US3410539A - Carburetor - Google Patents

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US3410539A
US3410539A US544246A US54424666A US3410539A US 3410539 A US3410539 A US 3410539A US 544246 A US544246 A US 544246A US 54424666 A US54424666 A US 54424666A US 3410539 A US3410539 A US 3410539A
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air
fuel
mixture
butterfly valve
carburetor
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Walker Brooks
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M3/00Idling devices for carburettors
    • F02M3/08Other details of idling devices

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  • the orifice for passing the idling air and the orifice for admitting rich fuel mixture are oriented such that the envelopes of idling air and rich fuel mixture are collided in a zone removed from the wall of the carburetor to produce proper atomizing of the fuel.
  • the envelopes are collided in a mixing conduit and the mixture is guided to a zone adjacent the center of the flow passage through the carburetor.
  • Adjusting means is usually provided for adjusting the orifices to regulate the flow of air and rich fuel to adjust the idling speed of the engine.
  • the adjustment for the orifice through the valve is arranged to be made by the use of a tool inserted through the carburetor throat.
  • the present invention concerns improvements in the operation and effectiveness of carburetors for internal combustion engines having socalled butterfly valves. More particularly, the invention concerns the idling phase of such devices or analogous phases, e.g. rapid deceleration and slowspeed cruises.
  • the arrangement according to the invention provides for a butterfly valve which is completely closed in the idling operation so that substantially no air is passing along its edges.
  • One or more ports are provided in the body of the butterfly valve through which the necessary air is admitted in such a way that substantially all incoming air collides with all of the incoming rich fuel mixture. This results first in a better atomization of the incoming fuel.
  • a second advantage is the more uniform distribution of the fuel in the air. Since the mixture resulting from the collision will move in a direction determined by the directional and kinetic characteristics if the two colliding streams, it is possible to control its movement by appropriate manipulation of the colliding streams.
  • FIG. 1 shows a cross-section through part of a conventional carburetor along the line 1-1 in FIG. 2;
  • FIG. 2 shows a plan'view of a section through a conventional carburetor; (such, as in FIG. 1);
  • FIG. 3 shows selected details of FIG. 1 to illustrate the mixing process in conventional carburetors
  • FIG. 4 shows selected details of FIG. 2 to illustrate other aspects of the mixing process in conventional carburetors
  • FIG. 5 shows the basic concept of the invention applied to the conventional arrangement shown in FIG. 1, some of the details conforming to a cross-section taken along the line 88 in FIG. 9;
  • FIG. 6 shows a special embodiment of the invention in application to the butterfly valve shown in FIG.
  • FIG. 7 shows a further embodiment of the invention, generally conforming to the disclosure of FIG. 5;
  • FIG. 8 shows a further embodiment of the invention, partially in cross-section taken along the line 88 in FIG. 9;
  • FIG. 9 shows a top view of the butterfly valve according to the invention.
  • FIG.- 10 shows further details of the concept disclosed in FIG. 5 in combination with elements of the embodiment of FIG. 8;
  • FIG. 11 ShOWs further details of the concept disclosed in FIG. 7 in combination with elements of FIG. 8;
  • FIG. 12 shows a practical modification of existing parts for the purpose of practicing the invention according to FIG. 8;
  • FIGS. 1 and 2 show, for reference only, a conventional carburetor, generally indicated at 1, attached to an intake manifold 2 above a hole 2a by means of screws 3, 3a, 3b and 30.
  • a butterfly valve 4 on a shaft 5 and fastened by means of screws 6, divides a vertical air passage formed by a wall 13 into an upper chamber 7 and a lower chamber 8.
  • An arm 9 is attached to the shaft 5 and controlled by a rod 10 whereby the shaft 5 and thus the butterfly valve 4 may be moved to various positions by the driver of the vehicle during the acceleration and cruising phases.
  • Conventional means (not shown) are provided, commonly in the form of a fine thread adjustment screw, to define some preferred position of the butterfly valve 4 in the idling operation in which it is not subject.
  • the intake manifold 2 (FIG. 1) communicates with the pistons of the engine (not shown) through valves, in such a manner that the receding pistons will create a suction effect by causing lower-than-ambient air pressure in the intake manifold 2.
