US1933380A - Carburetor - Google Patents
Carburetor Download PDFInfo
- Publication number
- US1933380A US1933380A US445922A US44592230A US1933380A US 1933380 A US1933380 A US 1933380A US 445922 A US445922 A US 445922A US 44592230 A US44592230 A US 44592230A US 1933380 A US1933380 A US 1933380A
- Authority
- US
- United States
- Prior art keywords
- air
- carburetor
- vanes
- section
- channels
- 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
Links
- 239000000446 fuel Substances 0.000 description 13
- 238000005192 partition Methods 0.000 description 9
- 239000007921 spray Substances 0.000 description 6
- 239000000203 mixture Substances 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000004512 die casting Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 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
- F02M1/00—Carburettors with means for facilitating engine's starting or its idling below operational temperatures
-
- 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
- F02M2700/00—Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
- F02M2700/43—Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel
- F02M2700/4302—Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel whereby air and fuel are sucked into the mixture conduit
- F02M2700/4373—Mixture improving devices
- F02M2700/4376—Mechanical devices
Definitions
- This invention relates to carburetors and more particularly to means for controlling the path of air flow, and fuel spray flow, in carburetors and in the intake passages of internal combustion engines.
- An object of our invention is to provide a means whereby the air passing through a carburetor is given a smooth stream line flow of substantially uniform velocity, and free from eddy currents.
- a further object of our invention is to provide a means for preventing distortion of currents in 40 the air flow through the passages of a carburetor and intake manifold of the engine.
- Another object of our invention is to provide a means whereby the air flow through a carburetor and the intake manifold to the engine is uniform across the section of the air passage.
- Still another object of. our invention is to provide a means whereby the fuel spray in a carburetor is evenly and centrally distributed in the air stream passing through the carburetor.
- Figure 2 is a section along the line 2'2 of Figure 1, looking in the direction of the arrows;
- Figure 3 is a vertical longitudinal section of a modified form of our invention.
- FIG. 4 is a similar view of still another modification of our invention.
- the numeral 1 designates the body of a carburetor
- 2 an engineintake manifold which is bolted to the carburetor by means of a usual flanged joint 3.
- a Venturi tube 4 and throttle valve 5 are positioned in the carburetor body 1, as clearly shown.
- a multiple jet' nozzle 6 is threaded through the bottom wall of the carburetor body 1 so that the jets discharge in the zone of the smallest section of Venturi tube 4..
- a constant level float chamber 7 supplies liquid fuel to nozzle 6 through a submerged metering orifice 8.
- Air horn 9 Cast integral with the carburetor body 1, is an intake air horn 9 arranged substantially at a right angle with the body 1.
- Air horn 9 has a flat square bottom wall 10 and back wall 11 which intersect in substantially a right angle, only the extreme junction'angle being rounded off, as at 12. It will be noted that the back wall 11 of the air horn is bulged out so as to enlarge the section of the 'elbow turn to a size greater than the section of the body 1, and thatthis wall merges with body 1 in a curve which is continuous with that of the Venturi 4. The same is true of the inner curved wall 13 joining the upper wall of air horn 9 with body 1.
- a continuous stream line surface is secured and no projections or interrupting surfaces are presented to disturb the air currents passing through the carburetor.
- a plurality of guide vanes or partitions 14 Positioned within the air horn 9 are a plurality of guide vanes or partitions 14 which commence in planes parallel to the axis of air horn 9, continue around the elbow bend, and terminate in planes at right angles to the axis of air horn 9 just below venturi 4. These guide vanes 14 are equispaced at all points so that the channels defined by them are of the same cross section along any intersecting plane.
- Partitions 14 and 15 may be cast integral with air horn 9 and body 1, as shown in Figures 1, 2 and 3, or they may be separate therefrom,as in Figure 4 where they are formed integral with the Venturi tube.
- vanes or partitions used to conduct the air flow around the angle of the air horn are preferably in the form of conjugate hyperbolas to facilitate stream line flow.
- vertical vanes parallel to the plane of the bend are helpful in breaking up vortices that tend to form from the corners where the firstmentioned ribs join the wall of the air passage.
- the shape and arrangement of these ribs were determined by experimenting with a Pitot search tube while a'current of air is forced through the carburetor.
