path 21 and the second flow path 22, and prevents the vortex from being generated in the fuel flowing through the step between the first flow path 21 and the second flow path 22.
- the taper portion 24 is provided in an annular shape on the outer side of the step provided between the first flow path 21 and the second flow path 22.
- the taper portion 24 is formed with an inner angle ⁇ b of 120 ° or less. This is because if the inner angle is larger than 120 °, a vortex is likely to occur in the fuel flowing there.
- the third flow path 23 has a larger inner diameter than the second flow path 22 and communicates with the second flow path 22 on the side opposite to the first flow path.
- the third flow path 23 adjusts the length of the second flow path 22.
- the inner wall of the third flow path 23 is substantially parallel to the inner wall of the second flow path 22.
- the inner diameter d1 on the second flow path side of the third flow path 23 is slightly smaller than the inner diameter d2 on the anti-second flow path side. That is, when the lower casing 14 is formed, the inner wall of the third flow path 23 has a taper that is about the draft for extracting the mold that forms the third flow path 23 from the material constituting the lower casing 14. Thereby, the workability of the third flow path 23 can be improved. Further, when the vapor discharge hole 20 is formed, it is possible to easily remove burrs generated at the connection portion between the second flow path 22 and the third flow path 23.
- the distance from the connection position of the lower fuel flow path 18 and the first flow path 21 to the connection position of the first flow path 21 and the second flow path 22 is L, and the first flow path 21 Let d be the inner diameter. At this time, the distance is also referred to as the length of the first flow path 21.
- the relationship between the length L of the first flow path 21 and its inner diameter d is preferably 2 ⁇ d / L ⁇ 5.
- FIG. 6 shows the relationship between d / L and the vapor discharge amount ratio when the impeller rotational speed, which is the rotational speed of the impeller 11, is changed from 3000 rpm to 10000 rpm, which is typical for the fuel pump 1.
- the vapor discharge ratio is 96.5% or more in the range of 1 ⁇ d / L ⁇ 6. Further, the vapor discharge ratio is 99% or more in the range of 2 ⁇ d / L ⁇ 5.
- the shape of the vapor discharge hole 20 can be adjusted to the angle of the fuel flowing from the first flow path 21 to the second flow path 22. It is possible to match. Thereby, the vapor
- the second flow path 220 is directly connected to the lower fuel flow path 18 and does not have the first flow path 21 and the taper portion 24.
- the taper angle of the third flow path 230 of the comparative example is formed larger than the taper angle of the third flow path 23 of the first embodiment.
- the fuel flowing into the vapor discharge hole from the lower fuel flow path 18 flows away from the inner wall on the upstream side of the vapor discharge hole 200 as indicated by an arrow A. Therefore, in the vicinity of the inner wall on the upstream side of the vapor discharge hole 200, as shown by the broken line B, a vortex is generated and the fuel pressure is reduced. Therefore, when vapor is generated from the vortex, the amount of vapor discharged from the lower fuel flow path 18 is reduced by the volume of the vapor.
- the fuel flows only in a part of the third flow path 230.
- a flow for drawing fuel from the outside of the third flow path 230 is generated.
- the vapor discharge hole 200 of the comparative example has a small amount of vapor discharged from the lower fuel flow path 18.
- the fuel flowing from the lower fuel flow path 18 into the vapor discharge hole 20 is the first flow path 21, the taper portion 24, and the second flow path. It flows along the inner wall without leaving the inner wall on the upstream side of 22. Therefore, no vortex flow is generated in the vicinity of the inner wall on the upstream side of the vapor discharge hole 20, so that the amount of vapor discharged from the lower fuel flow path 18 is increased as compared with the vapor discharge hole 200 of the comparative example.
- the third flow path 23 of the vapor discharge hole 20 of the first embodiment allows the fuel flow from the second flow path 22 to flow without drawing fuel from the outside of the third flow path 23. It is possible to discharge the fuel pump 1 to the outside. Therefore, the vapor discharge hole 20 of the first embodiment can increase the amount of vapor discharged from the lower fuel flow path 18 compared to the vapor discharge hole 200 of the comparative example.
