EP0891485B1 - Carburetor with fuel nozzle - Google Patents

Carburetor with fuel nozzle Download PDF

Info

Publication number
EP0891485B1
EP0891485B1 EP97902962A EP97902962A EP0891485B1 EP 0891485 B1 EP0891485 B1 EP 0891485B1 EP 97902962 A EP97902962 A EP 97902962A EP 97902962 A EP97902962 A EP 97902962A EP 0891485 B1 EP0891485 B1 EP 0891485B1
Authority
EP
European Patent Office
Prior art keywords
carburetor
orifice
downstream
upstream
fuel
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
EP97902962A
Other languages
German (de)
French (fr)
Other versions
EP0891485A1 (en
Inventor
Jerome Rasmussen
John D. Santi
Thomas G. Guntly
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.)
Briggs and Stratton Corp
Original Assignee
Briggs and Stratton 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 Briggs and Stratton Corp filed Critical Briggs and Stratton Corp
Publication of EP0891485A1 publication Critical patent/EP0891485A1/en
Application granted granted Critical
Publication of EP0891485B1 publication Critical patent/EP0891485B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • 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
    • F02M7/00Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
    • F02M7/02Carburettors having aerated fuel spray nozzles

Definitions

  • the present invention generally relates to the field of carburetors that mix air and fuel for internal combustion engines and, more particularly, to the field of fuel nozzles that provide fuel to the throat of such carburetors.
  • French reference FR-E-26,901 discloses a fuel nozzle (1) having a pair of upstream orifices (2) and which is interconnected to a fuel conduit (5).
  • French reference FR-A-555,986 discloses a fuel nozzle (1) disposed in a carburetor and in fluid communication with a fuel line (6).
  • Another background art reference is British reference GB-A-649,920, which discloses a fuel nozzle (13) having an upstream orifice (24) and a downstream orifice (23) disposed within a carburetor. The fuel nozzle is angled with respect to the flow of air through the carburetor, and fuel within the fuel nozzle blocks the upstream orifice (24) during high suction and low engine speeds.
  • Another background art reference is British reference GB-A-148,507, which discloses a fuel nozzle or choke tube (g) having an air inlet orifice (k) and a orifice for the outflow of fuel (k1). Fuel is drawn through the choke tube (g) from a chamber (d) containing a constant level (indicated by line 1-1) of fuel.
  • Another background art reference is GB-A-224 719 which discloses a carburetor according to the preamble of claim 1.
  • Fuel is typically provided to the air by a fuel nozzle that is operatively interconnected with a fuel supply (e.g., a fuel bowl).
  • the fuel nozzle extends transversely into the carburetor throat, and includes an outlet port in a tip thereof.
  • the outlet port commonly faces transverse to the air flow such that air passing over the port will create a negative pressure, thereby resulting in fuel being drawn from fuel nozzle.
  • air can also flow in the reverse direction (i.e., from the combustion chamber toward the carburetor intake), sometimes called "reverse flow.”
  • Reverse flow is typically caused by intake valve leakage, which can result from valve lash, inconsistent cam profiles or poor valve seals. Due to the presence of an air velocity, reverse flow creates a negative pressure at the outlet port, resulting in fuel being drawn from the fuel nozzle. When forward flow resumes, fuel is again drawn from the fuel nozzle, resulting in a "double charge” of fuel. This double charge creates an air/fuel ratio that is richer than the optimum air/fuel ratio of the carburetor, resulting in excess emissions and lower fuel economy.
  • a carburetor for use in an engine comprises a carburetor body (22) having a throat (24) extending from an intake (26) to a discharge (28), wherein a downstream direction is defined as extending from said intake toward said discharge, and wherein an upstream direction is defined as extending from said discharge toward said intake; and a fuel nozzle (32) having body, said body having a longitudinal axis positioned within said throat such that said longitudinal axis is substantially normal to said upstream and downstream directions, said nozzle including at least one upstream orifice (39) facing substantially upstream and at least one downstream orifice (40, 42, or 44) facing substantially downstream, said at least one upstream orifice being positioned closer to the carburetor body than said at least one downtstream orifice, characterized in
  • Fig. 1 is a side section view of a carburetor embodying the present invention and including a fuel nozzle.
  • Fig. 2 is a longitudinal section view of the fuel nozzle illustrated in Fig. 1.
  • Fig. 3 is a section view of the fuel nozzle taken along line 3-3 in Fig. 2.
  • Fig. 4 is an end view of the fuel nozzle taken along line 4-4 in Fig. 2.
  • Fig. 5 is a side section view of a different carburetor embodying the present invention and including a fuel nozzle.
  • Fig. 6 is a longitudinal section view of the fuel nozzle illustrated in Fig. 5.
  • Fig. 7 is an end view of the fuel nozzle taken along line 7-7 in Fig. 6.
  • Figs. 8-12 illustrate various fuel nozzles embodying the present invention.
  • Fig. 1 illustrates a carburetor 20 having a carburetor body 22 with a carburetor throat 24 extending therethrough from an intake region 26 to a discharge region 28.
  • the carburetor 20 further includes a throttle 30 that regulates the amount of air and fuel passing through the throat 24.
  • a fuel nozzle 32 is positioned to provide fuel to the throat 24.
  • the fuel nozzle 32 generally includes a base 34 mounted to the carburetor body 22, and a tip 36 extending from the base 34, through a carburetor wall 37, and at least partially positioned within the carburetor throat.
  • the tip 36 is provided with an upstream orifice and at least one downstream orifice having a surface area larger than a surface area of the upstream orifice.