- the numeral 16 denotes a detachable section of the engine intake manifold 2, which section is formed with a plurality of deflecting ribs or vanes 17 which define channels of equal cross section around the bend from the carburetor body 1 to the manifold body 2.
- These ribs or vanes 1'7 perform with the outgoing mixture the same function as is performed by partition 14 on the incoming air.
- By defining smooth stream line channels of equal cross section a steady flow of uniform velocity is obtained and unequal pressures and eddy currents are eliminated. This helps greatly to prevent liquid fuel deposits on the walls of the intake manifold.
- Figure 1 shows a fuel jet 6 having a submerged metering orifice 8 and larger multiple outlets arranged so that the fuel spray is not directed against the throttle valve 5 and its shaft.
- This advantageous form of jet can only be used with an air flow so even that the suction is equally balanced on the jet outlets. With the conventional elbow air passage, the suction would not be equal on the two outlets, consequently such a jet would discharge a large but uncertain proportion of its fuel from the outlet located in the highest air velocity.
- vanes 1'7 are so located with respect to the throttle valve 5 that a plane including the throttle axis and the axis of the mixing chamber bisects each of the vanes, so that when the throttle is in part open position, the two halves into which it divides the air stream will each be distributed uniformly among the manifold channels formed by the vanes.
- square elbows may be used with greater efficiency than curved elbows without the vanes.
- the enlarged square elbow shown in the air horn in Figure 1 is more eificient than the usual rounded elbow even without the vanes, although the vanes still further increase its efficiency.
- a carburetor having a body and an air horn at an angle, a plurality of curvilinear guide vanes extending from near the entrance to said air horn to said body and subdividing said air horn. into a plurality of smooth curvilinear channels whereby a condition of steady uniform air flow is maintained.
- an air horn having a square elbow of enlarged cross section as compared to said passage and a plurality of guide vanes subdividing said air passage into channels.
- aplurality of curved guide vanes paralleling the walls of said air passage and subdividing said passage into channels of substantially equal cross section.
- a carburetor having a curved air passage, a plurality of curved horizontal vanes paralleling the walls of said passage and subdividing said passage into channels of substantially equal cross section.
- a carburetor having an air passage, a plurality of intersecting horizontal and vertical partitions subdividing said passage intochannels of substantially equal cross section whereby a steady uniform flow of air through said passage is secured.
- a carburetor having a curved airinlet, a plurality of intersecting partitions subdividing said inlet into channels to provide a uniform flow of air through said inlet.
- a carburetor having an elongated mixing chamber and a throttle valve pivoted therein, a discharge pipe leading from the mixing chamber, and a plurality of guide vanes subdividing said pipe into channels, said vanes being so positioned that a plane including the axis of the mixing chamber and the throttle axis bisects each of the vanes.
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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
Oct. 31, 1933. c M K T AL 1,933,330
CARBURETOR Filed April 21, 1930 5 Sheets-Sheet l I N V EN TORS flank C. Mock ()Ct. 31, 1933. F c, MOCK r vAL 1,933,380
CARBURETOR Filed April 21, 1930 3 Sheets-Sheet "2 IN VEN TORS" Frank C. Heck Oct. 31, 1933. F, c MOCK ET AL 1,933,380
CARBURETOR Filed April 21 1930 s Sheets-Sheet 5 INVENTORS Frank C. jfl'fock flwan 15. Chandler Patented Oct. 31, 1933 CARBURETOR Frank C. Mock and Milton E. Chandler, Chicago,
Ill., assignors to Bendix Stromberg Carburetor Company, South Bend, Ind., a corporation of Illinois Application April 21, 1930. Serial No. 445,922 8 Claims. (Cl. 261-439 This invention relates to carburetors and more particularly to means for controlling the path of air flow, and fuel spray flow, in carburetors and in the intake passages of internal combustion engines.
In automobile engine practice in particular, it is common to have the air entrance of the carburetor at an angle to the direction of air flow past the jet. This results in the air flow not filling the airpassage, with consequent low capacity of air flow and the formation of eddy currents which have the effect of pulling the fuel spray out of the center of the air stream. Also, if the inequality of air flow extends as far asa point of division in the engine intake manifold, a condition of unequal pressures is formed, which tends still further toward inequality in the air stream distribution.
