US1625997A - Method of and apparatus for atomizing liquid fuel - Google Patents

Method of and apparatus for atomizing liquid fuel Download PDF

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Publication number
US1625997A
US1625997A US559035A US55903522A US1625997A US 1625997 A US1625997 A US 1625997A US 559035 A US559035 A US 559035A US 55903522 A US55903522 A US 55903522A US 1625997 A US1625997 A US 1625997A
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Prior art keywords
fuel
engine
liquid fuel
passage
gas
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Expired - Lifetime
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US559035A
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Gronkwist Oscar Robert
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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
    • F02M19/00Details, component parts, or accessories of carburettors, not provided for in, or of interest apart from, the apparatus of groups F02M1/00 - F02M17/00
    • F02M19/03Fuel atomising nozzles; Arrangement of emulsifying air conduits
    • 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
    • F02M17/00Carburettors having pertinent characteristics not provided for in, or of interest apart from, the apparatus of preceding main groups F02M1/00 - F02M15/00
    • F02M17/42Float-controlled carburettors not otherwise provided for
    • 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
    • F02M33/00Other apparatus for treating combustion-air, fuel or fuel-air mixture
    • F02M33/02Other apparatus for treating combustion-air, fuel or fuel-air mixture for collecting and returning condensed fuel
    • F02M33/08Other apparatus for treating combustion-air, fuel or fuel-air mixture for collecting and returning condensed fuel returning to the fuel tank
    • 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
    • Y10S261/00Gas and liquid contact apparatus
    • Y10S261/21Drawing excess fuel from carbureting passage
    • 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
    • Y10S261/00Gas and liquid contact apparatus
    • Y10S261/27Gas circulated in circuit
    • 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
    • Y10S261/00Gas and liquid contact apparatus
    • Y10S261/45Processes carburetors
    • 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
    • Y10S261/00Gas and liquid contact apparatus
    • Y10S261/51Carburetors with supercharging blowers

Definitions

  • the esent invention has for its object to avoid the said disadvantages.
  • the present method principally consists in causing the gas current utilized for the atomization wholly or partly to circulate.
  • the said circulation can take lace quite independently of the number 0 -revolutions and the output of the engine in a separate passage from which the quantity of fuel mist required at each time may be taken, and to which a corresponding new quantity of air or gas is automatically admitted.
  • a fan or the like may be connected in the path of circulation for generating and maintaining the gas current, and further there may be connected in the path of circulation a collecting chamber of greater volume which thus becomes filled with mist of the liquid, and from which said mist is taken, so that thus the required quantity of fuel mist is always at mmediate disposal.
  • 1 denotes a fan driven in any suitable manner
  • 2 is the pressure conduit from the fan which is constricted at 3 to form a nozzle and is afterwards enlarged to form a collecting chamber
  • 5 denotes the suction conduit which communicates with the atmosphere, or with a gas conduit, through a pipe connection 6;
  • the suction conduit 5 communicates with the chamber 4, so that the parts 1, 2, 4, and 5 form a continuous passage or circuit in which the circulation of the gas current may take place.
  • the fuel nozzle 7 which communicates with a float chamber, not illustrated in the drawing, opens into the said passage immediately beyond the constriction
  • a pipe 8 leads from the bottom of the chamber 4 to the fuel tank, so that the excess fuel may'flow back into the tank.
  • the chamber 4 also communicates through a 'pipe 9 with the air suction pipe 10 of the engine, which ipe leads to the cylinders of the engine and may be closed more or less bymeans of the throttle valve 11 which turns on the shaft 12.
  • the apparatus described operates in the following manner:
  • the throttle valve 11 serves for regulating the engine for different loads, said valve closing the suction conduit more or less and thus controlling the filling of the engine cylinders. It would of course also be possible to provide a throttle member in the pipe 9 and thus to influence the composition of the mixture. Finall b utilizing two throttle members it won (1 a so be possible to operate with control of the mixture as well as of the filling. Air or gas flowing in through the pipe connection 6 in the same proportion as fuel mist is taken from the collecting chamber 4, the gas current serving for atomizing the liquid fuel is 'of course in no manner influenced by the control and the running of the engine.
  • the fanl is of course preferably driven by the engine for the driving of which the atomizing apparatus serves.
  • preheating and vaporiza- 1 The method of atomizing liquid fuel' atomized fuel to the intake of the engine,
  • An apparatus for atomizing liquid fuel comprising in combination a circulationpassage, means for admitting liquid fuel into said passage, means for generating and maintaining a current of-gas in circulation through said passage past said liquid admitting means, an outlet from said circulation passage for discharging a mixture of gas and atomized fuel, and an inlet for fresh gas to said circulation passage.
  • An apparatus for atomizing liquid fuel comprising in combination a circulation passage, means for admitting liquid fuel into said passage, means for nerating and maintaining a current of gas in circula tion through said passage, means for discharging a mixture of gas and atomized fuel from said circulation passa e, means for admitting fresh gas into said circulation passage, and means for draining excess liquid fuel from said passage.