  • surface area is used to describe the orifice's propensity to discharge fuel. That is, the larger the surface area of the orifice, the more fuel it is likely to discharge given a particular pressure.
  • the surface area values used herein refer to the area of the orifice at the outer surface of the fuel nozzle. It should be appreciated, of course, that other techniques could be used to achieve the present invention. For example, by using narrow slot-shaped or pinhole openings, surface tension could also play a role in an orifice's propensity to dispense fuel. Further, orifices that change in area from the surface inward could also affect the orifice's performance.
  • the tip includes one upstream orifice 38 that is circular and has a diameter of about 0,5334 mm (.021 inches), corresponding with a cross-sectional surface area of about 0,226 square mm (.00035 square inches).
  • the illustrated embodiment includes three downstream orifices 40,42,44 that are each circular and have a diameter of about 0,9398 mm (.037 inches), corresponding with a total cross-sectional surface area of about 2,084 square mm (.00323 square inches). It should be appreciated that the orifices do not need to be round in cross-section, and could instead be configured in other appropriate shapes.
  • the middle downstream orifice 42 is approximately centered with respect to the throat 24, and the other two downstream orifices 40,44 are equally spaced on either side of the middle downstream orifice 42. Accordingly, the downstream orifices 40,42,44 are positioned in a pattern that is evenly distributed across the throat 24.
  • the upstream orifice 38 is positioned off-center with respect to the throat 24. More specifically, the upstream orifice 38 is positioned closer to the carburetor wall 37 than any of the downstream orifices 40,42,44, as shown in Figs. 1 and 2.
  • double charging is significantly reduced. More specifically, forward flow will create a low pressure at the downstream orifices, resulting in fuel being dispensed through the downstream orifices. During reverse flow, a high pressure is formed at the downstream orifices, resulting in little or no fuel being dispenses through the downstream orifices. Accordingly, double charging is significantly reduced.
  • the positioning of the upstream orifice allows air to enter the fuel nozzle at a right angle to the flow of fuel in the nozzle during forward flow.
  • the right angle motion of the air relative to the fuel causes shearing of the fuel in the fuel nozzle, resulting in better fuel atomization as the fuel and air exit the downstream orifices. Because of the small surface area of the upstream orifice relative to the downstream orifices, reverse flow will not result in significant dispersal of fuel through the upstream orifice.
  • the fuel nozzle 32 includes a tip 36 and a base 34.
  • the tip 36 and the base 34 can be made from a wide variety of materials, including metals and plastics.
  • the tip 36 and the base 34 are machined from metallic material, such as SAE CA 332 Brass, and the base 34 is press fit into the tip 36.
  • the utilization of a two-piece fuel nozzle facilitates production of a fuel nozzle 32 having a tip 36 with a thinner wall than the base 34. The thinner wall allows the tip to occupy less space within the throat, thereby improving engine performance.
  • the base 34 includes a flat surface 46 that corresponds with a flat segment 48 on the tip 36, as shown in Fig. 3.
  • the base 34 includes a flat portion 50 that matches the shape of the carburetor body 22, as shown in Fig. 4.
  • the carburetor 60 illustrated in Fig. 5 includes an integral fuel bowl 62 and associated float 64 for providing fuel to the carburetor throat 66 via a metering orifice 68 and a fuel nozzle 70.
  • the fuel nozzle 70 is a one-piece design made from plastic, such as acetal resin.
  • the lower portion of the fuel nozzle includes a D-shaped base portion 72, as shown in Fig. 7, to insure proper alignment of the fuel nozzle 70 with the carburetor body 74.
  • Fig. 8 illustrates another fuel nozzle 80 embodying the present invention.
  • the fuel nozzle 80 is a two-piece design, including a tip 82 and a base 84.
  • the tip 82 and the base 84 are both made of plastic material, such as Delrin, a trademark of E.I. Du Pont De Nemours of Wilmington, Delaware.
  • the tip 82 and the base 84 are interconnected by a snap fit, wherein a ridge 86 on the tip 82 fits into a groove 88 on the base 84.
  • the tip 82 has a wall thickness that is about the same as the wall thickness of the base 84.
  • Fig. 9 illustrates another fuel nozzle 90 embodying the present invention.
  • the illustrated fuel nozzle 90 is a one-piece design that is machined from a metallic material, such as brass. A tip portion 92 of the fuel nozzle 90 is blocked by a ball plug 94.
  • Fig. 10 illustrates a fuel nozzle 100 embodying the present invention. Similar to the fuel nozzle illustrated in Fig. 8, the fuel nozzle 100 of Fig. 10 is a two-piece Delrin design wherein a tip 102 is snap fit with a base 104. The end of the tip 102 includes a ball plug 106 integrally formed therewith via a flexible interconnecting member 108. The open end of the tip 102 can be selectively closed by inserting the ball plug 106 into the open end.
  • Fig. 11 illustrates another fuel nozzle 110 embodying the present invention.
  • the fuel nozzle 110 is identical to that illustrated in Fig. 8, except the tip 112 has a wall thickness that is significantly thinner than the wall thickness of the base 114.
  • Fig. 12 illustrates a two-piece brass fuel nozzle 120 having a tip 122 and a base 124 press fit into the tip 122.
  • the tip 122 illustrated in Fig. 12 extends only partially (e.g., less than halfway) into the carburetor throat 126.
  • the tip 122 illustrated in Fig. 12 includes only one downstream orifice 128, rather than the three downstream orifices illustrated in the other fuel nozzles.
  • the downstream orifice 128 has a cross-sectional surface area that is significantly larger than the surface area of the upstream orifice 130.