  • This suction will operate through a hole 2a in the intake manifold 2 to draw air all along the edges 11 and 12 of the butterfly valve 4, so that it passes from the upper chamber .7 intothe lower chamber 8.
  • the conventional arrangement also provides for a supply of fuel which enters the lower chamber 8 by virtue of the same suction which draws air past the butterfly valve 4, as explained above.
  • the fuel is drawn from a reservoir (not shown) through a duct 14, past ports 15 and 16 which are at this time operative to allow the aspiration of some air from the upper chamber 7 into the fuel moving in the duct 14, and further past an idle adjustment screw 18 in the form of a needle valve which controls the volume of what now constitutes a rich mixture of fuel and air, to a port 17 from which the rich mixture emerges in the form of a jet aimed to traverse the lower chamber -8.
  • the duct system provided for the delivery of the rich fuel mixture to the chamber 8, commonly in the form of holes cored or drilled in the wall of the car-buretor, is generally so arranged that fuel will not enter the lower chamber 8 by gravitational flow, nor syphon into it, but must be drawn in by the positive force of suction.
  • Such arrangements are well known in the art and need not be explained here.
  • FIGS. 3 and 4 shows that the jet of the rich fuel mixture, bounded by line 19, will encounter a relatively small portion of the first air sheet which is shown as bounded by the wall section 13a and the line 11a. It has been established that the jet of the rich fuel mixture is not broken up in this collision. Most of it survives and traverses the space below the butterfly valve 4, as shown in FIG. 3.
  • all or part of the surviving jet may then strike the butterfly valve 4.
  • Such collision of the massive jet of relatively raw fuel with a solid body results in a consolidation of the course fuel particles on the butterfly valve 4 in the form of droplets which run to the edge 12 and pass into the second air sheet bounded by the line 12a and the Wall section 13b. If the surviving jet does not strike the butterfly valve 4, it collides once more with a relatively small part of the second air sheet and, not being completely dissipated in the air, strikes the wall section 131:. The consequences of striking this solid body are the same as described above. Runs of fuel droplets are formed which pass along the wall downward.
  • FIG. 5 The inventive concept is shown in FIG. 5 in its fundamental application.
  • a butterfly valve 4 substantially identical with that of FIGS. 1, 2, 3 and 4, is provided on the shaft 5 and controlled as explained above by a rod 9 and arm 10 (these parts are not detailed in FIG. 5 for the sake of simplicity).
  • the slightly inclined position of the butterfly valve 4 is desirable to avoid a binding of its edges 11 and 12 against the wall 13 of the large air passage.
  • the contact of the edges 11 and 12 is ideally utilized to define the idle position of the butterfly valve 4 in relation to the air passage and also to insure a relatively airtight seal all around the circumference of the butterfly valve 4..
  • Such control means may take the form of a lid or valve 22 (FIGS. 5 and 9) which is rotatable about and arrestable by a screw 23 and may be set to reduce the cross-section of the port 21.
  • Such setting may be accomplished by tapping the lid 22 into a desired position.
  • a slot 24 has been found useful for this purpose. If the working end of a screwdriver is inserted into slot 24, the setting operation can be accomplished with greater ease and accuracy.
  • a further means to control the collision of the stream 20 with the jet 19 is shown in FIG. 6.
  • the place of the port 21 is taken here by a slot 28 while the port 21 is located in a slide 29 which may be set under the guidance of screws and 30a, which also serve to arrest it in a preferred position, so that the port 21 occupies various positions in the slot 28.
  • a slide 29 which may be set under the guidance of screws and 30a, which also serve to arrest it in a preferred position, so that the port 21 occupies various positions in the slot 28.
  • Such manipulation of the point of origin of the stream 20 will affect the collision with the jet 19 and the lid 22 affords thereafter further possibilities of adjustment, in the manner described.
  • elongated slots 31 and 31a embrace the screws 30 and 30a to allow the setting of the slide 29. Since the slide 29 is longer than the distance between the shaft 5 and the edge 11 of the butterfly valve 4, it is necessary to remove part of the shaft 5. This is entirely within conventional construction and causes no difficulty.
  • the arrangement according to the invention is effective, by means of the various adjustments, to bring substantially all air in the stream 20 into collision with substantially all of the rich fuel mixture in the jet 19.
