US3406951A - Fluid amplifier arrangement and fuel system incorporating same - Google Patents

Fluid amplifier arrangement and fuel system incorporating same Download PDF

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US3406951A
US3406951A US48786065A US3406951A US 3406951 A US3406951 A US 3406951A US 48786065 A US48786065 A US 48786065A US 3406951 A US3406951 A US 3406951A
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fuel
interaction region
stream
fuel stream
fluid
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Marks Craig
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Motors Liquidation Co
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Motors Liquidation Co
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Priority to GB3388066A priority patent/GB1116549A/en
Priority to DE19661526672 priority patent/DE1526672C/en
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15C—FLUID-CIRCUIT ELEMENTS PREDOMINANTLY USED FOR COMPUTING OR CONTROL PURPOSES
    • F15C1/00—Circuit elements having no moving parts
    • F15C1/002—Circuit elements having no moving parts for controlling engines, turbines, compressors (starting, speed regulation, temperature control or the like)
    • 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
    • F02M1/00—Carburettors with means for facilitating engine's starting or its idling below operational temperatures
    • 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
    • F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • 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
    • F02M7/00—Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
    • F02M7/10—Other installations, without moving parts, for influencing fuel/air ratio, e.g. electrical means
    • F02M7/106—Fluid amplifier as a device for influencing the fuel-air mixture
    • 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
    • F02M2700/00—Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
    • F02M2700/43—Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel
    • F02M2700/4302—Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel whereby air and fuel are sucked into the mixture conduit
    • F02M2700/4373—Mixture improving devices
    • 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
    • F02M2700/00—Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
    • F02M2700/43—Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel
    • F02M2700/4397—Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel whereby air or fuel are admitted in the mixture conduit by means other than vacuum or an acceleration pump
    • 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
    • Y10S261/00—Gas and liquid contact apparatus
    • Y10S261/69—Fluid amplifiers in carburetors
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/206—Flow affected by fluid contact, energy field or coanda effect [e.g., pure fluid device or system]
    • Y10T137/2065—Responsive to condition external of system
    • Y10T137/2071—And causing change or correction of sensed condition
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/206—Flow affected by fluid contact, energy field or coanda effect [e.g., pure fluid device or system]
    • Y10T137/2076—Utilizing diverse fluids

