US3404668A - Fuel injection pump - Google Patents

Fuel injection pump Download PDF

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US3404668A
US3404668A US537759A US53775966A US3404668A US 3404668 A US3404668 A US 3404668A US 537759 A US537759 A US 537759A US 53775966 A US53775966 A US 53775966A US 3404668 A US3404668 A US 3404668A
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fuel
pump
piston
working
engine
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Eheim Franz
Hoefer Gerald
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Robert Bosch GmbH
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Robert Bosch GmbH
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M41/00—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor
    • F02M41/08—Fuel-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
    • F02M41/10—Fuel-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
    • F02M41/12—Fuel-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
    • F02M41/123—Fuel-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
    • F02M41/125—Variably-timed valves controlling fuel passages
    • F02M41/127—Variably-timed valves controlling fuel passages valves being fluid-actuated slide-valves, e.g. differential rotary-piston pump

Definitions

  • a fuel injection pump for supplying fuel to an internal combustion engine having a first number of cylinders, a piston turnably and reciprocatably arranged in a working chamber of the pump, drive means for rotating 'the piston about its axis and for reciprocating the same during each revolution along second number of working and suction strokes greater than the above mentioned first number and including a first number of effective Working strokes during which fuel is fed from the working chamber to the cylinders of the engine and a number of ineffecting working strokes during which fuel is fed from the working chamber to a source of fuel yconnected to the working chamber.
  • the present invention relates to fuel injection pumps for internal combustion engines. More particularly, the invention relates to improvements in a fuel injection pump of the type which is capable of supplying accurately metered quantities of liquid fuel to one or more cylinders of an internal combustion engine.
  • Another object of the invention is to provide a fuel injection pump which, though originally produced for use in connection with a four, sixor eight-cylinder engine, can be rapidly converted for use in connection with one-, twoor three-cylinder engines without necessitating any major alterations in its appearance, operation and/ or space requirements.
  • a further object of the invention is to provide a pump of the above outlined characteristics wherein the amounts of metered fuel may Ibe regulated with utmost precision so that the pump invariably delivers to the cylinder or cylinders of an internal combustion engine fuel at a rate which is an accurate function of the rotational speed of the engine.
  • Still another object of the invention is to provide a novel pump housing or body which may be utilized in a pump of the above defined type.
  • An additional object of the invention is to provide a novel pumping member which can be used in the i-mproved pump to draw, meter and distribute jets of fuel to one or more cylinders of an internal combustion engine.
  • a further object of the invention is to provide a novel pump which comprises a so-called liquid stop and wherein the liquid stop may be adjusted or regulated with the same degree of precision as in a pump which is used in connection with an engine having a relatively large number of cylinders despite the fact that the novel pump serves to meet the requirements of an engine having a relatively small number of cylinders.
  • a concomitant object of the invention is to provide the improved pump with a novel system of passages or channels which convey fuel to and from the working chamber of the pump.
  • Still another object of the instant invention is to achieve unexpectedly high economies in storage facilities, manufacturing cost and assembly cost of fuel injection pumps for engines having a relatively small number of cylinders.
  • a further object of the instant invention is to provide a novel method of converting fuel injection pumps for use with engines having a first number of cylinders into fuel injection pumps capable of being used with engines having a second number of cylinders.
  • Another object of the invention is to provide fuel injection pumps for use with engines having one, two, three, four, six, eight or another number of cylinders and to construct such pumps in a way to insure that at least a majority of components useful in one type of pumps can ybe used, without any changes or with minimal changes, in each other type of pumps.
  • a fuel injection pump for supplying fuel to an internal combustion engine having a predetermined (first) number of cylinders, for example, three cylinders.
  • the pump comprises a source of fuel, housing means defining a working chamber, intake channel means adapted to connect the source with the working chamber, discharge channel means adapted to communicate with the Working chamber and comprising a first number of separate fuel lines each of which can supply 4'fuel to a separate cylinder of the engine (thus, if the engine comprises three cylinders, the discharge channel means comprises three fuel lines which are machined into or otherwise provided in the housing means), a pumping member movable in the housing means to perform alternating suction and working strokes to respectively draw fuel from the source via intake channel means and into the working chamber and to expel fuel from the working chamber, drive means for imparting to the pumping member, at a rate proportional with the speed of the engine, a series of consecutive movements each of which includes a second number of suction strokes and a second number of
