US3845750A - Fuel proportioning system for a combustion engine - Google Patents

Fuel proportioning system for a combustion engine Download PDF

Info

Publication number
US3845750A
US3845750A US00318400A US31840072A US3845750A US 3845750 A US3845750 A US 3845750A US 00318400 A US00318400 A US 00318400A US 31840072 A US31840072 A US 31840072A US 3845750 A US3845750 A US 3845750A
Authority
US
United States
Prior art keywords
fuel
valve
proportioning
supply
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
Application number
US00318400A
Inventor
W Enge
H Harings
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from DE19712164523 external-priority patent/DE2164523C/en
Application filed by Individual filed Critical Individual
Application granted granted Critical
Publication of US3845750A publication Critical patent/US3845750A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M69/00Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • F02M69/16Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by means for metering continuous fuel flow to injectors or means for varying fuel pressure upstream of continuously or intermittently operated injectors
    • F02M69/18Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by means for metering continuous fuel flow to injectors or means for varying fuel pressure upstream of continuously or intermittently operated injectors the means being metering valves throttling fuel passages to injectors or by-pass valves throttling overflow passages, the metering valves being actuated by a device responsive to the engine working parameters, e.g. engine load, speed, temperature or quantity of air
    • F02M69/22Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by means for metering continuous fuel flow to injectors or means for varying fuel pressure upstream of continuously or intermittently operated injectors the means being metering valves throttling fuel passages to injectors or by-pass valves throttling overflow passages, the metering valves being actuated by a device responsive to the engine working parameters, e.g. engine load, speed, temperature or quantity of air the device comprising a member movably mounted in the air intake conduit and displaced according to the quantity of air admitted to the engine

