US3924970A - Electrically controlled fuel pump - Google Patents
Electrically controlled fuel pump Download PDFInfo
- Publication number
- US3924970A US3924970A US419481A US41948173A US3924970A US 3924970 A US3924970 A US 3924970A US 419481 A US419481 A US 419481A US 41948173 A US41948173 A US 41948173A US 3924970 A US3924970 A US 3924970A
- Authority
- US
- United States
- Prior art keywords
- fuel
- chamber
- pump
- diaphragm
- pressure
- 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.)
- Expired - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C14/00—Control of, monitoring of, or safety arrangements for, machines, pumps or pumping installations
- F04C14/18—Control of, monitoring of, or safety arrangements for, machines, pumps or pumping installations characterised by varying the volume of the working chamber
- F04C14/22—Control of, monitoring of, or safety arrangements for, machines, pumps or pumping installations characterised by varying the volume of the working chamber by changing the eccentricity between cooperating members
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B49/00—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
- F04B49/06—Control using electricity
Definitions
- ABSTRACT An electrically controlled fuel pump assembly for use in the fuel system of an internal combustion engine which is adapted to deliver fuel at a regulated high
- ELECTRICALLY CONTROLLED FUEL PUMP [75] Inventors: Ralph H. Johnston; Leroy E. Lakey,
- the assembly including a variable displace ment vane pump, located in a distributor housing, which also contains ignition components for the engine, the vane pump being driven by the engine and has its discharge outlet connected to a diaphragm type pressure regulator, control pressure on one side of the diaphragm being regulated by electric current which biases a solenoid operated pilot valve, whereby the pressure regulator can modulate fluid pressure used to vary the pump output volume and discharge pressure over the operating speed and work load range of the engine in accordance with an electrical control signal, indicative of engine operating conditions, supplied to the solenoid. This is accomplished by having the displacement of the vane pump hydraulically varied by means of fuel, the flow of which is modulated by the pressure regulator.
- This invention relates to a fuel control system and, in particular, to an electrically controlled fuel pump for controlling the delivery rate of the fuel to an internal combustion engine as a function of the magnitude of an electric control current.
- Another object of this invention is to provide a variable displacement pump mechanism and a regulator therefor whereby a rather small current flowing through a solenoid biases a pilot valve which thus variably regulates a control pressure on one side of the regulator, this control pressure, relative to the discharge pressure from the pump mechanism, in turn controlling the delivery of fuel used to hydraulically vary the displacement of the pump to thereby regulate the flow and pressure of fuel discharged therefrom.
- a varaible displacement fuel pump the displacement of which is hydraulically varied by discharged fuel at a pressure modulated by a pressure regulator of the diaphragm type having fuel on one side thereof at pump outlet pressure and fuel on the other side thereof at a control pressure determined by fuel flowing through an inlet orifice from a fuel supply at outlet pressure and fuel flow through a discharge orifice, the flow from the discharge orifice being regulated by a control signal to a solenoid which in turn controls the position of a pilot valve in relation to the discharge orifice.
- FIG. 1 is an elevational view, partly in section, of a distributor assembly incorporating the electrically controlled fuel pump of the invention
- FIG. 2 is a sectioinal view taken along line 2-2 of FIG. 1 showing the variable displacement fuel pump and pressure regulator for controlling fuel delivery;
- variable displacement fuel pump assembly 14 is mounted on the base 11 and a pressure regulator unit 15 issecured to the pump assembly 14.
- a distributor cap 18, mounted on the distributor shell 17, contains an ignition coil, not shown, which may be of the type as shown and described in detail in U.S. Pat. No. 3,638,630, entitled Intemal Combustion Engine Ignition Distributor Cap and Coil Assembly, issued Feb. 1, 1972 to Lewis R. Hetzler et a1.
- housing 16 may be rotatably adjusted with respect to distributor base 11 without moving the fuel pump 14 or the pressure regulator 15.
- the fuel pump 14 includes an annular casing or stator housing 20 closed at opposite sides by top plate 21 and bottom plate 22, as seen in FIG. 1, to form a cavity or stator chamber 23 in which a control slide or slider 24 is slidably disposed, the opposed flat outer sides of the slider 24 slidably engaging the inner side walls 25 and 26 of the housing 20.
- a compression spring 27 is interposed between the top of the slider 24 and a connector 28 threaded in a return passage 30 extending through the housing 20 to normally bias the slider 24 in a direction, toward the bottom as seen in FIG.
- Connector 28 is provided with a restricted passage or orifice 28a for a purpose to be described.
