US2826400A - Carburetor construction - Google Patents
Carburetor construction Download PDFInfo
- Publication number
- US2826400A US2826400A US514908A US51490855A US2826400A US 2826400 A US2826400 A US 2826400A US 514908 A US514908 A US 514908A US 51490855 A US51490855 A US 51490855A US 2826400 A US2826400 A US 2826400A
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- Prior art keywords
- fuel
- air
- nozzle
- discharge
- carburetor
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- 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
Links
- 238000010276 construction Methods 0.000 title description 10
- 239000000446 fuel Substances 0.000 description 61
- 239000000839 emulsion Substances 0.000 description 19
- 239000007788 liquid Substances 0.000 description 8
- 238000000889 atomisation Methods 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 230000035945 sensitivity Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 230000006872 improvement Effects 0.000 description 2
- 239000003595 mist Substances 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 235000017276 Salvia Nutrition 0.000 description 1
- 241001072909 Salvia Species 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M7/00—Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
- F02M7/02—Carburettors having aerated fuel spray nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M19/00—Details, component parts, or accessories of carburettors, not provided for in, or of interest apart from, the apparatus of groups F02M1/00 - F02M17/00
- F02M19/02—Metering-orifices, e.g. variable in diameter
- F02M19/021—Metering-orifices, e.g. variable in diameter the cross-sectional area being changed mechanically
Definitions
- the present invention relates to a carburetor construction, and more particularly to an improvement in the main well and discharge tube.
- the main fuel nozzle is designed in association with the main fuel discharge tube so as to provide a venturi, the nozzle having relatively narrow elongated fuel discharge ports located substantially in the throat of the venturi.
- Figure 1 is a more or less diagrammatic sectional view of the features of a carburetor entering into the present invention.
- Figure 2 is a diagrammatic sectional view illustrating the operation of the nozzle illustrated in Figure 1.
- Figure 3 is a diagrammatic sectional view taken substantially on the line 33, Figure 2.
- Figure 4 is a side elevation of the main well tube and nozzle assembly illustrated in Figure 1.
- Figure 5 is a sectional view on the line ure 4.
- Figure 6 is an elevational view Figure 5.
- Figure 7 is a plan view of the structure shown in Figure 5.
- the size of the fuel pas-- sages is limited to the minimum that will handle the fuel required for satisfactory operation of the engine.
- the present invention is characterized in that it pro-' vides a nozzle operating in conjunction with the fuel discharge passage adapted to spray fuel in a mist and in. a thin sheet generally perpendicular to the direction of air flow so that the fuel is substantially completely atomized.
- the nozzle is designed to cooperate with the discharge passage to produce a venturi the throat of which surrounds the generally elongated narrow discharge port in the nozzle.
- means are associated with the discharge nozzle to provide a supply of air-fuel emulsion characterized in its relatively low mass so that it may respond substantially instantaneously to extremely small variations in the partial vacuum acting at the discharge ports of the nozzle.
- the foregoing provides an improvement which substantially eliminates a surge problem heretofore encountered as a result of large globs of fuel being introduced into the air stream.
- the present carburetor substantially avoids the surge problem by a three-fold action.
- the supply of fuel available to the discharge nozzle is in the form of an air-fuel emulsion so that in no case could relatively large drops or globs of liquid fuel be introduced into the air stream.
- the air-fuel emulsion is introduced into the airstream through a relatively elongated narrow slit-like port which thereby introduces a fine mist of the emulsion of air and fuel in a sheet generally perpendicular to the direction of flow of air so that the fuel, which is already in the form of a fuel-air emulsion, is further atomized in a most eificient manner.
- the operation of the carburetor in producing a smooth even flow of finely atomized fuel is enhanced by the design of discharge nozzle in association with the discharge passage so that the two cooperate to define a venturi the throat of which surrounds the discharge nozzle, and more particularly, receives the ports of the discharge nozzle.
- the drawings are more or less diagrammatic and are intended to show only the elements of the carburetor which enter into the present invention.
- the carburetor is shown as comprising a bowl 10 adapted to receive liquid fuel indicated at 12, the level of which will be maintained by suitable float controlled valve mechanism not shown.
- the bowl 10 is provided with a central portion having a main discharge passage 14 extending therethrough.
- a cover 16 having an aspirating opening 13 communicating with the main discharge passage.
- the main discharge passage 14 is provided at its lower end with a tubular extension 20 the lower end of which is located in the throat of a booster venturi indicated at 22.
- the lower edge of the booster venturi 22 is in turn located in the throat of the main venturi 24.