- the control of the fuel pump 1 is started when the engine is started.
- the ECU 5 determines the rotational speed of the motor unit 30 according to the target fuel pressure required by the internal combustion engine 4 and supplies power to the motor unit 30 of the fuel pump 1 via the FPC 6.
- the rotational speed of the motor unit 30 and the impeller rotational speed are the same.
- the ECU 5 detects the fuel pressure, which is the pressure of the fuel discharged from the fuel pump 1, based on the signal from the pressure sensor 7.
- the ECU 5 feedback-controls the rotational speed of the motor unit 30 of the fuel pump 1 by proportional-integral control (PI control) so that the target fuel pressure and the fuel pressure detected by the pressure sensor 7 coincide.
- PI control proportional-integral control
- the ECU 5 detects whether or not vapor is generated in the fuel in the pump chamber 16 of the fuel pump 1 based on the fuel pressure detected by the pressure sensor 7.
- vapor is generated by suction negative pressure in the vicinity of the suction port 12 and hinders fuel pressure increase. Therefore, it is possible to detect the occurrence of vapor based on a decrease in the fuel pressure discharged from the fuel pump 1.
- ECU5 judges that the vapor
- the predetermined threshold is set to 10 kPa, for example.
- the ECU 5 determines that no vapor is generated in S3
- the ECU 5 returns to S1 and continues the feedback control.
- the ECU 5 determines that the vapor is generated in S3
- the ECU 5 proceeds to S4 and switches the control of the fuel pump 1 to the feedforward control in order to discharge the vapor in the pump chamber 16 to the vapor discharge hole 20.
- the ECU 5 increases the rate of increase in the rotation speed of the motor unit 30 and supplies power to the motor unit 30 via the FPC 6.
- the ECU 5 When a predetermined time has elapsed in S5, the ECU 5 returns to S1 again and performs feedback control.
- the pressure sensor 7 and the ECU 5 of the present embodiment function as a detection unit.
- FIG. 10 shows a configuration used in the evaluation test related to the control of the fuel pump 1 described above.
- the fuel discharged from the fuel pump 1 passes through a pressure regulator (P / R) 50, the flow rate of which is measured by a flow meter 51, and then increased to a predetermined temperature by a heat exchange pipe 53 in the heat exchanger 52, Returned to the fuel tank 2.
- the pressure in the fuel tank 2 is set to a predetermined pressure by a negative pressure suction machine (NPSM) 54.
- FIG. 11 is a diagram showing test data when the fuel pump 1 is driven using the configuration of FIG.
- the ECU 5 drives the fuel pump 1 so that the pressure of the fuel discharged from the fuel pump 1 is maintained at a predetermined pressure Px.
- each solid line G, H, I is test data when the fuel pump 1 is driven by conventional control.
- the conventional control means that the ECU 5 performs only the feedback control (S1) described above and does not perform the predetermined feedforward control (S4, S5) described above.
- a solid line G indicates the fuel pressure
- a solid line H indicates the impeller rotational speed
- a solid line I indicates the flow rate.
- the broken lines J, K, and L indicate that the ECU 5 performs both feedback control (S1) and predetermined feedforward control (S4, S5) as in the control of the present embodiment described in the flowchart of FIG. Target value.
- the broken line J indicates the fuel pressure
- the broken line K indicates the impeller rotational speed
- the broken line L indicates the flow rate.
- the rotational speed indicated by the solid line H is increased by feedback control of the ECU 5.
- the ECU 5 performs both feedback control (S1) and predetermined feedforward control (S4, S5) by the control of this embodiment. It is obtained when done.
- the solid line M indicates the fuel pressure
- the broken line N indicates the impeller rotational speed
- the alternate long and short dash line O indicates the flow rate
- the ECU 5 switches the control of the fuel pump 1 from the feedback control (S1) to the predetermined feedforward control (S4, S5) when the occurrence of vapor is detected at time tx. That is, as indicated by the broken line N, the ECU 5 increases the rotation speed rapidly by increasing the increase rate of the rotation speed only from the time tx to the time ty.
