US3175499A - Piston pump having a variable stroke - Google Patents
Piston pump having a variable stroke Download PDFInfo
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- US3175499A US3175499A US248428A US24842862A US3175499A US 3175499 A US3175499 A US 3175499A US 248428 A US248428 A US 248428A US 24842862 A US24842862 A US 24842862A US 3175499 A US3175499 A US 3175499A
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- pressure
- piston
- fluid
- fuel
- pump
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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
- F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
- F02M59/02—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type
- F02M59/04—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by special arrangement of cylinders with respect to piston-driving shaft, e.g. arranged parallel to that shaft or swash-plate type pumps
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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
- F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
- F02M59/02—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type
- F02M59/10—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by the piston-drive
- F02M59/105—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by the piston-drive hydraulic drive
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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
- F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
- F02M59/20—Varying fuel delivery in quantity or timing
- F02M59/30—Varying fuel delivery in quantity or timing with variable-length-stroke pistons
Definitions
- the invention relates to pumps of the kind in which a piston, working in a coacting cylinder, is associated with operating means which is adapted intermittently to move the piston against the action of a progressively increasing bias (e.g., a spring) whereby to causethe piston to reciprocate to give a pumping action.
- the invention is primarily intended for application to pump-s of the kind set forth which are for supplying fuel to the induction system of an internal-combustion engine but has application in other fields.
- a pump of the kind set forth, has a control fluid under pressure adapted to exert a force on the piston, in opposition to the bias, whereby variations in the pressure of the control fluid determine the length of the induction stroke and consequently the output of the pump at any given speed.
- the piston has a head which is arranged to be acted on alternately by the control fluid to produce the induction stroke, and by the operating means, which is an operating fluid under such a pressure that the resultant force exerted on the piston produces the Working stroke.
- control fluid may be derived from the supply of lubricating oil for the engine.
- control fluid may be derived from the supply of fluid that is to be metered.
- the piston may be reciprocable in a cylinder block which is supported for rotation in a casing provided with two chambers that are respectively for applying the pressure of the control fluid, and for applying the pressure of the operating fluid, to the head of the piston, according to the angular position of the cylinder block relative to the casing, the cylinder block and the casing being provided with an inlet port for supplying fluid for the piston to pump, and with an outlet port for the fluid that has been pumped by the piston, the ports being so arranged that the piston is connected to the inlet port whenever its head is in communication with the control fluid chamber, and that the piston is connected to the outlet port whenever its head is in communication with the operating fluid chamber.
- the cylinder block may, according to another feature, have a circular end face coaxial with and lying in a plane normal to its axis of rotation, the end face having a communication with the piston head and being arranged to abut an axially-movable, but rotatively-stationary, piston which is guided by the casing and has the control fluid chamber and the operating fluid chamber defined in its end that abuts the cylinder block,
- Patented Mar. 30, 1965 head may also be circular and be coaxial with and lie in a plane normal to its axis of rotation, the end face remote from the piston head being arranged to abut an internal wall of the casing defining the inlet and outlet ports, the effective area of the said end of the rotativelystationary piston remote from the cylinder block being such that the end face of the cylinder block remote from the piston head is urged into sealing contact with the said internal wall of the casing to check leakage between the outlet port and the inlet port.
- the pressure of the control fluid may be altered by means, associated with the apparatus being supplied by the pump, which is actuated responsively to a supply requirement of the apparatus and which varies the stroke of the piston for the pump to satisfy that supply requirement.
- the pressure of the control fluid may, according to another feature, be altered by a variablepressure relief valve which is actuated by a movable operating member, arranged to be acted upon by an appropriate operating parameter of the said apparatus, whereby to adjust the pressure of the control fluid such that the delivery of fluid, from the pump to the said apparatus, at least, substantially matches the supply of fluid required by the apparatus.
- the movable operating member may be fast with diaphragm means connected to be acted upon by the said parameter.
- the movable operating member may be biased by a spring to close the variable-pressure relief valve when the said apparatus is not operating or is operating at very low speed, and means are provided for adjusting the bias exerted by the spring whereby to tune the pump.
- a pump may, according to still another feature, be adapted to be driven at a direct function of engine speed whereby to enable the pressure of the control fluid to be made independent of the engine speed.
- FIGURE 1 is an elevation of a pump
- FIGURE 2 is a plan of FIGURE 1;
- FIGURE 3 is a section taken on the line 33 of FIG- URE 1;
- FIGURE 4 is a section taken on the line 44 of FIG- URE 3;
- FIGURE 5 is a section taken on the line 55 of FIG- URE 2;
- FIGURE 6 is a section taken on the line 66 of FIG- URE 2;
- FIGURE 7 is a section taken on the line 77 of FIG- URE 2;
- FIGURE 8 is a section taken on the line 88 of FIG- URE 2, and
- FIGURE 9 shows, diagrammatically, the operation of the pump illustrated by FIGURES 1 to 8.