- the carburetor is provided in association with an internal combustion engine having an intake manifold maintained during operation of the engine at a variable partial vacuum designed to induce a flow of air through the venturi 24.
- Flow of air through the main venturi 24 provides a zone of reduced pressure at its throat which in turn induces a secondary flow of air through the booster venturi, thus establishing a zone of further reduced pressure or in ing 18.
- a discharge nozzle 26 Located in the main discharge passage 14 is a discharge nozzle 26 adapted to deliver fuel into the discharge passage. Fuel is drawn through the nozzle 26 as a re-. sult of the partial vacuum. existing thereat in the main discharge passage. Fuel in the bowl flows through the main jet 28 into the main well 30 and thence through a passage in the nozzle 26 to a discharge port 32 located in the main discharge passage 14. More specifically, the fiow of fuel through the jet 28, well 30 and nozzle 26 is the result of pressure differential between the substantially atmospheric pressure existing within the bowl 10 and the partial vacuum existing in the main discharge passage 14.
- the nozzle 26 is of a particular design to produce an improved action on the fuel as itis sprayed or discharged into the main discharge passage.
- the end of the discharge nozzle 32 is rounded preferably to a generally spherical construction as indicated at 34.
- the discharge nozzle includes a tubular portion which extends into the main discharge passage 14 through a side wall thereof as best illustrated in Figure 3. The parts are so proportioned that the discharge nozzle and the adjacent wall portions of the main discharge passage 14 cooperate to define a venturi the throat of which is of generally U-shaped configuration as indicated by the reference numeral 36 in Figure 3.
- the discharge port is provided in the form of an elongated relatively narrow slot.
- the slot 32 is disposed to extend along both sides and across the end of the nozzle 26 and occupies the throat of the venturi produced by the nozzle and discharge passage.
- the elongated relatively narrow slot which forms the discharge port causes the fuel to spray out into a sheet generally perpendicular to the direction of how of air past the nozzle. Accordingly, the fuel is presented to the air stream in a manner best calculated to produce complete and fine atomization.
- the construction involves a main well tube assembly comprising a main well tube 42 to which the discharge nozzle 26 is attached.
- the main well tube 42 at the side opposite the discharge nozzle 26 is provided with a flat surface as indicated at 44, and the air bleed restriction 40 is provided by a very small opening extending from the fiat surface 44 to the interior of the tube.
- the flat end wall 46 of the main well tube is provided with a channel 48 extending to the flat surface 44.
- the air Since the air is introduced through an extremely small bleed restriction it operates to produce an emulsion of fuel and air which moves upwardly in the well and through the passage in the laterally extending discharge nozzle. It is found that the air-fuel emulsion is suificiently permanent so that in operation a supply of the emulsion is at all times available to the discharge nozzle.
- the particular advantage of providing the fuel to the discharge nozzle in the form of an air-fuel emulsion is to increase sensitivity of the carburetor to relatively small changes in manifold vacuum. This is due primarily to the fact that the mass of air-fuel emulsion is greatly reduced from the corresponding mass of solid liquid fuel.
- the air-fuel emulsion is much more readily susceptible to complete atomization by the air stream in the main discharge passage 14 and particularly, in view of the fact that the emulsion is introduced inthe form of a thin sheet into the throat of a venturi, the sheet being disposed substantially perpendicular to the direction of air flow for most efficient atomization.
- a carburetor having a venturi, and a nozzle opening into said venturi and characterized by the delivery of a uniformly and finely divided fuel-air mixture by the nozzle to the throat of the carburetor venturi
- a tubular main fuel supply nozzle having a port communicatingwith atmosphere, and an open end adapted-to discharge into the venturi of the carburetor
- a tubular'fuel supply member extending into said nozzle from a side thereof, said member having a generally spherically rounded end provided with an elongated slot occupying the axis of said member and perpendicular to the'axis of said nozzle, said fuel supply member having a bleed connection. to atmosphere to bleed air into the fuel supply member to form a fuel-air emulsion whose rateof' flow is responsive to small variations in pressure within the throat of the carburetor venturi.
- a main nozzle for supplying a primary fuel-air mixture comprising a cylindrical primary air' passage, an atomizing nozzle in said passage comprising a tubular member having a spherically rounded end having its center on the axis of saidpassage to define an arcuate restriction in said passage, said end having a transverse slot occupying a plane containing the center of said rounded end and perpendicular to the axis of said passage, a'fuel passage connecting said tubular member to a supply of liquid fuel, and an air bleed in said fuel passageto bleed air into the fuel passage to provide a low gravity fuel-air mixture to the atomizing nozzle.