  • the pumping member may comprise a rotary piston which is reciprocable in a blind bore of the housing means and each movement of the piston includes a full revolution during which the piston performs an equal number of suction or working strokes, i.e., the number of working strokes during each revolution equals the number of suction strokes during the same revolution and such number is preferably a whole multiple of the number of cylinders in the engine which is associated with the fuel injection pump.
  • our novel method can -be decsribed as relating to injection of fuel into cylinders of an engine which has a relatively small number of cylinders.
  • the method comprises the steps of admitting into and expelling from the working chamber of a fuel injection pump (which was built for use in connection with an engine having a relatively large number of cylinders), during each revolution of the engine, metered quantities of fuel at such a frequency that the number of admissions and expulsions exceeds the number of cylinders in the engine ,having a relatively small number of cylinders, and introducing-during each revolution of the engine-one metered quantity into each cylinder so that at least one metered quantity of fuel expelled from the working chamber during any given revolution of the engine is not admitted into a cylinder.
  • the relatively low number of cylinders will be less than four.
  • FIG. 1 is an axial section through a fuel injection pump which is intended for use in a two-cylinder engine but whose pumping member is rotated at a speed corresponding to that of a pumping member in a fuel injection pump for a four-cylinder engine;
  • FIG. 2 is an enlarged fragmentary section as seen in the direction of arrows from the line II-II of FIG. 1 and illustrates the pumping member of the fuel injection pump in a rst angular position;
  • FIG. 3 is a similar fragmentary section and illustrates the pumping member in a different angular position
  • FIG. 4 is an enlarged fragmentary section as seen in the direction of arrows from the line IV-IV of FIG. 1;
  • FIG. 5 is a section similar to that of FIG. 2 but showing the pumping member and the housing of a fuel injection pump for use in a three-cylinder engine whereby the pumping member is driven at a speed corresponding to that of the pumping member in a pump f-or a sixcylinder engine;
  • FIG. 6 ⁇ is a section similar to that of FIG. 5 but showing the pumping member in an angular position corresponding to that of the pumping member shown in FIG. 3;
  • FIG. 7 is a section similar to that of FIG. 4 but showing the pumping member and housing of the pump shown in FIGS. 5 and 6;
  • FIG. 8 is a section similar to that of FIG. 2 but showing the pumping member and the housing of a fuel injection pump for a one-cylinder engine whereby by the pumping member is rotated at a speed corresponding to that of the pumping member in a pump for a four-cylinder engine;
  • FIG. 9 illustrates the structure of FIG. 8 with the pumping member in an angular position corresponding to that of the pumping member shown in FIG. 3;
  • FIG. 10 is a section similar to that of FIG. 4 but showing the pumping member and housing of FIGS 8 and 9;
  • FIG. 11 is a section through the housing and pumping member of a fuel injection pump for a two-cylinder engine wherein the injection of fuel takes place at unequal intervals;
  • FIG. 12 is a similar section but showing the pumping member of FIG. 11 in a different angular position
  • FIG. 13 is a section similar to that of FIG. 4 but showing the parts of FIGS. 11 and 12;
  • FIG. 14 is an axial section through a further fuel injection pump for use in connection with a one-cylinder engine
  • FIG. 15 is an enlarged fragmentary section as seen in the direction of arrows from the line XV-XV of FIG. 14;
  • FIG. 16 is a similar section but showing the pumping member and housing of a fuel injection pump for use in connection with a two-cylinder engine, the pump being constructed to deliver fuel at regular intervals;
  • FIG. 17 is a section similar to that of FIG. 16 but showing a modified housing which is utilized in pumps for use in connection with two-cylinder engines receiving fuel at irregular intervals;
  • FIG. 18 is a section similar to that of FIG. 15, 16 or 17 but showing the housing of a pump which can be used in connection with a three-cylinder engine.
  • a fuel injection pump which comprises a housing H and a pumping member here shown as a multistage piston P reciprocable in a composite blind bore 2 of the housing.
  • the bore 2 includes a first or working chamber 6 for a smaller-diameter first stage 1 of the piston, and a second chamber 4 (hereinafter called cylinder chamber) for a larger-diameter second stage 3.
  • the first stage 1 serves to inject fuel to the cylinders of an engine, not shown, and the second stage 3 serves to control the operation of a pressureresponsive regulating valve 5.
  • the shaft 3a at the outer axial end of the stage 3 forms part of a drive which causes the piston P to rotate and to simultaneously reciprocate with reference to the housing H at a rate depending on the speed of the engine and in a manner well known from the art of fuel injection pumps.
  • the shaft 3a may be coupled to a cam having an annular face provided with four equidistant lobes and being driven by a rotary output shaft which receives motion from the engine.
  • follower rollers which are rotatable about fixed axes track the face of the cam ⁇ and cause the piston P to move up and down while the piston rotates with the output shaft.
