Abstract:
A variable venturi carburetor including a fuel bypass duct bypassing the fuel metering portion of the fuel jet, the fuel jet being provided with an opening at its upper portion which opening is in opposed relation with the inlet of the fuel bypass duct for easily delivering fuel bubbles created in the fuel jet and also provided with a fuel inlet at its lower portion which is so constructed as for fuel to readily flow into the fuel jet.

Description:
BACKGROUND OF THE INVENTION 
     This invention relates to a variable venturi carburetor for an internal combustion engine, and more particularly to the variable venturi carburetor which prevents the influence of fuel bubbles created during engine running operation, especially under a heavy load condition so as to attain the stablization and improvement of engine power. 
     In a traditional variable venturi carburetor, especially during engine running operation under a heavy load condition, the atomized fuel stored in a fuel well of a fuel jet installed in the carburetor is vaporized to create fuel bubbles under the influence of vibration or pulsation of the engine, or increase in engine temperature. Such fuel bubbles are filled in the fuel well and intermittently delivered from a fuel metering portion of the fuel jet. As the result, an air-fuel ratio disadvantageously varies and the preset air-fuel ratio cannot be maintained constant for each engine running operation, or the drivability is likely to deteriorate during an engine running operation under a heavy load condition (see FIG. 7). 
     SUMMARY OF THE INVENTION 
     Accordingly, a primary object of the present invention is to provide a variable venturi carburetor for an internal combustion engine which prevents fuel bubbles created in the fuel well of the fuel jet from being filled therein especially during engine running operation under a heavy load condition, so that the fuel bubbles are readily delivered from the fuel jet without influencing the fuel metering portion. 
     Another object of the present invention is to provide a variable venturi carburetor for an internal combustion engine which maintains an air-fuel ratio at a constant value to attain the stabilization and improvement of engine power especially during engine running operation under a heavy load condition. 
     According to the present invention, the variable venturi carburetor includes a fuel bypass duct bypassing the fuel metering portion of the fuel jet. The fuel jet is provided with a slit at its upper portion which slit is in opposed relation with the inlet of the fuel bypass duct for easily delivering fuel bubbles created in the fuel jet, and also provided with a fuel inlet at its lower portion which is so constructed as for fuel to readily flow into the fuel jet. A bubble well is provided between the outer circumference of the fuel jet and the inner circumference of the fuel passage and is adapted to lead from the slit to the inlet of the fuel bypass duct. 
     Various general and specific objects, advantages and aspects of the invention will become apparent when reference is made to the following detailed description of the invention considered in conjunction with the related accompanying drawings. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     FIG. 1 is a vertical sectional view of the variable venturi carburetor according to the first preferred embodiment of the invention; 
     FIG. 2 is a top plan view of the fuel jet as shown in FIG. 1; 
     FIG. 3 is a sectional view of the fuel jet taken along the line III--III of FIG. 2; 
     FIG. 4 is a vertical sectional view of the variable venturi carburetor according to the second preferred embodiment of the invention; 
     FIG. 5 is a vertical sectional view of the fuel jet as shown in FIG. 4; 
     FIG. 6 is a vertical sectional view of the fuel jet according to the third preferred embodiment of the invention; 
     FIG. 7 is a vertical sectional view of the fuel jet in the prior art illustrating the operation thereof; and 
     FIGS. 8 and 9 are vertical sectional views of the fuel jets according to the preferred embodiments of the invention illustrating the operation thereof. 
    
    
     DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS 
     Referring now to FIG. 1, reference numeral 1 designates a carburetor body having a float chamber 2, an air intake passage 3, a throttle valve 4 and a venturi portion 5. Reference numeral 6 designates a fuel passage communicating with the float chamber 2 and the venturi portion 5. There is provided a fuel jet 7 in the fuel passage 6. The venturi portion 5 is defined upstream of the throttle valve 4 by the inside wall 3a of the air intake passage 3 and the bottom end 8a of a suction piston 8. A suction chamber 9 is defined by a cylindrical portion 1a of the carburetor body 1 and the suction piston 8 slidably inserted into the cylindrical portion 1a. A compression spring 8b is inserted in the suction chamber 9 and serves to at all times urge the suction piston 8 toward the inside wall 3a of the air intake passage 3. A vacuum communication port 9a is provided at the bottom end 8a  of the suction piston 8 and adapted to communicate with the suction chamber 9 and the venturi portion 5. An atmospheric pressure chamber 10 is defined by the sliding flange portion 8c of the suction piston 8 and the carburetor body 1, and provided with an atmospheric pressure communication port 10a in the vicinity of the inlet of the air intake passage 3, whereby ambient air is induced through the port 10a. A fuel metering needle 11 is fixed to the bottom end 8a of the suction piston 8 at its center position. The free end of the fuel metering needle 11 is laterally reciprocatingly inserted in the interior of the fuel jet 7. 
