US2746443A - Fuel injection pump - Google Patents

Fuel injection pump Download PDF

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US2746443A
US2746443A US338043A US33804353A US2746443A US 2746443 A US2746443 A US 2746443A US 338043 A US338043 A US 338043A US 33804353 A US33804353 A US 33804353A US 2746443 A US2746443 A US 2746443A
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fuel
plunger
pump
pumping chamber
ports
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US338043A
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Wolfgang E Meyer
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Texaco Inc
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Texaco Inc
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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
    • F02M41/00Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor
    • F02M41/08Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined
    • F02M41/10Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined pump pistons acting as the distributor
    • F02M41/12Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined pump pistons acting as the distributor the pistons rotating to act as the distributor
    • F02M41/123Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined pump pistons acting as the distributor the pistons rotating to act as the distributor characterised by means for varying fuel delivery or injection timing
    • F02M41/125Variably-timed valves controlling fuel passages
    • F02M41/126Variably-timed valves controlling fuel passages valves being mechanically or electrically adjustable sleeves slidably mounted on rotary piston

Definitions

  • the present invention relates to fuel injection pumps for internal combustion engines and particularly to an improved fuel-injection pump of the type wherein a single reciprocating and rotating pumping plunger serves a plurality of engine cylinders.
  • the conventional delivery valve has the disadvantage. that the valve itself requires space in which @to be housed, which space further adds to the compressible volume of the fuel discharge path and increases its elasticity. Also, by immediately closing in response to the reduction in pump output pressure which is intended to terminate fuel injection, the delivery valve blocks the fuel discharge path at its pump end and provides a reflecting surface for pressure waves in the discharge path which usually accompany termination of fuel injection. The reflection of such pressure waves increases the likelihood of secondary or after-injections into the engine and thus-renders more difiicult precise control of timing and duration of fuel injection.
  • the present invention provides a fuel injection pump of the type in which a single reciprocating and rotating plunger serves a plurality of engine cylinders, and from which :the conventional delivery valve is completely elimi-.
  • the compressibility of the fuel "tends to permit absorption of the fuel charge from the pump into the fuel discharge path without any corresponding displacement of 'fuel'through the fuel injector and 'into the engine. This may result in actual fuel delivery to the engine of only aportion of the desired fuel charge. Also, -this elasticity of the system produces an unpredictable delay between the desired beginning .and ending I of fuel injection, as controlled by starting and stopping of pumping 'in the fuel pump, and actual beginning and ending of fuelinjectionat the injector.
  • the fuel delivery valve also serves the .useful purpose .of isolating the fuel discharge path from thepump during the suction stroke of the pumping plunger. This prevents the rapid expansion of volume within the pumping chamber of the fuel pump from creating a vacuum in Because fuel vapor thus rupts the timing and accuracy of fuel metering.
  • An object of this invention therefore is to provide an improved fuel injection pump for'use -with internal com- :bustion engines, in which a single plunger is reciprocated and continuously rotated :for pumping and metering the ,fuel and fordistr-ibuting it to more than one engine cylinder.
  • Another object is to provide a fuel injection pump of the aforesaid type in which the conventional fuel pressure-actuated delivery valve is eliminated.
  • Another .object is to provide a fuel injection pump of the aforesaid type in which the path provided for the discharge of-fuel from'the pumping chamber to the engine is greatly simplified and substantially reduced in volume.
  • Another object is to provide a fuel pump of the aforesaid type in which vacuum formation or fuel vaporization in the fuel discharge path during the suction stroke of the pumping plunger is prevented.
  • Another object is to provide a fuel pump of the aforesaid type having an improved degree .of precision of meter-
  • Another object is to provide a fuel pump of the aforesaid type, which is particularly suited for metering fuel to engines operating at relatively high speeds.
  • Another object is to provide a fuel injection pump of the aforesaid type in which vacuum formation in the pumping chamber during the suction stroke of the pump plunger is eliminated.
  • Another object is to provide a fuel injection pump of the aforesaid type in which the beginning and the end of fuel injection can be varied independently of each other.
  • Another object is to provide a fuel injection pump of the aforesaid type in which the entire fuel discharge path from the pump is maintained in continuous fluid fuel contact with a low pressure fuel reservoir during the termination of fuel injection pressure in said discharge path, so that pressure waves in said fuel discharge path arising from abrupt termination of fuel injection pressure are substantially damped out in said reservoir without reflection, and secondary fuel injections are thereby eliminated.
  • Another object is to provide an improved fuel pump of the aforesaid type having a reduced number of parts of simplified design which can be manufactured with greater ease and at reduced cost.
  • Fig. 1 is a longitudinal sectional view of a pump constructed in accordance with the present invention and showing the plunger in an intermediate portion of its stroke.
  • Fig. 2 is an enlarged view of a portion of Fig. 1.
  • Fig. 3 is an enlarged sectional view of the portion of the pump shown in Fig. 2, taken on the line 3-3 of Fig. 2.
  • Fig. 4 is an enlarged sectional view of the portion of the pump shown in Fig. 2, taken on the line 4-4 of Fig. 2.
  • Fig. 5 is an enlarged sectional view of the portion of the pump shown in Fig. 2, taken on the line 55 of Fig. 2.
  • Fig. 6 is an enlarged cut-away perspective view of that portion of the pump shown in Fig. 2,. the portion cut away being defined by the line 66 in Figs. 3 and 4.
  • a single plunger fuel injection pump constructed in accordance with the present invention is shown by way of example as adapted to serve a four-cylinder engine.
  • the pump includes a housing 1 containing a body member 3 provided with a cylindrical bore 5 which is enlarged adjacent one end to form a fuel sump 7. Slidably fitted within the bore 5 is a cylindrical pumping plunger 9 adapted for reciprocation and simultaneous rotation therein in timed relation with the engine for which the pump supplies fuel.
  • an engine-driven cam shaft 11 supported in housing 1 and carrying a cam 13 which cooperates with a tappet roller 15 rotatably mounted in a tappet 17.
  • the tappet 17 is adapted to reciprocate within a bore 19 of housing 1 in coaxial alignment with the bore 5 in the body member 3.
  • One end of plunger 9 is maintained in continuous contact with reciprocating tappet 17 by means of compression springs 21 and 23 acting against a spring retainer 25 supported from the end of the plunger by the usual split collar 27.