Landscapes

  • 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)
  • Nozzles (AREA)

Description

FIELD OF THE INVENTION
The present invention generally relates to the field of carburetors that mix air and fuel for internal combustion engines and, more particularly, to the field of fuel nozzles that provide fuel to the throat of such carburetors.
BACKGROUND OF THE INVENTION
Background art includes French reference FR-E-26,901, which discloses a fuel nozzle (1) having a pair of upstream orifices (2) and which is interconnected to a fuel conduit (5). French reference FR-A-555,986 discloses a fuel nozzle (1) disposed in a carburetor and in fluid communication with a fuel line (6). Another background art reference is British reference GB-A-649,920, which discloses a fuel nozzle (13) having an upstream orifice (24) and a downstream orifice (23) disposed within a carburetor. The fuel nozzle is angled with respect to the flow of air through the carburetor, and fuel within the fuel nozzle blocks the upstream orifice (24) during high suction and low engine speeds. Another background art reference is British reference GB-A-148,507, which discloses a fuel nozzle or choke tube (g) having an air inlet orifice (k) and a orifice for the outflow of fuel (k1). Fuel is drawn through the choke tube (g) from a chamber (d) containing a constant level (indicated by line 1-1) of fuel. Another background art reference is GB-A-224 719 which discloses a carburetor according to the preamble of claim 1.
In conventional carburetors, air enters through an intake of a carburetor throat and travels through a venturi where the air is mixed with fuel and subsequently provided to a combustion chamber of the engine. Fuel is typically provided to the air by a fuel nozzle that is operatively interconnected with a fuel supply (e.g., a fuel bowl). The fuel nozzle extends transversely into the carburetor throat, and includes an outlet port in a tip thereof. The outlet port commonly faces transverse to the air flow such that air passing over the port will create a negative pressure, thereby resulting in fuel being drawn from fuel nozzle.
In some engines, air can also flow in the reverse direction (i.e., from the combustion chamber toward the carburetor intake), sometimes called "reverse flow." Reverse flow is typically caused by intake valve leakage, which can result from valve lash, inconsistent cam profiles or poor valve seals. Due to the presence of an air velocity, reverse flow creates a negative pressure at the outlet port, resulting in fuel being drawn from the fuel nozzle. When forward flow resumes, fuel is again drawn from the fuel nozzle, resulting in a "double charge" of fuel. This double charge creates an air/fuel ratio that is richer than the optimum air/fuel ratio of the carburetor, resulting in excess emissions and lower fuel economy.
SUMMARY OF THE INVENTION
The present invention provides a carburetor with a fuel nozzle that alleviates the problem of double charging by positioning orifices in the fuel nozzle such that more fuel is dispensed during downstream gas flow than during upstream gas flow. According to the invention, a carburetor for use in an engine comprises a carburetor body (22) having a throat (24) extending from an intake (26) to a discharge (28), wherein a downstream direction is defined as extending from said intake toward said discharge, and wherein an upstream direction is defined as extending from said discharge toward said intake; and a fuel nozzle (32) having body, said body having a longitudinal axis positioned within said throat such that said longitudinal axis is substantially normal to said upstream and downstream directions, said nozzle including at least one upstream orifice (39) facing substantially upstream and at least one downstream orifice (40, 42, or 44) facing substantially downstream, said at least one upstream orifice being positioned closer to the carburetor body than said at least one downtstream orifice,
characterized in that a surface area of said at least one upstream orifice is less than about 50 percent of a surface area of said at least one downstream orifice, whereby said upstream orifice is sized and positioned to allow air to enter said fuel nozzle at a right angle to a flow of fuel in said nozzle during downstream flow of air in said carburetor throat to cause improved fuel atomization in said fuel nozzle before said fuel and air exit said downstream orifice during normal operation of the engine.
