US2255296A - Carburetor nozzle - Google Patents

Carburetor nozzle Download PDF

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Publication number
US2255296A
US2255296A US248443A US24844338A US2255296A US 2255296 A US2255296 A US 2255296A US 248443 A US248443 A US 248443A US 24844338 A US24844338 A US 24844338A US 2255296 A US2255296 A US 2255296A
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United States
Prior art keywords
nozzle
fuel
orifice
carburetor
air
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
US248443A
Inventor
James T W Moseley
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Carter Carburetor Corp
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Carter Carburetor 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
Priority to BE480774D priority Critical patent/BE480774A/xx
Priority to FR961987D priority patent/FR961987A/fr
Application filed by Carter Carburetor Corp filed Critical Carter Carburetor Corp
Priority to US248443A priority patent/US2255296A/en
Application granted granted Critical
Publication of US2255296A publication Critical patent/US2255296A/en
Priority to GB5518/48A priority patent/GB649920A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • F02M7/00Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
    • F02M7/10Other installations, without moving parts, for influencing fuel/air ratio, e.g. electrical means
    • 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
    • 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
    • Y10S261/39Liquid feeding nozzles

Definitions

  • This invention relates to carburetorsfor in-H ternal combustion engines and consists, particularly, in novel fuel nozzle construction therefor.
  • main nozzle that is,.one in which the axis of the discharge orifice thereof is disposed at an angle of 90 or less to the direction of air flow therepast, more fuel is supplied in the lower suction ranges, but there may be a tendency toward excessive richness at the higher suctions when the associated engine is operating at a faster rate and a relatively lean mixture will sufllce.
  • inemcient type of main nozzle which discharges at an angle against the air stream, maintains the mixture proportions desirably.
  • the fuel mixture supperiods may be someplied during lower suction what enriched by the use of multiple venturis or by increasing the size of fuel passages through which the main nozzle is fed.
  • the quality -of-fuel and air mixture supplied byfthe carburetor may be improved, particularly during periods when relatively low suction is applied to the main nozzle, by constructing this nozzle with a main discharge outlet discharging either across or in the general direction of air flow, as in anf'eflcient" type nozzle, as described above, and a substantially I directly above the main. outlet and facing against the] air flow. 'During smaller orifice located periods of low suction, the air sweeps through the tip of the nozzle in a line from the small upper holeto outlet producing a kind the tip of the nozzle itself and, in general, facili tating the duel flow at such times.
  • Fig. 1 is a vertical sectional view showing an internal combustion engine carburetor embodying the invention.
  • Fig. 2 shows a portion of the structure in Fig. 1 substantially enlarged and Fig. 3 isa-n end view of the main nozzle.
  • the carburetor illustrated includes a downdraft mixture conduit having air inlet horn l with pivoted choke valve 2, venturis 3, mixing chamber 4, and flanged outlet portion 5 in which is mounted a pivoted throttle valve 6. Adjacent the mixture conduit is a bowl 1 within which fuel is maintained at a substantially constant level X-X by 'fioat 8 and needle valve mechanism 9 .within apertured boss in having a connection I! with aremote fuel tank.
  • Fuel is supplied to the mixture conduit throiigh a calibrated Jet i2 and-main nozzle it which discharges within the throat portion of the smallest venturl l.
  • Idling fuel is supplied through passages and i5 communicating with the main nozzle-and terminating in idling port It adjacent the edge of the throttle valve, operating with jet I2 is a stepped metering rod I! connected to the throttle valve by pivoted crank 20, link 2
  • hole 24 and orifice 23 may .be varied.
  • the mixture quality may be substantially varied merely by variation of the size and the position of upper hole 24.
  • Orifice 23 may face directly in line with the direction of fiow or it may face across the same.
  • the size and positioning of this orifice also are adjustable factors which may be utilized in calibrating the carburetor.
  • an induction conduit provided with a venturi, a constant level chamber, and a fuel nozzl extending upwardly at an angle from said chamber into said conduit and having a tip portion in said venturi, said portion having a fuel discharge orifice and an air inlet orifice, said air inlet orifice facing against the direction of air fiow in said venturi and said discharge orifice facing substantially transversely of said venturi, said orifices being horizontally offset and slightly above the normal fuel surface in said nozzle whereby air entering said inlet orifice may flow acrosssaid surface.
  • an induction conduit having a venturi, a constant level chamber, and a fuel nozzle extending upwardly at an angle into said venturi and having a tip portion with an air inlet orifice facing directly against the direction of air flow in said conduit and a discharge orifice facing transversely of said venturi, said orifices being located slightly above the normal fuel level in said nozzle and said air inlet orifice being above said discharge orifice and anterior thereto with respect to the fuel flow in said nozzle whereby air passes through said orifices in a gently curving stream.
  • an induction conduit having a venturi, and a fuel nozzle extending upwardly at anangle into said conduit and having a tip portion with a discharge orifice facing transversely of said venturi, said tip portion also having an air inlet orifice slightly anterior to and spaced horizontally of said discharge orifice and facing toward the inlet end of said conduit, said orifice being disposed relative to the normal fuel surface in said inlet during operation whereby air fiows therethrough in a smoothly curved streamline above and across said fuel surface.
  • an induction conduit having a venturi, a. constant level fuel chamber, and a fuel nozzle extending upwardly at an angle into said venturi and having a tip portion with an air inlet orifice facing directly against the direction of air flow in said conduit and a discharge orifice facing across said venturi, said outlet orifice being located slightly above the normal fuel level in said nozzle and said air inlet orifice being adjacent said discharge orifice and spaced transversely thereof whereby air may pass through said orifices and in contact with the fuel in said nozzle during operation.