- the slider 24 is provided with a centrally located cylindrical pumping chamber or cavity 32 which is in communication via an inlet chamber 33 and connecting passage 34 in the control slider to an inlet port 35 in the housing 20 and, via an outlet chamber 36 and connecting passage 37 in the slider 24 with the outlet port 38 in the housing 20.
- a cylindrical rotor 40 pressed on a pump shaft sleeve 41 keyed to the distributor drive shaft 12, is ro- 3 tatably disposed in the pumping chamber.
- a plurality of vanes 42 disposed in slots of the rotor, are outwardly biased by springs 43 into engagement with the cylindrical wall 44 of the slider forming the pumping cavity 32.
- the pressure regulator is provided with a threepiece housing including a regulator body 50 with an annular opening at its upper end, with reference to FIG. 2, an intermediate case 51 having a stepped bore 52 at its lower end and a bore 53 at its opposite or upper end with an intervening wall 54 therebetween having a central aperture 55 therethrough and a cover 56 partly closing off the upper bore 53 in the intermediate case.
- These elements are suitably secured together as by screws, not shown, with a regulator diaphragm in the form of roll diaphragm 57 having its outer periphery sandwiched between the regulator body 50 and intermediate case 51 to form with the opening in the regulator body 50 an accumulator chamber 58.
- a regulator diaphragm in the form of roll diaphragm 57 having its outer periphery sandwiched between the regulator body 50 and intermediate case 51 to form with the opening in the regulator body 50 an accumulator chamber 58.
- the regulator body 50 of the pressure regulator 15 is suitably secured to the pump housing with the inlet 61 therein, in communication with the chamber 58, aligned with the outlet port 38 in the housing 20.
- a fuel delivery outlet 62 in the regulator body 50 is in communication at one end with the chamber 58 and at its other end is provided with a spring biased ball check valve 63 to limit fuel flow in one direction.
- the chamber 58 in regulator body 50 is adapted to be placed in communication via a control pressure outlet 64 and a passage 45 in the pump housing 20 to the stator chamber 23 at one side of the slider 24, the bottom side as seen in FIG. 2, whereby high pressure fluid discharged from the pump can be supplied to this side of the chamber 23 to bias the slider 24 in an upward direction, as seen in this figure, against the biasing action of spring 27 to effect a reduction in the output capacity of the fuel pump, this side of the stator chamber 23 being vented by a properly sized, restricted orifice passage 46 in the slider to the inlet chamber 33 of the slider.
- valve member 65 slidably received in one end of the control pressure outlet 64 adjacent to the chamber 58, this valve being suitably fixed at its upper end to a retainer 66 having a pair of opposed radially extending ears or tangs 66a slidably received in suitable slots 67 formed in the walls of a bracket 68, shown in the form of an inverted cup, the valve member 65 being normally biased to its closed position by a spring 69 in abutment at one end against bracket 68 and at its other end against retainer 66.
- a piston 70 is reciprocally journalled in the stepped bore 52 of intermediate case 51 and this piston and bracket 68 are secured together on opposite sides of the roll diaphragm 57 by means of a hollow rivet 71 extending through central apertures in the bracket 68, diaphragm 57, the bottom wall of the piston 70 and a washer 72 in abutment against the bottom wall of the piston.
- the tubular rivet provides an axially extending restricted orifice passage 73 therethrough to effect communication between the accumulator chamber 58 and a bias pressure chamber 74 defined by the piston in the stepped bore 52.
- a spring 75 of predetermined force, positioned in the stepped bore 52 and piston 70 abuts at one end against the wall 54 of intermediate case 51 and at its other end against the washer 72 to normally bias the piston 70 and diaphragm 57 in a downward direction, with reference to FIG. 2, therefore moving barcket 68 also in a corresponding direction to allow seating of the valve member 65 by spring 69 to block fluid flow through the control pressure outlet 64.
- a solenoid operated pilot valve assembly is used to control the flow of fuel from the bias pressure chamber 74 whereby to regulate the bias pressure therein, this bias pressure in turn setting, through the operation of the valve member 65, as affected by the differential bias pressure and pump discharge pressure acting on opposite sides of diaphragm 57, the fuel flow used to hydraulically vary the displacement of the fuel pump and therefore, its discharge volume and pressure, as a function of an electrical signal applied to the solenoid, this electrical control signal reflecting the engine operating conditions, including, preferably, a measurement of the desired airfuel ratio of the combustion fluid to be supplied to the engine.
