US3714934A - Fuel feed devices for internal combustion engines - Google Patents

Fuel feed devices for internal combustion engines Download PDF

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US3714934A
US3714934A US00178217A US3714934DA US3714934A US 3714934 A US3714934 A US 3714934A US 00178217 A US00178217 A US 00178217A US 3714934D A US3714934D A US 3714934DA US 3714934 A US3714934 A US 3714934A
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fuel
throttle member
increases
valve
inlet conduit
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US00178217A
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F Mennesson
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Societe Industrielle de Brevets et dEtudes SIBE
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Societe Industrielle de Brevets et dEtudes SIBE
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    • 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
    • F02M51/00Fuel-injection apparatus characterised by being operated electrically
    • F02M51/02Fuel-injection apparatus characterised by being operated electrically specially for low-pressure fuel-injection
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D2200/00Input parameters for engine control
    • F02D2200/02Input parameters for engine control the parameters being related to the engine
    • F02D2200/06Fuel or fuel supply system parameters
    • F02D2200/0606Fuel temperature

Definitions

  • the fuel is fed to the [51] Int Cl Fozm 51/02 1.
  • 39/00 valve by a fuel pump whose delivery circuit includes a [58] Fieid Aw 140 39 AF pressure regulator comprising a discharge valve con- ⁇ 23/1 19 trolled by the suction in the intake pipe of the engine. Variation of richness of the air/fuel mixture through temperature changes is compensated by a bimetallic [56] References Clted element coupled to the discharge valve.
  • the invention relates to fuel feed devices for internal combustion engines, of the type which comprise, on the one hand, in their inlet conduit, upstream of an principal throttle member actuated by the driver, an auxiliary throttle member which opens automatically and progressively in proportion as the air flow rate in the said conduit increases, on the other hand, means for injecting under pressure liquid fuel into the portion of this conduit situated downstream of the principal throttle member, and, on the other hand lastly, a metering system sensitive to the position of the auxiliary throttle member and adapted to regulate the flow-rate of the fuel injected in such a way that the richness of the air/fuel mixture passing into the inlet conduit is substantially constant, at least under certain conditions of operation of the engine, the abovesaid injection
  • the invention relates more particularly to those of the devices of the type concerned which have been described in applicants Pat. No. 3,543,739 and of which the above-said metering system comprises a member driven in continuous rotary movement and capable, by acting on the energization of the electromagnet, of determining over a fraction only of each of its revolutions the opening of the valve, the system being arranged so that it increases the said fraction in proportion as the opening of the auxiliary throttle member increases and vice-versa.
  • the invention relates more particularly again to those devices of the type concerned of which the source of fuel under pressure is constituted by a fuel pump in the delivery pipe of which acts a pressure regulator which comprises a relief valve tending to open under the effect of the delivery pressure of the pump and to close under the effect of the suction existing in the section of the inlet conduit comprised between its two throttle members, which suction is transmitted by a connecting passage to a diaphragm to which is coupled the relief valve.
  • the position of the auxiliary throttle member is characteristic of the flow-rate of the air passing from upstream to downstream of this member, provided that the density of the air is practically constant.
  • the fuel flow-rate through a calibrated orifice tends to increase if the temperature of this fuel increases as a result of the decrease in its viscosity.
  • An increase in ambient temperature, hence an increase in the temperature of the fuel, is manifested consequently, also, by an increase in fuel flow-rate.
  • the fuel supply device of the type defined above is characterized by the fact that an elastic element, deformable under the effect of the temperature variation, exerts on the discharge valve of the above-said pressure regulator a force directed in the sense of its closing which increases (in algebraic value) in proportion as the temperature drops.
  • the said element can be adjusted so that, for an average position of-the discharge valve, the force that it exerts is null for an average temperature range and tends to close the valve or to open it according as its temperature is below or above this temperature range. In this latter case, the force directed in the sense of closing is considered by convention asa negative force.