- the pump is provided with a supply of fuel under high pressure through pipe union 52 and has an outlet 53 for metered fuel and a spill outlet 54 for by-passing excess fuel.
- the manifold depression is conveyed to the pump through pipe union 55, and the atmospheric pressure through an aperture 56.
- the metered fuel outlet 53 is arranged in a lower casing portion 57 which is integral with a boss 58 serving to locate the pump relatively to the engine casing.
- the lower casing portion 57 is formed with an arcuate mined value.
- the piston 67 is provided with two chambers 75, 76 which are of arcuate shape as will be appreciated from ing an eccentric boss 66 of a piston 67, whereby to pre- FIGURE 2.
- Chamber 75 communicates with'space 61 through a port 77, shown in FIGURE 6, and contains fuel under high pressure;
- An orifice 78 allows fuel to escape from space 61 to chamber 76 which is connected to spill outlet 54 through bore 79 in eccentric boss 66, as will be seen in'FIGURE 7, through port 80 to chamber 81 in the upper casing portion 64, see FIGURE 6, and through pintle valve 82 to spill outlet 83 as will be seen in FIGURE 5.
- pintle valve 82 will controlthe flow of fuel from chamber 76 to spill outlet 54 and, consequently, will control the flow of fuel through orifice 78 and the pressure of the fuel in chamber 76 and fuel to be pumped, which is permanently in communication with a port 89 in the lower portion 70 of the rotor.
- the piston 67 is arranged relatively to the arcuate ports 59 and 60 so that the pistons 84 are acted upon by the high pressure fuel in chamber 75 Whenever their respective ports 89 are registering with fuel outletport 60, and
- the pressure of the fuel inhigh pressure fuel chamber 75 is arranged to be sufficient to cause the heads 85 to abut portion 70 of the rotor.
- the induction stroke isv limited by the head 85 of the piston 84 abutting the upper portion ii 69 of the rotor and this prevents the pistons 84 fouling r 4 v the piston 67.
- the induction stroke is controlled by the pressure of fuel in low pressure fuel chamber 76 which exerts a force on thepiston 84 in opposition to the force of its spring 86.
- the induction stroke of the pistons 84, and consequently the output of the pump at any given speed may be controlled by operating the pintle valve 82 to control the pressure of the fuel in low pressure fuel chamber 76.
- pintle valve 82 when pintle valve 82 is fully open, the pressure of the fuel in low pressure fuel chamber 76 will be substantially zero, and the output of the pump at any given speed will be a maximum. Conversely, when the pintle valve 82 is closed, the pressure of the fuel in low pressure fuel chamber 76 will be equal to the pressure of the fuel in high pressure fuel chamber 75, and the output of the pump will be Zero irrespective of the speed of the pump.
- Chamber 81 is defined on one side by a diaphragm 43 which is sealingly anchored at its periphery between a plate 90 and upper casing portion 64, and is axially fast with pintle valve 82.
- a diaphragm 47 bears on pintle valve 82 and is sealingly anchored at its periphery between an end plate 91 and plate 90.
- Atmospheric pressure is applied to a chamber 49 through aperture 56 to act on one side of diaphragm 47, and the manifold depression is applied through pipe union 5 and passage 92,- see FIGURE 6, to act on the other side of diaphragm 47.
- the pressure of the fuel in arcuate inlet port 59 is applied through arcuate passage 92 inlower casing portion 57, see FIGURES 3 and 8, and passage 94 to chamber 50 to act on the side of diaphragrnr43 opposite to chamber 81.
- Spring 51 biases the pintle valve 82 to close spill outlet 83 when the pump is at'rest.
- a screwed adjuster 52 is a datum setting device which alters the setting of spring 51 for tuning the pump. As will be seen from FIGURE 6, the adjuster 52 is surrounded by a sleeve 95 which is held rotatively fast with end plate 91 by dog 96, and is urged into engagement with the adjuster 52 by a compression coil. spring 97 whereby to prevent the adjuster 52 from rotating accidentally due to vibration from the engine to which the pump is mounted.
- the plates 90v and 91 and the diaphragms 43 and 47 are secured to the. upper casing portion 64 by six bolts 98, and the casing portions 57, 64 and 68 are held together by three bolts 99 as will be seen in FIGURES 3 and 7.
- Three holes 100, see FIGURES 2,73 and 7, pass through the pump and are for receiving studs for holding the lower casing portion 57 to the engine casing.