  • the cam and follower assembly 3b and the engine E are shown diagrammatically in the lower part of FIG. 1.
  • the working chamber 6 can receive fuel from a suction space 7 which is formed in the housing H and is connected with a supply conduit 7a leading to a suitable source 7b of fuel, i.e., a fuel pump which draws fuel from a tank.
  • the working chamber 6 receives fuel from the space 7 when the piston P performs a suction (downward) stroke.
  • Such fuel can flow from the space 7 through two suction ports 8 whose outlets 9 are located in the surface surrounding the bore 2, four axially extending grooves 10 machined into the periphery of the stage 1, through an annular groove 11 which is also machined into the periphery of the stage 1 and communicates with the axial grooves 10, and through a T-shaped bore 12 formed in the stage 1 and connecting the annular groove 11 with the working chamber 6.
  • the ports 8, grooves 10, 11 and bore 12 together constitute a system of intake channels which can convey fuel from the source 7b to the working chamber 6 in response to each suction stroke of the piston or pumping member P.
  • each of these fuel lines 14 leads to the intake valve of an engine cylinder and contains a ball check valve 15.
  • the groove 13 and the lines 14 together form a system of discharge channels which can convey fuel from the chamber 6 to the cylinders of the internal combustion engine E when the piston P performs effective working strokes.
  • a relief bore 16 connects the working chamber 6 with an annular space 17 between the plungers 5a, 5b of the regulating valve 5.
  • the annular space 17 can connect the relief bore 16 with a duct 19 communicating with a duct 19a which discharges into a compartment 19b accommodating a return spring 18.
  • the spring 18 bears against a head or boss 29 of the valve 5 and urges the boss into sealing engagement with the internal surface 5c of the housing H.
  • the compartment 19b communicates with the suction space 7 through a return bore 19e.
  • the larger stage 3 can receive fuel through suction ports 20 whose inlets communicate with the suction space 7 and whose outlets 21 communicate with the cylinder chamber 4.
  • fuel filling the cylinder chamber 4 can escape through one of several axially extending groovesi 22 machined into the periphery of the stage 3, suchfuel then flowing into a connecting bore 23 which contains a ball check valve 24 and discharges into the auxiliary chamber 25.
  • the valve 5 can be displaced against the bias of the return spring 18 by the pressure of fuel which is supplied via connecting bore 23.
  • the spring 18 pushes the valve 5 back in a direction to the left, as viewed in FIG.
  • the spring 18 invariably returns the boss 29 into abutment with the surface 5c before the piston begins the next working stroke.
  • the valve 5 has no time to return to its starting position and the auxiliary chamber 25 receives from the connecting bore 23 fuel before the boss 29 returns into abutment with the surface 5c. Consequently, a shorter interval of time is needed to shift the valve 5 against the bias of the spring 18 to such an extent that the annular space 17 connects the relief bore 16 with the duct 19, i.e., the injection of fuel into one of the fuel lines 14 is terminated sooner and the corresponding cylinder of the engine receives less fuel.
  • fuel admitted by the connecting bore 23 acts not unlike a liquid stop and reduces the amount of fuel which is injected into a cylinder.
  • the reduct'on in the amounts of injected fuel is proportional with the rotational speed of the piston P, i.e., with the extent to which the speed of the piston exceeds the aforementioned predetermined speed.
  • theV first stage 1 is formed with four equidistant axial grooves (see FIG. 2), and the stage 3 is formed with four equidistant axial grooves 22 (see FIG. 4).
  • the piston P will perform four suction strokes and four working strokes.
  • two of the four working strokes must be ineffective, i.e., the fuel expelled from the working chamber 6 during two of four working strokes performed by the piston P during each of its revolutions must be returned into the suction space 7 or into another space defined by a. suitable receptacle connected to or spaced from the housing H.
  • the pump of FIG. 1 can produce such ineffective working strokes due to the provision of two overflow channels 30 (hereinafter called recesses) which are machined into the periphery of the stage 1 and each of which communicates with one of the axial grooves 10.
  • FIG. 2 shows that the recesses 30 are located substantially diametrically opposite each other and that each thereof is adjacent to one side of the corresponding groove 10, as seen in the circumferential direction of the stage 1.
  • the recesses 30 permit the working chamber 6 to remain in communication with the suction space 7 through the corresponding axial groove 10, annular groove 11, bore 12 and suction ports 8.
  • the housing H is formed with two ports 8 which are located diametrically opposite each other so that, when the piston P is to perform an ineffective working stroke, each recess 30 communicates with one of the ports 8.
  • the distribution of the ports 8 and 20, axial grooves 10 and 22, and recesses 30 in the pump of FIG. 1 is such that the stage 1 can inject fuel at regular intervals.
  • the common plane of the grooves 10 which are not connected with recesses 30 makes an angle of 90 degrees with the common plane of the remaining two grooves 10.
  • the grooves 22 and suction ports 20 are respectively equidistant from each other, and the ports 8 communicate with the bore 2 at points which are located diametrically oppo site each other.