Definitions

  • ABSTRACT A fuel proportioning system is provided for an internal combustion engine. Fuel is supplied under constant pressure through a throttle to a proportioning valve having one outlet through an injection nozzle and a return outlet through a diaphragm actuted needle valve to a throttle valve controlled in accordance with the volume of air admitted to the engine to return supply fuel to the pump.
  • the proportioning valve is spring urged to closed position and is opened by fuel pres sure in the proportioning valve, The valve closure member flutters between open and closed position to pulse the fuel delivered to the injector nozzle, the pulsed fuel flow being more readily controllable in small volumes than a continuous fuel flow.
  • the proportionality between the combustion air throughput and the rate of fuel supplied is continuously altered in accordance with certain engine operating magnitudes, by a method in which the fuel conveyed by the fuel pump is caused to move in a main flow past the proportioning valve, on which the air throughput measuring means acts direct, the pressure of the fuel being adjusted in the return flow by throttle valves which are adjusted by the engine operating values; the adjustment of flow serves to exert, on the proportioning valve, a force acting oppositely to that exerted by the air flow measuring means, and of which the magnitude corresponds to the particular pressure prevailing in the main fuel flow at the time.
  • the invention is directed towards providing a fuel proportioning system in which the fuel is accurately proportioned, not only at full-load and in the upper part-load range, but also under no-load conditions and in the lower part-load range.
  • the invention provides a fuel proportioning system for a combustion engine comprising a supply of fuel at constant pressure; a proportioning valve connected to the fuel supply having a delivery outlet for connection to injection apparatus in an inlet manifold of the engine, and a return outlet; an adjustable throttle valve connected between the return outlet and a return conduit to the supply, and controlling the rate of fuel returned to the supply; and means responsive to the throughput of combustion air for controlling the throttle valve and hence the fuel pressure in the proportioning valve; the proportioning valve comprising a springloaded pressure-responsive valve controlling the flow of fuel to the delivery outlet and means in the connection to the fuel supply to prevent instantaneous pressure equalisation in the valve on opening of the delivery outlet.
  • the system operates to supply fuel intermittently to the delivery outlet, the pressure-responsive valve opening and closing in a pulsating manner and allowing a small quantity of fuel to pass during each opening cycle. In that way, the problem is overcome of measuring very small quantities of fuel in a system designed for a large, maximum, fuel throughput.
  • the duration and frequency of the opening of the valve are determined by the pressure downstream of the valve, which in turn depends on the adjustment of the adjustable throttle valve controlled by the air throughput. Overall adjustment is made possible by making the spring loading of the pressure responsive valve adjustable.
  • FIG. 1 is a schematic diagram of the system
  • FIG. 2 shows in section a diaphragm controlled needle valve provided in the system.
  • a fuel pump II supplies fuel under pressure to a conduit 24 which contains a pressure governor 2 by which the pressure of the delivered fuel is kept constant in a distributor pipe 3.
  • a branch 5 leads to an inlet chamber 21 of a spring-loaded pressure-responsive valve 16 and from thence to the pressure chamber of a throttle valve 6.
  • the throttle valve 6 has an outlet conduit 7which returns fuel to the fuel reservoir (not Shown) to which pump 1 is connected. Open end of conduit 7 is shown as closed by a diaphragm 6A, but which can be opened as described below to permit passage of fuel through the conduit 7.
  • Throttle valve 6 is controlled in part by means responsive to the throughput of combustion air, indicated generally at 8. These means take the form of an air intake manifold 9 having the usual butterfly valve (not shown) and containing a disc I1.
  • Disc 11 is mounted on a sleeve 11A, slidably arranged on a shaft 118 which is secured in place by a transverse mounting 11C secured in the manifold 9.
  • the sleeve 11A is attached to a crank arm 11D, which is acted on by a spring I2, so that the sleeve 11A and hence the disc 11 is biased upwardly to close against a restricted part 10 of the manifold 9.
  • a spring 14 surrounding the shaft 118 acts at its ends against disc 11 and one end of a lever 15, which is pivoted intermediate its ends on the casing manifold 9. The other end of lever 15 acts on the diaphragm 6A of the throttle valve 6.
  • lever 15 acts in opposition to the pressure of fuel within the throttle valve 6.
  • the fuel pressure causes the diaphragm 6A to move downwardly and to open the conduit 7 for return of fuel to the reservoir, so that little fuel is directed to the engine.
  • the fuel pressure is progressively overcome, the throttle valve 6 closing and causing a greater supply of fuel to the engine.
  • valve 16 the inlet chamber 21 is closed on one side by a valve disc 22 which is biased upwardly against its seat by a spring 32, which can be adjusted by a screw 23.
