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US2291418A - Carburetor - Google Patents

Carburetor Download PDF

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Publication number
US2291418A
US2291418A US353449A US35344940A US2291418A US 2291418 A US2291418 A US 2291418A US 353449 A US353449 A US 353449A US 35344940 A US35344940 A US 35344940A US 2291418 A US2291418 A US 2291418A
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US
United States
Prior art keywords
fuel
nozzle
idle
passage
carburetor
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
Application number
US353449A
Inventor
Jr John E Storer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Borg Warner Corp
Original Assignee
Borg Warner Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Borg Warner Corp filed Critical Borg Warner Corp
Priority to US353449A priority Critical patent/US2291418A/en
Application granted granted Critical
Publication of US2291418A publication Critical patent/US2291418A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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
    • F02M3/00Idling devices for carburettors
    • F02M3/08Other details of idling devices
    • F02M3/12Passageway systems
    • 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
    • F02M19/06Other details of fuel conduits

Definitions

  • This invention relates to carburetors of the type wherein the idle jet takes its fuel supply from the lower portion of the main nozzle into which lower portion the fuel is delivered from the fuel reservoir by a power jet.
  • the general object of the invention is'to improve upon the construction of the type of carburetor mentioned so as to prevent the occurrence of the above described condition.
  • the invention provides means for preventing the fuel stream issuing from the power jet from being projected past the inlet of the idle jet.
  • Fig. 1 is an elevation of a carburetor, partly in section, embodying the invention.
  • Fig. 2 is a transverse sectional view of the main nozzle taken as indicated by the line 22 of Fig. 1.
  • Fig. 3 is a detailed sectional view illustrating a modified form of the invention.
  • Fig. 4 is a detailed sectional another modification of the invention.
  • Fig. 5 is a detailed sectional View illustrating a still further modification of the invention.
  • Fig. 6 is a perspective view of another modification of the invention.
  • Fig. 7 is a perspective view fication of the invention.
  • Fig. 8 is a sectional View form of the invention.
  • Fig. 9 is a sectional view of fied form of the invention.
  • Fig. 10 is a sectional View of a still further modified form of the invention.
  • a carburetor comprising a throttle barrel l2 in which is mounted a pair of Venturi tubes l4 and I6 which cooperate with the barrel l2 to form a fuel mixing passage.
  • Formed integral with the skirt [8 is a fuel bowl 20 from which fuel is adapted to flow through a fuel channel 22 to a power jet indicated generally at 24, which is threaded into the wall of the skirt IS in axial alignment with the main nozzle 26, which is mounted in a tubular boss 28 formed inside of the skirt I 8.
  • the lower end of the nozzle 26 is threaded as at 30 into the boss 28 and is provided with a delivery opening 32 through which fuel passes to the idle fuel orifice 34, formed in the lower end of the idle tube 36.
  • Air is adapted to pass through a nozzle air vent 33 into an annular passage 38 defined between the main nozzle 26 and the boss 28, and from the passage ii] the air may enter the main nozzle 26 through nozzle bleed holes 62 to form, together with the fuel that is being injected into the main nozzle by the power nozzle 2%, an emulsion which is delivered from the main nozzle outlet 44 into the throat of the Venturi It.
  • air may also flow to an annular passage 46 surrounding the idle nozzle 35, and then through idle vent 48 into the idle tube 36, there to form an emulsion which is delivered through an emulsion channel 59'] formed in the wall of the barrel l2 to an idle delivery opening 52, controlled by a needle valve 56.