- the pistons 84 are preferably made of hardened steel and the upper portion 69 of the rotor is preferably made tons 84. Lubrication difliculties occur when petroleum spirit is pumped and, for this purpose, the upper portion 69 of the rotor has a facing 101 of carbon graphite for bearing against the'piston 67 which is of hardened steel, Similarly, the lower casing portion 57 has a facing 1 02 of carbon graphite for bearing against the lower portion of the rotor which is also hardened steel.
- the piston '67 is axially movable in the intermediate casing portion 68 and the effective areas of its face definingspace 61, of its eccentric boss 66, and of the chambers 75 and 76 areso arranged that the vvarious fuel bers .75eand 76, and urges the rotor into contact with the graphite facing 102 to prevent leakage between ports 59 and 60. Leakage past the piston 67 is prevented by a seal 103, and leakage from space 61to eccentric recess 65 is prevented by a seal 104. It will be apparent to a person skilled in the art that the pump is self-compeneating for wear and obviates the need for a high degree of accuracy in many of its components.
- the power input shaft 73 is cooled and lubricated by fuel which passes from fuel inlet port 59 through groove 105 in graphite facing 102 to the shaft 73, and is returned to the spill side of relief valve 63 through passage 106 and arcuate port 107 in the lower casing portion 57.
- FIGURE 9 how the output of the pump, at any given speed, is varied to suit the operating conditions of the engine it supplies.
- Two pistons 84 have been shown but, for the purpose of distinguishing between them, one has been denoted 84a. Due to the diagrammatic arrangement of FIGURE 9, piston 67 has been omitted and chambers 75 and 76 are separated by a diametral web 108. Also, the pistons 84, 84a have been simplified and are retained by circlips 109 as shown, and space 61 is coincident with chamber 75.
- the piston 84a is shown in a position such that the pressure of the fuel in chamber 76 balances all other forces acting on it and, accordingly, prevents it from making a complete induction stroke by not allowing the head of piston 84a to abut circlip 109. If the pressure of the fuel in chamber 76 is increased, the stroke of the piston will decrease and vice versa. Thus, at any operating speed of the pump its output can be varied from zero, to a maximum for the speed at which it is operating, by varying the pressure of the fuel in chamber 76 which is achieved by controlling pintle valve 82 to adjust spill outlet 83.
- the diaphragms 43 and 47 are so arranged that the pressures of the atmosphere, fuel supply and induction depression are balanced against the pressure of the fuel in chamber 81, by varying the rate at which the fuel escapes through spill outlet 83.
- the pintle valve 82 moves, as a result of the unbalanced pressures, so as to reduce the escape of fuel through spill outlet 83 whereby to increase the pressure of the fuel in chamber 76 until balance is regained by -a higher fuel pressure which in turn reduces the stroke of the pistons 84 and thus reduces the fuel supply to the engine.
- the induction pressure is increasing, the power output of the engine will be increasing and the unbalanced pressures will cause the fuel pressure in chamber 76 to be reduced whereby to increase the output of the pump.
- a pump comprising a rotor defining a cylindrical bore with its axis parallel with but radially-spaced from the axis of the rotor, a piston coacting with said cylindrical bore, a casing surrounding said rotor, an inlet valve means and an outlet valve means for said cylindrical bore, said piston when moved in one direction in said cylindrical bore adapted to induce fluid into said cylindrical bore through said inlet valve means to provide an induction stroke, and said piston when moved in the opposite direction in said cylindrical bore adapted to educe fluid from said cylindrical bore through said outlet valve means to provide a working stroke, a compression coil spring acting between said rotor and said piston to exert thereon a force for producing said induction stroke, said rotor remote from said inlet valve means and said outlet valve means having an end face, said casing having an end face for coaction with said end face of said rotor, said rotor defining a fluid commuication between said piston and said end face of said rotor, said end face of said casing defining a chamber
- a pump comprising a rotor defining a cylindrical bore with its axis parallel with but radially-spaced from the axis of the rotor, a piston coacting with said cylindrical bore, a casing surrounding said rotor, an inlet valve means and an outlet valve means for said cylindrical bore, said piston when moved in one direction in said cylindrical bore adapted to induce fluid into said cylindrical bore through said inlet valve means to provide an induction stroke, and said piston when moved in the opposite direction in said cylindrical bore adapted to educe fluid from said cylindrical bore through said outlet valve means to provide a working stroke, a compression coil spring acting between said rotor and said piston to exert thereon a force for producing said induction stroke, said rotor remote from said inlet valve means and said outlet valve means having an end face, a rotatively-stationary piston guided by said casing and having an end face for coaction with said end face of said rotor, said rotor defining a fluid communication between said piston and said end face of said rotor, said end face of