- the fuel pressure pulsates but maintains a value close to the target fuel pressure. Further, as indicated by the one-dot chain line O, the flow rate discharged from the fuel pump 1 is maintained.
- FIG. 13 shows test data when the rate of increase of the impeller rotation speed is changed when vapor is generated in the pump chamber 16.
- Fig. 13 (A) shows the change in the fuel pressure
- Fig. 13 (B) shows the change in the increase rate of the impeller rotation speed.
- the broken lines P and Q are test data when the ECU 5 performs conventional control.
- the ECU 5 sets the increase rate of the impeller rotation speed to 1000 rpm / s when the fuel pressure discharged from the fuel pump 1 is reduced by, for example, 10 kPa, which is a threshold for detecting vapor generation.
- 10 kPa which is a threshold for detecting vapor generation.
- the fuel pressure continues to decrease.
- the solid lines R and S, the two-dot chain lines T and U, and the one-dot chain lines V and W are all controlled by the ECU 5 in the feedback control (S1) and the feedforward control (S4, S5) as described in the flowchart of FIG. It is the test data when performing.
- the ECU 5 sets the rate of increase of the impeller rotation speed to 30000 rpm / s only for 0.1 second from time tx to ty. In this case, as indicated by the solid line S, the fuel pressure pulsates but maintains a value close to the target fuel pressure.
- time tx to ty for maintaining the rate of increase of the impeller rotational speed can be arbitrarily set by experiments or the like.
- ty is set to 0.1 seconds from time tx, but this time may be shorter or longer than 0.1 seconds depending on, for example, the physique of the fuel pump 1.
- the ECU 5 sets the rate of increase of the impeller rotational speed to 20000 rpm / s. In this case, as indicated by a two-dot chain line U, the fuel pressure gradually increases.
- the ECU 5 sets the rate of increase of the impeller rotational speed to 10,000 rpm / s. In this case, as indicated by the alternate long and short dash line W, the fuel pressure is lowered.
- FIG. 14 summarizes the test data shown in FIG.
- the rate of decrease in the flow rate discharged from the fuel pump 1 decreases when the rate of increase in the impeller rotational speed is set to 20000 rpm / s or more.
- the increase rate of the impeller rotational speed is 30000 rpm / s, the decrease rate of the flow rate discharged from the fuel pump 1 becomes zero.
- the increase rate of the impeller rotation speed of 20000 rpm / s is 20 times the increase rate of the impeller rotation speed of 1000 rpm / s by the feedback control. Therefore, when vapor is generated in the pump chamber 16, the rate of decrease in the flow rate discharged from the fuel pump 1 is reduced when the rate of increase in the impeller rotation rate is set to 20 times or more the rate of increase in the impeller rotation rate by feedback control.
- the solid line X in FIG. 15 is data indicating the relationship between the negative pressure limit and the flow rate when the ECU 5 drives the fuel pump 1 under the control of this embodiment.
- the solid line Y in FIG. 15 is data indicating the relationship between the negative pressure limit and the flow rate when the ECU 5 drives the fuel pump 1 by conventional control.
- the negative pressure limit Pe of the flow rate Lc in the solid line X was 4 kPa or more lower than the negative pressure limit Pb of the flow rate Lc in the solid line Y. Therefore, the fuel pump 1 by the control of the present embodiment shown by the solid line X can lower the negative pressure limit by 4 kPa or more at the predetermined flow rate Lc compared to the fuel pump 1 by the conventional control shown by the solid line Y. That is, the fuel pump 1 according to the control of the present embodiment can reduce the flow rate under low pressure conditions.
- the fuel pump 1 of the present embodiment has the following operational effects.