Description

Ap l 2 8"; 1921 o. R. eR'ONKwlsT METHOD OF AND APPARATUS FOR ATOMIZING LIQUID FUEL Filed May 6, 1922 [Ivan/0r OscAfiRoBERT GRbNkwlsT' Patentd Apr 1927. I
' UNITED STATES PATENT OFFICE.
oscsn aonnn'r eaonxwisr, or srocxnom, swnnmt.
METHOD OF AND APPARATUS FOR ATOMIZITTG LIQUID FUEL.
Application filed May 6, 1922, Serial No. 559,035, and in Germany May 7, 1921.
which is admitted under excess of pressure,-
atomizes .each time the entire quantity .of fuel which is in readiness. For measuring the quantity of fuel required at such time .a fuel pump is thus necessary and for this reason this method is not very suitable for fast running engines. According to a method adapted for explosion engines the liquid fuel is in readiness in a practically unlimited quantity, and the measurin of the quantity of fuel required for a wor ing' cycle is effected in such manner that the total quantity of air required for a working cycle is led past the fuel nozzle and thus becomes char ed with fuel. This method has the 'disa vantage, however, that the composition of the combustible mixture is dependent to a great extentonthe numberof revolutions of the engine, and becomes too rich in fuel at a high speed, but too poor in fuel at low speed. A further disadvantage of the said method consists in that for .acceleration of the atomizing air current only the very small pressure diiferencebetween the atmospheric pressure and the vacuum in the engine is at disposal, so that in order to attain a sufficient high velocity of the air current the air conduit must be very much constricted in the vicinity of the fuel nozzle. The result will be that engines having such atomizing apparatus operate with'an unfavourable volumetric efliciency also .at full load and normal number of revolutions.
The esent invention has for its object to avoid the said disadvantages. For this purpose the present method principally consists in causing the gas current utilized for the atomization wholly or partly to circulate. In the case of atomization of liquid fuel for. internal combustion engines the said circulation can take lace quite independently of the number 0 -revolutions and the output of the engine in a separate passage from which the quantity of fuel mist required at each time may be taken, and to which a corresponding new quantity of air or gas is automatically admitted. For this purpose a fan or the like may be connected in the path of circulation for generating and maintaining the gas current, and further there may be connected in the path of circulation a collecting chamber of greater volume which thus becomes filled with mist of the liquid, and from which said mist is taken, so that thus the required quantity of fuel mist is always at mmediate disposal.
. In the accompanying drawing, an apparatus for atomiz ing liquid fuel for an internal combustion engine is illustrated by way of example.
' Referring to the drawing, 1 denotes a fan driven in any suitable manner, 2 is the pressure conduit from the fan which is constricted at 3 to form a nozzle and is afterwards enlarged to form a collecting chamber 4, and 5 denotes the suction conduit which communicates with the atmosphere, or with a gas conduit, through a pipe connection 6; The suction conduit 5 communicates with the chamber 4, so that the parts 1, 2, 4, and 5 form a continuous passage or circuit in which the circulation of the gas current may take place. The fuel nozzle 7 which communicates with a float chamber, not illustrated in the drawing, opens into the said passage immediately beyond the constriction A pipe 8 leads from the bottom of the chamber 4 to the fuel tank, so that the excess fuel may'flow back into the tank. The chamber 4 also communicates through a 'pipe 9 with the air suction pipe 10 of the engine, which ipe leads to the cylinders of the engine and may be closed more or less bymeans of the throttle valve 11 which turns on the shaft 12.
The apparatus described operates in the following manner:
When the fan 1 is driven with the necessary speed there is produced in the circuit or passage 2, 4,, 5 a circulating gas current. The current will of course obtain its highest velocity in the construction 3, and the gas current will therefore atomize very finely the fuel admitted through the nozzle 7, so that the collecting chamber 4 will always be filled with a fuel mist of approximately atmospheric pressure. If new the engine draws air through the pipe 10, a certain quantity of such fuel mist will be drawn from the chamber 4 by the air current flowing past the opening of the pipe 9 and will be mixed with the air. The air drawn in and the fuel mist practically following the same laws of flow, there will always be obtained a properly proportioned mixture of fuel mist and air, notwithstanding a 'varying number of revolutions of the engine, that is to say, notwithstanding a varying velocity of the air in the pipe 10. The throttle valve 11 serves for regulating the engine for different loads, said valve closing the suction conduit more or less and thus controlling the filling of the engine cylinders. It would of course also be possible to provide a throttle member in the pipe 9 and thus to influence the composition of the mixture. Finall b utilizing two throttle members it won (1 a so be possible to operate with control of the mixture as well as of the filling. Air or gas flowing in through the pipe connection 6 in the same proportion as fuel mist is taken from the collecting chamber 4, the gas current serving for atomizing the liquid fuel is 'of course in no manner influenced by the control and the running of the engine.
In practice the fanl is of course preferably driven by the engine for the driving of which the atomizing apparatus serves. It
is suitable to connect between the engine and the fan an intermediate gear which makes 1t possible to drive the fan with a constant number of revolutions independent of the speed of the engine. In order to avoid ignition in the atomizing apparatus, for in stance in the chamber 4, it may in certain cases be suitable to use instead of the air a neutral as free from oxygen, and it may exhaust as, for tion. of t e fuel. I claim:
preheating and vaporiza- 1. The method of atomizing liquid fuel' atomized fuel to the intake of the engine,
and admitting a. corresponding quantity of fresh gas to said circulating current.
2. An apparatus for atomizing liquid fuel, comprising in combination a circulationpassage, means for admitting liquid fuel into said passage, means for generating and maintaining a current of-gas in circulation through said passage past said liquid admitting means, an outlet from said circulation passage for discharging a mixture of gas and atomized fuel, and an inlet for fresh gas to said circulation passage.
3. An apparatus for atomizing liquid fuel, comprising in combination a circulation passage, means for admitting liquid fuel into said passage, means for nerating and maintaining a current of gas in circula tion through said passage, means for discharging a mixture of gas and atomized fuel from said circulation passa e, means for admitting fresh gas into said circulation passage, and means for draining excess liquid fuel from said passage.
4;. The combination with aninternal combustion engine, of a circulation passage for atomized fuel, a conduit for conveying fuel from said passage to the combustion chamber of said engine, and means for maintaining a quantity of atomized fuel in circulation in said passage during the operaalso be a vantageous' to mtroduce in the tion of Said englneatomizing circuit ahot gas, for instance hot OSCAR ROBERT GRfiNKWIST.
US559035A 1921-05-07 1922-05-06 Method of and apparatus for atomizing liquid fuel Expired - Lifetime US1625997A (en)