Further embodiments of the invention are disclosed in the dependent claims.
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is a side section view of a carburetor embodying the present invention and including a fuel nozzle.
Fig. 2 is a longitudinal section view of the fuel nozzle illustrated in Fig. 1.
Fig. 3 is a section view of the fuel nozzle taken along line 3-3 in Fig. 2.
Fig. 4 is an end view of the fuel nozzle taken along line 4-4 in Fig. 2.
Fig. 5 is a side section view of a different carburetor embodying the present invention and including a fuel nozzle.
Fig. 6 is a longitudinal section view of the fuel nozzle illustrated in Fig. 5.
Fig. 7 is an end view of the fuel nozzle taken along line 7-7 in Fig. 6.
Figs. 8-12 illustrate various fuel nozzles embodying the present invention.
DETAILED DESCRIPTION
Fig. 1 illustrates a carburetor 20 having a carburetor body 22 with a carburetor throat 24 extending therethrough from an intake region 26 to a discharge region 28. The carburetor 20 further includes a throttle 30 that regulates the amount of air and fuel passing through the throat 24. A fuel nozzle 32 is positioned to provide fuel to the throat 24. The fuel nozzle 32 generally includes a base 34 mounted to the carburetor body 22, and a tip 36 extending from the base 34, through a carburetor wall 37, and at least partially positioned within the carburetor throat.
In accordance with the present invention, the tip 36 is provided with an upstream orifice and at least one downstream orifice having a surface area larger than a surface area of the upstream orifice. As used herein, the term "surface area" is used to describe the orifice's propensity to discharge fuel. That is, the larger the surface area of the orifice, the more fuel it is likely to discharge given a particular pressure. The surface area values used herein refer to the area of the orifice at the outer surface of the fuel nozzle. It should be appreciated, of course, that other techniques could be used to achieve the present invention. For example, by using narrow slot-shaped or pinhole openings, surface tension could also play a role in an orifice's propensity to dispense fuel. Further, orifices that change in area from the surface inward could also affect the orifice's performance.
In the embodiment illustrated in Figs. 1 and 2, the tip includes one upstream orifice 38 that is circular and has a diameter of about 0,5334 mm (.021 inches), corresponding with a cross-sectional surface area of about 0,226 square mm (.00035 square inches). The illustrated embodiment includes three downstream orifices 40,42,44 that are each circular and have a diameter of about 0,9398 mm (.037 inches), corresponding with a total cross-sectional surface area of about 2,084 square mm (.00323 square inches). It should be appreciated that the orifices do not need to be round in cross-section, and could instead be configured in other appropriate shapes.
As best shown in Fig. 2, the middle downstream orifice 42 is approximately centered with respect to the throat 24, and the other two downstream orifices 40,44 are equally spaced on either side of the middle downstream orifice 42. Accordingly, the downstream orifices 40,42,44 are positioned in a pattern that is evenly distributed across the throat 24. In contrast, the upstream orifice 38 is positioned off-center with respect to the throat 24. More specifically, the upstream orifice 38 is positioned closer to the carburetor wall 37 than any of the downstream orifices 40,42,44, as shown in Figs. 1 and 2.
By virtue of the positioning of the downstream side of the nozzle tip, double charging is significantly reduced. More specifically, forward flow will create a low pressure at the downstream orifices, resulting in fuel being dispensed through the downstream orifices. During reverse flow, a high pressure is formed at the downstream orifices, resulting in little or no fuel being dispenses through the downstream orifices. Accordingly, double charging is significantly reduced.
The positioning of the upstream orifice allows air to enter the fuel nozzle at a right angle to the flow of fuel in the nozzle during forward flow. The right angle motion of the air relative to the fuel causes shearing of the fuel in the fuel nozzle, resulting in better fuel atomization as the fuel and air exit the downstream orifices. Because of the small surface area of the upstream orifice relative to the downstream orifices, reverse flow will not result in significant dispersal of fuel through the upstream orifice.
