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Publication numberUS2588522 A
Publication typeGrant
Publication dateMar 11, 1952
Filing dateJul 15, 1949
Priority dateJul 30, 1948
Publication numberUS 2588522 A, US 2588522A, US-A-2588522, US2588522 A, US2588522A
InventorsHarris Thomas Alfred
Original AssigneeLucas Ltd Joseph
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Regulating means for liquid fuel supply systems of prime movers or other apparatus
US 2588522 A
Abstract  available in
Images(1)
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Claims  available in
Description  (OCR text may contain errors)

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

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US2262173 *May 12, 1939Nov 11, 1941Siemens App Und Maschinen GmbhAutomatic regulating apparatus
US2390425 *Oct 14, 1942Dec 4, 1945Honeywell Regulator CoControl apparatus
US2403371 *Nov 30, 1942Jul 2, 1946Lucas Ltd JosephVariable output pump
US2403917 *Apr 20, 1942Jul 16, 1946Honeywell Regulator CoControl apparatus
US2498654 *Feb 26, 1945Feb 28, 1950Int Standard Electric CorpRemote position control system
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US2768613 *Jan 4, 1955Oct 30, 1956Jean MercierSynchronous servo-control
US2940429 *Jan 17, 1958Jun 14, 1960Plenty And Son LtdControl of variable-capacity pumps
US2956578 *Jun 29, 1954Oct 18, 1960Thompson Ramo Wooldridge IncFuel control unit
US3046895 *Feb 27, 1958Jul 31, 1962Veb ZekVariable displacement pump control
US3050257 *Mar 13, 1959Aug 21, 1962Barber Colman CoMeans for operating a valve or the like in accordance with a controlled condition
US3089306 *Dec 10, 1959May 14, 1963Power Jets Res & Dev LtdLimitation of thermal shock in engine components
US3146769 *Mar 30, 1962Sep 1, 1964Simmonds Precision ProductsFuel injection system
US3203178 *May 23, 1963Aug 31, 1965Bristol Siddeley Engines LtdFuel system for supplying gaseous fuel to a combustion chamber
US3212260 *May 20, 1963Oct 19, 1965Ass Elect IndStall trip protective device for gas turbines
US3236047 *May 28, 1962Feb 22, 1966Holley Carburetor CoTurbine engine fuel controls
US3411531 *Apr 26, 1966Nov 19, 1968Racine Hydraulics & MachineryRemotely controllable valves
US3455532 *Sep 15, 1965Jul 15, 1969Monsanto CoElectropneumatic valve positioner
US3462115 *May 14, 1965Aug 19, 1969Monsanto CoElectropneumatic valve positioner
US3486078 *Nov 30, 1966Dec 23, 1969Mini Ind Const MasiniConverter amplifier
US3694108 *Apr 14, 1970Sep 26, 1972Pensa CarloHydraulic apparatus for regulating the flow of one or more pumps
US3921503 *Jun 22, 1973Nov 25, 1975Kubik Philip AControl system for a fluid system
US3924970 *Nov 28, 1973Dec 9, 1975Gen Motors CorpElectrically controlled fuel pump
US4199303 *Feb 2, 1978Apr 22, 1980Gusmer CorporationFeeder for apparatus for ejecting a mixture of a plurality of liquids
USB419481 *Nov 28, 1973Jan 28, 1975 Title not available
USRE29333 *Sep 25, 1974Aug 2, 1977Massey-Ferguson Services N.V.Hydraulic apparatus for regulating the flow of one or more pumps
Classifications
U.S. Classification91/363.00R, 251/30.2, 60/911, 417/222.1, 91/49, 236/80.00R, 60/39.281, 236/84
International ClassificationF04B49/00, F02D1/08, F02M37/04
Cooperative ClassificationF04B49/00, Y10S60/911, F02M37/04, F02D1/08
European ClassificationF02D1/08, F02M37/04, F04B49/00