US2588522A - Regulating means for liquid fuel supply systems of prime movers or other apparatus - Google Patents

Regulating means for liquid fuel supply systems of prime movers or other apparatus Download PDF

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Publication number
US2588522A
US2588522A US104994A US10499449A US2588522A US 2588522 A US2588522 A US 2588522A US 104994 A US104994 A US 104994A US 10499449 A US10499449 A US 10499449A US 2588522 A US2588522 A US 2588522A
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Prior art keywords
liquid fuel
fuel supply
regulating means
supply systems
prime movers
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Expired - Lifetime
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US104994A
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Harris Thomas Alfred
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ZF International UK Ltd
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Joseph Lucas Ltd
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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
    • F02M37/00Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
    • F02M37/04Feeding by means of driven pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D1/00Controlling fuel-injection pumps, e.g. of high pressure injection type
    • F02D1/02Controlling fuel-injection pumps, e.g. of high pressure injection type not restricted to adjustment of injection timing, e.g. varying amount of fuel delivered
    • F02D1/08Transmission of control impulse to pump control, e.g. with power drive or power assistance
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B49/00Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S60/00Power plants
    • Y10S60/911Fluid motor system incorporating electrical system

Definitions

  • This invention relates tdsystems forsupplyin means,- and the object of thepresent inventionds.
  • the l invention comprises. the combination-of anelectromagnet. and. potentiometers having a rectifier-associated therewith;
  • FIGS 1 and 2 illustrate diagrammatically two embodiments of the invention.
  • a fluid operated servomechanism is employed for varying the rate of supply of fuel to the burner.
  • the pump comprises a pair of interengaging toothed rotors a adapted to draw liquid fuel from a supply tank as b and discharge it to a delivery pipe 0 leading to the burner.
  • a relief valve (1 is provided by which fuel can be returned to the inlet side of the pump in the event of excessive pressure being developed at the delivery side of the pump.
  • the rate of flow to the pipe 0 is controlled automatically by a slidable throttle e having a conical or otherwise shaped end for varying the effective area of an annular passage 1 leading to the pipe 0.
  • the throttle is movable by a fluid-operated servomechanism, which comprises a cylinder 9 and a piston h loaded by a spring 2', the piston being formed on or secured to one end of the throttle 6.
  • Liquid fuel from the pump can enter one end of the cylinder 9 by way of a passage 7', and can be returned to a sump or the inlet side of the pump by way of passages k, 121..
  • the ends of the cylinder are in communication by way of a restricted orifice n which may be formed in the piston as shown, or may be provided in a branch passage interconnecting the ends of the cylinder.
  • the discharge end of the passage It opens into a seating o with which co-operates a valve p.
  • the arrangement is such that when the. valve p is closed on to the seating o no fluid can flow through the cylinder 9.
  • seatin allowin fluid: o; fiowv throughi hee-nasasages; "b. 336; nrenonderating; fluid ressures i acting ononeiside ofitheuqiston hrmmlessthezlatter;
  • Therelectromagnetewindi es is energised by current derived fronriaabatterwt, or other convenient "sourcetoi:directcurrent; ,and this current is supplied through a bridge circuit having a pair of parallel branches It, ll formed in part by a pair of potentiometers u, 21, provided with adjustable contacts y, :13, the latter being connected to opposite ends of the electro-magnet winding, and the connection between one end of the solenoid winding and the potentiometer 12 being efiected through a rectifier w permitting current to flow in one direction only.
  • the movable contact a: of the potentiometer v is movable by hand or otherwise under the control of an attendant.
  • the movable contact 1/ of the potentiometer u is movable by the piston it through a rod z.
  • the arrangement is such that when the piston h is in equilibrium, that is to say, when the forces acting on opposite sides of the piston are equal, the bridge circuit above mentioned is slightly out of balance, and sufliciept current fiows through the electromagnet winding r to retain the valve p slightly open.
  • the attendant actuates the contact a: of the potentiometer v in one direction, current can flow to the Winding 1' for opening the valve p to a greater extent.
  • the servo-mechanism is thereby set in motion, and the contact 1 of the other potentiometer u is thereby moved until the original state of the bridge circuit is restored.
  • Figure 2 illustrates an application of the invention to a system in which the liquid fuel is supplied by a variable delivery pump of the swash-plate type.
  • the pump comprises a rotor 2 having bores 3 containing reciprocatory tion to theabove described apparatus;thezzvaivee plungers 4 which co-operate with an angularly adjustable swash plate 5 in known manner. Fluid enters the pump along a passage 6 and is delivered by the pump along a passage 1.
  • the swash-plate 5 is adjustable by a rod 8 connected to the piston h of the servo-mechanism.
  • the system illustrated by Figure 2 is similar to that illustrated by Figure 1, and the above description of Figure 1 is applicable also to Figure 2.
  • the contact :c shall be operable by or under the control of the attendant, as it may be actuated automatically in response to any predetermined variable condition.
  • it may be operable by a thermostatic device so that the fuel supply is restricted when a predetermined temperature is exceeded.
  • a thermo-c-ouple responsive to temperature changes instead of supplying current to the solenoid from a battery or other substantially constant source it may be supplied from a thermo-c-ouple responsive to temperature changes, the contact a: being then adjusted to determine the temperature at which it is desired to effect reduction of fuel supply.
  • Fuel supply regulating means comprising in combination a valve, an electromagnet having an exciting winding and a movable member responsive to excitation of the winding for moving the valve in one direction, a spring opposing movement of the valve by the movable member of the electromagnet, an electric current supply circuit having a pair of parallel branches, a pair of potentiometers forming parts of the circuit branches and having adjustable contacts connected to opposite ends of the electromagnet winding, a rectifier connected between one of the potentiometer contacts and the corresponding end of the electromagnet winding, a fuel regulating member, and a fluid-operated servo-mechanism operable under the control of the valve for actuating the fuel regulating member and imparting adjusting movement to one of the potentiometer contacts.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Magnetically Actuated Valves (AREA)