  • the fuel flow-rate is thus modified by acting on the injection pressure, so that the richness of the air/fuel mixture passing in the inlet conduit remains substantially constant, even for considerable variations in the air temperature.
  • FIG. 1 shows, in diagrammatic elevation with portions cut out, one embodiment of the fuel feed device constructed according to the invention
  • FIG. 2 shows a section along the line II-Il of FIG. 1.
  • the device As regards the whole, it is constituted in any suitable manner so that it comprises on the one hand, in its inlet conduit 1, upstream of a principal throttle member 2 actuated by the driver, an auxiliary throttle member 3 which opens automatically and progressively in proportion as the air flowrate in the conduit 1 increases, the direction of flow being indicated by the arrow F in FIG. 1
  • the auxiliary throttle member 3 is constituted by a butterfly-valve fixed on an axle 4.
  • This butterfly-valve is actuated by a pneumatic device comprising a diaphragm 5 separating two chambers 6 and 7 from one another.
  • the chamber 6 is connected by a passage 8 to a chamber 9 constituted by the section of the conduit 1 which is comprised between the principal throttle member 2 and the valve 3.
  • the axle 4 is rigidly fixed to a lever provided, at its free end, with a pin 11 which cooperates with the end of a rod 12, which is connected to the diaphragm 5.
  • Spring 13 tends constantly to close the valve 3 against the effect of the suction transmitted in the chamber 6.
  • the chamber 7 is placed at atmospheric pressure by passage 14 starting preferably from the air intake 15 of the conduit 1.
  • valve 3 corresponds to the air flow-rate which circulates in this conduit, as long as the density of the air remains practically constant.
  • the valve 3 could be replaced by equivalent throttle members, of which examples have been described in the abovesaid patent and its first certificate of addition.
  • the above-said injection means is constituted by source of fuel under pressure which will be described in more detail below and which the delivery circuit, opening into the conduit 1 downstream of the principal throttle member 2, is constrolled by at least one valve 16 actuated by an electromagnet 17.
  • the metering system comprises a flattened opaque disc 18 which is borne by a shaft 19, connected preferably to the internal combustion engine (not shown) supplied by the device, so that the disc is driven in a continuous movement of rotation around an axis perpendicular to its plane.
  • the disc 18 is interposed between a source of radiation, especially a light source 20 and a receiver such as a photodiode or a photoelectric cell 21, borne by a common support 22 connected to the auxiliary throttle member 3 and it is pierced by at least one aperture 23 adapted to allow the beam coming from source 20 to arrive at cell 21.
  • Cell 21 is arranged to control the energization the electromagnet 17 according as it is irradiated or not and the assembly is such that the electromagnet is energized over a fraction of each of the revolutions of disc 18 which varies in the same sense as the degree of opening of the throttle member 3.
  • the light source 20 may be constituted by a lamp which is adapted to be supplied by a battery 24 as soon as the ignition contact 25 of the engine is closed and which is arranged in a hollow boss 26 pierced by a hole. This hole is oriented in such a way as to direct a light beam onto the cell 21, through a hole passing through a hollow boss 27 wherein the said cell is lodged.
  • the bosses 26 and 27 are made to be carried by the ends of the U-shaped support 22 which straddles the disc 18 so that the source 20 and the cell 21 occur on each of the disc and which is rigidly fixed to the axle 4, the latter being parallel to the shaft 19 as well as to the light beam received by the cell 21.
  • an amplifying relay 28 To apply the currents generated in the cell 21, there is interposed between the latter and the electromagnet 17, an amplifying relay 28.
  • the internal combustion engine has several cylinders supplied by a valve 16 actuated by an individual electromagnet 17, all the electromagnets can be actuated simultaneously or a distributor 30 can be provided synchronized with the disc 18 to send successively intermittent energizing current into the various electromagnets, the disc possessing as many apertures 23 as cylinders to be supplied.
  • the apertures are distributed regularly around the shaft 19 and have each a shape such that the fraction of the revolution during which it normally permits the cell 21 to be illuminated increases in proportion as the throttle member 3 opens, that is to say (in the embodiment shown) in proportion as the bosses 26, 27 approach the shaft 19.