  • springs 21 and 23 are restrained by a plunger rotation gear 31 which is keyed to plunger 9 intermediate its length and which is adapted to bear against a surface 29 of the body member 3 while rotating.
  • a pinion 33 connected in driving relation with gear 31 is driven through a shaft 35 from a helical gear 37 mounted on cam shaft 11.
  • the bore 5 is permanently closed during operation of the pump, as by a plug 41.
  • Plunger 9 forms with cylindrical bore 5 at this permanently closed end thereof a pumping chamber 43.
  • fuel is admitted to pumping chamber 43 for compression therein to the high pressures suitable for delivery to the conventional engine fuel injection equipment, and discharged therefrom at a selected time in the engine cycle and in accurately metered amount.
  • cam 13 and cam shaft 11 are arranged to reciprocate plunger 9 through two complete cycles, consisting of two compression and two suction strokes, during one engine crankshaft revolution.
  • cam 13 is provided with two lobes
  • cam shaft 11 should turn at engine speed for a four-stroke cycle four cylinder engine. This could also be accomplished by providing cam 13 with four lobes and turning cam shaft 11 at one half engine speed. If the four-cylinder engine is of the two-stroke cycle type and cam shaft 11 turns at engine speed, cam 13 should have four lobes.
  • the ratio of the plunger rotating gear 31 and its driving pinion 33 should be such that plunger 9 completes one full revolution during four-pumping strokes for four-cylinder engine operation on either a two or four stroke cycle. That is, the plunger should rotate from the time it leaves its bottom dead center position on a compression stroke until it returns to bottom dead center after completing its suction stroke.
  • Body member 3 is provided with a plurality of fuel distributor ports 51, 52, 53, 54 (only two of which are shown in Fig. 1), one for each engine cylinder, which communicate with the cylindrical bore 5 at points preferably equally spaced about a circumference in a crosssectional plane thereof.
  • a fuel delivery line 55, 56, 57, 58 which conveys fuel to a particular engine cylinder fuel injection device.
  • Distributor ports 51, 52, 53, 54 are so located along cylindrical bore 5 as to be covered by plunger 9 during the whole of its reciprocating stroke.
  • plunger 9 is provided with a longitudinal fuel distributor slot 61 which is of a sufficient length to intersect the plane of the distributor ports during the entire reciprocating stroke of the plunger.
  • distributor slot 61 has a width in relation to the size of ports 51, 52, etc., suflicient to uncover a distributor port during substantially 45 of rotation of plunger 9.
  • Body member 3 is also provided with a plurality of fuel supply ports 71, 72, 75, 76 communicating with cylindrical bore 5 at points along its length between sump 7 and distributor ports 51, 52, 53, 54. These fuel supply ports 71, 72, etc., are connected through a fuel supply passage 45, in body member 3 to any desired source of low-pressure fuel, not shown. Sump 7 is also supplied with low pressure fuel through a connection 49 in body member 3 to fuel supply passage 45. Together sump 7 and the fuel supply passage 45 provide a low pressure fuel reservoir from which the pumping chamber 43 can be charged with fuel as the pump operates.
  • en arge -Fuel supply ports 71, 72, etc. are located .alo ngcylindrical bore 'sufficiently far from its closed end so that none of these ports will be uncovered by distributor slot 61 of plunger 9 during'any point in the plunger suct'ion stroke, regardless of the rotative position of the Plunger 9 is provided also with a longitudinal fuel by-pass passage 63 which opens into pumping chamber 43, and is of'sufiicient length within plunger 9 to extend into that portion of the plunger surrounded by fuel sump 7. At its fuel sump end the by-pass passage 63-is connected to the fuel sump 7 through two longitudinally spaced upper and lower control ports 81, 82 in plunger '9.
  • Control ports 81 and 82 are preferably aligned in the axial plane through'the plunger which bisects the distributor slot 61,'their longitudinal location and spacing preferably being suchthat these ports will be confined Within fuel sump 7 during the entire plunger excursion. Also provided within sump 7 are a pair of control sleeves 91, 92 which surround the plunger 9 with a close sliding fit. Control sleeves 91, 92 are slotted to receive pins 101, 162, respectively, which are eccentrically mountedion shafts 103, 104 supported in body member 3 for rotation by suitable means external to the pump, such ashand controls 105, 106, or any desired engine condition-responsive device.
  • control sleeves 91, 92 can be adjustably positioned along the plunger to cover the upper and lower control ports 81, 82, during any selected portion of the plunger compression stroke, and thereby prevent fuel flow between pumping chamber 43 and fuel sump 7.
  • Each control sleeve 9 1, 92 can be manipulated independently of the other,
  • plunger 9 is additionally provided with two fuel fill ports '73, 74, connecting to the longitudinal fuel by-pass passage 63.
  • Fill ports 73, '74 are disposed preferably on a common plunger diameter and inthe plunger axial plane of con- 1 trol ports 81, 82 and are so arranged as to uncover and come into fluid fuel contact with fuel supply ports 71, 72, etc., during certain portions of the plunger suction stroke, as will be explained more fully hereinafter.
  • Plunger 9 begins its excursion from an initial position at bottom dead center, and with a rotative orientation at which one of the distributor ports,
  • Plunger .9 continues 'to rotate while ascending, and by the time it reaches top dead center position, it has rotated a sufiicient extent so that fluid fuel contact has just .been broken between port 51 and distributor slot 61.
  • distributor port "51” is isolated from pumping chamber 43, and any tendency toward creationof a vacuum in the expanding volume of pumping chamber 43 is not communicated through port 51.to the fuel discharge path.
  • the width of slot .61 in relation to the size of distributor ports. 51 52, 53, and 54 is such that, during the entire angu 'lar rotation of plunger 9 while on its suction stroke, slot 61 does not .uncover the next succeeding distributor ,port52, but .as plunger 9 reaches bottom dead center the nearest edge of slot 61 is just about to be rotated into uncovering relationship with distributor port .52.
  • plunger 9 is rotated continuously in one direction and at constant speed by driving gear 31.
  • the plunger should complete one fourth of a full rotation, i. e., 90", during the period of one complete reciprocating excursion. Since plunger 9 rotates at constant speed, the proportion of its 90 rotation which accompanies its compression stroke, relative to the proportion of its 90 rotation which accompanies its suction stroke, will be determined by the profile of the lobe of cam 13. If the cam lobe is symmetrical, for example, 45 of plunger rotation will accompany its compression stroke and 45 will accompany its suction stroke.