Definitions

  • This invention relates to fluid amplifiers and to fuel systems utilizing fluid amplifier technology. Because spark ignition internal combustion engines are quite sensitive to the proportions of the air-fuel mixture in the combustion chamber, innumerable systems have been developed in attempts to supply the engine with an air-fuel mixture proper for the various operating conditions. The systems in common use, however, include a venturi located in the air inlet to create a pressure signal which varies with the rate of air flow to the engine; this pressure signal determines the rate at which fuel is delivered to the engine.
  • venturi signal does not vary linearly with air flow.
  • the venturi signal is very weak at low air flow rates. This weak signal would 'result in insnfiicient fuel delivery to the engine.
  • a small venturi which would provide an adequate fuel metering signal at low air flow rates would also'r'estrict air flow at high air flow rates.
  • a compromise is generally adopted in which a separate idle system provides fuel'at the lowest air flow rates, a large venturi and one or two small boost venturi provide a fuel metering signal over the part throttle and wide-open throttle operating ranges, and offidle discharge ports smooth the transition from the idle system to the venturi metering system as the throttle open's.
  • Fuel systems have recently been developed which utilize fluid amplifiers to amplify the venturi pressure signal and deliver fuel to the engine at a rate determined by the amplified signal. Such an arrangement makes a complex idle system unnecessary.
  • a fluid amplifier uses a relatively weak control signal to deflect the path of a fluid stream. Because relatively large deflections in the fluid path are obtained with weak control signals, a more sensitive control function is obtained by measuring the deflection of the path rather than by directlymeasuring the control signal.
  • a fuel system relying on a single amplifier for fuel metering may riot supply the most desirable air-fuel mixture throughout the entire range of engine operating conditions.
  • This invention provides a fuel system including a fluid amplifier arrangement which closely tailors the rate of fuel delivery for the wide range of engine air flow rates.
  • the fuel system includes a plurality of amplifiers which are sequentially actuated, each in a predetermined range of air flow rates, so that the pressure signal is sufficiently amplified to deliver fuel at a rate which closely approximates that required by the engine.
  • FIGURE 1 illustrates a fuel system carburetor embodying this invention
  • FIGURE 2 graphically illustrates the fuel metering characteristics of this invention.
  • a carburetor has an air inlet 12 controlled by a throttle 14 in the customary manner.
  • a venturi 16 provides a restriction Within air sa e Patent "ice inlet 12 which reduces the pressure of the air flow therethrough to create a control signal related to the rate of air flow.
  • a fluid amplifier arrangement indicated generally by 18, has a common inlet 20 connected to a fuel pump 22.
  • a series of amplifiers three being illustrated, each has an inlet 24, 26, and 28 opening into an interaction region 24a, 26a, 28a and a pair of outlets 3032, 34-36, and 3840 opening therefrom.
  • Fuel is drawn from a tank 42 by pump 22, passes through the common inlet 20, and is issued from the individual inlets 24, 26, 28 in streams each having a predetermined path within an interaction region 24a, 26a, 28a and a predetermined energy state.
  • the fuel streams are discharged from the interaction regions through outlets 30 through 40.
  • the proportion of fuel discharged from outlets 32, 36, 40 is determined by the location of the splitters 44, 46, 48.
  • Amplifiers which operate as described are known as proportional amplifiers since the proportion of the fluid discharged through the outlets 32, 36, 40 varies with the pressure drop in the venturi 16.
  • the venturi pressure signal varies as the square of the rate of air flow through the inlet 12. Because the engine requires fuel flow more directly proportional to air flow, it is desirable to have the venturi pressure signal also vary as the square of the rate of fuel flow. It will be appreciated that, as illustrated by the single amplifier curve of FIGURE 2, a single amplifier controlled by the venturi signal can only roughly approximate such a fuel delivery requirement.
  • this invention provides an amplifier arrangement 18 in which the splitters 44, 46, 48 of the various individual amplifiers are arranged so that splitter 44 initially divides fuel flow from inlet 24 between outlets 30 and 32 while splitters 46 and 48 direct the entire fuel flow from inlets 26 and 28 to outlets 34 and 38 and then to a sump 54 which drains back to tank 42