Description

March 11, 1952 HARR|$ 2,588,522
REGULATING MEANS FOR LIQUID FUEL SUPPLY SYSTEMS OF PRIME MOVERS OR OTHER APPARATUS Filed July 15, 1949 TAJia I IJ-S Patented Mar. 11, 1952 UNITED STATES REGUI ATINGI; MEANS, FOR. LIQUID FUEL. SjUPPLY'SYSTEMS" F PRIME MQVERSII 0R. QTH-ER'APPABATUS Thomas-Alfred Harris, Edgbjastom Birmin ham; England, assignor; to Joseph: Lncas- .Limited;, Birmingham, England.-v
Application -July,15', 1949; Serial -No=-'4',=994 In.-Great;B ritain July-, 30tl948 lTCJai m This invention relates tdsystems forsupplyin means,- and the object of thepresent inventionds.
toenable this requirementto zbeemet in .a simple and satisfactory. manner.
The l invention comprises. the combination-of anelectromagnet. and. potentiometers having a rectifier-associated therewith;
In the accompanying drawings:
Figures 1 and 2 illustrate diagrammatically two embodiments of the invention.
In one known system for supplying liquid fuel to a burner associated with a jet-propulsion engine, gas turbine, air heater or other analogous apparatus, a fluid operated servomechanism is employed for varying the rate of supply of fuel to the burner. In the example shown in Figure 1, the pump comprises a pair of interengaging toothed rotors a adapted to draw liquid fuel from a supply tank as b and discharge it to a delivery pipe 0 leading to the burner. In this example a relief valve (1 is provided by which fuel can be returned to the inlet side of the pump in the event of excessive pressure being developed at the delivery side of the pump. The rate of flow to the pipe 0 is controlled automatically by a slidable throttle e having a conical or otherwise shaped end for varying the effective area of an annular passage 1 leading to the pipe 0. The throttle is movable by a fluid-operated servomechanism, which comprises a cylinder 9 and a piston h loaded by a spring 2', the piston being formed on or secured to one end of the throttle 6. Liquid fuel from the pump can enter one end of the cylinder 9 by way of a passage 7', and can be returned to a sump or the inlet side of the pump by way of passages k, 121.. Also the ends of the cylinder are in communication by way of a restricted orifice n which may be formed in the piston as shown, or may be provided in a branch passage interconnecting the ends of the cylinder. The discharge end of the passage It opens into a seating o with which co-operates a valve p. The arrangement is such that when the. valve p is closed on to the seating o no fluid can flow through the cylinder 9. The fluid pressures acting on the opposite sides of the piston h are then equal, and the spring i can move the piston in;=. the. direction ;for restricting; the: area? of: the
passa e it. When: he-waive RJSRIILQVBCI; 011-: its;
seatin allowin fluid: o; fiowv throughi hee-nasasages; "b. 336; nrenonderating; fluid ressures i acting ononeiside ofitheuqiston hrmmlessthezlatter;
againstzthe;sprin wiirrthedireotionaior increasin the; areagof :the passage: 1; sovfargthe apparatus. above-describe ;;is:oie known ,form:
In:.one1manne1;of applyin ;the-:presen-t invenap is; carried rby; the; plunger-sq: oigameleotltomag net havingzan excitinauvinding r;;tlieznlun er:;bein loadecbbyempring s.-=. Therelectromagnetewindi es is energised by current derived fronriaabatterwt, or other convenient "sourcetoi:directcurrent; ,and this current is supplied through a bridge circuit having a pair of parallel branches It, ll formed in part by a pair of potentiometers u, 21, provided with adjustable contacts y, :13, the latter being connected to opposite ends of the electro-magnet winding, and the connection between one end of the solenoid winding and the potentiometer 12 being efiected through a rectifier w permitting current to flow in one direction only. The movable contact a: of the potentiometer v is movable by hand or otherwise under the control of an attendant. The movable contact 1/ of the potentiometer u is movable by the piston it through a rod z.