  • the flow of air through the mixing passage is controlled by a throttle valve 58 which when closed is adapted to establish high suction on its posterior side and to subtantially cut off the flow of air through the mixing passage, thereby causing a rich mixture to be drawn from the idle opening 52 into mixing passage posterior of the valve 58.
  • the valve 58 opens, the outlet 5% will become operative to assist the outlet 52 in delivering the rich mixture, and with further opening of the throttle, the fiow of air through the Venturi tubes will increase to a point where fuel will be delivered from the nozzle outlet M for high speed operation.
  • the demand upon the high speed nozzle will be such as to cause a continuous stream of fuel to be projected from the power jet 2! and the idle system will be reversed so that air is drawn from idle fuel orifice 34 into main nozzle 26 through delivery opening 32.
  • the stream of fuel from the jet 24 was projected beyond the inlet opening 32 of the idle jet, so that upon a sudden closing of the throttle from a wide open position, the momentum of the stream would momentarily preforms, comprises simply a pin 60 mounted in the 26 and extending diametriso that the stream of lower end of nozzle cally across the mouth,
  • the pin may be mounted in notches in the upper end of the nozzle 24, as indicated in Fig. 3, at 69 7
  • the baffle element may instead of being mounted at right angles to the axis of the nozzle, be mounted at an angle as shown at 601) in Fig. 4.
  • the bafile element may be secured at one end and extend only part way across the nozzle bore as indicated at 600 in Fig. 5.
  • the pin 68d shown in mounted in the notches in 24, is mounted in a position said notches.
  • the baffle element may, as shown in Fig. 7, be in the form of a washer 6
  • the baflie is formed by an extension 69] on the end of the idle tube 36F.
  • the battle element is in the form of a separate short tube 60g which comprises the inlet to the idle passage.
  • the baiiie is likewise in the form of a tube forming the inlet to the idle passage, the tube 60h in this case extending entirely across Fig. 6, instead of being the end of the nozzle at right angles to the nozzle 26 and having an opening 62 through which fuel passes to the idle passage.
  • a carburetor assembly including means defining a main air passage having a venturi therein, a butterfly throttle valve for controlling the flow therethrough and an upwardly extending nozzle having one end in communication with fuel from a fuel bowl, th other end being positioned within said venturi for delivering fuel thereto, said nozzle having a straight cylindrical bore leading from the inlet to th outlet thereof, means defining an idle fuel supply passage having the discharge end thereof under the control of said butterfly valve when moved to the idle position, said idle passage having an inlet terminal portion communicating directly with said nozzle bore at a point spaced along the axis of said bore from the inlet end thereof, means defining a metering power jet located below the inlet.
  • said arrangement being particularly characterized by the provision of a pinlike element projecting across the path of flow from said power jet at a point between said power jet defining means and said idle passage inlet, said pin-like element having a cross-sectional area less than the cross-sectional area of the bore of said nozzle, and being the sole obstruction to the free flow of fuel from said jet to the outlet of said nozzle, said power jet being directed against said pin-like element which functions to prevent the fuel from being projected beyond said idle inlet, thus providing a supply of fuel at said idle inlet to be drawn therein when said butterfly valve is moved to idle position to effect a change over from main nozzle feed to idle feed.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of The Air-Fuel Ratio Of Carburetors (AREA)