     As shown in FIGS. 2 and 3, the fuel jet 7 is of hollow cylindrical shape and provided with a slit 7a at the upper portion thereof. The slit 7a is opened longitudinally of and near the right end of the fuel jet 7. The fuel jet 7 is also provided with a fuel inlet 7b at the lower portion thereof. The fuel inlet 7b is obliquely opened toward the left end of the fuel jet 7. The fuel jet 7 is also provided with a fuel metering portion 7c at the left end thereof. The right end of the fuel jet 7 is closed by a plug P, whereby a fuel well 12 is defined in the interior of the fuel jet 7. As shown in FIG. 1, the fuel jet 7 is housed in the fuel passage 6 with a seal ring S fitted on the outer circumference of the left end of the fuel jet 7, whereby a bubble well 13 is defined between the outer circumference of the fuel jet 7 and the inner circumference of the fuel passage 6. The bubble well 13 communicates the slit 7a with an inlet of a fuel bypass duct 14. 
     The fuel bypass duct 14 bypasses the fuel metering portion 7c of the fuel jet 7 above the fuel passage 6. The inlet of the fuel bypass duct 14 opens to the upstream portion of the fuel passage 6 and the outlet of the fuel bypass duct 14 opens to the downstream portion of the fuel passage 6, which outlet is provided with a calibrated jet nozzle 15. The fuel pipe 16 installed in the float chamber 2 is positioned directly beneath the fuel inlet 7b of the fuel jet 7. 
     FIGS. 4 and 5 show a second preferred embodiment according to the present invention, in which like reference numerals designate identical parts with the first preferred embodiment. In this embodiment, a carburetor body 101 is provided with a fuel jet 107 which has two fuel inlets 107b and 107d as shown in FIG. 5. Two fuel tubes 116b and 116d are installed in a float chamber 102 directly beneath the fuel inlets 107b and 107d and in alignment with the same, respectively. Other components of this embodiment are substantially identical with that of the first preferred embodiment, and therefore the explanation thereof will be omitted. 
     FIG. 6 shows a fuel jet 207 of a third preferred embodiment according to the present invention, in which the fuel jet 207 is provided with two fuel inlets 207b and 207d, and two openings 207e and 207f which are substituted for a slit 7a or 107a of the preceding preferred embodiments. 
     In operation, during engine running operation under a heavy load condition, liquid fuel in the float chamber 2 is sucked up through the fuel pipe 16 into the fuel inlet 7b of the fuel jet 7. Such sucked fuel is directly supplied to the fuel metering portion 7c, the annular opening area of which is controlled by the fuel metering needle 11, or such sucked fuel is once stored in the fuel well 12 and thereafter supplied to the fuel metering portion 7c. Such metered fuel is injected through the fuel passage 6 to the venturi portion 5 of the air intake passage 3. Some of the fuel stored in the fuel well 12 is supplied through a bubble well 13 into the fuel bypass duct 14 and then metered by the calibrated jet nozzle 15 to be injected through the fuel passage 6 to the venturi portion 5 of the air intake passage 3. During engine running operation under a heavy load condition, the fuel stored in the fuel well 12 is vaporized, thereby causing bubbles of the vaporized fuel to be generated and stored in the fuel well 12 due to vibration or pulsation of the engine, or increase in engine temperature as referred to FIG. 7 illustrating a conventional fuel jet. On the contrary, since the fuel jet 7 of this preferred embodiment is provided with a slit 7a at its upper portion, the fuel bubbles stored in the fuel well 12 are continuously sucked up through the slit 7a to the bubble well 13, and then introduced via the fuel bypass duct 14 into the fuel passage 6. The fuel bubbles delivered from the fuel bypass duct 14 are mixed with the metered fuel delivered from the fuel metering portion 7c and the mixed fuel is then injected into the venturi portion 5 of the air intake passage 3 as referred to FIG. 8. Since the fuel inlet 7b of the fuel jet 7 in this preferred embodiment is constructed as a parallelogram configuration in its longitudinal cross-section, fuel flow toward the fuel metering portion 7c is hardly influenced by the fuel bubbles stored in the fuel well 12. Accordingly, the rate of fuel flow is properly metered by the fuel metering portion 7c of the fuel jet 7 to maintain a constant air-fuel ratio without being influenced by the fuel bubbles in the fuel well 12. 
     The operation of the second preferred embodiment as shown FIG. 4 is featured such that the fuel in the float chamber 102 is sucked up via two fuel pipes 116b and 116d through two fuel inlets 107b and 107d into the fuel well 112, thereby causing the fuel flowing into the fuel well 112 to successively flow out and also reducing creation of the fuel bubbles as referred to FIG. 9. 
     Although some preferred embodiments of the invention have been disclosed and described, it is apparent that other embodiments and modifications of the invention are possible within the scope of the appended claims.