  • the plunger will be returned on its suction stroke during a relatively small fraction of the total excursion time, with a correspondingly small amount of rotation.
  • the shape of the cam profile is a factor which affects the disposition of fuel supply ports 71, 72, 75, 76 relative to cylindrical bore 5.
  • the shape and size of the supply ports 71, 72, 75, 76, as well as fill ports 73, 74 may be varied as desired and as necessary to maintain fluid contact therebetween during the period above described, and the relative size and shape of the ports shown in the drawing is merely exemplary of one operative arrangement.
  • pumping chamber 43 is at no time out of fluid fuel contact with a source of low pressure fuel, either through fill ports 73, 74 or'through upper or lower control ports 81, 82. This completely eliminates the possibility of fuel vaporization due to vacuum formation in pumping chamber 43.
  • the two control sleeves 91 and 92 can be moved independently, the distance between them may be varied.
  • simultaneously raising upper control sleeve 91 and lowering lower control sleeve 92 delays the beginning of fuel discharge from pumping chamber 43, and also hastens its termination, thereby shortening the effective pumping stroke of the plunger.
  • bringing the two control sleeves 91 and 92 closer together lengthens the period in the plunger compression stroke during which fuel discharge takes place from pumping chamber 43.
  • upper and lower control sleeves 91 and 92 may be brought together until they are in contact and form one continuous enclosure about the control ports.
  • Pumps constructed in accordance with the present invention are moreover characterized by greatly simplified internal fuel fiow passages as well as provision for simple and effective control of the beginning and termination of effective pumping, thereby providing a pump which is less expensive to manufacture, and which enables precision control of fuel injection over a wide range of operating conditions.
  • a body having a bore therein closed at one end and enlarged at the other end to form a fuel sump, a plunger adapted to reciprocate and rotate in said bore and forming at the .closed end of said bore a pumping chamber, means for reciprocating and simultaneously continuously rotating said plunger in said bore, said fuel sump enclosini a portion of said plunger during the whole of said reciprocation thereof, a fuel passage in said plunger communicating with said pumping chamber, a plurality of control port means in said portion of said plunger enclosed within said fuel sump connected to said fuel passage and adapted to by-pass fuel from said pumping chamber to said sump during a plunger compression stroke, a first and a second movable means in said sump for isolating said control port means from said sump during a selected portion of said plunger compression stroke respectively to produce injection
  • a valveless fuel injection pump comprising, in combination, a low pressure fuel reservoir, a high-pressure pumping chamber, a fuel delivery line, a pump plunger, means connecting said high-pressure pumping chamber to said fuel delivery line during the initial portion of the compression stroke of said plunger While at the same time maintaining said high-pressure pumping chamber connected to said low pressure fuel reservoir,
  • a fuel injection pump according to claim 2, wherein the said pump plunger simultaneously reciprocates and rotates to control high-pressure fuel supply in sequence to a plurality of fuel delivery lines, each supplied from said high-pressure pumping chamber.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
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  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Description

y 1956 w. E. MEYER 2,746,443
FUEL INJECTION PUMP Filed Feb. 20, 1955 3 Sheets-Sheet 1 IN V EN TOR. WOLFGANG- 4. M5 YEA? BY fiTOENE Y May 22, 1956 w. E. MEYER 2,746,443
FUEL INJECTION PUMP Filed Feb. ,20, 1953 3 Sheets-Sheet 2 IN VEN TOR. WOLFGA N6 5 M5 YEP ATTOENEY United States 2,746,443 FUEL INJECTION PUMP Wolfgang E. Meyer, State College, Pa., assignor to The Patent Texas Company, New York, N. Y., a corporation of Delaware Application February 20, 1953, Serial No. 338,043
3 Claims. (Cl. 123-139 The present invention relates to fuel injection pumps for internal combustion engines and particularly to an improved fuel-injection pump of the type wherein a single reciprocating and rotating pumping plunger serves a plurality of engine cylinders.
in the operation of fuel injection pumps of the aforesaid itype withfuel pressure-actuated engine fuel injectors,
particularly when highly volatile fuels are used and when the pumping frequency is high, considerable difiicu'lty is commonly experienced in obtaining precise control of certain factors which are important to optimum engine operation and efiicient combustion. Such factors as timing of the beginning and end of each fuel injection, and the quantity of fuel metered from the pump in 'each injcction, are part-icularlydifiicult to control with precision, especially when the quantity of fuel delivered in each injection is small. This difliculty is caused basically by thecompressibility of fuel in the fuel discharge path from thepump to the engine fuel injector. 'When this fuel discharge path has a relatively large volume in comparison with the volume of fuel discharged by the pump Mice 2 at a rate several times the engine speed, with very little time afforded between successive fuel discharges for recondensation of any vaporized fuel inthe fueldischarge path. Hence, in preventing vacuum formation in the fuel discharge path the delivery valve is particularly important.
However, use of the conventional delivery valve has the disadvantage. that the valve itself requires space in which @to be housed, which space further adds to the compressible volume of the fuel discharge path and increases its elasticity. Also, by immediately closing in response to the reduction in pump output pressure which is intended to terminate fuel injection, the delivery valve blocks the fuel discharge path at its pump end and provides a reflecting surface for pressure waves in the discharge path which usually accompany termination of fuel injection. The reflection of such pressure waves increases the likelihood of secondary or after-injections into the engine and thus-renders more difiicult precise control of timing and duration of fuel injection.
The present invention provides a fuel injection pump of the type in which a single reciprocating and rotating plunger serves a plurality of engine cylinders, and from which :the conventional delivery valve is completely elimi-.
. fuel discharge path fromthe pumping chamber of the for each injection, the compressibility of the fuel "tends to permit absorption of the fuel charge from the pump into the fuel discharge path without any corresponding displacement of 'fuel'through the fuel injector and 'into the engine. This may result in actual fuel delivery to the engine of only aportion of the desired fuel charge. Also, -this elasticity of the system produces an unpredictable delay between the desired beginning .and ending I of fuel injection, as controlled by starting and stopping of pumping 'in the fuel pump, and actual beginning and ending of fuelinjectionat the injector.