The arrangement is such that when the piston h is in equilibrium, that is to say, when the forces acting on opposite sides of the piston are equal, the bridge circuit above mentioned is slightly out of balance, and sufliciept current fiows through the electromagnet winding r to retain the valve p slightly open. When the attendant actuates the contact a: of the potentiometer v in one direction, current can flow to the Winding 1' for opening the valve p to a greater extent. The servo-mechanism is thereby set in motion, and the contact 1 of the other potentiometer u is thereby moved until the original state of the bridge circuit is restored. When the attendant operates the movable contact w of the potentiometer v in the opposite direction no current will flow to the solenoid as it is intercepted by the rectifier w. Consequently the valve 10 will be closed by the spring 8, and the servo-mechanism will be moved in the opposite direction until the original state of the bridge circuit is restored.
Figure 2 illustrates an application of the invention to a system in which the liquid fuel is supplied by a variable delivery pump of the swash-plate type. The pump comprises a rotor 2 having bores 3 containing reciprocatory tion to theabove described apparatus;thezzvaivee plungers 4 which co-operate with an angularly adjustable swash plate 5 in known manner. Fluid enters the pump along a passage 6 and is delivered by the pump along a passage 1. The swash-plate 5 is adjustable by a rod 8 connected to the piston h of the servo-mechanism. In other respects the system illustrated by Figure 2 is similar to that illustrated by Figure 1, and the above description of Figure 1 is applicable also to Figure 2. When the valve p is closed on to its seating, the piston It moves the swash plate 5 in the direction for increasing the pump output, and when the valve p is opened the piston It moves in the direction for reducing the pump output.
In either of the systems above described it is not essential that the contact :c shall be operable by or under the control of the attendant, as it may be actuated automatically in response to any predetermined variable condition. Thus it may be operable by a thermostatic device so that the fuel supply is restricted when a predetermined temperature is exceeded. Further, instead of supplying current to the solenoid from a battery or other substantially constant source it may be supplied from a thermo-c-ouple responsive to temperature changes, the contact a: being then adjusted to determine the temperature at which it is desired to effect reduction of fuel supply.
By this invention the electrical control of the servo-mechanism for regulating the rate of fuel supply can be effected in a very simple and convenient manner. Y
Having thus described my invention what I 4 claim as new and desire to secure by Letters Patent is:
Fuel supply regulating means comprising in combination a valve, an electromagnet having an exciting winding and a movable member responsive to excitation of the winding for moving the valve in one direction, a spring opposing movement of the valve by the movable member of the electromagnet, an electric current supply circuit having a pair of parallel branches, a pair of potentiometers forming parts of the circuit branches and having adjustable contacts connected to opposite ends of the electromagnet winding, a rectifier connected between one of the potentiometer contacts and the corresponding end of the electromagnet winding, a fuel regulating member, and a fluid-operated servo-mechanism operable under the control of the valve for actuating the fuel regulating member and imparting adjusting movement to one of the potentiometer contacts.
THOMAS ALFRED HARRIS.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,262,173 Fischer Nov. 11, 1941 2,390,425 Crum Dec. 4, 1945 2,403,371 Ifield July 2, 1946 2,403,917 Gille July 16, 1946 2,498,654 Deakin Feb. 28, 1950
US104994A 1948-07-30 1949-07-15 Regulating means for liquid fuel supply systems of prime movers or other apparatus Expired - Lifetime US2588522A (en)