- the solenoid operated pilot valve assembly is mounted in the bore 53 in the upper half of the intermediate case 51 and is enclosed and retained by the cover 56.
- the space within the bore 53 contains fuel at fuel tank pressure, the space being vented to a fuel tank by radial passages 76 in the cap commuting with a stepped and threaded axial fuel return passage 77 having an axially apertured insert 78 positioned therein.
- the solenoid operated pilot valve assembly includes a plunger guide 80 for a valve plunger 81 which cooperates with an annular valve seat disk 82 which is clamped by the lower split collet portion 80a of the plunger guide in abutment against the wall 54 of the intermediate casing 51.
- the valve seat disk 82 has a central circular sized orifice 83 which overlies the aperture 55 in wall 54 in communication with the bias pressure chamber 74, the orifice 83 being of a larger diameter than the orifice 73 which controls the flow rate into chamber 74 from chamber 58.
- the solenoid coil assembly 84 of the solenoid is supported concentrically within the bore by means of a split annular coil housing 85 which also centrally aligns the plunger guide 80, the radial flange of the plunger guide engaging the inner peripheral surface of the coil housing 85.
- the radial flange portion of the plunger guide is provided with circumferentially spaced apart slots 80b at the outer periphery thereof to permit fuel flow through the openings thus provided adjacent to the inner periphery of coil housing 85.
- the armature 86 of the solenoid is slidably positioned within the armature core of coil assembly 84 and is magnetically attracted by energization of the coil assembly 84 to bias the plunger 81, by abutment therewith, into engagement with the valve seat 82.
- the armature 86 and plunger 81 are shown as separate elements, it is to be realized that they can be formed integral with each other.
- the orifice passage 83 in the valve seat 82 is of relatively small diameter so that the pressure exerted by fuel in the bias pressure chamber 74 on the plunger 81 is relatively small.
- the magnetic force on armature 86 tends to close the plunger 81 relative to orifice 83 and opposes the pressure of fuel tending to escape from the bias pressure chamber 74, fuel being supplied to this chamber through the orifice passage 73 from the discharge side of the fuel pump, whereby the static pressure of the fuel between the orifice 73 and orifice 83 is regulated as a function of current flow to the solenoid.
- this valve arrangement opens to bleed fluid out of the bias pressure chamber 74 at a value which is proportional to the closing force exerted by the solenoid.
- Fuel flow from accumulator chamber 58 into chamber 74 being regulated by the predetermined size of orifice passage 73.
- the magnetic structure of the solenoid is such that the displacement of the armature and therefore of plunger 81 is very slight and the force applied to the plunger 81 is substantially directly proportional to current flowing into the coil assembly 84.
- control of this current by a control device applying a control signal to the coil assembly determines the bias pressure in the bias pressure chamber 74.
- the coil assembly 84 of the solenoid is energized by a lead 87 which is connected to a terminal assembly 88 threaded into a corresponding threaded recess in the intermediate case 51.
- the solenoid valve is supplied with an electrical control signal mechanism 90.
- This control signal mechanism may be of any suitable type. Ordinarily, it will include means for transmitting a current to the solenoid which is determinative of the pressure of fuel to be supplied to the engine to run the engine at a predetermined air-fuel ratio at the desired power level.
- the details of the control signal mechanism 90 are immaterial to the subject invention, may take any desired form and, therefore, need not be described in detail.
- a fuel line 91 delivers fuel to the pump 14 at a predetermined relatively low pressure from a supply pump 92 located in a fuel tank 93, the fuel line being connected to the pump inlet 35.
- fuel is delivered from the pump through the outlet port 38 and inlet passage 61 of the pressure regulator unit 15 to the chamber 58 thereof at a pressure corresponding to the outlet pressure of the pump for discharge at a regulated high pressure through the one-way flow ball check valve 63 in the fuel delivery outlet 62 via a fuel metering valve 94 to the engine, not shown.
- Valve 94 may be any suitable type metering valve, not described since it forms no part of the subject invention and, if desired, it may take the form of a suitable fuel injector discharging into a common induction manifold or it may be in the form of a plurality of unit fuel injectors.
- the chamber 58 is in effect an accumulator chamber having an accumulating volume dependent on the upper movement of the diaphragm 57, without unseating of the valve member 65, which movement is determined by the lost motion distance provided by the slots 67 in bracket 68.
- the pressure of fuel discharged from chamber 58 will tend to decrease and in response to such a drop in pressure, the diaphragm 57 is moved downward, with reference to FIG. 2, by the spring 75 and the control pressure of fuel in the control pressure chamber 74 and, the accumulated fuel in chamber 58 is delivered through the outlet 62 to the fuel metering valve 94.