One attempt to remedy this situation which is conventional in prior art fuel injection pumps is the, provision of a fuel pressure-operated delivery valve which controls egress of fuel from the pumpand serves to maintain fuel pressure 'in the fuel discharge path from pump to injectorat a level close to .injection pressure during .theinterval between successive fuel discharges from the pump. This in effect maintains the fuel in the discharge path in a precompressedstate and reduces its ability to absorb a fresh fuel charge delivered .by .the pump.
The fuel delivery valve also serves the .useful purpose .of isolating the fuel discharge path from thepump during the suction stroke of the pumping plunger. This prevents the rapid expansion of volume within the pumping chamber of the fuel pump from creating a vacuum in Because fuel vapor thus rupts the timing and accuracy of fuel metering. This difficulty is aggravated during pump operation :at high engine speeds, and particularly so in the typeof fuel pump with which the present invention is concerned, wherein .a single pumping plunger serving fuel to .a plurality of engine cylinders must discharge successive fuel charges pumpduring the suction stroke of the plunger, andthere- 'by prevents vacuum formation in the fuel discharge path, but .does not bring about such isolation until well after the termination of fuel injection, so that any pressure waves accompanying injection termination, which might possibly be reflected in the discharge path, are effectively dissipated in .the fuel supply reservoir of the pump. This utilization of the rotating plunger as an effective delivery permits .a considerable simplification, with attendant re- 45 ductionin volume, of that portion of the fuel discharge path contained within-the fuel pump body. Thus, a fuel pump is provided from which the aforesaid difficulties are substantially eliminated, and which is particularly suited for precision control of fuel injection over a wide range of operating conditions.
An object of this invention therefore is to provide an improved fuel injection pump for'use -with internal com- :bustion engines, in which a single plunger is reciprocated and continuously rotated :for pumping and metering the ,fuel and fordistr-ibuting it to more than one engine cylinder.
Another object is to provide a fuel injection pump of the aforesaid type in which the conventional fuel pressure-actuated delivery valve is eliminated.
Another .object is to provide a fuel injection pump of the aforesaid type in which the path provided for the discharge of-fuel from'the pumping chamber to the engine is greatly simplified and substantially reduced in volume.
.ing fuel.
Another object is to provide a fuel pump of the aforesaid type in which vacuum formation or fuel vaporization in the fuel discharge path during the suction stroke of the pumping plunger is prevented.
,Another object is to provide a fuel pump of the aforesaid type having an improved degree .of precision of meter- Another object is to provide a fuel pump of the aforesaid type, which is particularly suited for metering fuel to engines operating at relatively high speeds.
Another object is to provide a fuel injection pump of the aforesaid type in which vacuum formation in the pumping chamber during the suction stroke of the pump plunger is eliminated.
Another object is to provide a fuel injection pump of the aforesaid type in which the beginning and the end of fuel injection can be varied independently of each other.
Another object is to provide a fuel injection pump of the aforesaid type in which the entire fuel discharge path from the pump is maintained in continuous fluid fuel contact with a low pressure fuel reservoir during the termination of fuel injection pressure in said discharge path, so that pressure waves in said fuel discharge path arising from abrupt termination of fuel injection pressure are substantially damped out in said reservoir without reflection, and secondary fuel injections are thereby eliminated.
Another object is to provide an improved fuel pump of the aforesaid type having a reduced number of parts of simplified design which can be manufactured with greater ease and at reduced cost.
These and other objects and advantages of the invention will be apparent from the following description taken in connection with the accompanying drawings wherein:
Fig. 1 is a longitudinal sectional view of a pump constructed in accordance with the present invention and showing the plunger in an intermediate portion of its stroke.
Fig. 2 is an enlarged view of a portion of Fig. 1.
Fig. 3 is an enlarged sectional view of the portion of the pump shown in Fig. 2, taken on the line 3-3 of Fig. 2.
Fig. 4 is an enlarged sectional view of the portion of the pump shown in Fig. 2, taken on the line 4-4 of Fig. 2.
Fig. 5 is an enlarged sectional view of the portion of the pump shown in Fig. 2, taken on the line 55 of Fig. 2.
Fig. 6 is an enlarged cut-away perspective view of that portion of the pump shown in Fig. 2,. the portion cut away being defined by the line 66 in Figs. 3 and 4.
Referring to the drawings, and particularly to Figs. 1 and 2, a single plunger fuel injection pump constructed in accordance with the present invention is shown by way of example as adapted to serve a four-cylinder engine. The pump includes a housing 1 containing a body member 3 provided with a cylindrical bore 5 which is enlarged adjacent one end to form a fuel sump 7. Slidably fitted within the bore 5 is a cylindrical pumping plunger 9 adapted for reciprocation and simultaneous rotation therein in timed relation with the engine for which the pump supplies fuel.
For reciprocating the plunger 9 within the bore 5 there is provided an engine-driven cam shaft 11 supported in housing 1 and carrying a cam 13 which cooperates with a tappet roller 15 rotatably mounted in a tappet 17. The tappet 17 is adapted to reciprocate within a bore 19 of housing 1 in coaxial alignment with the bore 5 in the body member 3. One end of plunger 9 is maintained in continuous contact with reciprocating tappet 17 by means of compression springs 21 and 23 acting against a spring retainer 25 supported from the end of the plunger by the usual split collar 27. At their other end springs 21 and 23 are restrained by a plunger rotation gear 31 which is keyed to plunger 9 intermediate its length and which is adapted to bear against a surface 29 of the body member 3 while rotating.
To enable rotation of plunger 9 simultaneously with its reciprocation in cylindrical bore 5, a pinion 33 connected in driving relation with gear 31 is driven through a shaft 35 from a helical gear 37 mounted on cam shaft 11.
At its end remote from sump 7, the bore 5 is permanently closed during operation of the pump, as by a plug 41. Plunger 9 forms with cylindrical bore 5 at this permanently closed end thereof a pumping chamber 43. During operation of the pump, fuel is admitted to pumping chamber 43 for compression therein to the high pressures suitable for delivery to the conventional engine fuel injection equipment, and discharged therefrom at a selected time in the engine cycle and in accurately metered amount.