As noted above, the fuel nozzle 32 includes a tip 36 and a base 34. The tip 36 and the base 34 can be made from a wide variety of materials, including metals and plastics. In the embodiment illustrated in Figs. 1-4, the tip 36 and the base 34 are machined from metallic material, such as SAE CA 332 Brass, and the base 34 is press fit into the tip 36. The utilization of a two-piece fuel nozzle facilitates production of a fuel nozzle 32 having a tip 36 with a thinner wall than the base 34. The thinner wall allows the tip to occupy less space within the throat, thereby improving engine performance. To insure proper alignment of the base 34 with the tip 36, the base 34 includes a flat surface 46 that corresponds with a flat segment 48 on the tip 36, as shown in Fig. 3. Further, to insure that the assembled fuel nozzle 32 is properly inserted into the carburetor body 22, the base 34 includes a flat portion 50 that matches the shape of the carburetor body 22, as shown in Fig. 4.
The carburetor 60 illustrated in Fig. 5 includes an integral fuel bowl 62 and associated float 64 for providing fuel to the carburetor throat 66 via a metering orifice 68 and a fuel nozzle 70. Referring to Fig. 6, the fuel nozzle 70 is a one-piece design made from plastic, such as acetal resin. The lower portion of the fuel nozzle includes a D-shaped base portion 72, as shown in Fig. 7, to insure proper alignment of the fuel nozzle 70 with the carburetor body 74.
Fig. 8 illustrates another fuel nozzle 80 embodying the present invention. The fuel nozzle 80 is a two-piece design, including a tip 82 and a base 84. The tip 82 and the base 84 are both made of plastic material, such as Delrin, a trademark of E.I. Du Pont De Nemours of Wilmington, Delaware. The tip 82 and the base 84 are interconnected by a snap fit, wherein a ridge 86 on the tip 82 fits into a groove 88 on the base 84. In the illustrated embodiment, the tip 82 has a wall thickness that is about the same as the wall thickness of the base 84.
Fig. 9 illustrates another fuel nozzle 90 embodying the present invention. The illustrated fuel nozzle 90 is a one-piece design that is machined from a metallic material, such as brass. A tip portion 92 of the fuel nozzle 90 is blocked by a ball plug 94.
Fig. 10 illustrates a fuel nozzle 100 embodying the present invention. Similar to the fuel nozzle illustrated in Fig. 8, the fuel nozzle 100 of Fig. 10 is a two-piece Delrin design wherein a tip 102 is snap fit with a base 104. The end of the tip 102 includes a ball plug 106 integrally formed therewith via a flexible interconnecting member 108. The open end of the tip 102 can be selectively closed by inserting the ball plug 106 into the open end.
Fig. 11 illustrates another fuel nozzle 110 embodying the present invention. The fuel nozzle 110 is identical to that illustrated in Fig. 8, except the tip 112 has a wall thickness that is significantly thinner than the wall thickness of the base 114.
Fig. 12 illustrates a two-piece brass fuel nozzle 120 having a tip 122 and a base 124 press fit into the tip 122. In contrast to the previously-described fuel nozzles, the tip 122 illustrated in Fig. 12 extends only partially (e.g., less than halfway) into the carburetor throat 126. Further, the tip 122 illustrated in Fig. 12 includes only one downstream orifice 128, rather than the three downstream orifices illustrated in the other fuel nozzles. As shown, the downstream orifice 128 has a cross-sectional surface area that is significantly larger than the surface area of the upstream orifice 130.
The foregoing description of the present invention has been presented for purposes of illustration and description. Furthermore, the description is not intended to limit the invention to the form disclosed herein. Consequently, variations and modifications commensurate with the above teachings, and the skill or knowledge of the relevant art, are within the scope of the present invention, as defined in the appended claims. The embodiments described herein are further intended to explain best modes known for practicing the invention and to enable others skilled in the art to utilize the invention in such, or other, embodiments and with various modifications required by the particular applications or uses of the present invention. It is intended that the appended claims be construed to include alternative embodiments to the extent permitted by the prior art.