  • the arrangement is such that when substantially the entire fuel flow from inlet 24 is discharged through outlet 32, the pressure in outlet 36 is sufficient to cause splitter 46 to divide the fuel flow from inlet 26 between outlets 34 and 36, and similarly, when substantially the entire .fuel flow from inlets 24 and 26 is directed through outlets 32 and 36, the pressure in outlet 40 is suflicient to cause splitter 48 to divide the fuel flow from inlet 28 between outlets 38 and 40.
  • FIGURE 2 The fuel metering characteristics of this invention are graphically illustrated in FIGURE 2 where it will be noted that the fuel delivery of the amplifier series very closely approximates the requirements of the engine.
  • This invention in providing a fuel system having a series of amplifiers to meter and deliver fuel in various ranges of engine operating conditions, therefore allows a close tailoring of the fuel delivery to the requirements of the engine.
  • enrichment of the air-fuel mixture under particular operating conditions may be easily accomplished by using an amplifier with an increased gain to control fuel delivery in the range of the desired air flow rate.
  • a proportional fluid amplifier arrangement comprising and splitter means for dividing the fluid stream among said outlet port means in accordance with variations in the path of the fluid stream and for continuously varying the division of the fluid stream over the range of variations in the path of the fluid stream, said splitter means having lateral portion means converging to line intersection means, said line intersection means forming that portion of said splitter means most closely adjacent said inlet port means and defining splitter apex means, said splitter apex means being disposed relative to said inlet port means for non-linearly changing the division of the fluid stream among said outlet port means upon a predetermined change in the path of the fluid stream to establish a fluid condition in a portion of said outlet port means which varies in predetermined accordance with variations in the control signal.
  • said inlet port means comprises an inlet port opening into each independent interaction region
  • said source of fluid is connected to said inlet ports for issuing a portion of the fluid stream within each independent interaction region
  • said pair of outlet port means comprises a pair of outlet ports opening from each independent interaction region
  • splitter means comprises a separate splitter apex associated with each pair of outlet ports
  • An internal combustion engine fuel system comprising a nozzle adapted to discharge fuel for mixture with air,
  • fluid amplifier means including interaction region means, and inlet port means opening into said interaction region means,
  • a source of liquid fuel connected to said inlet port means for issuing a liquid fuel stream along a predetermined path within said interaction region, said fuel stream having a predetermined energy state
  • control means connected to said interaction region means for supplying a control signal indicative of an engine demand for fuel and having an energy state substantially lower than the energy state of the fuel stream and variations of which cause the path of the ,liquid fuel stream to vary within said interaction region in proportion to the control signal variations,
  • said amplifier means further including outlet means opening from said interaction region forreceiving the liquid fuel stream, said outlet'means having a plurality of outlet port means, and splitter means for dividing the liquid fuel stream among said outlet port means in accordance with variations in the path 'of the fuel stream and for continuously varying the division of the fluid stream over the range of variations in the path of the fluid stream, said splitter means being disposed relative to said inlet port means to non-linearly change th division of the fuel stream among said outlet port means upon a predetermined change in the path of the fuel stream to establish a rate of liquid fuel flow through a portion of said outlet port means which varies in ac cordance with variations in the control signal,
  • passage means connecting said portion of said outlet means to said nozzle for directing liquid fuel flow from said portion to said nozzle.
  • said inlet port means comprises an inlet port opening into each independent interaction region
  • said source of liquid fuel is connected to said inlet ports for issuing a portion of the fuel stream within each independent interaction region
  • said plurality of outlet port means comprises a pair of outlet ports opening from each independent interaction region
  • said splitter means comprises a splitter associated with each pair of outlet ports
  • control means comprises an air inlet for air flow to the engine and a venturi in said air inlet connected to said interaction region means, the rate of air flow through said venturi providing an air flow pressure signal which forms the control signal indicative of an engine demand for fuel.