Such a condition manifests itself in the operation of the engine, as lack of smoothness, very narrow range of permissible mixture proportion, high fuel consumption and an unusual tendency to miss or backfire when the throttle is opened quickly. Also, the engine will usually pull better and smoother with the throttle partly closed than with it full open. All the circumstances causing this are not fully understood, but our experiments have repeatedly shown that the engine performance is very much better when the air stream, as measured by Pitot search tubes, is uniform across the section of the carburetor barrel, and when the fuel spray is then evenly and centrally distributed in the air stream.
An object of our invention is to provide a means whereby the air passing through a carburetor is given a smooth stream line flow of substantially uniform velocity, and free from eddy currents. A further object of our invention is to provide a means for preventing distortion of currents in 40 the air flow through the passages of a carburetor and intake manifold of the engine.
Another object of our invention is to provide a means whereby the air flow through a carburetor and the intake manifold to the engine is uniform across the section of the air passage.
Still another object of. our invention is to provide a means whereby the fuel spray in a carburetor is evenly and centrally distributed in the air stream passing through the carburetor.
With these and other objects in view, which are incidentto our improvements, our invention consists in the combination and arrangement of parts hereinafter described and illustrated in the accompanying drawings, in which the same referenge numerals denote similar elements throughou Figure 1 is a vertical longitudinal section of a plain tube type of carburetor embodying our improvements;
Figure 2 is a section along the line 2'2 of Figure 1, looking in the direction of the arrows;
Figure 3 is a vertical longitudinal section of a modified form of our invention; and
Figure 4 is a similar view of still another modification of our invention.
Referringv toFigures 1 and 2, the numeral 1 designates the body of a carburetor, 2 an engineintake manifold which is bolted to the carburetor by means of a usual flanged joint 3. A Venturi tube 4 and throttle valve 5 are positioned in the carburetor body 1, as clearly shown. A multiple jet' nozzle 6 is threaded through the bottom wall of the carburetor body 1 so that the jets discharge in the zone of the smallest section of Venturi tube 4.. A constant level float chamber 7 supplies liquid fuel to nozzle 6 through a submerged metering orifice 8.
Cast integral with the carburetor body 1, is an intake air horn 9 arranged substantially at a right angle with the body 1. Air horn 9 has a flat square bottom wall 10 and back wall 11 which intersect in substantially a right angle, only the extreme junction'angle being rounded off, as at 12. It will be noted that the back wall 11 of the air horn is bulged out so as to enlarge the section of the 'elbow turn to a size greater than the section of the body 1, and thatthis wall merges with body 1 in a curve which is continuous with that of the Venturi 4. The same is true of the inner curved wall 13 joining the upper wall of air horn 9 with body 1. In this way a continuous stream line surface is secured and no projections or interrupting surfaces are presented to disturb the air currents passing through the carburetor. Positioned within the air horn 9 are a plurality of guide vanes or partitions 14 which commence in planes parallel to the axis of air horn 9, continue around the elbow bend, and terminate in planes at right angles to the axis of air horn 9 just below venturi 4. These guide vanes 14 are equispaced at all points so that the channels defined by them are of the same cross section along any intersecting plane.
vided a plurality of vertical guide vanes or partitions 15, which further equally subdivide the channels defined by partitions 14. Partitions 14 and 15 may be cast integral with air horn 9 and body 1, as shown in Figures 1, 2 and 3, or they may be separate therefrom,as in Figure 4 where they are formed integral with the Venturi tube.
In Figures 1 and 2, we have shown our preferred embodiment. Here the vanes or partitions used to conduct the air flow around the angle of the air horn are preferably in the form of conjugate hyperbolas to facilitate stream line flow. We have also found that vertical vanes parallel to the plane of the bend are helpful in breaking up vortices that tend to form from the corners where the firstmentioned ribs join the wall of the air passage. The shape and arrangement of these ribs were determined by experimenting with a Pitot search tube while a'current of air is forced through the carburetor.
In Figures 3, we have illustrated a modified form of our invention, wherein the partitions 14 are reduced to small curvilinear guide vanes spaced equally across the plane of junction of the horizontal and vertical walls of air horn 9. The channels thus defined by these vanes are of equal cross section.