  • the hsusing H is formed with only two fuel lines 14 which communicate with the bore 2 at points located diametrically opposite each other.
  • FIG. 1 merely shows one of the lines 14.
  • FIG. 2 illustrates the stage 1 in an angular position while the piston P performs an effective working stroke.
  • the grooves 10 and recesses 30 cannot communicate with the suction ports 8, and the groove 13 connects Vthe working chamber 6 with one of the fuel lines 14. Therefore, and since the stage 1 moves upwardly, as viewed in FIG. l, the volume of the chamber 6 is reduced and a measured amount of fuel is compelled to overcome the bias of the spring in the check valve 15 and to flow on to the intake valve of the corresponding cylinder of the engine E.
  • FIG. 3 illustrates the stage 1 in an angular position when the piston P performs an ineffective working stroke.
  • the two suction ports 8 communicate with the recesses 30 and with the corresponding axial grooves 10 so that, as the piston P moves upwardly, the stage 1 expels fuel from the working chamber 6 via bore 12, annular groove 11, the two grooves 10, recesses 30, suction ports 8, and back into the space 7.
  • the stage 1 is displaced through degrees with with reference to the position shown in FIG. 2. While the two grooves 10 communicate with the suction ports 8 via recesses 30, the groove 13 does not communicate with either of the two fuel lines 14.
  • the auxiliary pump operates in a manner as shown in FIG. 4.
  • the grooves 22 of the stage 3 are sealed from the suction ports 20 ⁇ whenever the piston P performs a working stroke so that the stage 3 expels fuel into the connecting bore 23 and hence into the auxiliary charnber 25.
  • the grooves 22 connect the cylinder chamber 4 with the suction ports 20, and and one of the grooves 22 connects the chamber 4 with the connecting bore 23 during each working stroke.
  • the bore 23, chamber 25, duct 19a, compartment 19b and bore 19C together form a composite passage which connects the chamber 4 with the space 7 and wherein the flow of fuel is regulated by the valve 5.
  • the pump of FIGS. 1 to 4 may be used, with minor modifications, to supply fuel to the cylinders of a fourcylinder internal combustion engine.
  • the rotational speed of the piston P can remain the same which is important because the aforementioned cam-and-follower assembly 3b in the drive for the piston P can remain unchanged.
  • the piston will perform four suction strokes and four working strokes in response to each full revolution, regardless of whether it is used in a fuel injection pump for two-cylinder engines E or four-cylinder engines.
  • the housing of both types of pumps will be substantially the same, i.e., all that is necessary to use the housing H of FIG. 1 in a pump for a four-cylinder engine is to provide this housing with four equidistant fuel lines 14 and with four check valves 15.
  • the auxiliary pump including the stage 3 remains unchanged, and the same holds true for the regulating valve 5.
  • the stage 1 of the piston P will be without recesses 30.
  • the throttling passage 27a, the throttle 27, 28 and the number of working and suction strokes per revolution of the piston will remain unchanged.
  • Known fuel injection pumps which are used for engines having a large number of cylinders and which comprise a liquid stop operating on the samme principle as the liquid stop in the pump of FIG. 1 are provided with throttles which, as a rule, have a relatively large cross-sectional area. This reduces the likelihood of clogging by impurities which are present in the fuel and allows for more precise regulation of the injected amounts of fuel. It is to be borne in mind that a relatively small adjustment of the throttle can bring about a substantial change in the amounts of injected fuel if the passage which is throttled is of relatively small cross sectional area.
  • a pump which is built specifically for use with three-cylinder engines comprises a piston which performs only three working strokes.
  • the required cross-sectional area of the throttled passage is inversely proportional to the length of time intervals between successive working strokes, i.e., a pump for a six-cylinder engine can have a throttling passage whose cross-sectional area is twice the cross-sectional area of the throttling passage in a conventional pump for use with three-cylinder engines. This holds true for all types of fuel injection pumps including those which inject fuel into a manifold and wherein the metering operation is controlled by a suction throttle.
  • a pump which is constructed in accordance with our present invention can be provided with a more sensitive and more accurate liquid stop because the number of working strokes performed by the revolving piston per each revolution is much higher than in presently known fuel injection pumps for engines having a relatively small number of cylinders. This is due to the fact that, in using a fuel injection pump in connection with engines having one, two or three cylinders, the number of working strokes (including effective and ineffective working strokes) per full revolution of the piston is a whole multiple of the number of cylinders.
  • the throttling passage 27 has a cross-sectional area which suffices to prevent clogging by impurities and which allows for highly precise selection of the exact moment when, at a given r.p.m. of the engine E, the regulating valve 5 allows for ow of fuel from the relief bore 16 into the duct 19 and back to the source, e.g., to the suction space 7.
  • FIGS. 5, 6 and 7 illustrate certain details of a fuel injection pump which is used in connection with a threecylinder engine.