  • the valve disc 22 In the uppermost position of the valve disc 22, i.e., as shown in FIG. 1, the valve disc closes off a delivery outlet leading to an injection nozzle 4, by which fuel is injected into the intake manifold of the engine.
  • a throttle in the form of a restriction 19, is provided upstream of valve 16 to prevent rapid instantaneous equalisation of pressure between the distributor pipe 3 and the inlet chamber 21 of the valve 16, when valve disc 22 opens to allow fuel topass to the nozzle 4.
  • a further throttle is provided downstream of the valve 16, this throttle consisting of a diaphragm-controlled regulating valve which is shown in detail in FIG. 2.
  • the inlet connection 26 of the needle valve is connected to the return outlet 18 of the valve 16.
  • the needle valve 20 has an elongated discharage outlet which is connected to the throttle valve 6 and which contains a needle 30 carried on a diaphragm 27 within the valve chamber 25.
  • the fuel pressure acts on the diaphragm 27 and holds the valve in the open position, needle 30 being retracted in opposition to the force of a spring 29 acting on the diaphragm 27 and adjusted by means of an adjusting screw 28. Ifthe pressure in the inlet chamber 21 of valve 16 collapses instantaneously on opening of that valve, the resulting pressure drop in chamber of valve 20 permits spring 29 to cause needle 30 to close the discharge passage 31; the result is that throttle valve 6 is not affected by the pressure drop.
  • the system operates as follows:
  • Throttle valve 6 is thus opened to an extent dependent on the flow of combustion air to the engine. This in turn determines the fuel pressure within the chamber of valve 6.
  • Throttle l9 permits the existence of a fuel pressure in throttle valve 6, and therefore in inlet chamber 21 of a value less than that delivered by the fuel pump 1 and governor 2.
  • valve 32 While the engine is in operation, valve 32 operates intermittently to supply fuel to jet 4 in a pulsating manner.
  • the fuel pressure in chamber 21, controlled by throttle valve 6 as described, causes valve disc 22 to move away from its seat against the action of spring 32 and to allow fuel to pass to nozzle 4.
  • valve disc 22 opens, the pressure within chamber 21 drops as a consequence.
  • the pressures on the two sides of valve disc 22 are equalised, so that spring 32 causes the valve to reclose.
  • the delivery opening of valve 16 having therefore been closed, the pressure in chamber 21 rises again to cause a further short-term opening of valve disc 22.
  • the duration of each opening of valve 16 and the repetition rate of opening are determined by the pressure within throttle valve 6, which in turn is determined by the rate of flow of combustion air through mainfold 9.
  • Needle valve 20 operates as described above to ensure that throttle valve 6 is unaffected by the short term variations in the pressure in inlet chamber 21 as the valve 16 operates intermittently.
  • each branch 5 is connected to a separate pressure responsive valve 16, the return outlets of all the valves being connected to the single throttle valve 6.
  • Each valve 16 has a separate discharge outlet leading to a nozzle for one of the intake manifolds.
  • a fuel proportioning system for a combustion engine comprising a supply of fuel at constant pressure; a proportioning and pulsing valve connected to the fuel supply and having a delivery outlet for connection to injection apparatus in an inlet manifold of the engine, and a return outlet; an adjustable throttle valve connected between the return outlet and a return conduit to the supply, and controlling the rate of fuel returned to the supply; and means responsive to the throughput of combustion air for controlling the throttle valve and hence the fuel pressure in the proportioning valve; the proportioning and pulsing valve comprising a springloaded pressure responsive valve controlling the flow of fuel to the delivery outlet being spring urged toward closed position and being urged open by fuel pressure, said valve oscillating open and closed to pulse the fuel to the delivery outlet and means in the connection to the fuel supply to prevent instantaneous pressure equalisation in the valve on opening of the delivery outlet.
  • a fuel proportioning system in which the proportioning valve has an inlet chamber connected both to the return outlet and the fuel supply, and throttles are provided both in the return outlet and in the connection to the fuel supply.
  • a fuel proportioning system for a combustion engine comprising a supply of fuel at constant pressure; a proportioning valve connected to the fuel supply and having a delivery outlet for connection to injection apparatus in an inlet manifold of the engine, and a return outlet; an adjustable throttle valve connected between the return outlet and a return conduit to the supply, and controlling the rate of fuel returned to the supply; and means responsive to the throughput of combustion air for controlling the throttle valve and hence the fuel pressure in the proportioning valve; the proportioning valve comprising a spring-loaded pressure responsive valve controlling the flow of fuel to the delivery outlet under spring action when the pressure on the diaphragm decreases relative to that of the adjustable throttle valve.
  • a fuel proportioning system according to claim 3, in which the spring-loaded pressure-responsive valve includes adjustable spring loading means.