- the control of the fuel pump 1 is switched from the normal feedback control to the feed forward control for discharging the vapor to the vapor discharge 20 hole. Therefore, the vapor in the pump chamber 16 is reliably discharged from the vapor discharge hole 20 to the outside of the fuel pump 1. Therefore, the fuel pump 1 can discharge the requested flow rate without vapor locking.
- the rate of increase of the impeller rotational speed is set to 20000 rpm / s or more.
- the increase rate of the impeller rotation speed by feedforward control is 20 times the increase rate of the impeller rotation speed by feedback control according to the fuel pressure decrease. That's it.
- the fuel pump 1 discharges only the flow rate necessary for discharging the vapor, and the discharge of a larger flow rate than that is suppressed.
- the vapor in the pump chamber 16 can be reliably discharged.
- the feedforward control is performed only for a predetermined time and then switched to the feedback control.
- the fuel pump 1 discharges only the flow rate necessary for discharging the vapor, and the discharge of a larger flow rate than that is suppressed.
- the motor unit 30 of the fuel pump 1 is feedback-controlled at a rotational speed corresponding to the target pressure, so that the fuel pressure discharged by the fuel pump 1 during normal operation maintains the target pressure. Therefore, it is possible to estimate that vapor has occurred in the pump chamber 16 when the fuel pressure discharged from the fuel pump 1 has dropped from the target pressure by a predetermined pressure or more.
- the vapor discharge hole 20 has the first flow path 21 having an inner diameter larger than that of the second flow path 22 on the lower fuel flow path 18 side of the second flow path 22. Further, a tapered portion 24 is provided at a connection portion between the first flow path 21 and the second flow path 22.
- the fuel flowing through the lower fuel flow path 18 flows promptly along the inner walls of the first flow path 21, the tapered portion 24, and the second flow path 22 without leaving the inner wall on the upstream side of the vapor discharge hole 20. . Therefore, it is possible to flow the fuel through all the flow paths of the vapor discharge hole 20 without forming a swirl of fuel inside the inner wall of the first flow path 21. Therefore, the vapor in the lower fuel flow path 18 is reliably discharged from the vapor discharge hole 20, so that the vapor lock of the fuel pump 1 can be prevented.
- the first flow path 21, the second flow path 22 and the taper portion 24 are provided coaxially.
- the relationship between the length L of the first flow path 21 and the inner diameter d of the first flow path 21 is 2 ⁇ d / L ⁇ 5.
- the shape of the first flow path 21 can be adjusted to the angle of the fuel flowing from the lower fuel flow path 18 to the second flow path 22 through the first flow path 21. Is possible. Therefore, in the range of 2 ⁇ d / L ⁇ 5, the fuel that flows from the lower fuel flow path 18 to the vapor discharge hole 20 can be maximized.
- the vapor discharge hole 20 has a third flow path 23 having a larger inner diameter than the second flow path 22 on the side opposite to the first flow path of the second flow path 22.
- the inner wall of the third flow path 23 has a draft angle for extracting the mold forming the third flow path 23 from the material constituting the lower casing 14 when the lower casing 14 is formed. It has a taper.
- the workability of the third flow path 23 can be improved. Further, when the vapor discharge hole 20 is formed, it is possible to easily remove burrs generated at the connection portion between the second flow path 22 and the third flow path 23.
- the taper angle of the third flow path 23 it is possible to prevent the fuel from being drawn into the third flow path 23 from the outside of the lower casing 14. Therefore, the amount of vapor discharged from the vapor discharge hole 20 can be increased.
- the first flow path 21 of the vapor discharge hole 20 is connected to an inner curved surface portion 183 provided inside the lower fuel flow path 18.
- the centrifugal force due to the rotation of the impeller 11 acts on the fuel flowing through, the pressure of the fuel flowing in the radially outer side of the lower fuel flow path 18 is high. For this reason, the vapor contained in the fuel has a smaller mass than the fuel, and therefore flows inside the lower fuel flow path 18 in the radial direction. Therefore, by connecting the first flow path 21 of the vapor discharge hole 20 to the inner curved surface portion 183 of the lower fuel flow path 18, the vapor flowing through the lower fuel flow path 18 can be reliably introduced into the vapor discharge hole 20. .