  • the stage 1 of the piston is formed with six equidistant axial grooves 10 and with three equidistant overflow channels or recesses 30 each of which communicates with one of the grooves 10, i.e., grooves 10 communicating with recesses 30 alternate with the remaining three grooves 10.
  • the stage 3 has six equidistant axial grooves 22 and the housing of this pump is provided with six equidistant suction ports 20.
  • the piston which includes the stages 1 and 3 of FIGS. 5 to 7 performs six suction strokes and six working strokes.
  • FIG. 5 shows the stage 1 in an angular position when the piston performs an effective working stroke.
  • the grooves 10 and recesses 30 cannot communicate with the suction ports 8 and the groove 13 (see FIG. l) communicates with one of the three fuel lines 14.
  • FIG. 6 the stage 1 is shown in an angular position when the piston performs an ineffective working stroke.
  • Each of the three recesses 30 communicates with one of the three suction ports 8 so that the stage 1 can expel fuel from the working charnber 8 (see FIG. 1) back into the space 7.
  • a pump which is used in connection with a sixcylinder engine is very similar -to the pump of FIGS. 5 to 7. All that is necessary is to replace the piston with one whose stage 1 has six equidistant grooves 10 but is without recesses 30.
  • the housing of the pump for a six-cylinder engine may have a total of six equidistant suction ports 8. Otherwise, the pump for a six-cylinder engine operates in the same way as described in connection with FIG. l.
  • FIGS. 8 to 10 there are shown certain details of a pump which is used in connection with a onecylinder engine.
  • the piston which includes the stages 1 and 3 respectively shown in FIGS. 8-9 and l0 performs four suction strokes and four working strokes during each of its full revolutions; however, three of the working strokes are ineffective because the stage 1 is formed with four axial grooves 10 and with three overflow channels or recesses 30.
  • the housing of this pump has a single port 8 which communicates with a different recess 30 during three of each four successive working strokes. Furthermore, the housing has a single fuel line 14, not shown in FIGS. 8 to l0.
  • the stage 3 (see FIG. 10) is constructed in the same way as described in connection with FIG. 4. In FIG.
  • the stage 1 is shown in an angular position when the piston performs an effective working stroke be cause the grooves 10 and recesses 30 cannot communicate with the single port 8 and the piston is assumed to expel fuel from ⁇ the chamber 6 (see FIG. 1) through the groove 13 and into the single fuel line 14.
  • the stage 1 assumes an angular position in which the piston performs an ineffective working stroke because one of the recesses 30 communicates with the port 8.
  • the advantages yof the fuel injection pump for a onecylinder engine are the same as those described in connection with FIGS. 1 to 4.
  • the free cross-sectional area of the throttle 27, 28 which is used in this pump is four times the size of the cross-sectional area of the throttle in a fuel injection pump which is built especially for a one-cylinder engine.
  • FIGS. 11, 12 and 13 again show certain parts of a fuel injection pump for a two-cylinder engine.
  • This pump is very similar to that of FIGS. 1 to 4 with the exception that the stage 1 of [the piston has ia single overflow channel or recess 30 and that the annular distance between the ports 8 is only 90 degrees.
  • the piston will perform two consecutive ineffective working strokes followed by two effective working strokes.
  • the angular distance between a first position in which the piston performs a first effective working stroke land a second position in which the piston performs the next effective working stroke is 270 degrees, and the angular distance between the second and first positions (as seen in the direction in which the piston rotates) is only degrees.
  • the recess 30 When the piston rotates, the recess 30 first sweeps one of the ports 8 during a rst working stroke to make such stroke ineffective and thereupon sweeps the second port 8 during the next working stroke, 4again to render such second working stroke ineffective.
  • the two ineffective working strokes are followed by two effective working strokes.
  • 1the angular distance between the two fuel lines of the housing H shown in FIGS. 11 to 13 must be 90 degrees.
  • the auxiliary pump including the stage 3 (see FIG. 13) is constructed and operates in the same way as described in connection with FIG. 4.
  • overflow channels have portions which are common to intake channels and such common portions are provided in part in the periphery of the piston.
  • FIG. 14 shows a modified fuel injection pump which differentiates from the previously described pumps in that fuel which escapes or is expelled from the working chamber 6 when the piston P is to perform an ineffective working stroke flows through the distributor groove 13 of the first stage 1, i.e., along the same route as such fuel which is actually injected into a cylinder.
  • the overflow channel means and the discharge channel means of the pump shown in FIG. 14 have a common portion 13 which is -machined into the periphery of the stage 1. This is -achieved by forming the housing H with three overflow bores 31 which are located at the level of the fuel line 14 and tare distributed circumferentially of the stage 1 in a manner as shown in FIG. 15.
  • FIG. 15 shows the stage 1 of the modified pump in an angular position when the piston P performs a suction stroke.
  • the groove 13 is out of communication with the fuel line 14 or with the overflow bores 31 and the bore 12 (see FIG. 14) communicates with the suction space 7 via ports 8, annular groove 11, and axial grooves 10.