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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

P .1. T. w. MOSELEY 2,255,296
CARBURETOR NOZZLE Filed Dec. 30, 1938 I g /1 9 1 (7 I l I 5 [5 l 1 v I r I X 6 IL X l I 7 12 h U 1 i 1 Ii fl l f -7 L|' no.1. i
INVENTOR ATTORNEY JAMES T. W. Moszuzv the transfer point is, generally,
Patented Sept. 9, 1941 James T. W. Moseley,
signer to Carter Carburetor Corporation, St.
Webster Groves, Mo., as-' Louis, Mo.,' a corporation Application December 30, 1938, Serial No. 248,443 Claims. (01. 261-16) This invention relates to carburetorsfor in-H ternal combustion engines and consists, particularly, in novel fuel nozzle construction therefor.
Considerable difliculty'has been experienced by carburetor engineers in designing internal com bustion engine carburetors in which the main fuel nozzle functions satisfactorily when exposed to relatively low suctions, as'at the transfer point when this nozzle starts to supply fuel during opening movement of the throttle and also when the throttle valve is substantially opened and uAccordingly, it is an object of this invention" to provide a main fuel nozzle construction which functions more efiicientl'y at periods of low suc-v tion than other nozzles now in use and which,
at the same time, provides a properly proportioned mixture at other times.
This object and other more .detailed objects hereafter appearing are attained substantially the associated engine is operating slowly due to being subjected to a heavy load. Where the idling or low speed system is interconnected to the main nozzle, as is usually the case in modern automotive carburetors, the mixture supplied at leaner than may be desirable, due to the holding back effect of the idling system. If a so-called eficient type of main nozzle is used, that is,.one in which the axis of the discharge orifice thereof is disposed at an angle of 90 or less to the direction of air flow therepast, more fuel is supplied in the lower suction ranges, but there may be a tendency toward excessive richness at the higher suctions when the associated engine is operating at a faster rate and a relatively lean mixture will sufllce. Onthe other hand, a so-called inemcient type of main nozzle which discharges at an angle against the air stream, maintains the mixture proportions desirably. uniform durin p riods of higher suction, but the discharge therefrom tends to decrease too rapidly in the lower suction ranges; In a'carburetor using such an inefficient typeof nozzle, the fuel mixture supperiods, may be someplied during lower suction what enriched by the use of multiple venturis or by increasing the size of fuel passages through which the main nozzle is fed.
I have found thatthe quality -of-fuel and air mixture supplied byfthe carburetor may be improved, particularly during periods when relatively low suction is applied to the main nozzle, by constructing this nozzle with a main discharge outlet discharging either across or in the general direction of air flow, as in anf'eflcient" type nozzle, as described above, and a substantially I directly above the main. outlet and facing against the] air flow. 'During smaller orifice located periods of low suction, the air sweeps through the tip of the nozzle in a line from the small upper holeto outlet producing a kind the tip of the nozzle itself and, in general, facili tating the duel flow at such times.
by the structures illustrated in the accompanying drawing in which: 4 Fig. 1 is a vertical sectional view showing an internal combustion engine carburetor embodying the invention.
Fig. 2 shows a portion of the structure in Fig. 1 substantially enlarged and Fig. 3 isa-n end view of the main nozzle.
The carburetor illustrated includes a downdraft mixture conduit having air inlet horn l with pivoted choke valve 2, venturis 3, mixing chamber 4, and flanged outlet portion 5 in which is mounted a pivoted throttle valve 6. Adjacent the mixture conduit is a bowl 1 within which fuel is maintained at a substantially constant level X-X by 'fioat 8 and needle valve mechanism 9 .within apertured boss in having a connection I! with aremote fuel tank.
Fuel is supplied to the mixture conduit throiigh a calibrated Jet i2 and-main nozzle it which discharges within the throat portion of the smallest venturl l. Idling fuel is supplied through passages and i5 communicating with the main nozzle-and terminating in idling port It adjacent the edge of the throttle valve, operating with jet I2 is a stepped metering rod I! connected to the throttle valve by pivoted crank 20, link 2|, and lever 22. shown more clearly in Figs.