  • the throttle member 3 opens thereby driving the support 22 in the sense which brings closer together the shaft 19 and the bosses 26 and 27.
  • Each of the positions of the bosses corresponds to a different radius of the disc 18.
  • each aperture 23 Since the shape of each aperture 23 has been determined so that the fraction of a revolution, during which it allows to pass towards the cell 21 the light ray coming from the source 20 (creation of a current in the conductor 3l),.increases in proportion as the latter elements approach the shaft 19, it is insured that the fuel flow-rate delivered by each injection valve 16 varies in the same sense as the air flow-rate in conduit 1.
  • the source of liquid fuel under pressure is constituted by a fuel p mp of which the intake pipe 51 dips into a fuel reservoir 52 and on the delivery pipe 53 of which acts a pressure regulator 54.
  • a relief valve 55 tending to open under the effect of the delivery pressure of the pump and to close under the effect of the suction existing in the chamber 9, which suction is transmitted by a connecting passage 56 to a diaphragm 57 to which is coupled the valve 55 by a rod 58.
  • the valve 55 cooperates with a seat 59 which constitutes the'exit of a chamber 60 connected through a branch channel 61 to the delivery pipe 53.
  • the connecting passage 56 ends in a variable volume chamber 62 bounded by one surface of the diaphragm, the other surface being placed at atmospheric pressure for example through an orifice 63. The whole is such that the valve 55 opens as soon as the pressure in the pipe 53 exceeds a value determined by the surface of the diaphragm 57 and by the suction exerting on the latter.
  • a bimetallic strip 83 is fixed on the body of the regu? lator 54, the other end is coupled to the rod 58.
  • the strip 83 has a temperature which depends on that of the ambient air and of the fuel, due to the fact of thermal conduction in the regulator. lt-is arranged so that, on an increase in temperature, the bimetallic strip 83 has a tendency to open the valve 55.
  • the air flow-rate by weight passing in the inlet conduit 1 is greater or less according as the air temperature is higher or lower, and the fuel flow-rate is greater or less according as its temperature is higher or lower.
  • the bimetallic strip 83 serves to increase the fuel flow-rate if the temperature decreases and to reduce the fuel flow-rate if the temperature increases.
  • the effort of the bimetallic strip 83 is added to that exerted by the diaphragm 57 under the effect of the suction in the chamber 62 and tends to close the valve 55 a little more, which causes an increase in fuel pressure upstream of the injection orifice actuated by the valve 16, and consequently an increase in the flow-rate of the fuel in the inlet conduit 1.
  • This correction in the richness of the air/fuel mixture is all more effective as the air flow-rate in the conduit 1 is less, but in practice, this correction is not generally necessary for high air flow-rates.
  • the invention is in no way limited to those of its methods of application, nor to those of its methods of production of its various parts, which have been more especially indicated it encompasses, on the contrary, all variations.
  • the bimetallic strip 83 may be replaced by any other element, elastic and deformable under the effect of temperature variation.
  • Fuel feed device for an internal combustion engine, comprising in an inlet conduit, upstream of a principal throttle member adapted to be actuated by the operator, an auxiliary throttle member which opens automatically and progressively as the air-flow rate in said conduit increases, and means for injecting liquid fuel under pressure into the portion of this conduit situated downstream of the principal throttle member and, a metering system sensitive to the position of the auxiliary throttle member and adapted to regulate the flowrate of the fuel injected in such a way that the richness of the air/fuel mixture passing in the inlet conduit is substantially constant, at least for certain conditions of operation of the engine, the above-said injection means being constituted by a source of fuel under pressure of which the delivery circuit opening into the said portion of the inlet conduit is controlled by at least one valve actuated by an electromagnet, the metering system comprising a member driven in a movement of continuous rotation and capable, by acting on the energization of the electromagnet, of determining over a fraction only of each of these revolutions, the opening of the valve
  • Fuel feed device according to claim 1, wherein said elastic element is adjusted in such a way that, for an average position of the relief valve, the force that it exerts is nil for an average temperature range and tends to close the valve or to open it according as its temperature is respectively below or above said temperature range.