- a pressure regulator for controlling delivery of fuel from said pump comprising a housing defining a cavity divided by a diaphragm to provide a first chamber for receiving fuel discharged from said pump and a second chamber in communication with said first chamber by a sized orifice, said housing further defining a fuel delivery outlet extending from said first chamber for discharge of fuel and a regulating pressure outlet extending from said first chamber in communication with said stator chamber on the opposite side of said slider from said spring, said diaphragm being movable away from said regulating pressure outlet in response to an increase in fuel pressure within said first chamber, spring means biasing said diaphragm toward said regulating pressure outlet, a bracket secured to said diaphragm within said first chamber, a valve member disposed in said first chamher and engageable with said regulating pressure
- An electrically controlled fuel pump for use in the fuel system of an internal combustion engine comprising, in combination, a variable displacement pump having an inlet and an outlet, said pump including a housing having a stator chamber, a slider with a pump cavity therein slidable in said stator chamber, engine driven pump rotor means operative in said pump cavity, spring means in said stator chamber on one side of said slider to normally bias said slider in a first direction relative to said pump rotor means, a regulator housing having a fuel inlet connected to said outlet, a fuel discharge outlet, a regulating pressure outlet operatively connected to said stator chamber on the opposite side of said slider from said spring means, and a fuel return passage, a diaphragm positioned in said regulator housing to provide with the interior thereof a first chamber in communication with said fuel inlet, said discharge outlet and said regulating pressure outlet and a second chamber in communication with said fuel return passage, conduit means including an orifice and a variably controllable pressure regulating pilot valve in communication with said second chamber connecting said first chamber to
- said lost motion means is a bracket secured to said diaphragm and wherein said spring biased valve means includes a valve member engageable with said bracket upon a predetermined movement of said bracket to effect opening movement of said valve member relative to said regulating pressure outlet.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US419481A US3924970A (en) | 1973-11-28 | 1973-11-28 | Electrically controlled fuel pump |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US419481A US3924970A (en) | 1973-11-28 | 1973-11-28 | Electrically controlled fuel pump |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| USB419481I5 USB419481I5 (it) | 1975-01-28 |
| US3924970A true US3924970A (en) | 1975-12-09 |
Family
ID=23662461
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US419481A Expired - Lifetime US3924970A (en) | 1973-11-28 | 1973-11-28 | Electrically controlled fuel pump |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3924970A (it) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1993021424A1 (en) * | 1992-04-14 | 1993-10-28 | Ab Volvo | Variable displacement pump |
| FR2764336A1 (fr) * | 1997-06-05 | 1998-12-11 | Hydraulique Chateaudun L | Dispositif d'alimentation en carburant d'un moteur rotatif a combustion |
| US6524076B2 (en) * | 2000-04-27 | 2003-02-25 | Bosch Braking Systems Co., Ltd. | Variable displacement pump including a control valve |
| KR100399103B1 (ko) * | 2001-04-18 | 2003-09-22 | 성갑제 | 압력 스위치용 파일럿 밸브를 이용한 공기압축기 |
| US20060127229A1 (en) * | 2002-04-03 | 2006-06-15 | Borgwarner Inc. | Variable displacement pump and control therefor |
| US20080240935A1 (en) * | 2007-03-28 | 2008-10-02 | Goodrich Pump & Engine Control Systems, Inc. | Balanced variable displacement vane pump with floating face seals and biased vane seals |
| US7726948B2 (en) * | 2002-04-03 | 2010-06-01 | Slw Automotive Inc. | Hydraulic pump with variable flow and variable pressure and electric control |
| US20100319654A1 (en) * | 2009-06-17 | 2010-12-23 | Hans-Peter Messmer | Rotary vane engines and methods |
| US20110200463A1 (en) * | 2007-08-16 | 2011-08-18 | Friedrich Boecking | Pump, particularly high-pressure fuel pump |