Abstract

A fuel proportioning system is provided for an internal combustion engine. Fuel is supplied under constant pressure through a throttle to a proportioning valve having one outlet through an injection nozzle and a return outlet through a diaphragm actuted needle valve to a throttle valve controlled in accordance with the volume of air admitted to the engine to return supply fuel to the pump. The proportioning valve is spring urged to closed position and is opened by fuel pressure in the proportioning valve. The valve closure member flutters between open and closed position to pulse the fuel delivered to the injector nozzle, the pulsed fuel flow being more readily controllable in small volumes than a continuous fuel flow.

Description

United States Patent 11 1 Harings, deceased Nov. 5, 1974 1 1 FUEL PROPORTIONING SYSTEM FOR A COMBUSTION ENGINE [76] Inventor: Horst Harings, deceased, late of 289 Nordenham, Germany by Willi Enge, administrator [221 Filed: Dec. 26, 1972 [211 Appl. No: 318,400
[301 Foreign Application Priority Data Dec, 24, 1971 Germany 2164523 [52] US. Cl 123/139 AW, 123/119 R, 123/32 R [51] Int. Cl. F02m 51/00 58 Field of Search 123/139, 119, 32
[56] References Cited UNITED STATES PATENTS 2,447,267 8/1948 Mock 123/119 R 2.591.356 4/1952 Howe i 123/119 R 2,899,948 8/1959 Groves i 123/119 R 3,650,258 3/1972 Jackson i 123/139 AW 3,688,751) 9/1972 O'Neill 123/32 EA Primary ExaminerLaurence M. Goodridge Assistant ExaminerCort Flint Attorney, Agent, or Firm-Olson, Trexler, Wolters, Bushnell & Fosse, Ltd.
[57] ABSTRACT A fuel proportioning system is provided for an internal combustion engine. Fuel is supplied under constant pressure through a throttle to a proportioning valve having one outlet through an injection nozzle and a return outlet through a diaphragm actuted needle valve to a throttle valve controlled in accordance with the volume of air admitted to the engine to return supply fuel to the pump. The proportioning valve is spring urged to closed position and is opened by fuel pres sure in the proportioning valve, The valve closure member flutters between open and closed position to pulse the fuel delivered to the injector nozzle, the pulsed fuel flow being more readily controllable in small volumes than a continuous fuel flow.
4 Claims, 2 Drawing Figures PMENTEBRBV 5 I974 LJ LID Ill mrl/llrlw FUEL PROPORTIONING SYSTEM FOR A COMBUSTION ENGINE This invention relates to a fuel proportioning system for a combustion engine.
Such a system has been known for some time, as from US. Pat. Nos. 2,318,216 and 2,591,356, in order to maintain the required proportionality between the fuel supply and the combustion air throughput, so that the optimum fuel/air mixture is formed. Means mounted in the intake manifold continuously measures the air throughput and adjusts a fuel proportioning valve in accordance with the measurements. Usually, the required adjustment is effected by direct control of the fuel proportioning valve, which is subjected to a constant pressure of fuel.
It has also been proposed, as in German Pat. specification No. 1,960,144, to effect control by means of an adjustable throttle valve in the return flow of the fuel back to the supply; the proportioning valve is then connected to the supply upstream of the adjustable throttle valve and has a delivery outlet connected to injection apparatus in the intake manifold of the engine. In these proposals, however, the proportionality between the combustion air throughput and the rate of fuel supplied is continuously altered in accordance with certain engine operating magnitudes, by a method in which the fuel conveyed by the fuel pump is caused to move in a main flow past the proportioning valve, on which the air throughput measuring means acts direct, the pressure of the fuel being adjusted in the return flow by throttle valves which are adjusted by the engine operating values; the adjustment of flow serves to exert, on the proportioning valve, a force acting oppositely to that exerted by the air flow measuring means, and of which the magnitude corresponds to the particular pressure prevailing in the main fuel flow at the time.
All the known systems suffer from a difficulty arising from the wide regulating range ofa combustion engine between idling and full load. In all cases, the proportioning valves are continuously open, even in the partial-load range. Since, however, the proportioning valves and their regulating devices have to be designed for maximum fuel throughput at full load, the quantity of fuel to be passed under no-load conditions is of the same order of magnitude as the limits of error dictated by tolerances and other factors of the regulating system. This results in incorrect fuel metering, particularly in the no-load and lower part-load ranges.
The invention is directed towards providing a fuel proportioning system in which the fuel is accurately proportioned, not only at full-load and in the upper part-load range, but also under no-load conditions and in the lower part-load range.
This is achieved, in the present invention, by having the means responsive to the throughput of combustion air adjust the throttle valve in the return fuel flow, and having the proportioning valve consist of a springloaded pressure-responsive valve controlling the fuel to the delivery output, means in the connection of the fuel supply to the proportioning valve preventing instantaneous pressure equalisation in the valve on opening of the valve to deliver fuel to the engine.