Description

Oct. 22, 1968 c. MARKS 3,406,951
FLUID AMPLIFIER ARRANGEMENT AND FUEL SYSTEM INCORPORATING SAME Filed Sept. 16, 1965 f 29 {64 f6 2 j? 7 TANK //--AMPLIFIER SERIES SINGLE AMPLIFIER INVENTOR.
BY fray 5 50/5 ATTORNEY VENTURI PRE SSURE SIGNAL FUEL FLOW 3,406,951 FLUID AMPLIFIER ARRANGEMENT AND FUEL SYSTEM INCORPORATING SAME Craig Marks, Grosse Pointe Woods, Mich., assignor to General Motors Corporation, Detroit, Mich., a corporation of Delaware 7 Filed Sept. 16, 1965, Ser. No. 487,860 Claims. (Cl. 261-36) This invention relates to fluid amplifiers and to fuel systems utilizing fluid amplifier technology. Because spark ignition internal combustion engines are quite sensitive to the proportions of the air-fuel mixture in the combustion chamber, innumerable systems have been developed in attempts to supply the engine with an air-fuel mixture proper for the various operating conditions. The systems in common use, however, include a venturi located in the air inlet to create a pressure signal which varies with the rate of air flow to the engine; this pressure signal determines the rate at which fuel is delivered to the engine.
' Unfortunately however, the venturi signal does not vary linearly with air flow. When utilizing a large venturi to avoid restricting air flow at high air flow rates, the venturi signal is very weak at low air flow rates. This weak signal would 'result in insnfiicient fuel delivery to the engine. On the other hand, a small venturi which would provide an adequate fuel metering signal at low air flow rates would also'r'estrict air flow at high air flow rates. For these reasons, a compromise is generally adopted in which a separate idle system provides fuel'at the lowest air flow rates, a large venturi and one or two small boost venturi provide a fuel metering signal over the part throttle and wide-open throttle operating ranges, and offidle discharge ports smooth the transition from the idle system to the venturi metering system as the throttle open's.
Fuel systems have recently been developed which utilize fluid amplifiers to amplify the venturi pressure signal and deliver fuel to the engine at a rate determined by the amplified signal. Such an arrangement makes a complex idle system unnecessary.
As more extensively discussed in recent literature, Control'Engineering of January 1963, for example, a fluid amplifier uses a relatively weak control signal to deflect the path of a fluid stream. Because relatively large deflections in the fluid path are obtained with weak control signals, a more sensitive control function is obtained by measuring the deflection of the path rather than by directlymeasuring the control signal. However, when an amplifier has a linear response to a control signal, a fuel system relying on a single amplifier for fuel metering may riot supply the most desirable air-fuel mixture throughout the entire range of engine operating conditions.
This invention provides a fuel system including a fluid amplifier arrangement which closely tailors the rate of fuel delivery for the wide range of engine air flow rates. The fuel system includes a plurality of amplifiers which are sequentially actuated, each in a predetermined range of air flow rates, so that the pressure signal is sufficiently amplified to deliver fuel at a rate which closely approximates that required by the engine.
'The details as well as other objects and advantages of this invention are disclosed'in the following description and in the drawing in which:
FIGURE 1 illustrates a fuel system carburetor embodying this invention; and
FIGURE 2 graphically illustrates the fuel metering characteristics of this invention.
Referring to FIGURE 1, a carburetor has an air inlet 12 controlled by a throttle 14 in the customary manner. A venturi 16 provides a restriction Within air sa e Patent "ice inlet 12 which reduces the pressure of the air flow therethrough to create a control signal related to the rate of air flow.
A fluid amplifier arrangement, indicated generally by 18, has a common inlet 20 connected to a fuel pump 22. In the amplifier arrangement 18, a series of amplifiers, three being illustrated, each has an inlet 24, 26, and 28 opening into an interaction region 24a, 26a, 28a and a pair of outlets 3032, 34-36, and 3840 opening therefrom. Fuel is drawn from a tank 42 by pump 22, passes through the common inlet 20, and is issued from the individual inlets 24, 26, 28 in streams each having a predetermined path within an interaction region 24a, 26a, 28a and a predetermined energy state. The fuel streams are discharged from the interaction regions through outlets 30 through 40. With the amplifier arrangement so far described, the proportion of fuel discharged from outlets 32, 36, 40 is determined by the location of the splitters 44, 46, 48.
As air flows through the carburetor inlet 12 and the venturi 16, a pressure drop is produced to create a signal which is transferred through a fuel inlet nozzle 50, a passage 52, and the outlets 32, 36, 40 to the individual amplifiers. This pressure signal has an energy state much lower than that of the fuel streams issued from ports 24, 26, 28, but deflects fuel stream to change the proportion of fuel discharged through outlets 32, 36, 40.
Amplifiers which operate as described are known as proportional amplifiers since the proportion of the fluid discharged through the outlets 32, 36, 40 varies with the pressure drop in the venturi 16.
As' is well-known, the venturi pressure signal varies as the square of the rate of air flow through the inlet 12. Because the engine requires fuel flow more directly proportional to air flow, it is desirable to have the venturi pressure signal also vary as the square of the rate of fuel flow. It will be appreciated that, as illustrated by the single amplifier curve of FIGURE 2, a single amplifier controlled by the venturi signal can only roughly approximate such a fuel delivery requirement.