| US20130121867A1 (en) * | 2011-11-11 | 2013-05-16 | Schwäbische Hüttenwerke Automotive GmbH | Rotary pump with improved seal |
| US20140096852A1 (en) * | 2012-10-08 | 2014-04-10 | Hyundai Motor Company | Hydraulic pressure supply system of automatic transmission |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3347015A1 (de) * | 1983-12-24 | 1985-07-04 | Alfred Teves Gmbh, 6000 Frankfurt | Druckregelvorrichtung fuer eine hydraulikpumpe, insbesondere eine fluegelzellenpumpe |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2588522A (en) * | 1948-07-30 | 1952-03-11 | Lucas Ltd Joseph | Regulating means for liquid fuel supply systems of prime movers or other apparatus |
| US3067693A (en) * | 1958-12-24 | 1962-12-11 | United Aircraft Corp | Control means for variable delivery pump |
| US3165068A (en) * | 1960-06-27 | 1965-01-12 | American Brake Shoe Co | Fluid power apparatus |
| US3252419A (en) * | 1963-12-16 | 1966-05-24 | Bendix Corp | Pump inlet pressurizing system |
| US3724972A (en) * | 1971-12-27 | 1973-04-03 | Gen Motors Corp | Fuel injection pump |
| US3732041A (en) * | 1971-06-10 | 1973-05-08 | Sperry Rand Corp | Power transmission |
-
1973
- 1973-11-28 US US419481A patent/US3924970A/en not_active Expired - Lifetime
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2588522A (en) * | 1948-07-30 | 1952-03-11 | Lucas Ltd Joseph | Regulating means for liquid fuel supply systems of prime movers or other apparatus |
| US3067693A (en) * | 1958-12-24 | 1962-12-11 | United Aircraft Corp | Control means for variable delivery pump |
| US3165068A (en) * | 1960-06-27 | 1965-01-12 | American Brake Shoe Co | Fluid power apparatus |
| US3252419A (en) * | 1963-12-16 | 1966-05-24 | Bendix Corp | Pump inlet pressurizing system |
| US3732041A (en) * | 1971-06-10 | 1973-05-08 | Sperry Rand Corp | Power transmission |
| US3724972A (en) * | 1971-12-27 | 1973-04-03 | Gen Motors Corp | Fuel injection pump |
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1993021424A1 (en) * | 1992-04-14 | 1993-10-28 | Ab Volvo | Variable displacement pump |
| US5618165A (en) * | 1992-04-14 | 1997-04-08 | Ab Volvo | Variable displacement and constant pressure pump |
| FR2764336A1 (fr) * | 1997-06-05 | 1998-12-11 | Hydraulique Chateaudun L | Dispositif d'alimentation en carburant d'un moteur rotatif a combustion |
| US6524076B2 (en) * | 2000-04-27 | 2003-02-25 | Bosch Braking Systems Co., Ltd. | Variable displacement pump including a control valve |
| KR100399103B1 (ko) * | 2001-04-18 | 2003-09-22 | 성갑제 | 압력 스위치용 파일럿 밸브를 이용한 공기압축기 |
| US7726948B2 (en) * | 2002-04-03 | 2010-06-01 | Slw Automotive Inc. | Hydraulic pump with variable flow and variable pressure and electric control |
| US7396214B2 (en) * | 2002-04-03 | 2008-07-08 | Borgwarner Inc. | Variable displacement pump and control therefor |
| US20060127229A1 (en) * | 2002-04-03 | 2006-06-15 | Borgwarner Inc. | Variable displacement pump and control therefor |
| US20080240935A1 (en) * | 2007-03-28 | 2008-10-02 | Goodrich Pump & Engine Control Systems, Inc. | Balanced variable displacement vane pump with floating face seals and biased vane seals |
| US8011909B2 (en) | 2007-03-28 | 2011-09-06 | Goodrich Pump & Engine Control Systems, Inc. | Balanced variable displacement vane pump with floating face seals and biased vane seals |
| US20110200463A1 (en) * | 2007-08-16 | 2011-08-18 | Friedrich Boecking | Pump, particularly high-pressure fuel pump |
| US8337178B2 (en) * | 2007-08-16 | 2012-12-25 | Robert Bosch Gmbh | Pump, particularly high-pressure fuel pump |
| US20100319654A1 (en) * | 2009-06-17 | 2010-12-23 | Hans-Peter Messmer | Rotary vane engines and methods |
| US20130121867A1 (en) * | 2011-11-11 | 2013-05-16 | Schwäbische Hüttenwerke Automotive GmbH | Rotary pump with improved seal |
| US8814544B2 (en) * | 2011-11-11 | 2014-08-26 | Schwabische Huttenwerke Automotive Gmbh | Rotary pump with improved seal |
| US20140096852A1 (en) * | 2012-10-08 | 2014-04-10 | Hyundai Motor Company | Hydraulic pressure supply system of automatic transmission |
Also Published As
| Publication number | Publication date |
|---|---|
| USB419481I5 (it) | 1975-01-28 |
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