In the case of thepump shown in the drawings, which is designed to provide injection fuel to a four-cylinder engine, if the engine is of the four-stroke cycle type requiring two engine cylinder fuel injections for each engine crankshaft revolution, then cam 13 and cam shaft 11 are arranged to reciprocate plunger 9 through two complete cycles, consisting of two compression and two suction strokes, during one engine crankshaft revolution. Thus, if cam 13 is provided with two lobes, cam shaft 11 should turn at engine speed for a four-stroke cycle four cylinder engine. This could also be accomplished by providing cam 13 with four lobes and turning cam shaft 11 at one half engine speed. If the four-cylinder engine is of the two-stroke cycle type and cam shaft 11 turns at engine speed, cam 13 should have four lobes. Also, in order that the pump may deliver its entire fuel discharge during a given plunger compression stroke to but one engine cylinder, the ratio of the plunger rotating gear 31 and its driving pinion 33 should be such that plunger 9 completes one full revolution during four-pumping strokes for four-cylinder engine operation on either a two or four stroke cycle. That is, the plunger should rotate from the time it leaves its bottom dead center position on a compression stroke until it returns to bottom dead center after completing its suction stroke.
Body member 3 is provided with a plurality of fuel distributor ports 51, 52, 53, 54 (only two of which are shown in Fig. 1), one for each engine cylinder, which communicate with the cylindrical bore 5 at points preferably equally spaced about a circumference in a crosssectional plane thereof.
To each of the distributor ports 51, 52, 53, 54 is connected a fuel delivery line 55, 56, 57, 58 which conveys fuel to a particular engine cylinder fuel injection device. Distributor ports 51, 52, 53, 54 are so located along cylindrical bore 5 as to be covered by plunger 9 during the whole of its reciprocating stroke. At its pumping chamber end plunger 9 is provided with a longitudinal fuel distributor slot 61 which is of a sufficient length to intersect the plane of the distributor ports during the entire reciprocating stroke of the plunger. By this arrangement, any one of fuel distributor ports 51, 52, 53, 54 can be kept in fluid fuel contact with pumping chamber 43 during the entire length of a plunger compression or suction stroke by proper rotative orientation of plunger 9 to uncover the distributor port by distributor slot 61. Conversely, by so rotating plunger 9 that distributor slot 61 does not uncover and come into fluid contact with any of the distributor ports 51, 52, 53, 54, all of the distributor ports can be isolated from pumping chamber 43 during the whole of a plunger compression or suction stroke. In the embodiment shown, slot 61 has a width in relation to the size of ports 51, 52, etc., suflicient to uncover a distributor port during substantially 45 of rotation of plunger 9.
Body member 3 is also provided with a plurality of fuel supply ports 71, 72, 75, 76 communicating with cylindrical bore 5 at points along its length between sump 7 and distributor ports 51, 52, 53, 54. These fuel supply ports 71, 72, etc., are connected through a fuel supply passage 45, in body member 3 to any desired source of low-pressure fuel, not shown. Sump 7 is also supplied with low pressure fuel through a connection 49 in body member 3 to fuel supply passage 45. Together sump 7 and the fuel supply passage 45 provide a low pressure fuel reservoir from which the pumping chamber 43 can be charged with fuel as the pump operates.
l plunger.
en arge -Fuel supply ports 71, 72, etc., are located .alo ngcylindrical bore 'sufficiently far from its closed end so that none of these ports will be uncovered by distributor slot 61 of plunger 9 during'any point in the plunger suct'ion stroke, regardless of the rotative position of the Plunger 9 is provided also with a longitudinal fuel by-pass passage 63 which opens into pumping chamber 43, and is of'sufiicient length within plunger 9 to extend into that portion of the plunger surrounded by fuel sump 7. At its fuel sump end the by-pass passage 63-is connected to the fuel sump 7 through two longitudinally spaced upper and lower control ports 81, 82 in plunger '9. Control ports 81 and 82 are preferably aligned in the axial plane through'the plunger which bisects the distributor slot 61,'their longitudinal location and spacing preferably being suchthat these ports will be confined Within fuel sump 7 during the entire plunger excursion. Also provided within sump 7 are a pair of control sleeves 91, 92 which surround the plunger 9 with a close sliding fit. Control sleeves 91, 92 are slotted to receive pins 101, 162, respectively, which are eccentrically mountedion shafts 103, 104 supported in body member 3 for rotation by suitable means external to the pump, such ashand controls 105, 106, or any desired engine condition-responsive device. By this arrangement, control sleeves 91, 92 can be adjustably positioned along the plunger to cover the upper and lower control ports 81, 82, during any selected portion of the plunger compression stroke, and thereby prevent fuel flow between pumping chamber 43 and fuel sump 7. Each control sleeve 9 1, 92 can be manipulated independently of the other,
to cover and uncover the different control ports 81, 82 at different points in the plunger excursion.
Inthe vicinity of fuel supply ports '71, 72, etc., plunger 9 is additionally provided with two fuel fill ports '73, 74, connecting to the longitudinal fuel by-pass passage 63. Fill ports 73, '74 are disposed preferably on a common plunger diameter and inthe plunger axial plane of con- 1 trol ports 81, 82 and are so arranged as to uncover and come into fluid fuel contact with fuel supply ports 71, 72, etc., during certain portions of the plunger suction stroke, as will be explained more fully hereinafter.
Operation of the pump will be described in terms of the sequence of events' taking place during one complete pressure fuel is .displaced' through distributor slot 61 n and the fuel discharge path consisting of distributor port '51 and'its connected fuel delivery line 55, to the appropriate fuel injection device onthe engine.
, tion of supply ports 71, 72, 75, 76 and distributor ports 51, 52, 53,54, while slot 61 remains in contact with distributor port 51 fill ports 73 74 are carried upward be tween adjacent supply ports without uncovering them.