Therefore, this invention provides an amplifier arrangement 18 in which the splitters 44, 46, 48 of the various individual amplifiers are arranged so that splitter 44 initially divides fuel flow from inlet 24 between outlets 30 and 32 while splitters 46 and 48 direct the entire fuel flow from inlets 26 and 28 to outlets 34 and 38 and then to a sump 54 which drains back to tank 42 The arrangement is such that when substantially the entire fuel flow from inlet 24 is discharged through outlet 32, the pressure in outlet 36 is sufficient to cause splitter 46 to divide the fuel flow from inlet 26 between outlets 34 and 36, and similarly, when substantially the entire .fuel flow from inlets 24 and 26 is directed through outlets 32 and 36, the pressure in outlet 40 is suflicient to cause splitter 48 to divide the fuel flow from inlet 28 between outlets 38 and 40.
The fuel metering characteristics of this invention are graphically illustrated in FIGURE 2 where it will be noted that the fuel delivery of the amplifier series very closely approximates the requirements of the engine.
This invention, in providing a fuel system having a series of amplifiers to meter and deliver fuel in various ranges of engine operating conditions, therefore allows a close tailoring of the fuel delivery to the requirements of the engine. In addition, enrichment of the air-fuel mixture under particular operating conditions may be easily accomplished by using an amplifier with an increased gain to control fuel delivery in the range of the desired air flow rate. Those skilled in fuel system and fluid amplifier technologies will readily appreciate that this invention may be utilized in many other arrangements to supply fuel to an engine.
3 I'claim: 1. A proportional fluid amplifier arrangement comprising and splitter means for dividing the fluid stream among said outlet port means in accordance with variations in the path of the fluid stream and for continuously varying the division of the fluid stream over the range of variations in the path of the fluid stream, said splitter means having lateral portion means converging to line intersection means, said line intersection means forming that portion of said splitter means most closely adjacent said inlet port means and defining splitter apex means, said splitter apex means being disposed relative to said inlet port means for non-linearly changing the division of the fluid stream among said outlet port means upon a predetermined change in the path of the fluid stream to establish a fluid condition in a portion of said outlet port means which varies in predetermined accordance with variations in the control signal.
2. The fluid amplifier arrangement of claim 1 wherein said interaction region comprises a number of independent interaction regions,
said inlet port means comprises an inlet port opening into each independent interaction region,
said source of fluid is connected to said inlet ports for issuing a portion of the fluid stream within each independent interaction region,
said pair of outlet port means comprises a pair of outlet ports opening from each independent interaction region,
and said splitter means comprises a separate splitter apex associated with each pair of outlet ports,
and which includes means connected to one outlet port of each pair of outlet ports to form a common outlet passage comprising said portion of said outlet port means,
and wherein the apexes are disposed relative to the inlet ports to sequentially divide the portions of the fluid stream issued within said independent interaction regions.
3. An internal combustion engine fuel system comprising a nozzle adapted to discharge fuel for mixture with air,
fluid amplifier means including interaction region means, and inlet port means opening into said interaction region means,
a source of liquid fuel connected to said inlet port means for issuing a liquid fuel stream along a predetermined path within said interaction region, said fuel stream having a predetermined energy state,
Cir
control means connected to said interaction region means for supplying a control signal indicative of an engine demand for fuel and having an energy state substantially lower than the energy state of the fuel stream and variations of which cause the path of the ,liquid fuel stream to vary within said interaction region in proportion to the control signal variations,
said amplifier means further including outlet means opening from said interaction region forreceiving the liquid fuel stream, said outlet'means having a plurality of outlet port means, and splitter means for dividing the liquid fuel stream among said outlet port means in accordance with variations in the path 'of the fuel stream and for continuously varying the division of the fluid stream over the range of variations in the path of the fluid stream, said splitter means being disposed relative to said inlet port means to non-linearly change th division of the fuel stream among said outlet port means upon a predetermined change in the path of the fuel stream to establish a rate of liquid fuel flow through a portion of said outlet port means which varies in ac cordance with variations in the control signal,
and passage means connecting said portion of said outlet means to said nozzle for directing liquid fuel flow from said portion to said nozzle.
4. The fuel system of claim 3 wherein said interaction region comprises a number of independent interaction regions,
said inlet port means comprises an inlet port opening into each independent interaction region,
said source of liquid fuel is connected to said inlet ports for issuing a portion of the fuel stream within each independent interaction region,
said plurality of outlet port means comprises a pair of outlet ports opening from each independent interaction region,
said splitter means comprises a splitter associated with each pair of outlet ports,
and said passage means connects One outlet port of each pair of outlet ports to said nozzle.
5. The fuel system of claim 3 wherein said control means comprises an air inlet for air flow to the engine and a venturi in said air inlet connected to said interaction region means, the rate of air flow through said venturi providing an air flow pressure signal which forms the control signal indicative of an engine demand for fuel.
References Cited UNITED STATES PATENTS 2,676,602 4/1954 Fox 26111O X 3,001,539 9/1961 Hurritz 137-815 3,132,191 5/1965 Kennedy 261-69 X 3,258,023 6/1966 Bowles 137-81.5 3,248,053 4/1966 Phillips 137-81.5
FOREIGN PATENTS 1,257,050 2/1961 France.
694,387 7/1953 Great Britain.
289,804 3 1953 Switzerland.
966,660 8/1964 Great Britain.
HARRY B. THORNTON, Primary Examiner.
T. R. MILES, Assistant Examiner.