when closed. (20-- 2 and 3, is of general tubu'lar form and the tip portion thereof has a fuel outlet orifice 23 facing slightly downwardly at an angle, that is, in the general direction of air flow through the mixture conduit, and a substantially smaller hole 24 immediately anteriorv to orifice and facing upwardly, that is, directly against the direction of air flow and so as to direct a to'orifice 24, both being positioned so that air may smooth curve or streamthe larger main of Venturi action within 'flowf therethrough in a gentle curve particularly .during low speed operation.
I have found thatthis nozzle results in materialenrichment of the mixture supplied by the carburetor during periods of low suction, while the mixture supplied during periods of higher j suction and air flow is substantially uniformly proportioned in a desirable manner. Also better portion of the air against the fuel stream in the'nozzle. Lower hole 23 is posterior at an angle as shown or at 90.
gradation of mixture proportions is obtained during transfer of the fueldischarge between the idling and main fuel systems which permits the use of a less efficient idling system. These advantageous results are'apparently due to the fact that at low suctions, air sweeping through the sage, and where a lesser number of venturis are used. Also, the disposition of the main nozzle,
itself, and the size and disposition of hole 24 and orifice 23 may .be varied. The mixture quality may be substantially varied merely by variation of the size and the position of upper hole 24. Orifice 23 may face directly in line with the direction of fiow or it may face across the same The size and positioning of this orifice also are adjustable factors which may be utilized in calibrating the carburetor.
The invention is not limited to the structure shown but may be modified in various respects as will occur to those skilled in the art, and the exclusive use of all such modifications'as come within the scope of the appended claims is contemplated.
I claim:
1. In a downdraft carburetor, an induction conduit provided with a venturi, a constant level chamber, and a fuel nozzl extending upwardly at an angle from said chamber into said conduit and having a tip portion in said venturi, said portion having a fuel discharge orifice and an air inlet orifice, said air inlet orifice facing against the direction of air fiow in said venturi and said discharge orifice facing substantially transversely of said venturi, said orifices being horizontally offset and slightly above the normal fuel surface in said nozzle whereby air entering said inlet orifice may flow acrosssaid surface.
2. In a downdraft carburetor, an induction conduit having a venturi, a constant level chamber, and a fuel nozzle extending upwardly at an angle into said venturi and having a tip portion with an air inlet orifice facing directly against the direction of air flow in said conduit and a discharge orifice facing transversely of said venturi, said orifices being located slightly above the normal fuel level in said nozzle and said air inlet orifice being above said discharge orifice and anterior thereto with respect to the fuel flow in said nozzle whereby air passes through said orifices in a gently curving stream.
, 3. In a carburetor as specified in claim 2 in which said air inlet orifice is small compared to the nozzle bore and said discharge orifice.
4. In a downdraft carburetor, an induction conduit having a venturi, and a fuel nozzle extending upwardly at anangle into said conduit and having a tip portion with a discharge orifice facing transversely of said venturi, said tip portion also having an air inlet orifice slightly anterior to and spaced horizontally of said discharge orifice and facing toward the inlet end of said conduit, said orifice being disposed relative to the normal fuel surface in said inlet during operation whereby air fiows therethrough in a smoothly curved streamline above and across said fuel surface.
5. In' a downdraft carburetor, an induction conduit having a venturi, a. constant level fuel chamber, and a fuel nozzle extending upwardly at an angle into said venturi and having a tip portion with an air inlet orifice facing directly against the direction of air flow in said conduit and a discharge orifice facing across said venturi, said outlet orifice being located slightly above the normal fuel level in said nozzle and said air inlet orifice being adjacent said discharge orifice and spaced transversely thereof whereby air may pass through said orifices and in contact with the fuel in said nozzle during operation.
JAMES T. W. MOSELEY. 1
US248443A 1938-12-30 1938-12-30 Carburetor nozzle Expired - Lifetime US2255296A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
BE480774D BE480774A (en) 1938-12-30
FR961987D FR961987A (en) 1938-12-30
US248443A US2255296A (en) 1938-12-30 1938-12-30 Carburetor nozzle
GB5518/48A GB649920A (en) 1938-12-30 1948-02-24 Improvements in and relating to spray carburettors for internal combustion engines