Referring again to Figures 1 and 2, the numeral 16 denotes a detachable section of the engine intake manifold 2, which section is formed with a plurality of deflecting ribs or vanes 17 which define channels of equal cross section around the bend from the carburetor body 1 to the manifold body 2. These ribs or vanes 1'7 perform with the outgoing mixture the same function as is performed by partition 14 on the incoming air. By defining smooth stream line channels of equal cross section, a steady flow of uniform velocity is obtained and unequal pressures and eddy currents are eliminated. This helps greatly to prevent liquid fuel deposits on the walls of the intake manifold.
It will be noticed that Figure 1 shows a fuel jet 6 having a submerged metering orifice 8 and larger multiple outlets arranged so that the fuel spray is not directed against the throttle valve 5 and its shaft. This advantageous form of jet can only be used with an air flow so even that the suction is equally balanced on the jet outlets. With the conventional elbow air passage, the suction would not be equal on the two outlets, consequently such a jet would discharge a large but uncertain proportion of its fuel from the outlet located in the highest air velocity.
With the manifold vanes shown in Figures 1 and 2, even and straight discharge of air and fuel spray may be obtained at the point of division of the manifold above the carburetor. Provided the fuel and air stream are equally spread across the outlet of the carburetor, this equality may be maintained by suitably formed guide vanes 1'7. These vanes extend into the manifold from a plate-like cover 16, the purpose of this construction being to permit more accurate forming of the vanes by casting the piece in a die casting or metallic mold. It is to be noted that the vanes 1'7 are so located with respect to the throttle valve 5 that a plane including the throttle axis and the axis of the mixing chamber bisects each of the vanes, so that when the throttle is in part open position, the two halves into which it divides the air stream will each be distributed uniformly among the manifold channels formed by the vanes.
By the provision of guide vanes in the air horn and intake manifold, square elbows may be used with greater efficiency than curved elbows without the vanes. We have also found that the enlarged square elbow shown in the air horn in Figure 1 is more eificient than the usual rounded elbow even without the vanes, although the vanes still further increase its efficiency.
While we have disclosed the preferred form of our invention, we desire it to be understood that We do not intend to be limited to the precise form, which for purposes of illustration, we have shown and described herein, as many changes in details of construction, form and arrangement can be madeby those skilled in the art without departing from the spirit of our invention or exceeding the scope of the appended claims.
We claim:
1. In a carburetor having a body and an air horn at an angle, a plurality of curvilinear guide vanes extending from near the entrance to said air horn to said body and subdividing said air horn. into a plurality of smooth curvilinear channels whereby a condition of steady uniform air flow is maintained.
2. In a carburetor having a body with an air passage therethrough, an air horn having a square elbow of enlarged cross section as compared to said passage and a plurality of guide vanes subdividing said air passage into channels.
of substantially equal cross section.
3. In a carburetor having a curved air passage, aplurality of curved guide vanes paralleling the walls of said air passage and subdividing said passage into channels of substantially equal cross section.
4. In a carburetor having a curved air passage, a plurality of curved horizontal vanes paralleling the walls of said passage and subdividing said passage into channels of substantially equal cross section.
5. In a carburetor having an air passage, a plurality of intersecting horizontal and vertical partitions subdividing said passage intochannels of substantially equal cross section whereby a steady uniform flow of air through said passage is secured.
6. The combination of a carburetor having a throttle valve and a discharge pipe therefor having a plurality of guide vanes subdividing said pipe into channels, said vanes being in planes perpendicular -tothe plane of said throttle axis, so that when 'said throttle is in part open posi tion it does not interferewith the effect of said vanes on the air-fuel mixture passing through said discharge pipe.
'7. In a carburetor having a curved airinlet, a plurality of intersecting partitions subdividing said inlet into channels to provide a uniform flow of air through said inlet.
- 8. In a carburetor having an elongated mixing chamber and a throttle valve pivoted therein, a discharge pipe leading from the mixing chamber, and a plurality of guide vanes subdividing said pipe into channels, said vanes being so positioned that a plane including the axis of the mixing chamber and the throttle axis bisects each of the vanes.