  • the quality of the mixture leaving the site of the collision and the direction of the departure may be controlled.
  • the arrangement disclosed in FIGS. 5 and 6 may thus be utilized to deliver a mixture of fuel and air which conforms to a preferred standard of quality to be center of the hole 2a in the intake manifold 2 where it will be available for further transport to the various cylinders.
  • FIG. 7 shows a further application of the concept of a collision of substantially all air admitted through the butterfly valve with substantially all of the rich fuel mixture entering through port 17.
  • a second part 21:! is provided in the butterfly valve 4 and controllable by a lid 22a with a screw 23a.
  • the stream of air admitted through the port 21a is designated as 20b and it may be manipulated in the same manner as the stream 20 discussed in connection with FIG. 5.
  • One function intended for stream 20b is to effect a collision of fresh air with the mixture which resulted from the first collision which then moves in the direction 20a.
  • This second collision serves to further atomize the fuel and to impart to the mixture'leaving the site of the second collision a direction of movement which is generally parallel to the center of the air passage formed by the wall 13, as indicated by the arrow 20a.
  • a second port 210 augments the disclosure of FIGS. 5 and 6 when it is used to handle all air being ad mitted through the butterfly valve 4. If the port 21a is used in conjunction with the port 21, it supplements the disclosure of FIGS. 5 and 6.
  • FIG. 8 shows essentially the concept of FIG. 5, but subjected to the regimen of a guide tube 25 which receives the air passing from the port 21 with its upper end 25a.
  • the collision of the air with the jet of rich fuel mixture is confined to the center part of the guide tube 25 and the resultant mixture departs through the lower end 25b.
  • the inventor has found this to be an effective arrangement.
  • the guide tube 25 is attached by means of a solder deposit 2612 to an upright tab extending from a ring 26 which is imbedded in the wall 13 of the carburetor throat.
  • any conventional method of maintaining the guide tube 25 in the position shown would suffice.
  • FIG. 12 An approach to the conversion of existing carburetors for the utilization of the arrangement of FIG. 8 is shown in FIG. 12.
  • the Guide tube 25 is attached to a tab 26a extending from a ring 26 which forms an integral part of a gasket plate 27. While it would be generally desirable to have the ring 26 imbedded in the wall 13, its insertion in a throat which has not been modified would be acceptable since the arrangement according to FIG. 8 delivers the idle mixture to the center of the chamber 8 so that the edge of the ring 26 would not impair its flow. The theoretical impairment of the massive flow in the full-speed operation may be disregarded as negligible in practical terms. The same observation can be made for the presence of the guide tube 25 in the path of the mixture of fuel and air passing in the full-speed operation.
  • FIG. 10 shows a modified application of the principle disclosed in FIG. 8.
  • the upper end 25a of the guide tube 25 is integrally attached to the underside of the butterfly valve 4 and moves with it. In the idle phase, it serves as a guide means for the stream of air passing from the port 21, delivering it in compact form to the site of the collision with the jet of the rich fuel mixture coming from the port 17.
  • a lower lip 25c is provided substantially in the geometric path of the rich fuel mixture to delimit its movement in the mixing chamber in any event and to guide the mixture resulting from the collision to a predetermined area within the mixing chamber with somewhat Fore freedom than is allowed by the guide tube 25 in FIG. 11 shows the principle disclosed in FIG. 8 in combination with that of FIG. 7.
  • a guide tube 25 is provided as in FIG. 8.
  • the upper end 25a is cut at an angle, so that it does not make a close contact with the butterfly valve 4, a gap being left on the inside through which a stream of air 20d bypasses the collision in the guide tube 25 in order to combine later with the prodnot of the collision, which then moves in the direction 20a, in a less violent manner, but essentially on the same theory as disclosed in connection with FIG. 7.
  • FIG. 12 showing a practical application of the invent1ve concept with emphasis on cost reduction and ease of installation, has been discussed above.
  • FIG. 13 shows another low cost approach in practicing the invention.
  • An interponent 28 is sandwiched between the carburetor 1 and the intake manifold 2. It is contemplated that this solution would be particularly economical even though it requires two gaskets 27 instead of the one in the conventional arrangement. Gaskets are inexpensive and since they are identical, no stocking problem arises.