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Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2768613A (en) * 1948-02-27 1956-10-30 Mercier Jean Synchronous servo-control
US2940429A (en) * 1957-01-21 1960-06-14 Plenty And Son Ltd Control of variable-capacity pumps
US2956578A (en) * 1949-10-08 1960-10-18 Thompson Ramo Wooldridge Inc Fuel control unit
US3046895A (en) * 1957-02-27 1962-07-31 Veb Zek Variable displacement pump control
US3050257A (en) * 1959-03-13 1962-08-21 Barber Colman Co Means for operating a valve or the like in accordance with a controlled condition
US3089306A (en) * 1958-12-11 1963-05-14 Power Jets Res & Dev Ltd Limitation of thermal shock in engine components
US3146769A (en) * 1962-03-30 1964-09-01 Simmonds Precision Products Fuel injection system
US3203178A (en) * 1962-06-06 1965-08-31 Bristol Siddeley Engines Ltd Fuel system for supplying gaseous fuel to a combustion chamber
US3212260A (en) * 1962-05-22 1965-10-19 Ass Elect Ind Stall trip protective device for gas turbines
US3236047A (en) * 1962-05-28 1966-02-22 Holley Carburetor Co Turbine engine fuel controls
US3411531A (en) * 1966-04-26 1968-11-19 Racine Hydraulics & Machinery Remotely controllable valves
US3455532A (en) * 1965-09-15 1969-07-15 Monsanto Co Electropneumatic valve positioner
US3462115A (en) * 1965-05-14 1969-08-19 Monsanto Co Electropneumatic valve positioner
US3486078A (en) * 1965-12-04 1969-12-23 Mini Ind Const Masini Converter amplifier
US3694108A (en) * 1969-04-23 1972-09-26 Carlo Pensa Hydraulic apparatus for regulating the flow of one or more pumps
USB419481I5 (en) * 1973-11-28 1975-01-28
US3921503A (en) * 1972-03-21 1975-11-25 Philip A Kubik Control system for a fluid system
USRE29333E (en) * 1969-04-23 1977-08-02 Massey-Ferguson Services N.V. Hydraulic apparatus for regulating the flow of one or more pumps
US4199303A (en) * 1976-09-29 1980-04-22 Gusmer Corporation Feeder for apparatus for ejecting a mixture of a plurality of liquids

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2262173A (en) * 1938-05-17 1941-11-11 Siemens App Und Maschinen Gmbh Automatic regulating apparatus
US2390425A (en) * 1942-10-14 1945-12-04 Honeywell Regulator Co Control apparatus
US2403371A (en) * 1941-09-16 1946-07-02 Lucas Ltd Joseph Variable output pump
US2403917A (en) * 1942-04-20 1946-07-16 Honeywell Regulator Co Control apparatus
US2498654A (en) * 1945-02-26 1950-02-28 Int Standard Electric Corp Remote position control system

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2262173A (en) * 1938-05-17 1941-11-11 Siemens App Und Maschinen Gmbh Automatic regulating apparatus
US2403371A (en) * 1941-09-16 1946-07-02 Lucas Ltd Joseph Variable output pump
US2403917A (en) * 1942-04-20 1946-07-16 Honeywell Regulator Co Control apparatus
US2390425A (en) * 1942-10-14 1945-12-04 Honeywell Regulator Co Control apparatus
US2498654A (en) * 1945-02-26 1950-02-28 Int Standard Electric Corp Remote position control system

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2768613A (en) * 1948-02-27 1956-10-30 Mercier Jean Synchronous servo-control
US2956578A (en) * 1949-10-08 1960-10-18 Thompson Ramo Wooldridge Inc Fuel control unit
US2940429A (en) * 1957-01-21 1960-06-14 Plenty And Son Ltd Control of variable-capacity pumps
US3046895A (en) * 1957-02-27 1962-07-31 Veb Zek Variable displacement pump control
US3089306A (en) * 1958-12-11 1963-05-14 Power Jets Res & Dev Ltd Limitation of thermal shock in engine components
US3050257A (en) * 1959-03-13 1962-08-21 Barber Colman Co Means for operating a valve or the like in accordance with a controlled condition
US3146769A (en) * 1962-03-30 1964-09-01 Simmonds Precision Products Fuel injection system
US3212260A (en) * 1962-05-22 1965-10-19 Ass Elect Ind Stall trip protective device for gas turbines
US3236047A (en) * 1962-05-28 1966-02-22 Holley Carburetor Co Turbine engine fuel controls
US3203178A (en) * 1962-06-06 1965-08-31 Bristol Siddeley Engines Ltd Fuel system for supplying gaseous fuel to a combustion chamber
US3462115A (en) * 1965-05-14 1969-08-19 Monsanto Co Electropneumatic valve positioner
US3455532A (en) * 1965-09-15 1969-07-15 Monsanto Co Electropneumatic valve positioner
US3486078A (en) * 1965-12-04 1969-12-23 Mini Ind Const Masini Converter amplifier
US3411531A (en) * 1966-04-26 1968-11-19 Racine Hydraulics & Machinery Remotely controllable valves
US3694108A (en) * 1969-04-23 1972-09-26 Carlo Pensa Hydraulic apparatus for regulating the flow of one or more pumps
USRE29333E (en) * 1969-04-23 1977-08-02 Massey-Ferguson Services N.V. Hydraulic apparatus for regulating the flow of one or more pumps
US3921503A (en) * 1972-03-21 1975-11-25 Philip A Kubik Control system for a fluid system
USB419481I5 (en) * 1973-11-28 1975-01-28
US3924970A (en) * 1973-11-28 1975-12-09 Gen Motors Corp Electrically controlled fuel pump
US4199303A (en) * 1976-09-29 1980-04-22 Gusmer Corporation Feeder for apparatus for ejecting a mixture of a plurality of liquids

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