- means for supplying a mixture of'fuel and air to the venturi comprising a fuel bowl having a central block provided with a vertically extending cylindrical primary air supply passage,
- a main well extending downwardly from the top of said block and a jet connecting the bottom of the well to the interior of the bowl, an air bleed tube in the upper portion of said well having ports therein communicating with atmosphere, a tubular member extending from the top of the air bleed tube laterally into the cylindrical primary air supply passage, said tubular member having a spherically rounded end the center of which lies on the axis of said primary air supply passage and which defines therewith a restricted U-shaped passage, the end of said tubular member being provided with a slot passing through the center of the spherical end portion thereof and occupying a plane perpendicular to the axis of the primary air supply passage, a cover for said bowl having a restricted 6 aspirating port communicating with the primary air supply passage and a second port communicating with said air bleed tube.
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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
March 11, 1958 r 40 /7 J; Z
M. F. STERNER ET AL 6,4W CARBURETOR CONSTRUCTION Filed June 13, 1955 INVENTORS MELVIN E STERNER 5 MILTON J.KITTLER United States Patent G 2,826,400 CARBURETOR CONSTRUCTION Melvin F. Sterner, Bloomfield Hills, and Milton J. Kittler,-
Detroit, Mich., assignors to Holley Carburetor Company, Detroit, Mich., a corporation of Michigan The present invention relates to a carburetor construction, and more particularly to an improvement in the main well and discharge tube.
It is an object of the present invention to provide a carburetor characterized by its ability to deliver completely atomized fuel and to avoid irregularity in flow which would result from entrance into the air stream of relatively large drops of liquid fuel.
It is a further object of the present invention to provide a carburetor characterized in its sensitivity in response to extremely small variations in partial vacuum at the main fuel nozzle.
More specifically, it is an object of the present invention to provide a carburetor characterized in that the main fuel nozzle is designed in association with the main fuel discharge tube so as to provide a venturi, the nozzle having relatively narrow elongated fuel discharge ports located substantially in the throat of the venturi.
It is a further object of the present invention to provide a carburetor having a main well connected at one end to a fuel supply jet and connected at the other end to a discharge nozzle characterized in the provision of an air bleed restriction in the Well intermediate the jet and nozzle constructed and arranged to introduce air into the liquid fuel between the restriction and the nozzle in a manner to produce an air-fuel emulsion.
It is a feature of the present invention to provide a carburetor having a discharge nozzle extending laterally into a discharge passage, the nozzle having a rounded end and shaped to define in cooperation with the adjacent wall surfaces of the discharge passage a venturi having a generally U-shaped throat, said discharge nozzle havmg a narrow elongated fuel discharge slot extending along both sides and around the end of the nozzle and located substantially in the throat of the U-shaped venturi.
Other objects and features of the invention will become more apparent as the description proceeds, especially when taken in conjunction with the accompanying drawings, wherein:
Figure 1 is a more or less diagrammatic sectional view of the features of a carburetor entering into the present invention.
Figure 2 is a diagrammatic sectional view illustrating the operation of the nozzle illustrated in Figure 1.
Figure 3 is a diagrammatic sectional view taken substantially on the line 33, Figure 2.
Figure 4 is a side elevation of the main well tube and nozzle assembly illustrated in Figure 1.
Figure 5 is a sectional view on the line ure 4.
Figure 6 is an elevational view Figure 5.
Figure 7 is a plan view of the structure shown in Figure 5.
It is a requirement of present day carburetors that fuel be kept under very accurate control and that there be no fuel which is not at all times under control. Modern carburetors are required to operate with relatively small 55, Figlooking to the right in forces and to produce variations in fuel supply in ac-- cordance with extremely small changes in the operating forces. In fact, the amount of gasoline moved under extremely accurate control presents a rather monumental task to the relatively small force available from the air flow.
In the present construction the size of the fuel pas-- sages is limited to the minimum that will handle the fuel required for satisfactory operation of the engine.
The present invention is characterized in that it pro-' vides a nozzle operating in conjunction with the fuel discharge passage adapted to spray fuel in a mist and in. a thin sheet generally perpendicular to the direction of air flow so that the fuel is substantially completely atomized. In addition, the nozzle is designed to cooperate with the discharge passage to produce a venturi the throat of which surrounds the generally elongated narrow discharge port in the nozzle. Finally, means are associated with the discharge nozzle to provide a supply of air-fuel emulsion characterized in its relatively low mass so that it may respond substantially instantaneously to extremely small variations in the partial vacuum acting at the discharge ports of the nozzle.