Claims (11)

  1. A carburetor (20) for use in an engine, said carburetor comprising:
    a carburetor body (22) having a throat (24) extending from an intake (26) to a discharge (28), wherein a downstream direction is defined as extending from said intake toward said discharge, and wherein an upstream direction is defined as extending from said discharge toward said intake; and
    a fuel nozzle (32, 70, 80, 100, 120) having a body, said body having a longitudinal axis positioned within said throat such that said longitudinal axis is substantially normal to said upstream and downstream directions, said nozzle including at least one upstream orifice (38, 130) facing substantially upstream and at least one downstream orifice (40, 42, 44 or 128) facing substantially downstream, said at least one upstream orifice being positioned closer to the carburetor body than said at least one downstream orifice, characterized in that
    a surface area of said at least one upstream orifice is less than about 50 percent of a surface area of said at least one downstream orifice, whereby said upstream orifice is sized and positioned to allow air to enter said fuel nozzle at a right angle to a flow of fuel in said nozzle during downstream flow of air in said carburetor throat to cause improved fuel atomization in said fuel nozzle before said fuel and air exit said downstream orifice during normal operation of the engine.
  2. A carburetor as claimed in claim 1, wherein said surface area of said at least one upstream orifice is less than about 25 percent of said surface area of said at least one downstream orifice.
  3. A carburetor as claimed in claim 1, wherein said surface area of said at least one upstream orifice is between about 5 percent and about 20 percent of said surface area of said at least one downstream orifice.
  4. A carburetor as claimed in claim 1, wherein said at least one upstream orifice is positioned adjacent the carburetor body that forms the throat.
  5. A carburetor as claimed in claim 1, wherein said at least one downstream orifice includes a second downstream orifice (40, 42, or 44).
  6. A carburetor as claimed in claim 5, wherein said first and second downstream orifices have an average position that is centered with respect to said throat.
  7. A carburetor as claimed in claim 5, wherein said at least one downstream orifice includes a third downstream orifice (40, 42, or 44).
  8. A carburetor as claimed in claim 7, wherein said first downstream orifice is centered with respect to said throat, and wherein said second and third downstream orifices are evenly spaced on opposing sides of said first downstream orifice.
  9. The carburetor as claimed in claim 7, wherein said at least one upstream orifice further comprises a second upstream orifice, and wherein a combined surface area of said first and second upstream orifices is less than about 50 percent of a combined surface area of said first, second and third downstream orifices.
  10. The carburetor as claimed in claim 1, wherein said fuel nozzle further comprises a base portion (34) that is keyed to fit into said carburetor body in a discrete orientation.
  11. The carburetor as claimed in claim 1, wherein said fuel nozzle further comprises:
       a body including first (34, 84, 104, 114, or 124) and second (36, 82, 102, 112 or 122) distinct pieces, said body having an open first end and a second end closed by said first piece.
EP97902962A 1996-04-02 1997-01-22 Carburetor with fuel nozzle Expired - Lifetime EP0891485B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US627737 1984-07-03
US62773796A 1996-04-02 1996-04-02
PCT/US1997/000684 WO1997037120A1 (en) 1996-04-02 1997-01-22 Carburetor with fuel nozzle

Publications (2)

Publication Number Publication Date
EP0891485A1 EP0891485A1 (en) 1999-01-20
EP0891485B1 true EP0891485B1 (en) 2000-08-16