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- General Engineering & Computer Science (AREA)
- Reciprocating Pumps (AREA)
Description
March 1965 A. F. VARNEY ETAL 3,175,499
PISTQN PUMP HAVING A VARIABLE STROKE Filed Dec. 31. 1962 4 Sheets-Sheet l March 30, 1965 A, F. VARNEY ETAL 3,175,499
PISTON PUMP HAVING A VARIABLE STROKE Filed Dec. 31, 1962 4 Sheets-Sheet 2 IOI e4 v 69 85 85 March 30, 1965 A. F. VARNEY ETAL 3,175,499
PISTON PUMP HAVING A VARIABLE STROKE Filed Dec. 31, 1962 4 Sheets-Sheet 3 7 IO FIGG 6 &
7s 5%IO3 67 lOl g i I00 99 FIG7 n02 -s7 Q March 30, 1965 A. F. VARNEY ETAL 3,175,499
PISTON PUMP HAVING A VARIABLE STROKE Filed Dec. 31, 1962 4 Sheets-Sheet 4 43 8I 64 83 lO3 69 ::67 FIG 8 85,41 lOl "-68 United States Patent 3,175,499 PISTON PUMP HAVING A VARIABLE STROKE Arthur Francis Varney, Coventry, and Alfred John Bailey, Berkswell, near Coventry, England, assignors to Alvis Limited, Coventry, England Filed Dec. 31, 1962, Ser. No. 248,428 3 Claims. (Cl. 103-38) The invention relates to pumps of the kind in which a piston, working in a coacting cylinder, is associated with operating means which is adapted intermittently to move the piston against the action of a progressively increasing bias (e.g., a spring) whereby to causethe piston to reciprocate to give a pumping action. The invention is primarily intended for application to pump-s of the kind set forth which are for supplying fuel to the induction system of an internal-combustion engine but has application in other fields.
According to the invention a pump, of the kind set forth, has a control fluid under pressure adapted to exert a force on the piston, in opposition to the bias, whereby variations in the pressure of the control fluid determine the length of the induction stroke and consequently the output of the pump at any given speed.
According to the invention, the piston has a head which is arranged to be acted on alternately by the control fluid to produce the induction stroke, and by the operating means, which is an operating fluid under such a pressure that the resultant force exerted on the piston produces the Working stroke.
In the case where a pump is for supplying fuel to the induction system of an internal-combustion engine, the control fluid may be derived from the supply of lubricating oil for the engine. In the case where a pump is to be used as a metering device, the control fluid may be derived from the supply of fluid that is to be metered.
According to one feature, the piston may be reciprocable in a cylinder block which is supported for rotation in a casing provided with two chambers that are respectively for applying the pressure of the control fluid, and for applying the pressure of the operating fluid, to the head of the piston, according to the angular position of the cylinder block relative to the casing, the cylinder block and the casing being provided with an inlet port for supplying fluid for the piston to pump, and with an outlet port for the fluid that has been pumped by the piston, the ports being so arranged that the piston is connected to the inlet port whenever its head is in communication with the control fluid chamber, and that the piston is connected to the outlet port whenever its head is in communication with the operating fluid chamber.
In the case where the piston is arranged with its axis parallel with but radially-spaced from the axis of rotation of the cylinder block, the cylinder block may, according to another feature, have a circular end face coaxial with and lying in a plane normal to its axis of rotation, the end face having a communication with the piston head and being arranged to abut an axially-movable, but rotatively-stationary, piston which is guided by the casing and has the control fluid chamber and the operating fluid chamber defined in its end that abuts the cylinder block,
the operating fluid chamber being supplied with operating fluid from a space situated between the end of the rotatively-stationary piston remote from the cylinder block 3,175,499. Patented Mar. 30, 1965 head may also be circular and be coaxial with and lie in a plane normal to its axis of rotation, the end face remote from the piston head being arranged to abut an internal wall of the casing defining the inlet and outlet ports, the effective area of the said end of the rotativelystationary piston remote from the cylinder block being such that the end face of the cylinder block remote from the piston head is urged into sealing contact with the said internal wall of the casing to check leakage between the outlet port and the inlet port.
According to a still further feature, the pressure of the control fluid may be altered by means, associated with the apparatus being supplied by the pump, which is actuated responsively to a supply requirement of the apparatus and which varies the stroke of the piston for the pump to satisfy that supply requirement.
In such a case the pressure of the control fluid may, according to another feature, be altered by a variablepressure relief valve which is actuated by a movable operating member, arranged to be acted upon by an appropriate operating parameter of the said apparatus, whereby to adjust the pressure of the control fluid such that the delivery of fluid, from the pump to the said apparatus, at least, substantially matches the supply of fluid required by the apparatus. When the said appropriate operating parameter is a fluid pressure, the movable operating member may be fast with diaphragm means connected to be acted upon by the said parameter.