The foregoing provides an improvement which substantially eliminates a surge problem heretofore encountered as a result of large globs of fuel being introduced into the air stream. The present carburetor substantially avoids the surge problem by a three-fold action. In the first place, the supply of fuel available to the discharge nozzle is in the form of an air-fuel emulsion so that in no case could relatively large drops or globs of liquid fuel be introduced into the air stream. In the second place, the air-fuel emulsion is introduced into the airstream through a relatively elongated narrow slit-like port which thereby introduces a fine mist of the emulsion of air and fuel in a sheet generally perpendicular to the direction of flow of air so that the fuel, which is already in the form of a fuel-air emulsion, is further atomized in a most eificient manner. Finally, the operation of the carburetor in producing a smooth even flow of finely atomized fuel is enhanced by the design of discharge nozzle in association with the discharge passage so that the two cooperate to define a venturi the throat of which surrounds the discharge nozzle, and more particularly, receives the ports of the discharge nozzle.
The drawings are more or less diagrammatic and are intended to show only the elements of the carburetor which enter into the present invention. The carburetor is shown as comprising a bowl 10 adapted to receive liquid fuel indicated at 12, the level of which will be maintained by suitable float controlled valve mechanism not shown. The bowl 10 is provided with a central portion having a main discharge passage 14 extending therethrough. Associated with the bowl 10 is a cover 16 having an aspirating opening 13 communicating with the main discharge passage. The main discharge passage 14 is provided at its lower end with a tubular extension 20 the lower end of which is located in the throat of a booster venturi indicated at 22. The lower edge of the booster venturi 22 is in turn located in the throat of the main venturi 24. It will of course be appreciated that the carburetor is provided in association with an internal combustion engine having an intake manifold maintained during operation of the engine at a variable partial vacuum designed to induce a flow of air through the venturi 24. Flow of air through the main venturi 24 provides a zone of reduced pressure at its throat which in turn induces a secondary flow of air through the booster venturi, thus establishing a zone of further reduced pressure or in ing 18.
Patented Mar. 11, 1958 Located in the main discharge passage 14 is a discharge nozzle 26 adapted to deliver fuel into the discharge passage. Fuel is drawn through the nozzle 26 as a re-. sult of the partial vacuum. existing thereat in the main discharge passage. Fuel in the bowl flows through the main jet 28 into the main well 30 and thence through a passage in the nozzle 26 to a discharge port 32 located in the main discharge passage 14. More specifically, the fiow of fuel through the jet 28, well 30 and nozzle 26 is the result of pressure differential between the substantially atmospheric pressure existing within the bowl 10 and the partial vacuum existing in the main discharge passage 14.
In accordance with the present construction the nozzle 26 is of a particular design to produce an improved action on the fuel as itis sprayed or discharged into the main discharge passage. In the first place, the end of the discharge nozzle 32 is rounded preferably to a generally spherical construction as indicated at 34. The discharge nozzle includes a tubular portion which extends into the main discharge passage 14 through a side wall thereof as best illustrated in Figure 3. The parts are so proportioned that the discharge nozzle and the adjacent wall portions of the main discharge passage 14 cooperate to define a venturi the throat of which is of generally U-shaped configuration as indicated by the reference numeral 36 in Figure 3.
As a result of this construction the flow of air induced through the main discharge passage from the partial vacuum existing within the intake manifold and enhanced by the cooperating actions of the venturi Y24 and 22, produces a further diminution of pressure or increase in partial vacuum available at the discharge port 32 provided in the discharge nozzle. 7
In order that the fuel passing through the discharge port 32 shall be most completely and finely atomized the discharge port is provided in the form of an elongated relatively narrow slot. The slot 32 is disposed to extend along both sides and across the end of the nozzle 26 and occupies the throat of the venturi produced by the nozzle and discharge passage. As a result of this, the elongated relatively narrow slot which forms the discharge port causes the fuel to spray out into a sheet generally perpendicular to the direction of how of air past the nozzle. Accordingly, the fuel is presented to the air stream in a manner best calculated to produce complete and fine atomization.