- FIG. 1 An enlarged view of the fuel pump of the second embodiment is shown in FIG.
- substantially the same configurations as those in the first embodiment described above are denoted by the same reference numerals, and description thereof is omitted.
- the vapor discharge hole 20 is connected to the inner periphery of the tapered portion 25 on the inner diameter side and the inner periphery of the second flow path on the fuel flow path side. Therefore, in the second embodiment, there is no step between the first flow path 21 and the second flow path 22.
- the tapered portion 25 prevents vortexes from occurring in the fuel flowing from the first flow path 21 to the second flow path 22. Therefore, fuel can flow through all the flow paths of the vapor discharge hole 20, and the vapor of the lower fuel flow path 18 can be reliably discharged from the vapor discharge hole 20.
- FIG. 1 An enlarged view of the fuel pump of the third embodiment is shown in FIG.
- the tapered portion 26 of the vapor discharge hole 20 is connected to the lower fuel flow path 18.
- the third embodiment there is no step between the first flow path 21 and the second flow path 22, and a vortex may be generated in the fuel flowing from the first flow path 21 or the tapered portion 26 to the second flow path 22. It is prevented. Therefore, the vapor of the lower fuel flow path 18 can be reliably discharged from the vapor discharge hole 20.
- the fuel pump provided with the brushless motor has been described.
- the fuel pump may include a motor with a brush.
- the ECU detects whether or not vapor is generated based on the fuel pressure detected by the pressure sensor.
- the ECU may detect whether or not vapor is generated based on a change in flow rate, a relationship between fuel pressure and fuel temperature, a fluctuation rate of fuel pressure, and the like.
- the vapor discharge hole has the first flow path, the second flow path, the third flow path, and the tapered portion.
- the vapor discharge hole may have a configuration in which the second flow path directly opens on the outer wall of the lower casing 14 without having the third flow path.
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Abstract
Description
本開示の第1実施形態を図1から図15に示す。本実施形態の燃料ポンプ1は、可変燃圧システムによる燃料供給系統に用いられ、燃料タンク2の燃料を燃料配管3を通じて内燃機関(ICE)4に圧送するものである。
第2実施形態の燃料ポンプの拡大図を図16に示す。以下、複数の実施形態について、上述した第1実施形態と実質的に同一の構成には同一の符号を付して説明を省略する。