Thus, the invention provides a fuel proportioning system for a combustion engine comprising a supply of fuel at constant pressure; a proportioning valve connected to the fuel supply having a delivery outlet for connection to injection apparatus in an inlet manifold of the engine, and a return outlet; an adjustable throttle valve connected between the return outlet and a return conduit to the supply, and controlling the rate of fuel returned to the supply; and means responsive to the throughput of combustion air for controlling the throttle valve and hence the fuel pressure in the proportioning valve; the proportioning valve comprising a springloaded pressure-responsive valve controlling the flow of fuel to the delivery outlet and means in the connection to the fuel supply to prevent instantaneous pressure equalisation in the valve on opening of the delivery outlet.
The system operates to supply fuel intermittently to the delivery outlet, the pressure-responsive valve opening and closing in a pulsating manner and allowing a small quantity of fuel to pass during each opening cycle. In that way, the problem is overcome of measuring very small quantities of fuel in a system designed for a large, maximum, fuel throughput.
The duration and frequency of the opening of the valve are determined by the pressure downstream of the valve, which in turn depends on the adjustment of the adjustable throttle valve controlled by the air throughput. Overall adjustment is made possible by making the spring loading of the pressure responsive valve adjustable.
The invention will be more readily understood by way of example from the following description of a fuel proportioning system for a combustion engine, reference being made to the accompanying drawings, in which FIG. 1 is a schematic diagram of the system, and
FIG. 2 shows in section a diaphragm controlled needle valve provided in the system.
Referring to FIG. 1, a fuel pump II supplies fuel under pressure to a conduit 24 which contains a pressure governor 2 by which the pressure of the delivered fuel is kept constant in a distributor pipe 3. From the distributor pipe 3, a branch 5 leads to an inlet chamber 21 of a spring-loaded pressure-responsive valve 16 and from thence to the pressure chamber of a throttle valve 6. The throttle valve 6 has an outlet conduit 7which returns fuel to the fuel reservoir (not Shown) to which pump 1 is connected. Open end of conduit 7 is shown as closed by a diaphragm 6A, but which can be opened as described below to permit passage of fuel through the conduit 7.
Throttle valve 6 is controlled in part by means responsive to the throughput of combustion air, indicated generally at 8. These means take the form of an air intake manifold 9 having the usual butterfly valve (not shown) and containing a disc I1. Disc 11 is mounted on a sleeve 11A, slidably arranged on a shaft 118 which is secured in place by a transverse mounting 11C secured in the manifold 9. The sleeve 11A is attached to a crank arm 11D, which is acted on by a spring I2, so that the sleeve 11A and hence the disc 11 is biased upwardly to close against a restricted part 10 of the manifold 9. A spring 14 surrounding the shaft 118 acts at its ends against disc 11 and one end of a lever 15, which is pivoted intermediate its ends on the casing manifold 9. The other end of lever 15 acts on the diaphragm 6A of the throttle valve 6.
When the engine is inoperative, the disc 11 closes the manifold. However, during operation of the engine, the engine suction, acting in the direction of the arrow A,
opens disc 11 and, through the spring 14 and lever 15, loads the diaphragm 6A upwardly. The greater the throughput of air through the manifold, the greater the displacement of the disc 11, the stressing of the spring 14 and the force exerted by lever 15 on the diaphragm 6A.
The force exerted by lever 15 acts in opposition to the pressure of fuel within the throttle valve 6. When the throughput of air is small, the fuel pressure causes the diaphragm 6A to move downwardly and to open the conduit 7 for return of fuel to the reservoir, so that little fuel is directed to the engine. However, when the air flow increases, the fuel pressure is progressively overcome, the throttle valve 6 closing and causing a greater supply of fuel to the engine.
Turning now to the valve 16, the inlet chamber 21 is closed on one side by a valve disc 22 which is biased upwardly against its seat by a spring 32, which can be adjusted by a screw 23. In the uppermost position of the valve disc 22, i.e., as shown in FIG. 1, the valve disc closes off a delivery outlet leading to an injection nozzle 4, by which fuel is injected into the intake manifold of the engine.
A throttle, in the form of a restriction 19, is provided upstream of valve 16 to prevent rapid instantaneous equalisation of pressure between the distributor pipe 3 and the inlet chamber 21 of the valve 16, when valve disc 22 opens to allow fuel topass to the nozzle 4.