According to yet another feature, the movable operating member may be biased by a spring to close the variable-pressure relief valve when the said apparatus is not operating or is operating at very low speed, and means are provided for adjusting the bias exerted by the spring whereby to tune the pump.
In the case where the said apparatus is an internalcombustion engine and the pump is for supplying fuel at the necessary rate to the induction manifold of the engine, a pump may, according to still another feature, be adapted to be driven at a direct function of engine speed whereby to enable the pressure of the control fluid to be made independent of the engine speed.
The invention as specifically applied to pumps for supplying fuel to the inlet manifold of a reciprocating spark ignition internal-combustion engine is illustrated, by Way of example, in the accompanying drawings, in which:
FIGURE 1 is an elevation of a pump;
FIGURE 2 is a plan of FIGURE 1;
FIGURE 3 is a section taken on the line 33 of FIG- URE 1;
FIGURE 4 is a section taken on the line 44 of FIG- URE 3;
FIGURE 5 is a section taken on the line 55 of FIG- URE 2;
FIGURE 6 is a section taken on the line 66 of FIG- URE 2;
FIGURE 7 is a section taken on the line 77 of FIG- URE 2;
FIGURE 8 is a section taken on the line 88 of FIG- URE 2, and
FIGURE 9 shows, diagrammatically, the operation of the pump illustrated by FIGURES 1 to 8.
The pump is provided with a supply of fuel under high pressure through pipe union 52 and has an outlet 53 for metered fuel and a spill outlet 54 for by-passing excess fuel. For control purposes, the manifold depression is conveyed to the pump through pipe union 55, and the atmospheric pressure through an aperture 56. It will be seen from FIGURES 1, 3 and 4 that the metered fuel outlet 53 is arranged in a lower casing portion 57 which is integral with a boss 58 serving to locate the pump relatively to the engine casing.
The lower casing portion 57 is formed with an arcuate mined value. a
-'is permanently" Connected to supply space 61 with fuel under high pressure, and to supply arcuate fuel inlet port 59 through an orifice 62 with fuel under low pressure. The pressure of the fuel in the arcuate fuel inlet port 59 is determined by the pressure drop across the orifice 62 and, when the supply of fuel to the inlet port exceeds the flow required by the pump,-the excess fuel is passed to spill outlet 54 through relief valve 63 to prevent the pressure of the fuel in port 59 from exceeding a predeter- Fuel supply union 52, spill outlet 54, and pipe union 55 for manifold depression, are carried by an upper casing portion 64 which has an eccentric recess 65 for locatlower casing portion 57 and has splines 74 for being driven by the camshaft of the engine.
The piston 67 is provided with two chambers 75, 76 which are of arcuate shape as will be appreciated from ing an eccentric boss 66 of a piston 67, whereby to pre- FIGURE 2. Chamber 75 communicates with'space 61 through a port 77, shown in FIGURE 6, and contains fuel under high pressure; An orifice 78 allows fuel to escape from space 61 to chamber 76 which is connected to spill outlet 54 through bore 79 in eccentric boss 66, as will be seen in'FIGURE 7, through port 80 to chamber 81 in the upper casing portion 64, see FIGURE 6, and through pintle valve 82 to spill outlet 83 as will be seen in FIGURE 5. It will be appreciated that the pintle valve 82 will controlthe flow of fuel from chamber 76 to spill outlet 54 and, consequently, will control the flow of fuel through orifice 78 and the pressure of the fuel in chamber 76 and fuel to be pumped, which is permanently in communication with a port 89 in the lower portion 70 of the rotor.
The piston 67 is arranged relatively to the arcuate ports 59 and 60 so that the pistons 84 are acted upon by the high pressure fuel in chamber 75 Whenever their respective ports 89 are registering with fuel outletport 60, and
"are acted upon by the low pressure fuel in chamber 76 whenever their respective ports 89 arercgistering with fuel inlet port 59. Thus, when the rotor 69, 70 carries a piston 84 from high pressure fuel chamber 75 to 10W pressurefuel chamber76,the piston 84 will perform an induction stroke'and fuel will flow from fuel inlet port 59 into cylinder 88 and, whenjthe rotor 69, 70 carries a piston 84 from low pressure fuel chamber-76 to high pressure fuel chamber 75, the piston 84 will performa. 7 working stroke and will expel fuel from its cylinder 88 into fuel outlet port 60. The Working stroke is limited by the head 85 of the piston 84 abutting the lower portion 70. of the rotor and, under normal operating conditions,
' the pressure of the fuel inhigh pressure fuel chamber 75 is arranged to be sufficient to cause the heads 85 to abut portion 70 of the rotor. The induction stroke isv limited by the head 85 of the piston 84 abutting the upper portion ii 69 of the rotor and this prevents the pistons 84 fouling r 4 v the piston 67. However, the induction stroke is controlled by the pressure of fuel in low pressure fuel chamber 76 which exerts a force on thepiston 84 in opposition to the force of its spring 86. Thus, the induction stroke of the pistons 84, and consequently the output of the pump at any given speed, may be controlled by operating the pintle valve 82 to control the pressure of the fuel in low pressure fuel chamber 76. It will be appreciated that, when pintle valve 82 is fully open, the pressure of the fuel in low pressure fuel chamber 76 will be substantially zero, and the output of the pump at any given speed will be a maximum. Conversely, when the pintle valve 82 is closed, the pressure of the fuel in low pressure fuel chamber 76 will be equal to the pressure of the fuel in high pressure fuel chamber 75, and the output of the pump will be Zero irrespective of the speed of the pump.