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US58412A US1824540A (en) 1922-05-06 1925-09-24 Apparatus for producing a lubricating oil mist

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DE1625997X 1921-05-07

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2450418A (en) * 1943-07-13 1948-10-05 Delphis C Breault Oil burner
US2578501A (en) * 1948-07-21 1951-12-11 Westinghouse Electric Corp Fuel trap for combustion apparatus of gas turbine engines
US2682454A (en) * 1951-01-17 1954-06-29 Wilfred W Ray Vaporizer
US2822792A (en) * 1956-11-08 1958-02-11 Adolphe C Peterson Direct and indirect injection means for combustion engines
US3042015A (en) * 1957-06-20 1962-07-03 Adolphe C Peterson High or low compression injection fuel system
US3282573A (en) * 1963-09-05 1966-11-01 Harold E Phelps Fuel feeding system
US3326538A (en) * 1964-08-12 1967-06-20 Marvin D Merritt Vapor generator
US3386709A (en) * 1965-09-16 1968-06-04 Gen Motors Corp Fuel system and method of operation
US3456636A (en) * 1967-07-14 1969-07-22 Vernon F J Marcoux Carburetor for rotary engines
US3498028A (en) * 1966-06-22 1970-03-03 Shell Oil Co Apparatus for contacting liquids and gases
US4092962A (en) * 1974-09-23 1978-06-06 Steven P. Corrigan Precarburetor ignition system
US4157084A (en) * 1977-09-20 1979-06-05 Wallis Marvin E Fuel injection system and method for internal combustion engine
US4543939A (en) * 1983-01-20 1985-10-01 Pierburg Gmbh & Co. K.G. Fuel supply assembly for mixture-compressing internal combustion engines and associated methods of operation

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2450418A (en) * 1943-07-13 1948-10-05 Delphis C Breault Oil burner
US2578501A (en) * 1948-07-21 1951-12-11 Westinghouse Electric Corp Fuel trap for combustion apparatus of gas turbine engines
US2682454A (en) * 1951-01-17 1954-06-29 Wilfred W Ray Vaporizer
US2822792A (en) * 1956-11-08 1958-02-11 Adolphe C Peterson Direct and indirect injection means for combustion engines
US3042015A (en) * 1957-06-20 1962-07-03 Adolphe C Peterson High or low compression injection fuel system
US3282573A (en) * 1963-09-05 1966-11-01 Harold E Phelps Fuel feeding system
US3326538A (en) * 1964-08-12 1967-06-20 Marvin D Merritt Vapor generator
US3386709A (en) * 1965-09-16 1968-06-04 Gen Motors Corp Fuel system and method of operation
US3498028A (en) * 1966-06-22 1970-03-03 Shell Oil Co Apparatus for contacting liquids and gases
US3456636A (en) * 1967-07-14 1969-07-22 Vernon F J Marcoux Carburetor for rotary engines
US4092962A (en) * 1974-09-23 1978-06-06 Steven P. Corrigan Precarburetor ignition system
US4157084A (en) * 1977-09-20 1979-06-05 Wallis Marvin E Fuel injection system and method for internal combustion engine
US4543939A (en) * 1983-01-20 1985-10-01 Pierburg Gmbh & Co. K.G. Fuel supply assembly for mixture-compressing internal combustion engines and associated methods of operation

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