Similarly, a further throttle is provided downstream of the valve 16, this throttle consisting of a diaphragm-controlled regulating valve which is shown in detail in FIG. 2. ln that figure, the inlet connection 26 of the needle valve is connected to the return outlet 18 of the valve 16. The needle valve 20 has an elongated discharage outlet which is connected to the throttle valve 6 and which contains a needle 30 carried on a diaphragm 27 within the valve chamber 25. In the chamber 25, the fuel pressure acts on the diaphragm 27 and holds the valve in the open position, needle 30 being retracted in opposition to the force of a spring 29 acting on the diaphragm 27 and adjusted by means of an adjusting screw 28. Ifthe pressure in the inlet chamber 21 of valve 16 collapses instantaneously on opening of that valve, the resulting pressure drop in chamber of valve 20 permits spring 29 to cause needle 30 to close the discharge passage 31; the result is that throttle valve 6 is not affected by the pressure drop.
The system operates as follows:
While the engine is operating, the passage of combustion air through the manifold 9 causes a force to be applied, as described above, against the diaphragm 6A in opposition to the fuel pressure acting on that diaphragm. Throttle valve 6 is thus opened to an extent dependent on the flow of combustion air to the engine. This in turn determines the fuel pressure within the chamber of valve 6. Throttle l9 permits the existence of a fuel pressure in throttle valve 6, and therefore in inlet chamber 21 of a value less than that delivered by the fuel pump 1 and governor 2.
While the engine is in operation, valve 32 operates intermittently to supply fuel to jet 4 in a pulsating manner. The fuel pressure in chamber 21, controlled by throttle valve 6 as described, causes valve disc 22 to move away from its seat against the action of spring 32 and to allow fuel to pass to nozzle 4. When valve disc 22 opens, the pressure within chamber 21 drops as a consequence. At the same time, the pressures on the two sides of valve disc 22 are equalised, so that spring 32 causes the valve to reclose. The delivery opening of valve 16 having therefore been closed, the pressure in chamber 21 rises again to cause a further short-term opening of valve disc 22. The duration of each opening of valve 16 and the repetition rate of opening are determined by the pressure within throttle valve 6, which in turn is determined by the rate of flow of combustion air through mainfold 9. Thus, the rate of supply of fuel to nozzle 4 is kept strictly proportional to the supply of air and the required fuel/air mixture is maintained. Needle valve 20 operates as described above to ensure that throttle valve 6 is unaffected by the short term variations in the pressure in inlet chamber 21 as the valve 16 operates intermittently.
The above description has been concerned with a system in which there is a single branch 5 from the distributor pipe 3, the fuel being supplied by the valve 16 to a single nozzle 4 feeding fuel to the main intake mainfold. However, there may be additional branches 5, as shown in the lower part of FIG. 1, the total number of branches corresponding to the number of intake manifolds provided on the vehicle. In that case, each branch 5 is connected to a separate pressure responsive valve 16, the return outlets of all the valves being connected to the single throttle valve 6. Each valve 16 has a separate discharge outlet leading to a nozzle for one of the intake manifolds.
We claim:
1. A fuel proportioning system for a combustion engine comprising a supply of fuel at constant pressure; a proportioning and pulsing valve connected to the fuel supply and having a delivery outlet for connection to injection apparatus in an inlet manifold of the engine, and a return outlet; an adjustable throttle valve connected between the return outlet and a return conduit to the supply, and controlling the rate of fuel returned to the supply; and means responsive to the throughput of combustion air for controlling the throttle valve and hence the fuel pressure in the proportioning valve; the proportioning and pulsing valve comprising a springloaded pressure responsive valve controlling the flow of fuel to the delivery outlet being spring urged toward closed position and being urged open by fuel pressure, said valve oscillating open and closed to pulse the fuel to the delivery outlet and means in the connection to the fuel supply to prevent instantaneous pressure equalisation in the valve on opening of the delivery outlet.
2. A fuel proportioning system according to claim 1, in which the proportioning valve has an inlet chamber connected both to the return outlet and the fuel supply, and throttles are provided both in the return outlet and in the connection to the fuel supply.
3. A fuel proportioning system for a combustion enginecomprising a supply of fuel at constant pressure; a proportioning valve connected to the fuel supply and having a delivery outlet for connection to injection apparatus in an inlet manifold of the engine, and a return outlet; an adustable throttle valve connected between the return outlet and a return conduit to the supply, and controlling the rate of fuel returned to the supply; and means responsive to the throughput of combustion air for controlling the throttle valve and hence the fuel pressure in the proportioning valve; the proportioning valve comprising a spring-loaded pressure responsive valve controlling the flow of fuel to the delivery outlet under spring action when the pressure on the diaphragm decreases relative to that of the adjustable throttle valve.
4. A fuel proportioning system according to claim 3, in which the spring-loaded pressure-responsive valve includes adjustable spring loading means.