Description

y 1942- J. E. STCRER, JR 2,291,418
I I CARBURE'fOR Filed Aug. 21, 1940 f P J6 I J \fd/ire. EJZorer:
Patente d July 28, 1942 CARBURETOR John E. Storer, Jr., Flint, Warner Corporation,
tion of Illinois Mich., assignor to Borg- Chicago, 111., a corpora- Application August 21, 1940, Serial No. 353,449
1 Claim.
This invention relates to carburetors of the type wherein the idle jet takes its fuel supply from the lower portion of the main nozzle into which lower portion the fuel is delivered from the fuel reservoir by a power jet.
In the operation of such a carburetor, there sometimes occurs a hiatus in the delivery of the proper mixture from the carburetor and a consequent momentary misfiring of the engine, when the throttle is moved from a full open position to a position corresponding to a lower speed than cruising speed, i. e., about half open or slightly less. Where the carburetor is applied to aircraft, such mis-firing of the engine, even though restricted to only one or two cylinders, is particularly objectionable.
The general object of the invention is'to improve upon the construction of the type of carburetor mentioned so as to prevent the occurrence of the above described condition. To this end the invention provides means for preventing the fuel stream issuing from the power jet from being projected past the inlet of the idle jet.
Other objects, the advantages and uses of my invention will become more apparent after reading the following specification and claim, and after consideration of the drawing forming a part of the specification, wherein:
Fig. 1 is an elevation of a carburetor, partly in section, embodying the invention.
Fig. 2 is a transverse sectional view of the main nozzle taken as indicated by the line 22 of Fig. 1.
Fig. 3 is a detailed sectional view illustrating a modified form of the invention.
Fig. 4 is a detailed sectional another modification of the invention.
Fig. 5 is a detailed sectional View illustrating a still further modification of the invention.
Fig. 6 is a perspective view of another modification of the invention.
Fig. 7 is a perspective view fication of the invention.
Fig. 8 is a sectional View form of the invention.
Fig. 9 is a sectional view of fied form of the invention.
Fig. 10 is a sectional View of a still further modified form of the invention.
As an illustration of one form in which the invention may be embodied, there is shown in Fig. 1 a carburetor comprising a throttle barrel l2 in which is mounted a pair of Venturi tubes l4 and I6 which cooperate with the barrel l2 to form a fuel mixing passage. Secured to the barrel I2 is a skirt of a further modiof another modified a still further modiview illustrating I8 through which air flows to the mixture passage. Formed integral with the skirt [8 is a fuel bowl 20 from which fuel is adapted to flow through a fuel channel 22 to a power jet indicated generally at 24, which is threaded into the wall of the skirt IS in axial alignment with the main nozzle 26, which is mounted in a tubular boss 28 formed inside of the skirt I 8.
The lower end of the nozzle 26 is threaded as at 30 into the boss 28 and is provided with a delivery opening 32 through which fuel passes to the idle fuel orifice 34, formed in the lower end of the idle tube 36.
Air is adapted to pass through a nozzle air vent 33 into an annular passage 38 defined between the main nozzle 26 and the boss 28, and from the passage ii] the air may enter the main nozzle 26 through nozzle bleed holes 62 to form, together with the fuel that is being injected into the main nozzle by the power nozzle 2%, an emulsion which is delivered from the main nozzle outlet 44 into the throat of the Venturi It.
From the vent 38, air may also flow to an annular passage 46 surrounding the idle nozzle 35, and then through idle vent 48 into the idle tube 36, there to form an emulsion which is delivered through an emulsion channel 59'] formed in the wall of the barrel l2 to an idle delivery opening 52, controlled by a needle valve 56.
The flow of air through the mixing passage is controlled by a throttle valve 58 which when closed is adapted to establish high suction on its posterior side and to subtantially cut off the flow of air through the mixing passage, thereby causing a rich mixture to be drawn from the idle opening 52 into mixing passage posterior of the valve 58. As the valve 58 opens, the outlet 5% will become operative to assist the outlet 52 in delivering the rich mixture, and with further opening of the throttle, the fiow of air through the Venturi tubes will increase to a point where fuel will be delivered from the nozzle outlet M for high speed operation.
During such high speed or full throttle operation, the demand upon the high speed nozzle will be such as to cause a continuous stream of fuel to be projected from the power jet 2! and the idle system will be reversed so that air is drawn from idle fuel orifice 34 into main nozzle 26 through delivery opening 32. It has been found that in the high speed operation of this type of carburetor the stream of fuel from the jet 24 was projected beyond the inlet opening 32 of the idle jet, so that upon a sudden closing of the throttle from a wide open position, the momentum of the stream would momentarily preforms, comprises simply a pin 60 mounted in the 26 and extending diametriso that the stream of lower end of nozzle cally across the mouth,
fuel issuing from the nozzle 24 may impinge thereon and be broken up, this form being illustrated in Fig. 1.