Claims (1)

  1. 3. AN INTERNAL COMBUSTION ENGINE FUEL SYSTEM COMPRISING A NOZZLE ADAPTED TO DISCHARGE FUEL FOR MIXTURE WITH AIR, FLUID AMPLIFIER MEANS INCLUDING INTERACTION REGION MEANS, AND INLET PORT MEANS OPENING INTO SAID INTERACTION REGION MEANS, A SOURCE OF LIQUID FUEL CONNECTED TO SAID INLET PORT MEANS FOR ISSUING A LIQUID FUEL STREAM ALONG A PREDETERMINED PATH WITHIN SAID INTERACTION REGION, SAID FUEL STREAM HAVING A PREDETERMINED ENERGY STATE, CONTROL MEANS CONNECTED TO SAID INTERACTION REGION MEANS FOR SUPPLYING A CONTROL SIGNAL INDICATIVE OF AN ENGINE DEMAND FOR FUEL AND HAVING AN ENERGY STATE SUBSTANTIALLY LOWER THAN THAN THE ENERGY STATE OF THE FUEL STREAM AND VARIATIONS OF WHICH CAUSE THE PATH OF THE LIQUID FUEL STREAM TO VARY WITHIN SAID INTERACTION REGION IN PROPERTION TO THE CONTROL SIGNAL VARIATIONS, SAID AMPLIFIER MEANS FURTHER INCLUDING OUTLET MEANS OPENING FROM SAID INTERACTION REGION FOR RECEIVING THE LIQUID FUEL STREAM, SAID OUTLET MEANS HAVING A PLURALITY OF OUTLET PORT MEANS, AND SPLITTER MEANS FOR DIVIDING THE LIQUID FUEL STREAM AMONG SAID OUTLET PORT MEANS IN ACCORDANCE WITH VARIATIONS IN THE PATH OF THE FUEL STREAM AND FOR CONTINUOUSLY VARYING THE DIVISION OF THE FLUID STREAM OVER THE RANGE
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GB3388066A GB1116549A (en) 1965-09-16 1966-07-28 Internal combustion engine fuel systems
DE19661526672 DE1526672C (en) 1965-09-16 1966-08-05 Carburetors for internal combustion engines

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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3530600A (en) * 1967-10-26 1970-09-29 Westinghouse Air Brake Co Earthmoving scrapper with fluidic control means
US3533606A (en) * 1968-02-06 1970-10-13 Arthur K Thatcher Ultrasonic carburetor system
US3556063A (en) * 1969-06-25 1971-01-19 Borg Warner Fuel system
US3556488A (en) * 1968-07-10 1971-01-19 Aisan Kogyo Co Ltd Carburetor with fluid elements
US3557811A (en) * 1968-10-18 1971-01-26 Factory Mutual Res Corp Dynamic flow sensor
US3570823A (en) * 1968-07-12 1971-03-16 Aisan Kogyo Co Ltd Carburetor with fluid amplifying elements
US3590840A (en) * 1968-05-29 1971-07-06 Bendix Corp Fluidic control apparatus
US3608872A (en) * 1968-07-18 1971-09-28 Aisan Kogyo Co Ltd Engine fuel supply having separate air and fuel mixing bores
US3648987A (en) * 1969-04-07 1972-03-14 Aisan Kogyo Co Ltd Fluidic two-stage carburetor
US3690625A (en) * 1969-08-18 1972-09-12 Mikuni Kogyo Kk Carburetor utilizing fluidics
US4202061A (en) * 1978-12-29 1980-05-13 The Boeing Company Lavatory wastewater disposal system for aircraft
US6776183B1 (en) 2003-02-28 2004-08-17 Goodrich Corporation Aircraft drain device