  • FIG. 16 shows a portion of a different pump which is similar to the pump of FIGS. 14 and 15 with the exception that its housing H comprises two fuel lines 14 alternating with tw-o overflow bores 31.
  • This pump is intended for use in connection with a two-cylinder engine and each second working stroke of the piston 1P is ineffective.
  • the fuel lines 14 and the overflow bores 31 are respectively located dametrically opposite each other and each overflow bore 31 is located exactly midway between the fuel lines 14.
  • the piston P of the pump shown in FIG. 16 performs four working strokes (including two effective working strokes which alternate with two ineffective working strokes) and four suction strokes.
  • FIG. 17 shows a portion of a further fuel injection pump wherein the housing H comprises the same number of overflow bores 31 and fuel lines 14 as in FIG. 16.
  • the angular distance between the overflow bores 31 is only 90 degrees and the angular distance between the fuel lines 14 is also only 90 degrees. Therefore, this pump will operate in the same way as described in connection with FIGS. 11 and 12, i.e., two effective working strokes (when the distributor groove 13 communicates with one of the fuel lines 14) will be followed by two ineffective working strokes when the distributor groove 13 communicates with one of the overflow bores 31.
  • This pump is used in connection lwith a two-cylinder engine and its piston P performs a total of four working strokes and four suction strokes during each full revolution of its drive shaft 3a.
  • the remaining parts of this pump are constructed in the same way as shown in FIG. 14.
  • FIG. 18 illustrates a portion of a further pump wherein the housing H comprises three equidistant fuel lines 14 alternating with three equidistant overflow bores 31.
  • This pump is used in connection with a three-cylinder engine but can be readily modified to be used in connection with a six-cylinder engine. This can be done by replacing the housing H with a housing having no overflow bores 31 but provided with six equidistant fuel lines 14.
  • the angular distance between the adjoining fuel lines 14 and overflow bores 31 shown in FIG. 18 is 60 degrees.
  • FIGS. 14 and 18 The advantages of the pumps shown in FIGS. 14 and 18 are the same as those which ⁇ were described in connection with FIG. 1.
  • a pump which is used in connection with a three-cylinder or two-cylinder engine can be rapidly converted into a pump for use with la six-cylinder or four-cylinder engine.
  • a pump in use for a one-cylinder engine can be converted for use 'in connection with a four-cylinder engine.
  • a fuel injection pump for supplying fuel to an internal combustion engine having a predetermined number of cylinders, in combination: a source of fuel; housing means defining a working chamber; passage means extending from said source of fuel to said working chamber; discharge channel means adapted to communicate with said working chamber; a piston mounted in said working chamber rotatable about its axis and axially reciprocable to perform alternate suction and working strokes to respectively draw fuel from said passage means into said chamber and to expel fuel from said chamber into said discharge channel means; a plurality of angularly displaced axial grooves formed in the periphery of said piston and equal in number to a multiple of said predetermined number and respectively adapted to establish communication between said chamber and said passage means during each suction stroke of said piston; a plurality of recesses connected respectively to some of said grooves and each extending from the respective groove in a direction opposite to the direction of rotation of said piston for such a distance as to establish also during the respective working stroke communication between said chamber and said passage means so as to render the pump in
  • said discharge channel means comprises a substantially axially extending distributor groove provided in the periphery of said piston and communicating with said working chamber, and fuel line means provided in said housing means and positioned to communicate with said groove when said piston performs an effective working stroke, the number of said fuel line means being equal to said rst number and each such fuel line means being arranged to feed fuel to a separate cylinder of the engine, said passage means comprising bore means provided in said housing means to connect said recess with said source when said piston performs an ineffective working stroke, the number of said bore means being equal to the difference between said second and irst numbers,
  • said piston comprises a second stage operating in a second chamber of said housing means, said second chamber being connected with said source and further comprising regulating valve means responsive to pressure of fuel expelled from said second chamber by said second stage to provide a liquid stop which reduces the quantity of fuel entering said discharge channel means when the rotational speed of said piston exceeds a predetermined value.
  • said regulating valve means comprises a slide valve movable in an auxiliary chamber provided in said housing means
  • said housing means further having a connecting bore for conveying fuel from said second chamber to said auxiliary chamber and a throttling passage connecting said last named chambers.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
US537759A 1965-04-01 1966-03-28 Fuel injection pump Expired - Lifetime US3404668A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR11638A FR1449640A (fr) 1965-04-01 1965-04-01 Perfectionnements apportés aux pompes d'injection de combustible à distributeur rotatif