Claims (4)

1. A fuel proportioning system for a combustion engine comprising a supply of fuel at constant pressure; a proportioning and pulsing valve connected to the fuel supply and having a delivery outlet for connection to injection apparatus in an inlet manifold of the engine, and a return outlet; an adjustable throttle valve connected between the return outlet and a return conduit to the supply, and controlling the rate of fuel returned to the supply; and means responsive to the throughput of combustion air for controlling the throttle valve and hence the fuel pressure in the proportioning valve; the proportioning and pulsing valve comprising a spring-loaded pressure responsive valve controlling the flow of fuel to the delivery outlet being spring urged toward closed position and being urged open by fuel pressure, said valve oscillating open and closed to pulse the fuel to the delivery outlet and means in the connection to the fuel supply to prevent instantaneous pressure equalisation in the valve on opening of the delivery outlet.
2. A fuel proportioning system according to claim 1, in which the proportioning valve has an inlet chamber connected both to the return outlet and the fuel supply, and throttles are provided both in the return outlet and in the connection to the fuel supply.
3. A fuel proportioning system for a combustion engine comprising a supply of fuel at constant pressure; a proportioning valve connected to the fuel supply and having a delivery outlet for connection to injection apparatus in an inlet manifold of the engine, and a return outlet; an adustable throttle valve connected between the return outlet and a return conduit to the supply, and controlling the rate of fuel returned to the supply; and means responsive to the throughput of combustion air for controlling the throttle valve and hence the fuel pressure in the proportioning valve; the proportioning valve comprising a spring-loaded pressure responsive valve controlling the flow of fuel to the delivery outlet and means in the connection to the fuel supply to prevent instantaneous pressure equalisation in the valve on opening of the delivery outlet, the proportioning valve having an inlet chamber connected both to the return outlet and the fuel supply, throttles being provided both in the return outlet and in the connection to the fuel supply, the throttle in the return outlet comprising a diaphragm regulated needle valve arranged to close under spring action when the pressure on the diaphragm decreases relative to that of the adjustable throttle valve.
4. A fuel proportioning system according to claim 3, in which the spring-loaded pressure-responsive valve includes adjustable spring loading means.
US00318400A 1971-12-24 1972-12-26 Fuel proportioning system for a combustion engine Expired - Lifetime US3845750A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19712164523 DE2164523C (en) 1971-12-24 Fuel metering device for internal combustion engines