Abstract

Valves supplied from a source of fuel under pressure are each actuated by an electromagnet energized over a variable fraction of each revolution of a rotary member driven by the engine. The energizing current is governed by a light source which illuminates a photo-sensitive element according to the position of an intermediate rotary member. The fuel is fed to the valve by a fuel pump whose delivery circuit includes a pressure regulator comprising a discharge valve controlled by the suction in the intake pipe of the engine. Variation of richness of the air/fuel mixture through temperature changes is compensated by a bimetallic element coupled to the discharge valve.

Description

United States Patent Mennesson 1 5] Feb. 6, 1973 541 FUEL FEED DEVICES FOR INTERNAL 2,921,569 1/1960 Gold ..123 140 MC COMBUSTION ENGINES 2,876,758 3/1959 Armstrong ..l23/l79 A 2,161,743 6/[939 Heinrich et'al... ..l23/l40 MC [75] Inv n or: Francois Menness'on, 92 Nanterr 3.620.202 11 1971 Ross ..123 119 R X France [73] Assigncc: Societe lndustrielle de Brevets ct f 'i smith dEmdes SDI'BE. Ncumy sur scinc ASSISIHNI bxammer-Denms Toth France A/mrney-Stevens, Davis, Miller & Mosher [22] Filed: Sept. 7, 1971 [57] ABSTRACT 21 1 NO l782l7 Valves supphed from a source of fuel under pressure are each actuated by an electromagnet energized over [30] Foreign Application Priority Data a variable fraction of each revolution of a rotary member driven by the engine. The energizing current Sept. 15, 1970 France ..703345l is governed y a light Source which illuminates a photo-sensitive element according to the position of [52] Cl "123/139 k fi g an intermediate rotary member. The fuel is fed to the [51] Int Cl Fozm 51/02 1. 39/00 valve by a fuel pump whose delivery circuit includes a [58] Fieid Aw 140 39 AF pressure regulator comprising a discharge valve con- {23/1 19 trolled by the suction in the intake pipe of the engine. Variation of richness of the air/fuel mixture through temperature changes is compensated by a bimetallic [56] References Clted element coupled to the discharge valve.
UNITED STATES PATENTS 3,596,645 8/1971 Mennesson ..123 139 AW 2 Clams 2 D'awmg figures 3.714.934 SHEET 10F 2 PATENTED FEB 6 I975 FUEL FEED DEVICES FOR INTERNAL COMBUSTION ENGINES The invention relates to fuel feed devices for internal combustion engines, of the type which comprise, on the one hand, in their inlet conduit, upstream of an principal throttle member actuated by the driver, an auxiliary throttle member which opens automatically and progressively in proportion as the air flow rate in the said conduit increases, on the other hand, means for injecting under pressure liquid fuel into the portion of this conduit situated downstream of the principal throttle member, and, on the other hand lastly, a metering system sensitive to the position of the auxiliary throttle member and adapted to regulate the flow-rate of the fuel injected in such a way that the richness of the air/fuel mixture passing into the inlet conduit is substantially constant, at least under certain conditions of operation of the engine, the abovesaid injection means being constituted by a source of fuel under pressure whose delivery circuit, opening into the above-said portion of the inlet conduit, is controlled by at least one valve actuated by an electromagnet.
The invention relates more particularly to those of the devices of the type concerned which have been described in applicants Pat. No. 3,543,739 and of which the above-said metering system comprises a member driven in continuous rotary movement and capable, by acting on the energization of the electromagnet, of determining over a fraction only of each of its revolutions the opening of the valve, the system being arranged so that it increases the said fraction in proportion as the opening of the auxiliary throttle member increases and vice-versa.
The invention relates more particularly again to those devices of the type concerned of which the source of fuel under pressure is constituted by a fuel pump in the delivery pipe of which acts a pressure regulator which comprises a relief valve tending to open under the effect of the delivery pressure of the pump and to close under the effect of the suction existing in the section of the inlet conduit comprised between its two throttle members, which suction is transmitted by a connecting passage to a diaphragm to which is coupled the relief valve.
Of course the position of the auxiliary throttle member is characteristic of the flow-rate of the air passing from upstream to downstream of this member, provided that the density of the air is practically constant.
However, for large variations of temperature of the air, the variation of its density becomes important and the position of the auxiliary throttle member no longer gives accurate indication of the air flow-rate in terms of mass passing from upstream to downstream of this throttle member. In fact, for a given position of'the latter and hence for an identical fuel flow-rate (provided that the temperature of the latter is constant), the air flow-rate in terms of mass passing from upstream to downstream of the auxiliary throttle member is all the greater as the air temperature is lower.
Additionally, the fuel flow-rate through a calibrated orifice tends to increase if the temperature of this fuel increases as a result of the decrease in its viscosity. An increase in ambient temperature, hence an increase in the temperature of the fuel, is manifested consequently, also, by an increase in fuel flow-rate.
As a result, at low ambient temperatures, the richness of the air/fuel mixture passing in the inlet conduit is too weak and, on the other hand, at high temperatures, the richness of the mixture is too strong.
With the object of overcoming this drawback, the fuel supply device of the type defined above is characterized by the fact that an elastic element, deformable under the effect of the temperature variation, exerts on the discharge valve of the above-said pressure regulator a force directed in the sense of its closing which increases (in algebraic value) in proportion as the temperature drops. The said element can be adjusted so that, for an average position of-the discharge valve, the force that it exerts is null for an average temperature range and tends to close the valve or to open it according as its temperature is below or above this temperature range. In this latter case, the force directed in the sense of closing is considered by convention asa negative force.