However, complete reliance is not placed upon the provision of the fuel supply port in the form of an elongated relatively narrow slot. Instead, means are provided which serves to form an air-fuel emulsion to be supplied to the nozzle to further insure complete atomization of the fuel and to prevent introduction of drops or globs of liquid fuel into the air stream. This is accomplished by the provision of an air bleed restriction 40 which introduces air into the main well 30 at a point between the jet 28 and nozzle 26 so as to form an emulsion of air and fuel in that portion of the main well located above the bleed restriction 40. More specifically, and as best illustrated in Figures 4-7, the construction involves a main well tube assembly comprising a main well tube 42 to which the discharge nozzle 26 is attached. The main well tube 42 at the side opposite the discharge nozzle 26 is provided with a flat surface as indicated at 44, and the air bleed restriction 40 is provided by a very small opening extending from the fiat surface 44 to the interior of the tube. At its upper end the flat end wall 46 of the main well tube is provided with a channel 48 extending to the flat surface 44. When the upper end of the main well tube 42 is in contact with the underside of the cover 16 of the bowl 10, the channel 48 is in registration with an air inlet port 50 provided in the cover. Thus, air at atmospheric pressure is available to the air bleed restriction 40 and is drawn into the liquid fuel as it rises through the well 30. Since the air is introduced through an extremely small bleed restriction it operates to produce an emulsion of fuel and air which moves upwardly in the well and through the passage in the laterally extending discharge nozzle. It is found that the air-fuel emulsion is suificiently permanent so that in operation a supply of the emulsion is at all times available to the discharge nozzle.
The particular advantage of providing the fuel to the discharge nozzle in the form of an air-fuel emulsion is to increase sensitivity of the carburetor to relatively small changes in manifold vacuum. This is due primarily to the fact that the mass of air-fuel emulsion is greatly reduced from the corresponding mass of solid liquid fuel.
Accordingly, movement of the emulsion in response to variations in partial vacuum are quick and reflect more accurately the quantitative changes in partial vacuum.
In addition to the increase in sensitivity produced by the supply of the air-fuel emulsion, it is of course apparent that the air-fuel emulsion is much more readily susceptible to complete atomization by the air stream in the main discharge passage 14 and particularly, in view of the fact that the emulsion is introduced inthe form of a thin sheet into the throat of a venturi, the sheet being disposed substantially perpendicular to the direction of air flow for most efficient atomization.
From the foregoing it will be observed that the structural modifications involving (1) the production of the venturi throat 36 surrounding the end of the discharge nozzle 26, (2) the provision of the elongated relatively narrow discharge slot at both sides and extending around the end of the discharge nozzle 26, and (3) the provision ofthe air bleed restriction 40 to provide a supply of airfuel emulsion for the discharge nozzle, all cooperate to produce a continuous smooth finely atomized flow completely devoid of irregularities due to introduction into the air stream of relatively large globs or drops and further, enhance sensitivity of fuel supply in accordance with extremely small variations in manifold vacuum.
The drawings and the foregoing specification constitute a description of the improved carburetor construction in such full, clear, concise and exact terms as to enable any person skilled in the art to practice the invention, the scope of which is indicated by the appended claims.
What we claim as our invention is:
1. In a carburetor having a venturi, and a nozzle opening into said venturi and characterized by the delivery of a uniformly and finely divided fuel-air mixture by the nozzle to the throat of the carburetor venturi comprising a tubular main fuel supply nozzle having a port communicatingwith atmosphere, and an open end adapted-to discharge into the venturi of the carburetor, a tubular'fuel supply member extending into said nozzle from a side thereof, said member having a generally spherically rounded end provided with an elongated slot occupying the axis of said member and perpendicular to the'axis of said nozzle, said fuel supply member having a bleed connection. to atmosphere to bleed air into the fuel supply member to form a fuel-air emulsion whose rateof' flow is responsive to small variations in pressure within the throat of the carburetor venturi.
2. In a carburetor, a main nozzle for supplying a primary fuel-air mixture comprisinga cylindrical primary air' passage, an atomizing nozzle in said passage comprising a tubular member having a spherically rounded end having its center on the axis of saidpassage to define an arcuate restriction in said passage, said end having a transverse slot occupying a plane containing the center of said rounded end and perpendicular to the axis of said passage, a'fuel passage connecting said tubular member to a supply of liquid fuel, and an air bleed in said fuel passageto bleed air into the fuel passage to provide a low gravity fuel-air mixture to the atomizing nozzle.