As plunger 9 ascends further on its pumping stroke, lower control port 82 emerges from lower control sleeve 92, thereby spilling high pressure fuel from pumping chamber 43 through longitudinal fuel ,by-pass passage 63. This immediately terminates displacement of fuel at injection pressure from pumping chamber 43. The abrupt drop in fuelpressure in pumping chamber 43, is
immediately communicated, through the still maintained fluidfuel'contact between chamber 43 and port 51, to the .pressure actuated engine fuel injection device, and fuel injection ceases. However, since plunger slot 61 remains in contact with port 51 during and after the termination of injection, the pressure waves which are plunger excursion, and with particular reference to Fig. 6 V
- of the drawings, wherein is shown in enlarged schematic form the plunger 9, the ports .of bore 5, and control sleeves 91 and 92. Plunger 9 begins its excursion from an initial position at bottom dead center, and with a rotative orientation at which one of the distributor ports,
rotation. At this point lower controlp ort $82 is normally covered by lower control sleeve 92, while upper control port81 is below the lower edge of upper control sleeve "91 and hence open to fuel sump '7. Also plunger fill ports 73, 74 are at this point below the vicinity of supply ports 71, 72, etc., and the rotative position of fill ports "'73, 74 is therefore not asyet important in determining compression stroke, as determined by the axial position of upper control sleeve 91, upper control port 81*enters A upper control sleeve 91 and thereby closes olf pumping chamber '43 from fluid fuel contact with fuel sump 7. The compression :of plunger 9 builds fuehpressure up rapidly thereafter in pumping chamber and high-I n say 51, is just about to be uncovered by slot 61. This rotative orientation may, for reference, be termed 0 .of
usually present in the fuel dischargepath after theabrupt injection termination are allowed to travel back through the discharge path to pumping chamber 43 and thence to fuel sump 7., wherein they are effectively damped out without undesired reflection back to the engine injection device.
Plunger .9 continues 'to rotate while ascending, and by the time it reaches top dead center position, it has rotated a sufiicient extent so that fluid fuel contact has just .been broken between port 51 and distributor slot 61.
Thus, when plunger 9 begins its downward or suction stroke under the influence of springs 21,23, and as permitted by .the rotation of cam 13., distributor port "51 "is isolated from pumping chamber 43, and any tendency toward creationof a vacuum in the expanding volume of pumping chamber 43 is not communicated through port 51.to the fuel discharge path. The width of slot .61 in relation to the size of distributor ports. 51 52, 53, and 54 is such that, during the entire angu 'lar rotation of plunger 9 while on its suction stroke, slot 61 does not .uncover the next succeeding distributor ,port52, but .as plunger 9 reaches bottom dead center the nearest edge of slot 61 is just about to be rotated into uncovering relationship with distributor port .52. Thus, during the whole suction stroke of plunger 9'dis- .tributor slot 61 is rotatively positioned between adja- .cent distributor ports, which thereby completely isolates all distributor ports 51, 52, .etc., from pumping chamber 43 during the plunger suction stroke.
As plunger 9 descends on the first portion .of its vsuction stroke,the fact that pumping chamber 43 .is .in communication with sump '7 through .by pass passage 63 and lower control port 82 prevents any vacuum .formation in pumping chamber 43. Later in the plunger descent, lower control .port .82 reenters lower control sleeve 92. Since the order .of events .is reversed from the compression stroke, upper control .port 81 has not as yet emerged from upper control sleeve 91. The .fluid fuel connection between pumping chamber 43 and fuel sump ,7 is thereby .severed. This would .tend .to vcreate a vacuum in pumping chamber 43, but for the fact that the supply ports 71, 72, 75, 76 aresso positioned that, at this plunger reciprocative and rotative ,position, at least one supply port is uncovered by a plunger fill port 73, 574. Thus, fuel .is admittedto pumping chamber 43 from .supply passage 45, and creation -of a vac- 7 uum in chamber 43 is prevented. The disposition of supply ports 71, 72, 75, 76 is thus determined by this requirement, namely that at least one supply port must be uncovered by a plunger fill port at the time when pumping chamber 43 becomes isolated from sump 7 during the plunger suction stroke. The supply and fill ports must also be of such a size as to maintain fluid fuel contact until further plunger descent permits upper control port 81 to emerge from upper control sleeve 91.
As has heretofore been stated, plunger 9, is rotated continuously in one direction and at constant speed by driving gear 31. As has also been explained, when serving a four-cylinder engine the plunger should complete one fourth of a full rotation, i. e., 90", during the period of one complete reciprocating excursion. Since plunger 9 rotates at constant speed, the proportion of its 90 rotation which accompanies its compression stroke, relative to the proportion of its 90 rotation which accompanies its suction stroke, will be determined by the profile of the lobe of cam 13. If the cam lobe is symmetrical, for example, 45 of plunger rotation will accompany its compression stroke and 45 will accompany its suction stroke. If, however, it is desired that a larger proportion of the 90 rotation should accompany a plunger compression stroke, then the plunger will be returned on its suction stroke during a relatively small fraction of the total excursion time, with a correspondingly small amount of rotation. Thus, the shape of the cam profile is a factor which affects the disposition of fuel supply ports 71, 72, 75, 76 relative to cylindrical bore 5. Provision as here shown of a plurality of supply ports, two of which are spaced 90 about a circumference of bore 5, and the other two of which are spaced somewhat less than 90 and in a cross-sectional plane displaced slightly from the first two, and provision of two diametrically opposite fill ports 73, 74 in the plunger, permits a lengthened period of fluid contact between supply ports and fill ports during the plunger suction stroke without requiring unusually large fill or supply ports. Of course it will be understood that the shape and size of the supply ports 71, 72, 75, 76, as well as fill ports 73, 74, may be varied as desired and as necessary to maintain fluid contact therebetween during the period above described, and the relative size and shape of the ports shown in the drawing is merely exemplary of one operative arrangement.
As the plunger 9 approaches bottom dead center, and upper control port 81 emerges from the lower side of upper control sleeve 91 and reestablishes fluid contact between pumping chamber 43 and sump 7, the additional plunger descent and plunger rotation carries fill ports 73, 74 out of fluid contact with supply ports 71, 72, etc., and severs this connection between fuel source and"- pumping chamber 43. However, pumping chamber 43 remains connected to the low pressure fuel reservoir through upper control port 81 and sump 7 during the remainder of its suction stroke until it reaches bottom dead center. Thus, it will be seen that during the entire plunger suction stroke, pumping chamber 43 is at no time out of fluid fuel contact with a source of low pressure fuel, either through fill ports 73, 74 or'through upper or lower control ports 81, 82. This completely eliminates the possibility of fuel vaporization due to vacuum formation in pumping chamber 43.
Since the four distributor ports 51, 52, 53 and 54 are spaced equally about the circumference of bore 5, operation of the pump on subsequent plunger excursions, during which fuel is distributed through the remaining ports 52, 53, and 54, is identical with the pumping cycle for port 51 previously described, and hence need not be described.