The fuel flow-rate is thus modified by acting on the injection pressure, so that the richness of the air/fuel mixture passing in the inlet conduit remains substantially constant, even for considerable variations in the air temperature.
The invention will, in any case, be well understood by means of the following complementary description, as well as from the accompanying drawings, which complementary description and drawings relate to a preferred embodiment, given purely by way of illustrative and non-limiting example.
In these drawings,
FIG. 1 shows, in diagrammatic elevation with portions cut out, one embodiment of the fuel feed device constructed according to the invention FIG. 2 shows a section along the line II-Il of FIG. 1.
According to the invention, and more particularly according to that of its methods of application, as well as according to those of its methods of production of the various parts, to which it would appear that preference should be given, in order to contruct a fuel feed device for automobile engines or the like, procedure is as follows.
As regards the device as the whole, it is constituted in any suitable manner so that it comprises on the one hand, in its inlet conduit 1, upstream of a principal throttle member 2 actuated by the driver, an auxiliary throttle member 3 which opens automatically and progressively in proportion as the air flowrate in the conduit 1 increases, the direction of flow being indicated by the arrow F in FIG. 1
on the other hand, means for injecting under pressure liquid fuel into the portion of the conduit 1 situated downstream of the principal throttle member 2 on the other hand, lastly, a metering system sensitive to the position of the auxiliary throttle member 3 and adapted to regulate the flow-rate of injected fuel in such a way that the richness of the air/fuel mixture passing in the conduit 1 is substantially constant, at least for certain conditions of operation of the engine.
In the embodiment shown, the auxiliary throttle member 3 is constituted by a butterfly-valve fixed on an axle 4. This butterfly-valve is actuated by a pneumatic device comprising a diaphragm 5 separating two chambers 6 and 7 from one another. The chamber 6 is connected by a passage 8 to a chamber 9 constituted by the section of the conduit 1 which is comprised between the principal throttle member 2 and the valve 3. The axle 4 is rigidly fixed to a lever provided, at its free end, with a pin 11 which cooperates with the end of a rod 12, which is connected to the diaphragm 5. Spring 13 tends constantly to close the valve 3 against the effect of the suction transmitted in the chamber 6. The chamber 7 is placed at atmospheric pressure by passage 14 starting preferably from the air intake 15 of the conduit 1.
Of course the angular position adopted at any moment inside the conduit 1 by the valve 3 corresponds to the air flow-rate which circulates in this conduit, as long as the density of the air remains practically constant. The greater the air flow-rate the more the valve 3 opens, a substantially constant suction (or varying according to the characteristics of the spring 13) being established in the chamber 9 comprised between the two throttle members 2 and 3. The valve 3 could be replaced by equivalent throttle members, of which examples have been described in the abovesaid patent and its first certificate of addition.
The above-said injection means is constituted by source of fuel under pressure which will be described in more detail below and which the delivery circuit, opening into the conduit 1 downstream of the principal throttle member 2, is constrolled by at least one valve 16 actuated by an electromagnet 17.
The metering system comprises a flattened opaque disc 18 which is borne by a shaft 19, connected preferably to the internal combustion engine (not shown) supplied by the device, so that the disc is driven in a continuous movement of rotation around an axis perpendicular to its plane. The disc 18 is interposed between a source of radiation, especially a light source 20 and a receiver such as a photodiode or a photoelectric cell 21, borne by a common support 22 connected to the auxiliary throttle member 3 and it is pierced by at least one aperture 23 adapted to allow the beam coming from source 20 to arrive at cell 21. Cell 21 is arranged to control the energization the electromagnet 17 according as it is irradiated or not and the assembly is such that the electromagnet is energized over a fraction of each of the revolutions of disc 18 which varies in the same sense as the degree of opening of the throttle member 3.
The light source 20 may be constituted by a lamp which is adapted to be supplied by a battery 24 as soon as the ignition contact 25 of the engine is closed and which is arranged in a hollow boss 26 pierced by a hole. This hole is oriented in such a way as to direct a light beam onto the cell 21, through a hole passing through a hollow boss 27 wherein the said cell is lodged. in the embodiment shown, the bosses 26 and 27 are made to be carried by the ends of the U-shaped support 22 which straddles the disc 18 so that the source 20 and the cell 21 occur on each of the disc and which is rigidly fixed to the axle 4, the latter being parallel to the shaft 19 as well as to the light beam received by the cell 21.
To apply the currents generated in the cell 21, there is interposed between the latter and the electromagnet 17, an amplifying relay 28.
When the internal combustion engine has several cylinders supplied by a valve 16 actuated by an individual electromagnet 17, all the electromagnets can be actuated simultaneously or a distributor 30 can be provided synchronized with the disc 18 to send successively intermittent energizing current into the various electromagnets, the disc possessing as many apertures 23 as cylinders to be supplied. The apertures are distributed regularly around the shaft 19 and have each a shape such that the fraction of the revolution during which it normally permits the cell 21 to be illuminated increases in proportion as the throttle member 3 opens, that is to say (in the embodiment shown) in proportion as the bosses 26, 27 approach the shaft 19.
Of course the fuel feed device which has just been described operates as follows.