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US3404668A true US3404668A (en) 1968-10-08

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US537759A Expired - Lifetime US3404668A (en) 1965-04-01 1966-03-28 Fuel injection pump

Country Status (6)

Country Link
US (1) US3404668A (pt)
AT (1) AT268781B (pt)
BR (1) BR6678333D0 (pt)
DE (1) DE1273903B (pt)
FR (1) FR1449640A (pt)
GB (1) GB1145977A (pt)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4112902A (en) * 1975-08-09 1978-09-12 Talleres Diesel, S.A. Hydraulic speed control systems for internal combustion engines
US4385610A (en) * 1980-05-06 1983-05-31 Robert Bosch Gmbh Fuel injection pump for combustion engines
US4387686A (en) * 1981-01-27 1983-06-14 Robert Bosch Gmbh Fuel injection apparatus for internal combustion engines, in particular for diesel engines
US4398519A (en) * 1980-07-02 1983-08-16 Robert-Bosch Gmbh Fuel injection apparatus for internal combustion engines, in particular for diesel engines
US4398518A (en) * 1980-01-12 1983-08-16 Robert-Bosch Gmbh Fuel injection apparatus for internal combustion engines, in particular for diesel engines
US4489684A (en) * 1981-05-06 1984-12-25 Diesel Kiki Co., Ltd. Fuel injection pump assembly
US4501246A (en) * 1981-07-22 1985-02-26 Robert Bosch Gmbh Fuel injection pump
US4510908A (en) * 1982-03-31 1985-04-16 Robert Bosch Gmbh Fuel injection pump
US4567868A (en) * 1983-09-30 1986-02-04 Nissan Motor Company, Limited Fuel injection system for an internal combustion engine