When the pump is running, any unbalance of the pressures acting on diaphragms 43, 47 will cause the pintle valve 82 to move, thus altering the flow of fuel through orifice 78 until the pressure of the fuel in low pressure fuel chamber 76, and thus chamber 81, has changed to such a value that equilibrium is regained.
The plates 90v and 91 and the diaphragms 43 and 47 are secured to the. upper casing portion 64 by six bolts 98, and the casing portions 57, 64 and 68 are held together by three bolts 99 as will be seen in FIGURES 3 and 7. Three holes 100, see FIGURES 2,73 and 7, pass through the pump and are for receiving studs for holding the lower casing portion 57 to the engine casing.
The pistons 84 are preferably made of hardened steel and the upper portion 69 of the rotor is preferably made tons 84. Lubrication difliculties occur when petroleum spirit is pumped and, for this purpose, the upper portion 69 of the rotor has a facing 101 of carbon graphite for bearing against the'piston 67 which is of hardened steel, Similarly, the lower casing portion 57 has a facing 1 02 of carbon graphite for bearing against the lower portion of the rotor which is also hardened steel.
The piston '67 is axially movable in the intermediate casing portion 68 and the effective areas of its face definingspace 61, of its eccentric boss 66, and of the chambers 75 and 76 areso arranged that the vvarious fuel bers .75eand 76, and urges the rotor into contact with the graphite facing 102 to prevent leakage between ports 59 and 60. Leakage past the piston 67 is prevented by a seal 103, and leakage from space 61to eccentric recess 65 is prevented by a seal 104. It will be apparent to a person skilled in the art that the pump is self-compeneating for wear and obviates the need for a high degree of accuracy in many of its components.
As will be seen from FIGURES 3 and 4, the power input shaft 73 is cooled and lubricated by fuel which passes from fuel inlet port 59 through groove 105 in graphite facing 102 to the shaft 73, and is returned to the spill side of relief valve 63 through passage 106 and arcuate port 107 in the lower casing portion 57.
It will now be described with reference to FIGURE 9 how the output of the pump, at any given speed, is varied to suit the operating conditions of the engine it supplies. Two pistons 84 have been shown but, for the purpose of distinguishing between them, one has been denoted 84a. Due to the diagrammatic arrangement of FIGURE 9, piston 67 has been omitted and chambers 75 and 76 are separated by a diametral web 108. Also, the pistons 84, 84a have been simplified and are retained by circlips 109 as shown, and space 61 is coincident with chamber 75.
The piston 84a is shown in a position such that the pressure of the fuel in chamber 76 balances all other forces acting on it and, accordingly, prevents it from making a complete induction stroke by not allowing the head of piston 84a to abut circlip 109. If the pressure of the fuel in chamber 76 is increased, the stroke of the piston will decrease and vice versa. Thus, at any operating speed of the pump its output can be varied from zero, to a maximum for the speed at which it is operating, by varying the pressure of the fuel in chamber 76 which is achieved by controlling pintle valve 82 to adjust spill outlet 83.
The diaphragms 43 and 47 are so arranged that the pressures of the atmosphere, fuel supply and induction depression are balanced against the pressure of the fuel in chamber 81, by varying the rate at which the fuel escapes through spill outlet 83.
When the induction pressure is decreasing and the power output of the internal-combustion engine being supplied by the pump is being reduced, the atmospheric and fuel supply pressures remaining constant, the pintle valve 82 moves, as a result of the unbalanced pressures, so as to reduce the escape of fuel through spill outlet 83 whereby to increase the pressure of the fuel in chamber 76 until balance is regained by -a higher fuel pressure which in turn reduces the stroke of the pistons 84 and thus reduces the fuel supply to the engine. When the induction pressure is increasing, the power output of the engine will be increasing and the unbalanced pressures will cause the fuel pressure in chamber 76 to be reduced whereby to increase the output of the pump.