In proportion as the air flow-rate in the conduit 1 increases, the throttle member 3 opens thereby driving the support 22 in the sense which brings closer together the shaft 19 and the bosses 26 and 27. Each of the positions of the bosses corresponds to a different radius of the disc 18.
Since the shape of each aperture 23 has been determined so that the fraction of a revolution, during which it allows to pass towards the cell 21 the light ray coming from the source 20 (creation of a current in the conductor 3l),.increases in proportion as the latter elements approach the shaft 19, it is insured that the fuel flow-rate delivered by each injection valve 16 varies in the same sense as the air flow-rate in conduit 1.
This being so the source of liquid fuel under pressure is constituted by a fuel p mp of which the intake pipe 51 dips into a fuel reservoir 52 and on the delivery pipe 53 of which acts a pressure regulator 54. The
latter comprises a relief valve 55 tending to open under the effect of the delivery pressure of the pump and to close under the effect of the suction existing in the chamber 9, which suction is transmitted by a connecting passage 56 to a diaphragm 57 to which is coupled the valve 55 by a rod 58. The valve 55 cooperates with a seat 59 which constitutes the'exit of a chamber 60 connected through a branch channel 61 to the delivery pipe 53. The connecting passage 56 ends in a variable volume chamber 62 bounded by one surface of the diaphragm, the other surface being placed at atmospheric pressure for example through an orifice 63. The whole is such that the valve 55 opens as soon as the pressure in the pipe 53 exceeds a value determined by the surface of the diaphragm 57 and by the suction exerting on the latter.
According to the invention, recourse is had to an element, elastic and deformable under the effect of temperature variation, such that a bimetallic strip 83. One of the ends of this strip is fixed on the body of the regu? lator 54, the other end is coupled to the rod 58. Thus positioned, the strip 83 has a temperature which depends on that of the ambient air and of the fuel, due to the fact of thermal conduction in the regulator. lt-is arranged so that, on an increase in temperature, the bimetallic strip 83 has a tendency to open the valve 55.
The operation of the regulator according to the present improvement is as follows As explained above, for a same position of the auxiliary throttle member 3, the air flow-rate by weight passing in the inlet conduit 1 is greater or less according as the air temperature is higher or lower, and the fuel flow-rate is greater or less according as its temperature is higher or lower. To maintain an approximately constant air/fuel mixture richness, the bimetallic strip 83 serves to increase the fuel flow-rate if the temperature decreases and to reduce the fuel flow-rate if the temperature increases.
In fact, for a drop in temperature, the effort of the bimetallic strip 83 is added to that exerted by the diaphragm 57 under the effect of the suction in the chamber 62 and tends to close the valve 55 a little more, which causes an increase in fuel pressure upstream of the injection orifice actuated by the valve 16, and consequently an increase in the flow-rate of the fuel in the inlet conduit 1.
A reverse effect is obtained for an increase of temperature.
This correction in the richness of the air/fuel mixture is all more effective as the air flow-rate in the conduit 1 is less, but in practice, this correction is not generally necessary for high air flow-rates.
As is self-evident, and as emerges already from the foregoing, the invention is in no way limited to those of its methods of application, nor to those of its methods of production of its various parts, which have been more especially indicated it encompasses, on the contrary, all variations. In particular, the bimetallic strip 83 may be replaced by any other element, elastic and deformable under the effect of temperature variation.
1 claim 1. Fuel feed device, for an internal combustion engine, comprising in an inlet conduit, upstream ofa principal throttle member adapted to be actuated by the operator, an auxiliary throttle member which opens automatically and progressively as the air-flow rate in said conduit increases, and means for injecting liquid fuel under pressure into the portion of this conduit situated downstream of the principal throttle member and, a metering system sensitive to the position of the auxiliary throttle member and adapted to regulate the flowrate of the fuel injected in such a way that the richness of the air/fuel mixture passing in the inlet conduit is substantially constant, at least for certain conditions of operation of the engine, the above-said injection means being constituted by a source of fuel under pressure of which the delivery circuit opening into the said portion of the inlet conduit is controlled by at least one valve actuated by an electromagnet, the metering system comprising a member driven in a movement of continuous rotation and capable, by acting on the energization of the electromagnet, of determining over a fraction only of each of these revolutions, the opening of the valve, said system being arranged so that it increases the said fraction in proportion as the opening of the auxiliary throttle member increases and vice-versa, the said source of fuel under pressure being constituted by a fuel pump in whose delivery circuit acts a pressure regulator which comprises a relief valve tending to open under the action of the delivery pressure of the pump and to close under the action of the suction existing in the section of the inlet conduit comprised between its two throttle members, which suction is transmitted through a connecting passage to a diaphragm to which the relief valve is coupled, characterized by the fact that an elastic element which engages said relief valve and is deformable under the effect of the variation of temperature, is arranged to exert on said relief valve, a force directed in the sense of its closing which increases (in algebraic value) in proportion as the temperature decreases.
2. Fuel feed device according to claim 1, wherein said elastic element is adjusted in such a way that, for an average position of the relief valve, the force that it exerts is nil for an average temperature range and tends to close the valve or to open it according as its temperature is respectively below or above said temperature range.