Since the relative position of upper control port 81 and upper control sleeve 91 at the start of the plunger compression stroke determines what portion of the compression stroke will be completed before upper control 'port 81 becomes enclosed Within upper control sleeve 91 and fuel displacement from pumping chamber 43 begins, it will be appreciated that raising the upper control sleeve 91 delays the start of fuel discharge from pumping chamber 43, and'lowering upper control sleeve 91 begins fuel discharge earlier. Likewise, raising lower control sleeve 92 delays uncovering of lower control port 82 and terminates fuel discharge from chamber 43 later in the plunger'compression stroke, and lowering the lower control sleeve 92 terminates the fuel discharge earlier in the plunger compression stroke. Thus, varying the position of the two sleeves in unison varies the timing of fuel injection at the engine, relative to the engine crankshaft position.
Also, it should be recognized that since the two control sleeves 91 and 92 can be moved independently, the distance between them may be varied. Thus, simultaneously raising upper control sleeve 91 and lowering lower control sleeve 92 delays the beginning of fuel discharge from pumping chamber 43, and also hastens its termination, thereby shortening the effective pumping stroke of the plunger. Conversely, bringing the two control sleeves 91 and 92 closer together lengthens the period in the plunger compression stroke during which fuel discharge takes place from pumping chamber 43. As an extreme example of this latter condition, upper and lower control sleeves 91 and 92 may be brought together until they are in contact and form one continuous enclosure about the control ports. In this case, there will be no by-pass connection through passage 63 between pumping chamber 43 and fuel sump 7 during any portion of the plunger compression stroke. When the control sleeves 91 and 92 are in this specialized position therefor, the plunger delivers fuel to a fuel delivery line during its entire compression stroke, thus effectively expelling air from the pumping chamber 43 and the delivery line. Since the connection between the pumping chamber and the delivery line is broken, when the plunger reaches its topmost position, and the delivery line thereafter remains isolated until the plunger completes a full rotation, fuel once pumped into this particular fuel delivery line has no opportunity to return to the fuel sump. This arrangement therefore progressively expels air from the various delivery lines, and enables effective priming of the pump.
Thus, there has been shown and described an internal combustion engine fuel injection pump from which the conventional delivery valve has been completely eliminated, enabling a substantial reduction in volume of the fuel delivery path between pump and engine without incurring vacuum formation and fuel vaporization in the discharge path or pumping chamber even during high speed operation and'with volatile fuels. Pumps constructed in accordance with the present invention are moreover characterized by greatly simplified internal fuel fiow passages as well as provision for simple and effective control of the beginning and termination of effective pumping, thereby providing a pump which is less expensive to manufacture, and which enables precision control of fuel injection over a wide range of operating conditions.
Obviously many modifications and variations of the invention, as hereinbefore set forth, may be made without departing from the spirit and scope thereof, and therefore only such limitations should be imposed as are indicated in the appended claims.
I claim:
1. In an internal combustion engine fuel injection pump of the type wherein a single plunger is employed for pumping and metering fueland distributing it to a plurality of engine cylinders, a body having a bore therein closed at one end and enlarged at the other end to form a fuel sump, a plunger adapted to reciprocate and rotate in said bore and forming at the .closed end of said bore a pumping chamber, means for reciprocating and simultaneously continuously rotating said plunger in said bore, said fuel sump enclosini a portion of said plunger during the whole of said reciprocation thereof, a fuel passage in said plunger communicating with said pumping chamber, a plurality of control port means in said portion of said plunger enclosed within said fuel sump connected to said fuel passage and adapted to by-pass fuel from said pumping chamber to said sump during a plunger compression stroke, a first and a second movable means in said sump for isolating said control port means from said sump during a selected portion of said plunger compression stroke respectively to produce injection fuel pressure in said pumping chamber and to release said injection fuel pressure, a plurality of fuel distributing ports communicating with said bore at points equally spaced around a circumference of said plunger and located between said pump and said pumping chamber, a fuel distributing slot in said plunger adapted to connect one of said fuel distributing ports to said pumping chamber during a plunger compression stroke and to isolate said distributing ports from said pumping chamber during a plunger suction stroke, fuel supply ports communicating with said bore and located between said fuel distributing ports and said fuel sump, and supply ports in said plunger connected to said plunger passage and adapted to overlapsaid fuel supply ports to admit fuel to said pumping chamber during the portion of said plunger suction stroke when said plurality of control port means are otherwise isolated from said fuel sump.
2. A valveless fuel injection pump comprising, in combination, a low pressure fuel reservoir, a high-pressure pumping chamber, a fuel delivery line, a pump plunger, means connecting said high-pressure pumping chamber to said fuel delivery line during the initial portion of the compression stroke of said plunger While at the same time maintaining said high-pressure pumping chamber connected to said low pressure fuel reservoir,
individual means on the continued compression stroke of said plunger first operatively disconnecting said low pressure fuel reservoir from said high-pressure pumping chamber to initiate high-pressure fuel supply to said delivery line, and then reconnecting said low pressure fuel reservoir with said high pressure pumping chamber to terminate high-pressure fuel supply to said delivery line respectively, said last mentioned means then maintaining connection of said delivery line and high-pressure pumping chamber with said low pressure fuel reservoir during the completion of said plunger compression stroke to damp out pressure waves in said system, means independently varying the timing of the initiation and termination of high-pressure fuel supply to said delivery line during the plunger compression stroke, and means during the entire succeeding plunger suction stroke disconnecting said fuel delivery line from said high-pressure pumping chamber while maintaining connection of said high'pressure chamber with said low pressure fuel reservoir to prevent vacuum formation and vaporization of fuel in said high-pressure pumping chamber.
3. A fuel injection pump according to claim 2, wherein the said pump plunger simultaneously reciprocates and rotates to control high-pressure fuel supply in sequence to a plurality of fuel delivery lines, each supplied from said high-pressure pumping chamber.