What we claim as our invention and desire to secure by Letters Patent of the United States is:
l. A pump for use as a metering device and comprising a cylinder and a coacting piston, conduit means adapted to receive a supply of fluid under pressure, a first pressure-reducing means, a second pressure-reducing means, an inlet valve means and an outlet valve means for said cylinder, said inlet valve means connected to be supplied with fluid through said first pressurereducing means from said conduit means, said piston when moved in one direction in said cylinder adapted to induce fluid into said cylinder through said inlet valve means to provide an induction stroke, and said piston when moved in the opposite direction in said cylinder adapted to educe fluid from said cylinder through said outlet valve means to provide a Working stroke, biasing means acting on said piston to exert thereon a force for producing said induction stroke, said biasing means such that the force it produces decreases progressively during said induction stroke, means for alternately applying the pressure of a control fluid and the pressure of an operating fluid to said piston in opposition to said biasing means, said operating fluid derived from the supply of fluid under pressure in said conduit means, said control fluid derived from said operating fluid through said second pressure-reducing means, the length of said induction stroke to be determined by equilibrium of the force exerted by said control fluid and the force produced by said biasing means, the pressure of said operating fluid such that the resultant of the forces acting on said piston produces said working stroke, and control means for varying the pressure of the control fluid whereby to vary the length of said induction stroke.
2. A pump comprising a rotor defining a cylindrical bore with its axis parallel with but radially-spaced from the axis of the rotor, a piston coacting with said cylindrical bore, a casing surrounding said rotor, an inlet valve means and an outlet valve means for said cylindrical bore, said piston when moved in one direction in said cylindrical bore adapted to induce fluid into said cylindrical bore through said inlet valve means to provide an induction stroke, and said piston when moved in the opposite direction in said cylindrical bore adapted to educe fluid from said cylindrical bore through said outlet valve means to provide a working stroke, a compression coil spring acting between said rotor and said piston to exert thereon a force for producing said induction stroke, said rotor remote from said inlet valve means and said outlet valve means having an end face, said casing having an end face for coaction with said end face of said rotor, said rotor defining a fluid commuication between said piston and said end face of said rotor, said end face of said casing defining a chamber for a control fluid under pressure and a separate chamber for an operating fluid under pressure whereby during rotation of said rotor said piston is alternately subjected through said fluid communication to the pressure of said control fluid and to the pressure of said operating fluid, the length of said induction stroke to be determined by equilibrium of the force exerted by said control fluid and the force produced by said compression coil spring, the pressure of said operating fluid such that the resultant of the forces acting on said piston produces said working stroke, and control means for varying the pressure of the control fluid whereby to vary the length of said induction stroke.
3. A pump comprising a rotor defining a cylindrical bore with its axis parallel with but radially-spaced from the axis of the rotor, a piston coacting with said cylindrical bore, a casing surrounding said rotor, an inlet valve means and an outlet valve means for said cylindrical bore, said piston when moved in one direction in said cylindrical bore adapted to induce fluid into said cylindrical bore through said inlet valve means to provide an induction stroke, and said piston when moved in the opposite direction in said cylindrical bore adapted to educe fluid from said cylindrical bore through said outlet valve means to provide a working stroke, a compression coil spring acting between said rotor and said piston to exert thereon a force for producing said induction stroke, said rotor remote from said inlet valve means and said outlet valve means having an end face, a rotatively-stationary piston guided by said casing and having an end face for coaction with said end face of said rotor, said rotor defining a fluid communication between said piston and said end face of said rotor, said end face of said rotativelystationary piston defining a chamber for a control fluid under pressure and a separate chamber for an operating fluid under pressure whereby during rotation of said rotor said piston is alternately subjected through said fluid communication to the pressure of said control fluid and to the pressure of said operating fluid, the length of said induction stroke to be determined by equilibrium of the force exerted by said control fluid and the force produced by said compression coil spring, the pressure of said operating fluid such that the resultant of the forces acting on said piston produces said working stroke, a bias reacting between said rotatively-stationary piston and said casing whereby to urge said end face ofsaid rotativelystationary-piston into sealing engagement with said end face of said rotor to prevent leakage from said chamber 7 'of said operating fluid to said chamber for said control 8' References Cited by the'Exarniner j AV UNITED STATES PATENTS 7 2,946,287
7/60 Bessiere 103--41 5 3,002,462 10/61 Raymond -L 10338 3,007,415 11/61 -Bessi ere .V 10341 LAURENCE'V'. EFNER, Primary Examiner.