Claims (2)

1. Fuel feed device, for an internal combustion engine, comprising in an inlet conduit, upstream of a principal throttle member adapted to be actuated by the operator, an auxiliary throttle member which opens automatically and progressively as the air-flow rate in said conduit increases, and means for injecting liquid fuel under pressure into the portion of this conduit situated downstream of the principal throttle member and, a metering system sensitive to the position of the auxiliary throttle member and adapted to regulate the flow-rate of the fuel injected in such a way that the richness of the air/fuel mixture passing in the inlet conduit is substantially constant, at least for certain conditions of operation of the engine, the above-said injection means being constituted by a source of fuel under pressure of which the delivery circuit opening into the said portion of the inlet conduit is controlled by at least one valve actuated by an electromagnet, the metering system comprising a member driven in a movement of continuous rotation and capable, by acting on the energization of the electromagnet, of determining over a fraction only of each of these revolutions, the opening of the valve, said system being arranged so that it increases the said fraction in proportion as the opening of the auxiliary throttle member increases and vice-versa, the said source of fuel under pressure being constituted by a fuel pump in whose delivery circuit acts a pressure regulator which comprises a relief valve tending to open under the action of the delivery pressure of the pump and to close under the action of the suction existing in the section of the inlet conduit comprised between its two throttle members, which suction is transmitted through a connecting passage to a diaphragm to which the relief valve is coupled, characterized by the fact that an elastic element which engages said relief valve and is deformable under the effect of the variation of temperature, is arranged to exert on said relief valve, a force directed in the sense of its closing which increases (in algebraic value) in proportion as the temperature decreases.
1. Fuel feed device, for an internal combustion engine, comprising in an inlet conduit, upstream of a principal throttle member adapted to be actuated by the operator, an auxiliary throttle member which opens automatically and progressively as the air-flow rate in said conduit increases, and means for injecting liquid fuel under pressure into the portion of this conduit situated downstream of the principal throttle member and, a metering system sensitive to the position of the auxiliary throttle member and adapted to regulate the flow-rate of the fuel injected in such a way that the richness of the air/fuel mixture passing in the inlet conduit is substantially constant, at least for certain conditions of operation of the engine, the above-said injection means being constituted by a source of fuel under pressure of which the delivery circuit opening into the said portion of the inlet conduit is controlled by at least one valve actuated by an electromagnet, the metering system comprising a member driven in a movement of continuous rotation and capable, by acting on the energization of the electromagnet, of determining over a fraction only of each of these revolutions, the opening of the valve, said system being arranged so that it increases the said fraction in proportion as the opening of the auxiliary throttle member increases and vice-versa, the said source of fuel under pressure being constituted by a fuel pump in whose delivery circuit acts a pressure regulator which comprises a relief valve tending to open under the action of the delivery pressure of the pump and to close under the action of the suction existing in the section of the inlet conduit comprised between its two throttle members, which suction is transmitted through a connecting passage to a diaphragm to which the relief valve is coupled, characterized by the fact that an elastic element which engages said relief valve and is deformable under the effect of the variation of temperature, is arranged to exert on said relief valve, a force directed in the sense of its closing which increases (in algebraic value) in proportion as the temperature decreases.
US00178217A 1970-09-15 1971-09-07 Fuel feed devices for internal combustion engines Expired - Lifetime US3714934A (en)