Instead of being mounted on the lower end of nozzle 26, the pin may be mounted in notches in the upper end of the nozzle 24, as indicated in Fig. 3, at 69 7 The baffle element may instead of being mounted at right angles to the axis of the nozzle, be mounted at an angle as shown at 601) in Fig. 4.
Instead of taking the form of a pin extending entirely across the nozzle mouth, the bafile element may be secured at one end and extend only part way across the nozzle bore as indicated at 600 in Fig. 5.
The pin 68d shown in mounted in the notches in 24, is mounted in a position said notches.
Instead of being in the form of a pin, the baffle element may, as shown in Fig. 7, be in the form of a washer 6| having an integral web portion Bile extending across the fuel passage.
In the modification of the invention shown in Fig. 8, the baflie is formed by an extension 69] on the end of the idle tube 36F.
In the modification of the invention shown in Fig, 9, the baiile element is in the form of a separate short tube 60g which comprises the inlet to the idle passage.
In Fig. 10, the baiiie is likewise in the form of a tube forming the inlet to the idle passage, the tube 60h in this case extending entirely across Fig. 6, instead of being the end of the nozzle at right angles to the nozzle 26 and having an opening 62 through which fuel passes to the idle passage.
Tests have shown that the invention very effectively corrects the difficulty that has been experienced in connection with the sudden closing of the throttle after a period of wide open throttle operation. For a long time, the problem remained unsolved until I realized that the condition was caused by the fuel being thrown past the idle inlet opening, and I devised the above dlsclOsed solution to this problem.
While I have described my invention in connection with certain specific-embodiments thereof, it is to be understood that this is not by way of limitation and that the scope of my invention is defined solely by the appended claim which should be construed as broadly as the prior art will permit.
I claim:
In a carburetor assembly including means defining a main air passage having a venturi therein, a butterfly throttle valve for controlling the flow therethrough and an upwardly extending nozzle having one end in communication with fuel from a fuel bowl, th other end being positioned within said venturi for delivering fuel thereto, said nozzle having a straight cylindrical bore leading from the inlet to th outlet thereof, means defining an idle fuel supply passage having the discharge end thereof under the control of said butterfly valve when moved to the idle position, said idle passage having an inlet terminal portion communicating directly with said nozzle bore at a point spaced along the axis of said bore from the inlet end thereof, means defining a metering power jet located below the inlet. end of said nozzle bore for delivering fuel from said fuel bowl generally coaxially into said fuel nozzle bore, said arrangement being particularly characterized by the provision of a pinlike element projecting across the path of flow from said power jet at a point between said power jet defining means and said idle passage inlet, said pin-like element having a cross-sectional area less than the cross-sectional area of the bore of said nozzle, and being the sole obstruction to the free flow of fuel from said jet to the outlet of said nozzle, said power jet being directed against said pin-like element which functions to prevent the fuel from being projected beyond said idle inlet, thus providing a supply of fuel at said idle inlet to be drawn therein when said butterfly valve is moved to idle position to effect a change over from main nozzle feed to idle feed.
JOHN E. STORER, JR.
US353449A 1940-08-21 1940-08-21 Carburetor Expired - Lifetime US2291418A (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2568987A (en) * 1946-12-20 1951-09-25 Bendix Aviat Corp Carburetor
US2611594A (en) * 1948-10-27 1952-09-23 Thompson Prod Inc Supplementary fluid feed device with automatic tandem metering valves
US2621030A (en) * 1949-08-26 1952-12-09 Carter Carburetor Corp Carburetor nozzle system
US2656165A (en) * 1948-05-15 1953-10-20 Bendix Aviat Corp Carburetor
US2680605A (en) * 1950-10-20 1954-06-08 R F Bracke & Company Carburetor
US2698168A (en) * 1950-10-25 1954-12-28 Gen Motors Corp Carburetor
US3104272A (en) * 1959-02-09 1963-09-17 Acf Ind Inc Secondary fuel control for two-stage carburetor
WO1993001406A1 (en) * 1991-07-04 1993-01-21 Frederik Mannes Reefman Operating procedure and construction for the conditioning of a combustible mixture in a combustion engine

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2568987A (en) * 1946-12-20 1951-09-25 Bendix Aviat Corp Carburetor
US2656165A (en) * 1948-05-15 1953-10-20 Bendix Aviat Corp Carburetor
US2611594A (en) * 1948-10-27 1952-09-23 Thompson Prod Inc Supplementary fluid feed device with automatic tandem metering valves
US2621030A (en) * 1949-08-26 1952-12-09 Carter Carburetor Corp Carburetor nozzle system
US2680605A (en) * 1950-10-20 1954-06-08 R F Bracke & Company Carburetor
US2698168A (en) * 1950-10-25 1954-12-28 Gen Motors Corp Carburetor
US3104272A (en) * 1959-02-09 1963-09-17 Acf Ind Inc Secondary fuel control for two-stage carburetor
WO1993001406A1 (en) * 1991-07-04 1993-01-21 Frederik Mannes Reefman Operating procedure and construction for the conditioning of a combustible mixture in a combustion engine

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