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US248443A US2255296A (en) 1938-12-30 1938-12-30 Carburetor nozzle

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US2255296A true US2255296A (en) 1941-09-09

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GB (1) GB649920A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2512085A (en) * 1947-01-27 1950-06-20 Carter Carburetor Corp Carburetor nozzle
US2628826A (en) * 1948-07-08 1953-02-17 Carter Carburetor Corp Antisurge carburetor
US2635625A (en) * 1948-08-04 1953-04-21 Carter Carburetor Corp Fuel supply device
US2768819A (en) * 1951-02-19 1956-10-30 Jr Albert G Bodine Engine fuel system
US2772866A (en) * 1953-03-17 1956-12-04 Ridley John Cecil Means for supplying anti-detonant to an internal-combustion engine
US2836160A (en) * 1955-02-28 1958-05-27 Akers Cecil Lynn Carbureting means
US3012676A (en) * 1958-12-03 1961-12-12 Julius L Englesberg Liquid purifier
US3738336A (en) * 1971-04-19 1973-06-12 N Holland Method and arrangement for controlling fuel delivery in a charge forming apparatus
US5904130A (en) * 1997-05-06 1999-05-18 Pacer Industries, Inc. Gaseous fuel injection system
US10830183B2 (en) 2018-12-05 2020-11-10 William R. Krup Individual cylinder tuning booster for a carburetor
US11131274B1 (en) 2018-12-05 2021-09-28 William R. Krup Individual cylinder tuning booster for a carburetor

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997037120A1 (en) * 1996-04-02 1997-10-09 Briggs & Stratton Corporation Carburetor with fuel nozzle

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2512085A (en) * 1947-01-27 1950-06-20 Carter Carburetor Corp Carburetor nozzle
US2628826A (en) * 1948-07-08 1953-02-17 Carter Carburetor Corp Antisurge carburetor
US2635625A (en) * 1948-08-04 1953-04-21 Carter Carburetor Corp Fuel supply device
US2768819A (en) * 1951-02-19 1956-10-30 Jr Albert G Bodine Engine fuel system
US2772866A (en) * 1953-03-17 1956-12-04 Ridley John Cecil Means for supplying anti-detonant to an internal-combustion engine
US2836160A (en) * 1955-02-28 1958-05-27 Akers Cecil Lynn Carbureting means
US3012676A (en) * 1958-12-03 1961-12-12 Julius L Englesberg Liquid purifier
US3738336A (en) * 1971-04-19 1973-06-12 N Holland Method and arrangement for controlling fuel delivery in a charge forming apparatus
US5904130A (en) * 1997-05-06 1999-05-18 Pacer Industries, Inc. Gaseous fuel injection system
US10830183B2 (en) 2018-12-05 2020-11-10 William R. Krup Individual cylinder tuning booster for a carburetor
US11131274B1 (en) 2018-12-05 2021-09-28 William R. Krup Individual cylinder tuning booster for a carburetor

Also Published As

Publication number Publication date
GB649920A (en) 1951-02-07
FR961987A (en) 1950-05-26
BE480774A (en)

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