3. Ina carburetor having a venturi, means for supplying a mixture of'fuel and air to the venturi comprising a fuel bowl having a central block provided with a vertically extending cylindrical primary air supply passage,
a main well extending downwardly from the top of said block and a jet connecting the bottom of the well to the interior of the bowl, an air bleed tube in the upper portion of said well having ports therein communicating with atmosphere, a tubular member extending from the top of the air bleed tube laterally into the cylindrical primary air supply passage, said tubular member having a spherically rounded end the center of which lies on the axis of said primary air supply passage and which defines therewith a restricted U-shaped passage, the end of said tubular member being provided with a slot passing through the center of the spherical end portion thereof and occupying a plane perpendicular to the axis of the primary air supply passage, a cover for said bowl having a restricted 6 aspirating port communicating with the primary air supply passage and a second port communicating with said air bleed tube.
References Cited in the file of this patent UNITEDSTATES PATENTS 1,261,756 Britton Apr. 9, 1918 1,477,280 Pordes Dec. 11, 1923 1,816,756 Whatmough et al. July 28, 1931 1,895,470 Matln'eu Jan. 31, 1933 2,589,559 Lebeda Mar. 18, 1952 2,676,004 Bimberg Apr. 20, 1954 2,681,216 Knecht June 15, 1954
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US514908A US2826400A (en) | 1955-06-13 | 1955-06-13 | Carburetor construction |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US514908A US2826400A (en) | 1955-06-13 | 1955-06-13 | Carburetor construction |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2826400A true US2826400A (en) | 1958-03-11 |
Family
ID=24049177
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US514908A Expired - Lifetime US2826400A (en) | 1955-06-13 | 1955-06-13 | Carburetor construction |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2826400A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2966312A (en) * | 1958-03-06 | 1960-12-27 | Norgren Co C A | Aerosol generator and lubricator and method of generating micronic size aerosol |
| US3677241A (en) * | 1970-05-08 | 1972-07-18 | Laprade Usines Sa | Carburettors operating under a constant reduced pressure |
| US4263233A (en) * | 1979-10-09 | 1981-04-21 | Chrysler Corporation | Fuel preparation for internal combustion engines |
| US4518542A (en) * | 1979-12-31 | 1985-05-21 | Rogers Jerry L | Carburetor attachment |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1261756A (en) * | 1914-09-28 | 1918-04-09 | Britton Carbureter Company | Carbureter. |
| US1477280A (en) * | 1920-08-06 | 1923-12-11 | P S Vergaser Und App Bau Ag Fa | Carburetor for internal-combustion engines |
| US1816756A (en) * | 1928-04-02 | 1931-07-28 | Whatmough Wilfred Ambrose | Spray carburetor |
| US1895470A (en) * | 1929-04-30 | 1933-01-31 | Mathieu Eugene | Carburetor |
| US2589559A (en) * | 1948-01-09 | 1952-03-18 | Paul A Lebeda | Fuel nozzle |
| US2676004A (en) * | 1949-03-30 | 1954-04-20 | Bendix Aviat Corp | Carburetor |
| US2681216A (en) * | 1951-04-10 | 1954-06-15 | Knecht Henry | Slotted jet carburetor |
-
1955
- 1955-06-13 US US514908A patent/US2826400A/en not_active Expired - Lifetime
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1261756A (en) * | 1914-09-28 | 1918-04-09 | Britton Carbureter Company | Carbureter. |
| US1477280A (en) * | 1920-08-06 | 1923-12-11 | P S Vergaser Und App Bau Ag Fa | Carburetor for internal-combustion engines |
| US1816756A (en) * | 1928-04-02 | 1931-07-28 | Whatmough Wilfred Ambrose | Spray carburetor |
| US1895470A (en) * | 1929-04-30 | 1933-01-31 | Mathieu Eugene | Carburetor |
| US2589559A (en) * | 1948-01-09 | 1952-03-18 | Paul A Lebeda | Fuel nozzle |
| US2676004A (en) * | 1949-03-30 | 1954-04-20 | Bendix Aviat Corp | Carburetor |
| US2681216A (en) * | 1951-04-10 | 1954-06-15 | Knecht Henry | Slotted jet carburetor |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2966312A (en) * | 1958-03-06 | 1960-12-27 | Norgren Co C A | Aerosol generator and lubricator and method of generating micronic size aerosol |
| US3677241A (en) * | 1970-05-08 | 1972-07-18 | Laprade Usines Sa | Carburettors operating under a constant reduced pressure |
| US4263233A (en) * | 1979-10-09 | 1981-04-21 | Chrysler Corporation | Fuel preparation for internal combustion engines |
| US4518542A (en) * | 1979-12-31 | 1985-05-21 | Rogers Jerry L | Carburetor attachment |
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