Claims (1)
1. A PUMP FOR USE AS A METERING DEVICE AND COMPRISING A CYLINDER AND A COACTING PISTON, CONDUIT MEANS ADAPTED TO RECEIVE A SUPPLY OF FLUID UNDER PRESSURE, A FIRST PRESSURE-REDUCING MEANS, A SECOND PRESSURE-REDUCING MEANS, AN INLET VALVE MEANS AND AN OUTLET VALVE MEANS FOR SECOND CYLINDER, SAID INLET VALVE MEANS CONNECTED TO BE SUPPLIED WITH FLUID THROUGH SAID FIRST PRESSURE-REDUCING MEANS FROM SAID CONDUIT MEANS, SAID PISTON WHEN MOVED IN ONE DIRECTION IN SAID CYLINDER ADAPTED TO INDUCE FLUID INTO SAID CYLINDER THROUGH SAID INLET VALVE MEANS TO PROVIDE AN INDUCTION STROKE, AND SAID PISTON WHEN MOVED IN THE OPPOSITE DIRECTION IN SAID CYLINDER ADAPTED TO EDUCE FLUID FROM SAID CYLINDER THROUGH SAID OUTLET VALVE MEANS TO PROVIDE A WORKING STROKE, BIASING MEANS ACTING ON SAID PISTON TO EXERT THEREON A FORCE FOR PRODUCING SAID INDUCTION STROKE, SAID BIASING MEANS SUCH THAT THE FORCE IT PRODUCES DECREASES PROGRESSIVELY DURING SAID INDUCTION STROKE, MEANS FOR ALTERNATELY APPLYING THE PRESSURE OF A CONTROL FLUID AND THE PRESSURE OF AN OPERATING FLUID TO SAID PISTON IN OPPOSITE TO SAID BIASING MEANS, SAID OPERATING FLUID DERIVED FROM THE SUPPLY OF FLUID UNDER PRESSURE IN SAID CONDUIT MEANS, SAID CONTROL FLUID DERIVED FROM SAID OPERATING FLUID THROUGH SAID SECOND PRESSURE-REDUCING MEANS, THE LENGTH OF SAID INDUCTION STROKE TO BE DETERMINED BY EQUILIBRIUM OF THE FORCE EXERTED BY SAID CONTROL FLUID AND THE FORCE PRODUCED BY SAID BIASING MEANS, THE PRESSURE OF SAID OPERATING FLUID SUCH THAT THE RESULTANT OF THE FORCES ACTING ON SAID PISTON PRODUCES SAID WORKING STROKE, AND N CONTROL MEANS FOR VARYING THE PRESSURE OF THE CONTROL FLUID WHEREBY TO VARY THE LENGTH OF SAID INDUCTION STROKE.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US248428A US3175499A (en) | 1961-11-14 | 1962-12-31 | Piston pump having a variable stroke |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4061361A GB1004080A (en) | 1961-11-14 | 1961-11-14 | Piston pump having a variable stroke |
US248428A US3175499A (en) | 1961-11-14 | 1962-12-31 | Piston pump having a variable stroke |
Publications (1)
Publication Number | Publication Date |
---|---|
US3175499A true US3175499A (en) | 1965-03-30 |
Family
ID=26264453
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US248428A Expired - Lifetime US3175499A (en) | 1961-11-14 | 1962-12-31 | Piston pump having a variable stroke |
Country Status (1)
Country | Link |
---|---|
US (1) | US3175499A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3431747A (en) * | 1966-12-01 | 1969-03-11 | Hadi T Hashemi | Engine for exchanging energy between high and low pressure systems |
US4714411A (en) * | 1985-06-24 | 1987-12-22 | Normalair-Garrett (Holdings) Limited | Fluid pressure intensifier device |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2946267A (en) * | 1957-10-07 | 1960-07-26 | Cedeno Arturo Olivero | Traffic intersection |
US3002462A (en) * | 1957-08-13 | 1961-10-03 | Racine Hydraulics & Machinery | Fluid translating apparatus |
US3007415A (en) * | 1957-12-18 | 1961-11-07 | Bessiere Pierre Etienne | Self-regulating reciprocating action pumps, and in particular in fuel injection pumps |
-
1962
- 1962-12-31 US US248428A patent/US3175499A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3002462A (en) * | 1957-08-13 | 1961-10-03 | Racine Hydraulics & Machinery | Fluid translating apparatus |
US2946267A (en) * | 1957-10-07 | 1960-07-26 | Cedeno Arturo Olivero | Traffic intersection |
US3007415A (en) * | 1957-12-18 | 1961-11-07 | Bessiere Pierre Etienne | Self-regulating reciprocating action pumps, and in particular in fuel injection pumps |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3431747A (en) * | 1966-12-01 | 1969-03-11 | Hadi T Hashemi | Engine for exchanging energy between high and low pressure systems |
US4714411A (en) * | 1985-06-24 | 1987-12-22 | Normalair-Garrett (Holdings) Limited | Fluid pressure intensifier device |
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