第3実施形態の燃料ポンプの拡大図を図17に示す。第3実施形態では、ベーパ排出孔20のテーパ部26は、下燃料流路18に接続している。
(1)上述した実施形態では、可変燃圧システムに用いられる燃料ポンプについて説明した。これに対し、他の実施形態では、燃料ポンプは、他の燃料供給システムに用いることも可能である。
Claims (14)
- 周方向に複数の羽根溝(15)を有するインペラ(11)と、
前記インペラを回転するモータ部(30)と、
前記インペラを回転可能に収容するポンプ室(16)を有するケーシング(13,14)と、
前記ケーシングの外側から前記ポンプ室に燃料を導入する吸入口(12)と、
前記ポンプ室から前記ケーシングの外側へ燃料を吐出する吐出口(17)と、
前記吸入口から前記吐出口に亘り、前記インペラの羽根溝に対応して前記ケーシングに環状に形成された燃料流路(18,19)と、
前記燃料流路から前記ケーシングの外側へベーパを排出可能なベーパ排出孔(20)と、
前記ポンプ室及び前記燃料流路にベーパが発生したことを検出する検出部(7,5)と、
前記検出部がベーパの発生を検出していないとき、前記モータ部を制御して前記インペラの回転数を目標燃圧に応じた回転数にする通常制御部(5,6)と、
前記検出部がベーパの発生を検出したとき、前記インペラの回転数を所定時間、前記通常制御部が定める目標回転数よりも高くすることにより、前記ポンプ室及び前記燃料流路のベーパを前記ベーパ排出孔へ排出するベーパ制御部(5,6)と、を備える燃料ポンプ(1)。 - 前記ベーパ制御部は、前記インペラの回転数の上昇率を20000rpm/s以上にする請求項1に記載の燃料ポンプ。
- 前記通常制御部は、前記インペラの回転数を目標燃圧に応じた回転数にフィードバック制御するものであり、
前記ベーパ制御部は、前記インペラの回転数の上昇率を、前記通常制御部が燃圧低下に応じて定める前記インペラの回転数の上昇率に対し、20倍以上にする請求項1に記載の燃料ポンプ。 - 前記ベーパ制御部は、前記検出部がベーパの発生を検出したとき、前記インペラの回転数をベーパ排出に必要な時間のみ制御する請求項1から3のいずれか一項に記載の燃料ポンプ。
- 前記検出部がベーパの発生を検出したとき、前記通常制御部が行う前記モータ部のフィードバック制御を、前記ベーパ制御部が行うフィードフォワード制御に切り替える請求項1から4のいずれか一項に記載の燃料ポンプ。
- 前記ベーパ制御部が前記フィードフォワード制御を所定時間行った後、前記通常制御部による前記フィードバック制御に切り替える請求項5に記載の燃料ポンプ。
- 前記検出部は、前記吐出口から吐出する燃料の圧力が目標圧から所定圧以上低下したとき、ベーパが発生したことを検出する請求項1から6のいずれか一項に記載の燃料ポンプ。
- 前記ベーパ排出孔は、
前記燃料流路に連通する第1流路(21)と、
その第1流路よりも内径が小さく形成され前記第1流路の反燃料流路側に連通する第2流路(22)と、
前記第1流路と前記第2流路との接続箇所に設けられたテーパ部(24,25,26)とを有する請求項1から7のいずれか一項に記載の燃料ポンプ。 - 前記第1流路と前記第2流路と前記テーパ部とは、同軸に設けられる請求項8に記載の燃料ポンプ。
- 前記燃料流路と前記第1流路との接続位置から前記第1流路と前記第2流路との接続位置までの距離をLとし、前記第1流路の内径をdとしたとき、2≦d/L≦5である請求項8または9に記載の燃料ポンプ。
- 前記ベーパ排出孔は、前記第2流路の反第1流路側に連通する第3流路(23)をさらに有し、
前記第3流路の内径は、前記第2流路の内径よりも大きい請求項8から10のいずれか一項に記載の燃料ポンプ。 - 前記第3流路の内壁は、前記ケーシングを形成する際、前記ケーシングを構成する材料から前記第3流路を形成する金型を抜くための抜き勾配程度のテーパを有する請求項11に記載の燃料ポンプ。
- 前記燃料流路は、
径外側から径内側に向かい徐々に深くなる外曲面部(181)と、
その外曲面部の径内側に設けられ、深さが一定の平面部(182)と、
その平面部の径内側に設けられ、前記平面部から径内側に向かい徐々に浅くなる内曲面部(183)と、を有し、
前記ベーパ排出孔の前記第1流路は、前記内曲面部に接続する請求項8から12のいずれか一項に記載の燃料ポンプ。 - 請求項1に記載の燃料ポンプの駆動を制御する制御方法において、
前記ポンプ室及び前記燃料流路にベーパが発生したことを検出する検出行程(S3)と、
前記検出部がベーパの発生を検出していないとき、前記モータ部を制御して前記インペラの回転数を目標燃圧に応じた回転数にする通常制御行程(S2)と、
前記検出部がベーパの発生を検出したとき、前記インペラの回転数を所定時間、前記通常制御部が定める目標回転数よりも高くすることにより、前記ポンプ室及び前記燃料流路のベーパを前記ベーパ排出孔へ排出するベーパ制御行程(S4,S5)と、を含む燃料ポンプの制御方法。
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US14/914,388 US10260465B2 (en) | 2013-08-30 | 2014-08-21 | Fuel pump and control method therefor including control of rotation speed of impeller |
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