References Cited in the file of this patent UNITED STATES PATENTS 2,478,528 Edwards Aug. 9, 1949 2,544,561. Meyer Mar. 6, 1951 2,624,327 Hogeman Jan. 6, 1953 2,640,419 Evans et a1. June 2, 1953 2,667,840 High Feb. 2, 1954 FOREIGN PATENTS 359,603 Great Britain Oct. 29, 1931
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Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2965087A (en) * 1958-01-29 1960-12-20 Bosch Arma Corp Fuel injection pump
US3064579A (en) * 1958-09-17 1962-11-20 Staege Werner Fuel injection pump for internal combustion engines
US3099217A (en) * 1959-11-12 1963-07-30 Bessiere Pierre Etienne Fuel injection pumps having distributing pistons
US3138103A (en) * 1961-12-26 1964-06-23 Allis Chalmers Mfg Co Fuel supplying mechanism
US3146716A (en) * 1961-12-26 1964-09-01 Allis Chalmers Mfg Co Fuel supplying mechanism
US3186344A (en) * 1963-11-13 1965-06-01 Bosch Arma Corp Fuel injection pump
US3353492A (en) * 1965-01-26 1967-11-21 Bosch Gmbh Robert Lubricating pump
US3371610A (en) * 1966-02-16 1968-03-05 Bosch Arma Corp Auxiliary filling means for fuel injection pumps
US3455246A (en) * 1968-02-28 1969-07-15 Frank Borowiec Balanced fuel injection pump
US3630643A (en) * 1969-02-28 1971-12-28 Bosch Gmbh Robert Fuel injection pump
US3673996A (en) * 1970-10-02 1972-07-04 Allis Chalmers Mfg Co Fuel injection pump timing and metering arrangement
US4082072A (en) * 1975-03-17 1978-04-04 Johnson Lloyd E Sealing in fuel injection pumps
US4083662A (en) * 1975-05-21 1978-04-11 Robert Bosch Gmbh Fuel injection pump for internal combustion engine
EP0027790A1 (en) * 1979-10-15 1981-04-29 Friedmann & Maier Aktiengesellschaft Injection pump
US4486155A (en) * 1981-06-06 1984-12-04 Spica S.P.A. Control of the pistons in injection pumps of internal-combustion engines
US4598863A (en) * 1983-01-20 1986-07-08 Usui Kokusai Sangyo Kabushiki Kaisha Fuel injector
US4705005A (en) * 1984-12-24 1987-11-10 Robert Bosch Gmbh Fuel injection pump for internal combustion engines
US4708114A (en) * 1984-12-24 1987-11-24 Robert Bosch Gmbh Fuel injection pump for internal combustion engines
US20060266846A1 (en) * 2005-05-27 2006-11-30 Mario Ricco Fuel-control servo valve, and fuel injector provided with such servo valve

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB359603A (en) * 1930-08-02 1931-10-29 Napier & Son Ltd Improvements in or relating to fuel injection pumps
US2478528A (en) * 1946-08-22 1949-08-09 Timken Roller Bearing Co Fuel injection pump
US2544561A (en) * 1945-06-11 1951-03-06 American Bosch Corp Fuel injection pump
US2624327A (en) * 1950-03-30 1953-01-06 American Bosch Corp Fuel injection apparatus
US2640419A (en) * 1950-05-23 1953-06-02 Cav Ltd Liquid fuel injection pump for internal-combustion engines
US2667840A (en) * 1951-03-28 1954-02-02 Carl F High Fuel injection apparatus and control mechanism therefor

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB359603A (en) * 1930-08-02 1931-10-29 Napier & Son Ltd Improvements in or relating to fuel injection pumps
US2544561A (en) * 1945-06-11 1951-03-06 American Bosch Corp Fuel injection pump
US2478528A (en) * 1946-08-22 1949-08-09 Timken Roller Bearing Co Fuel injection pump
US2624327A (en) * 1950-03-30 1953-01-06 American Bosch Corp Fuel injection apparatus
US2640419A (en) * 1950-05-23 1953-06-02 Cav Ltd Liquid fuel injection pump for internal-combustion engines
US2667840A (en) * 1951-03-28 1954-02-02 Carl F High Fuel injection apparatus and control mechanism therefor

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2965087A (en) * 1958-01-29 1960-12-20 Bosch Arma Corp Fuel injection pump
US3064579A (en) * 1958-09-17 1962-11-20 Staege Werner Fuel injection pump for internal combustion engines
US3099217A (en) * 1959-11-12 1963-07-30 Bessiere Pierre Etienne Fuel injection pumps having distributing pistons
US3138103A (en) * 1961-12-26 1964-06-23 Allis Chalmers Mfg Co Fuel supplying mechanism
US3146716A (en) * 1961-12-26 1964-09-01 Allis Chalmers Mfg Co Fuel supplying mechanism
US3186344A (en) * 1963-11-13 1965-06-01 Bosch Arma Corp Fuel injection pump
US3353492A (en) * 1965-01-26 1967-11-21 Bosch Gmbh Robert Lubricating pump
US3371610A (en) * 1966-02-16 1968-03-05 Bosch Arma Corp Auxiliary filling means for fuel injection pumps
US3455246A (en) * 1968-02-28 1969-07-15 Frank Borowiec Balanced fuel injection pump
US3630643A (en) * 1969-02-28 1971-12-28 Bosch Gmbh Robert Fuel injection pump
US3673996A (en) * 1970-10-02 1972-07-04 Allis Chalmers Mfg Co Fuel injection pump timing and metering arrangement
US4082072A (en) * 1975-03-17 1978-04-04 Johnson Lloyd E Sealing in fuel injection pumps
US4083662A (en) * 1975-05-21 1978-04-11 Robert Bosch Gmbh Fuel injection pump for internal combustion engine
EP0027790A1 (en) * 1979-10-15 1981-04-29 Friedmann & Maier Aktiengesellschaft Injection pump
US4486155A (en) * 1981-06-06 1984-12-04 Spica S.P.A. Control of the pistons in injection pumps of internal-combustion engines
US4598863A (en) * 1983-01-20 1986-07-08 Usui Kokusai Sangyo Kabushiki Kaisha Fuel injector
US4705005A (en) * 1984-12-24 1987-11-10 Robert Bosch Gmbh Fuel injection pump for internal combustion engines
US4708114A (en) * 1984-12-24 1987-11-24 Robert Bosch Gmbh Fuel injection pump for internal combustion engines
US20060266846A1 (en) * 2005-05-27 2006-11-30 Mario Ricco Fuel-control servo valve, and fuel injector provided with such servo valve
US7793862B2 (en) * 2005-05-27 2010-09-14 C.R.F. Societa Consortile Per Azioni Fuel-control servo valve, and fuel injector provided with such servo valve

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