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2239692C2 (pt) * 1972-08-12 1989-11-30 Robert Bosch Gmbh, 7000 Stuttgart, De

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3044404A (en) * 1959-12-01 1962-07-17 Bessiere Pierre Etienne Self-regulating reciprocating pumps, in particular for the injection of fuel into internal combustion engines
US3057299A (en) * 1960-02-29 1962-10-09 Vernon D Roosa Fuel pump
US3157173A (en) * 1961-06-29 1964-11-17 Mono Cam Ltd Fuel injection pumps
US3168042A (en) * 1960-01-08 1965-02-02 Expl Des Procedes Chimiques Et Pumps, and in particular fuel injection pumps having opposed pistons and a rotary distributing valve element
US3185140A (en) * 1963-07-02 1965-05-25 Clessie L Cummins Fuel supply system for compression ignition internal combustion engines
US3319616A (en) * 1964-02-25 1967-05-16 Cav Ltd Liquid fuel pumps for use with internal combustion engines

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1423310A (fr) * 1965-02-01 1966-01-03 Cav Ltd Pompe à combustible liquide pour moteur à combustion interne

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3044404A (en) * 1959-12-01 1962-07-17 Bessiere Pierre Etienne Self-regulating reciprocating pumps, in particular for the injection of fuel into internal combustion engines
US3168042A (en) * 1960-01-08 1965-02-02 Expl Des Procedes Chimiques Et Pumps, and in particular fuel injection pumps having opposed pistons and a rotary distributing valve element
US3057299A (en) * 1960-02-29 1962-10-09 Vernon D Roosa Fuel pump
US3157173A (en) * 1961-06-29 1964-11-17 Mono Cam Ltd Fuel injection pumps
US3185140A (en) * 1963-07-02 1965-05-25 Clessie L Cummins Fuel supply system for compression ignition internal combustion engines
US3319616A (en) * 1964-02-25 1967-05-16 Cav Ltd Liquid fuel pumps for use with internal combustion engines

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4112902A (en) * 1975-08-09 1978-09-12 Talleres Diesel, S.A. Hydraulic speed control systems for internal combustion engines
US4398518A (en) * 1980-01-12 1983-08-16 Robert-Bosch Gmbh Fuel injection apparatus for internal combustion engines, in particular for diesel engines
US4385610A (en) * 1980-05-06 1983-05-31 Robert Bosch Gmbh Fuel injection pump for combustion engines
US4398519A (en) * 1980-07-02 1983-08-16 Robert-Bosch Gmbh Fuel injection apparatus for internal combustion engines, in particular for diesel engines
US4387686A (en) * 1981-01-27 1983-06-14 Robert Bosch Gmbh Fuel injection apparatus for internal combustion engines, in particular for diesel engines
US4489684A (en) * 1981-05-06 1984-12-25 Diesel Kiki Co., Ltd. Fuel injection pump assembly
US4501246A (en) * 1981-07-22 1985-02-26 Robert Bosch Gmbh Fuel injection pump
US4510908A (en) * 1982-03-31 1985-04-16 Robert Bosch Gmbh Fuel injection pump
US4567868A (en) * 1983-09-30 1986-02-04 Nissan Motor Company, Limited Fuel injection system for an internal combustion engine

Also Published As

Publication number Publication date
DE1273903B (de) 1968-07-25
GB1145977A (en) 1969-03-19
FR1449640A (fr) 1966-05-06
BR6678333D0 (pt) 1973-07-10
AT268781B (de) 1969-02-25

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