Publications (1)

Publication Number Publication Date
US3845750A true US3845750A (en) 1974-11-05

Family

ID=5829184

Family Applications (1)

Application Number Title Priority Date Filing Date
US00318400A Expired - Lifetime US3845750A (en) 1971-12-24 1972-12-26 Fuel proportioning system for a combustion engine

Country Status (4)

Country Link
US (1) US3845750A (en)
FR (1) FR2170536A5 (en)
GB (1) GB1361359A (en)
IT (1) IT976189B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5359977A (en) * 1991-11-20 1994-11-01 Abbey Harold Fluidic metering system

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2447267A (en) * 1940-01-19 1948-08-17 Bendix Aviat Corp Fuel feeding system
US2591356A (en) * 1950-05-24 1952-04-01 Jr William L Howe Carbureting mechanism
US2899948A (en) * 1959-08-18 groves
US3650258A (en) * 1969-01-08 1972-03-21 Petrol Injection Ltd Fuel injection systems
US3688750A (en) * 1970-04-30 1972-09-05 Physics Int Co Mass flow metered fuel injection system

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2899948A (en) * 1959-08-18 groves
US2447267A (en) * 1940-01-19 1948-08-17 Bendix Aviat Corp Fuel feeding system
US2591356A (en) * 1950-05-24 1952-04-01 Jr William L Howe Carbureting mechanism
US3650258A (en) * 1969-01-08 1972-03-21 Petrol Injection Ltd Fuel injection systems
US3688750A (en) * 1970-04-30 1972-09-05 Physics Int Co Mass flow metered fuel injection system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5359977A (en) * 1991-11-20 1994-11-01 Abbey Harold Fluidic metering system

Also Published As

Publication number Publication date
FR2170536A5 (en) 1973-09-14
DE2164523A1 (en) 1973-01-11
GB1361359A (en) 1974-07-24
DE2164523B1 (en) 1973-01-11
IT976189B (en) 1974-08-20

Similar Documents

Publication Publication Date Title
US2996051A (en) Carburetor
SU545269A4 (en) Fuel injection device for internal combustion engine
US2957464A (en) Fuel injection system
US2382625A (en) Manifold injection carburetor
US3929114A (en) Fuel injector arrangement for compressive mixture internal combustion engines
US2905455A (en) Fuel supply
US4206735A (en) Mechanical throttle body injection apparatus
JPS5824622B2 (en) carburetor device
US3845750A (en) Fuel proportioning system for a combustion engine
US3967608A (en) Fuel feed devices for internal combustion engines
US3431900A (en) Fuel injection systems
US4090486A (en) Fuel injection system
GB680701A (en) Improvements in auxiliary charge regulating devices for internal combustion engines
US2447793A (en) Auxiliary charge regulating device
US2749898A (en) Fuel injection control
GB1478150A (en) Fuel supply control system for an internal combustion engine
US2548150A (en) Fuel and water system
US4341192A (en) Fuel injection system
US2552056A (en) Carburetor priming means
US4172436A (en) Carburation devices for internal combustion engines
US4326487A (en) Fuel injection system
US2882883A (en) Fuel induction system
GB1577412A (en) Arrangements for overcoming vapour lock in fuel injection systems
US2904026A (en) Fuel injection system
US4144858A (en) Fuel supply apparatus for an internal combustion engine