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 PDFInfo
- 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
- Authority
- US
- United States
- Prior art keywords
- liquid fuel
- fuel supply
- regulating means
- supply systems
- prime movers
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
-
- 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
- F02M37/00—Apparatus 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
- F02M37/04—Feeding by means of driven pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D1/00—Controlling fuel-injection pumps, e.g. of high pressure injection type
- F02D1/02—Controlling fuel-injection pumps, e.g. of high pressure injection type not restricted to adjustment of injection timing, e.g. varying amount of fuel delivered
- F02D1/08—Transmission of control impulse to pump control, e.g. with power drive or power assistance
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B49/00—Control, 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
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S60/00—Power plants
- Y10S60/911—Fluid 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2588522X | 1948-07-30 |
Publications (1)
Publication Number | Publication Date |
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US2588522A true US2588522A (en) | 1952-03-11 |
Family
ID=10910888
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US104994A Expired - Lifetime US2588522A (en) | 1948-07-30 | 1949-07-15 | Regulating means for liquid fuel supply systems of prime movers or other apparatus |
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US (1) | US2588522A (en) |
Cited By (19)
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)
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 |
-
1949
- 1949-07-15 US US104994A patent/US2588522A/en not_active Expired - Lifetime
Patent Citations (5)
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)
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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