IVULTON E. CHANDLER. FRANK C. MOCK.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US445922A US1933380A (en) | 1930-04-21 | 1930-04-21 | Carburetor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US445922A US1933380A (en) | 1930-04-21 | 1930-04-21 | Carburetor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1933380A true US1933380A (en) | 1933-10-31 |
Family
ID=23770705
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US445922A Expired - Lifetime US1933380A (en) | 1930-04-21 | 1930-04-21 | Carburetor |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1933380A (en) |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2443326A (en) * | 1944-10-05 | 1948-06-15 | Avco Mfg Corp | Carburetor air box |
| US2462797A (en) * | 1946-07-20 | 1949-02-22 | Westinghouse Electric Corp | Gas-cleaning means |
| US2580706A (en) * | 1946-11-22 | 1952-01-01 | Gen Motors Corp | Fuel supply system |
| US2640471A (en) * | 1950-04-24 | 1953-06-02 | Haltenberger Jules | Automobile v engine symmetrical manifold |
| US2640470A (en) * | 1949-10-20 | 1953-06-02 | Haltenberger Jules | Combustion engine inlet manifold |
| US2661239A (en) * | 1949-04-15 | 1953-12-01 | Farquhar Company Ab | Mist blower |
| US2759462A (en) * | 1954-01-07 | 1956-08-21 | Haltenberger Jules | Internal combustion ram inlet manifold |
| US2791409A (en) * | 1952-09-26 | 1957-05-07 | Lauder Alfred Ernest | Carburetors |
| US3038706A (en) * | 1959-06-04 | 1962-06-12 | Chrysler Corp | Carburetor construction |
| US3166059A (en) * | 1961-02-13 | 1965-01-19 | Bendix Corp | Aircraft fuel injection system |
| US3374775A (en) * | 1966-02-14 | 1968-03-26 | Hunt Foods And Ind Inc | Diesel engine intake and exhaust system |
| US3730496A (en) * | 1968-07-01 | 1973-05-01 | H Morgenroth | Carburetor for automotive engines with a metering suction partly derived from a laminar air flow matrix |
| DE2436556A1 (en) * | 1973-11-07 | 1975-05-15 | Toyota Motor Co Ltd | Carburettor for multi cylindered engine - is compound unit with deflector tube below the throttle valve |
-
1930
- 1930-04-21 US US445922A patent/US1933380A/en not_active Expired - Lifetime
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2443326A (en) * | 1944-10-05 | 1948-06-15 | Avco Mfg Corp | Carburetor air box |
| US2462797A (en) * | 1946-07-20 | 1949-02-22 | Westinghouse Electric Corp | Gas-cleaning means |
| US2580706A (en) * | 1946-11-22 | 1952-01-01 | Gen Motors Corp | Fuel supply system |
| US2661239A (en) * | 1949-04-15 | 1953-12-01 | Farquhar Company Ab | Mist blower |
| US2640470A (en) * | 1949-10-20 | 1953-06-02 | Haltenberger Jules | Combustion engine inlet manifold |
| US2640471A (en) * | 1950-04-24 | 1953-06-02 | Haltenberger Jules | Automobile v engine symmetrical manifold |
| US2791409A (en) * | 1952-09-26 | 1957-05-07 | Lauder Alfred Ernest | Carburetors |
| US2759462A (en) * | 1954-01-07 | 1956-08-21 | Haltenberger Jules | Internal combustion ram inlet manifold |
| US3038706A (en) * | 1959-06-04 | 1962-06-12 | Chrysler Corp | Carburetor construction |
| US3166059A (en) * | 1961-02-13 | 1965-01-19 | Bendix Corp | Aircraft fuel injection system |
| US3374775A (en) * | 1966-02-14 | 1968-03-26 | Hunt Foods And Ind Inc | Diesel engine intake and exhaust system |
| US3730496A (en) * | 1968-07-01 | 1973-05-01 | H Morgenroth | Carburetor for automotive engines with a metering suction partly derived from a laminar air flow matrix |
| DE2436556A1 (en) * | 1973-11-07 | 1975-05-15 | Toyota Motor Co Ltd | Carburettor for multi cylindered engine - is compound unit with deflector tube below the throttle valve |
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