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CH289804A (en) * 1950-03-09 1953-03-31 Gianini Carlo Process for the intermittent forced pulverization of fuel in internal combustion engines and carburetor for carrying out the process.
GB694387A (en) * 1950-03-09 1953-07-22 Carlo Gianini System of carburation in internal combustion engines, and a carburettor embodying the system
US2676602A (en) * 1952-10-28 1954-04-27 Pure Oil Co Stream divider for proportioning the flow of liquids
FR1257050A (en) * 1960-02-13 1961-03-31 App Control Equip Moteurs Improvements made to carburetion devices, in particular for two-stroke engines, and to engines fitted with these devices
US3001539A (en) * 1960-08-15 1961-09-26 Hurvitz Hyman Suction amplifier
US3132191A (en) * 1962-03-09 1964-05-05 Sr Walter L Kennedy Fuel injection device
GB966660A (en) * 1962-04-23 1964-08-12 Sperry Rand Corp Pure fluid amplifier
US3248053A (en) * 1964-06-18 1966-04-26 Sperry Rand Corp Monostable fluid amplifier and shift register employing same
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CH289804A (en) * 1950-03-09 1953-03-31 Gianini Carlo Process for the intermittent forced pulverization of fuel in internal combustion engines and carburetor for carrying out the process.
GB694387A (en) * 1950-03-09 1953-07-22 Carlo Gianini System of carburation in internal combustion engines, and a carburettor embodying the system
US2676602A (en) * 1952-10-28 1954-04-27 Pure Oil Co Stream divider for proportioning the flow of liquids
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US3001539A (en) * 1960-08-15 1961-09-26 Hurvitz Hyman Suction amplifier
US3132191A (en) * 1962-03-09 1964-05-05 Sr Walter L Kennedy Fuel injection device
GB966660A (en) * 1962-04-23 1964-08-12 Sperry Rand Corp Pure fluid amplifier
US3258023A (en) * 1963-04-12 1966-06-28 Romald E Bowles Pneumatic eye
US3248053A (en) * 1964-06-18 1966-04-26 Sperry Rand Corp Monostable fluid amplifier and shift register employing same

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3530600A (en) * 1967-10-26 1970-09-29 Westinghouse Air Brake Co Earthmoving scrapper with fluidic control means
US3533606A (en) * 1968-02-06 1970-10-13 Arthur K Thatcher Ultrasonic carburetor system
US3590840A (en) * 1968-05-29 1971-07-06 Bendix Corp Fluidic control apparatus
US3556488A (en) * 1968-07-10 1971-01-19 Aisan Kogyo Co Ltd Carburetor with fluid elements
US3570823A (en) * 1968-07-12 1971-03-16 Aisan Kogyo Co Ltd Carburetor with fluid amplifying elements
US3608872A (en) * 1968-07-18 1971-09-28 Aisan Kogyo Co Ltd Engine fuel supply having separate air and fuel mixing bores
US3557811A (en) * 1968-10-18 1971-01-26 Factory Mutual Res Corp Dynamic flow sensor
US3648987A (en) * 1969-04-07 1972-03-14 Aisan Kogyo Co Ltd Fluidic two-stage carburetor
US3556063A (en) * 1969-06-25 1971-01-19 Borg Warner Fuel system
US3690625A (en) * 1969-08-18 1972-09-12 Mikuni Kogyo Kk Carburetor utilizing fluidics
US4202061A (en) * 1978-12-29 1980-05-13 The Boeing Company Lavatory wastewater disposal system for aircraft
US6776183B1 (en) 2003-02-28 2004-08-17 Goodrich Corporation Aircraft drain device

Also Published As

Publication number Publication date
DE1526672B1 (en) 1972-11-16
GB1116549A (en) 1968-06-06

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