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FR7033451A FR2105638A6 (en) 1970-09-15 1970-09-15

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US (1) US3714934A (en)
JP (1) JPS5118015B1 (en)
BR (1) BR7104687D0 (en)
DE (1) DE2129443A1 (en)
ES (1) ES392037A1 (en)
FR (1) FR2105638A6 (en)
GB (1) GB1333961A (en)
IT (1) IT1045057B (en)
SE (1) SE360708B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4098235A (en) * 1974-08-28 1978-07-04 Repco Research Proprietary Limited Fuel feed control apparatus and system
US5337718A (en) * 1992-06-02 1994-08-16 Walbro Corporation Electronic fuel injection system with heat-pressure response

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2161743A (en) * 1936-09-07 1939-06-06 Bosch Gmbh Robert Control means for the fuel supply of internal combustion engines
US2876758A (en) * 1956-11-19 1959-03-10 Acf Ind Inc Starter controlled priming system for a fuel injection operated internal combustion engine
US2921569A (en) * 1957-12-27 1960-01-19 Gold Harold Fuel injection system
US3596645A (en) * 1968-12-12 1971-08-03 Sibe Fuel feed devices for internal-combustion engines
US3620202A (en) * 1968-12-17 1971-11-16 Zenith Carburetter Co Ltd Fuel supply devices for cold starting of internal combustion engines

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2161743A (en) * 1936-09-07 1939-06-06 Bosch Gmbh Robert Control means for the fuel supply of internal combustion engines
US2876758A (en) * 1956-11-19 1959-03-10 Acf Ind Inc Starter controlled priming system for a fuel injection operated internal combustion engine
US2921569A (en) * 1957-12-27 1960-01-19 Gold Harold Fuel injection system
US3596645A (en) * 1968-12-12 1971-08-03 Sibe Fuel feed devices for internal-combustion engines
US3620202A (en) * 1968-12-17 1971-11-16 Zenith Carburetter Co Ltd Fuel supply devices for cold starting of internal combustion engines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4098235A (en) * 1974-08-28 1978-07-04 Repco Research Proprietary Limited Fuel feed control apparatus and system
US5337718A (en) * 1992-06-02 1994-08-16 Walbro Corporation Electronic fuel injection system with heat-pressure response

Also Published As

Publication number Publication date
FR2105638A6 (en) 1972-04-28
GB1333961A (en) 1973-10-17
AU3309271A (en) 1973-03-08
JPS5118015B1 (en) 1976-06-07
DE2129443A1 (en) 1972-03-23
ES392037A1 (en) 1973-08-16
BR7104687D0 (en) 1973-02-20
SE360708B (en) 1973-10-01
IT1045057B (en) 1980-05-10

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