Family

ID=24515922

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97902962A Expired - Lifetime EP0891485B1 (en) 1996-04-02 1997-01-22 Carburetor with fuel nozzle

Country Status (5)

Country Link
EP (1) EP0891485B1 (en)
JP (1) JPH11506519A (en)
CA (1) CA2247866C (en)
DE (1) DE69702840T2 (en)
WO (1) WO1997037120A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022250549A1 (en) * 2021-05-25 2022-12-01 Rommel Bernardo A unidirectional fuel nozzle for improving fuel atomization in a carburetor or similar apparatus

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8333366B2 (en) * 2010-03-08 2012-12-18 Briggs & Stratton Corporation Carburetor including one-piece fuel-metering insert

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB148507A (en) * 1916-10-27 1921-10-10 Jean Ferdinand Michel Bocchi Improvements in carburetters
FR555986A (en) * 1922-09-13 1923-07-10 vacuum ejector sprayer for power supply units of explosion engines
FR26901E (en) * 1922-09-28 1924-03-20 vacuum ejector sprayer for power supply units of internal combustion engines
GB224719A (en) * 1923-11-14 1924-11-20 Henry Frederick Rae Improvements in spray carburetters
US1707350A (en) * 1924-01-21 1929-04-02 Clarence V Elliott Carburetor
FR626943A (en) * 1926-12-31 1927-09-22 Carburetor improvements
BE480774A (en) * 1938-12-30
FR1081900A (en) * 1953-05-11 1954-12-23 Solex Improvements made to fuel systems for internal combustion engines
US2986381A (en) * 1959-09-08 1961-05-30 Acf Ind Inc Carburetor for internal combustion engines
FR2299521A1 (en) * 1975-02-03 1976-08-27 Peugeot & Renault WEALTH CORRECTION DEVICE FOR CARBURETORS
DE8812554U1 (en) * 1988-10-05 1988-11-17 Proizvodstvennoe Ob"edinenie Leningradskij Armaturno-Karbjuratornyj Zavod Imeni V.V. Kujbyševa, Leningrad Carburettor for a crankcase-scavenged two-stroke engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022250549A1 (en) * 2021-05-25 2022-12-01 Rommel Bernardo A unidirectional fuel nozzle for improving fuel atomization in a carburetor or similar apparatus

Also Published As

Publication number Publication date
DE69702840T2 (en) 2001-01-25
DE69702840D1 (en) 2000-09-21
CA2247866A1 (en) 1997-10-09
EP0891485A1 (en) 1999-01-20
CA2247866C (en) 2005-03-29
JPH11506519A (en) 1999-06-08
WO1997037120A1 (en) 1997-10-09

Similar Documents

Publication Publication Date Title
EP1096138B1 (en) Engine fuel supply system
JP2002070651A (en) Diaphragm type carburetor
JPH0381559A (en) Injection valve for fuel injector of internal combustion engine
US7090203B2 (en) Carburetor for internal combustion engine
EP0891485B1 (en) Carburetor with fuel nozzle
JPS6135720Y2 (en)
CA2271503C (en) A fuel injector for an internal combustion engine
US6123322A (en) Single screw carburetor
JP2006189043A (en) Carburetor and method of manufacturing it
US4377538A (en) Variable venturi type carburetor
US6478288B1 (en) High performance carburetor
US3669423A (en) Carburetor
US6164631A (en) Carburetor with elliptical venturi
US4153650A (en) Idling fuel supplying system of a carburetor
US4465643A (en) Variable venturi carburetor
US3937186A (en) Rotary combustion engine with improved fuel control
US6086054A (en) Diaphragm type carburetor
US4765933A (en) Carburetor
US4519957A (en) Variable-venturi carburetor
JP2605532B2 (en) Variable venturi carburetor
JPH0141886Y2 (en)
JPS626277Y2 (en)
JPH0238060Y2 (en)
JPH0238061Y2 (en)
JPS6034763Y2 (en) vaporizer main nozzle

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19980223

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE IT

17Q First examination report despatched

Effective date: 19990226

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE IT

REF Corresponds to:

Ref document number: 69702840

Country of ref document: DE

Date of ref document: 20000921

ITF It: translation for a ep patent filed
EN Fr: translation not filed
PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20120114

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20130116

Year of fee payment: 17

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 69702840

Country of ref document: DE

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 69702840

Country of ref document: DE

Effective date: 20140801

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140801

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140122