  • the interponent 28 may be inexpensively die cast for use without reworking or special adaptation.
  • An 0 ring may be provided as shown to take up any tolerances which cannot be controlled in mass production. The function of the interponent is described as follows.
  • An upright member 29, which extends from the body of the interponent 28, contains a duct 32 which guides the air passing through the port 21 in the butterfly valve 4 into a horizontal passage 31 which receives the rich fuel mixture from the port 17 and conducts the mixture resulting from the collision between the fresh air and the rich fuel mixture to a discharge passage 33 which is aimed at some preferred part of the mixing chamber, for example the center. While it would be possible, and might in many cases be desirable, to provide passages in the upright member 29 which follow the operative principle of the guide tube 25, the
  • FIG. 14 deals further with the problem of possible practical applications of the invention to existing devices but also to newly manufactured carburetors.
  • the substantially horizontal passage 31 in FIG. 13 is now designated as 36 and oriented in the general direction of the flow indicated at 2001 in FIG. 5.
  • a flared terminal passage 33 is provided as in FIG. 13 to allow expansion of the mixture of air and fuel being delivered to the intake manifold.
  • a special tubular port 37 is provided which extends into the passage 36 to forestall the possibility of back pressure into the port 17 in cases in which extreme conditions require a favoring of the fresh air flow in the adjustment of the mixing ratio which has been referred to earlier.
  • a space 29a is shown between the upright member 29 and the wall 13.
  • Such a space may be the result of unintended tolerance in the parts. It may also be intentionally provided to manufacture and assemble less costly.
  • the O ring 30 insures that the rich fuel mixture coming from the port 17 reaches the site of the collision with the fresh air undiminished by leakage.
  • FIG. 15 shows the structure of FIG. 14 with provisions for a choking effect upon the mixture without impairment of the ratio of fuel to air.
  • a choke valve 38 in the form of a conventional needle valve is provided in the interponent 28 into which a hole 43 has been drilled and tapped for this purpose.
  • the choke valve 38 is settable against the pressure of a spring 41 from a first position in which its point 42 is substantially retracted from the passage 33 to another position in which is provides maximum obstruction in the passage 33.
  • the point of maximum obstruction is defined by an end 40 on the interponent 28 which stops the screw when its shoulder 39 comes in contact with it.
  • FIG. 15 is merely illustrative of the principle of providing a throttle down stream from the site of the collision of the rich fuel mixvention in various forms and in its application to certain embodiments.
  • a carburetor comprising a tubular body member, a valve pivotally mounted in said member for movement between an open position to allow maximum fluid flow therethrough and a closed position preventing fluid flow therethrough, means for admitting a stream of a rich fuel mixture through the wall of the member downstream of the valve in its closed position, a single opening through the valve for passage of a stream of fluid therethrough, said opening and admitting means being oriented to direct the envelopes of the streams into an intersecting zone removed from the wall whereby the collided streams become intermixed to atomize the fuel, a conduit secured to the member and having one end thereof adjacent the opening in the valve, another end adjacent the center area of the member, and a passage between the ends of the conduit connecting the admitting means to the conduit whereby the streams intersect in the conduit and the mixture is exhausted in the center area of the member.
  • conduit is an an-gulated tube, the end of the conduit adjacent the valve lying in a plane making a small divergent angle with the valve.
  • a carburetor as defined in claim 1 further including means mounting the valve and end of the conduit in sealing engagement with each other when the valve is in the closed position.
  • a carburetor as defined in claim 3 wherein the means securing the conduit comprises a ring secured to the body and the conduit comprises an extension integral with the ring and positioned adjacent the tubular wall of the member, and sealing means sealing the admitting means and passage against escape of fluid between the wall and extension.
  • a canburetor as defined in claim 7 further including means in the conduit for obstructing the flow of fluid from the discharge opening.
  • a carburetor comprising a tubular body member, a valve pivotally mounted in said member for movement between an open position to allow maximum fluid flow therethrough and a closed position preventing fiuid flow therethrough, means for admitting a stream of a rich fuel mixture through the wall of the member downstream of the valve in its closed position, a single opening through the valve for passage of a stream of fluid therethrough, said opening and admitting means being oriented to direct the envelopes of the streams into an intersecting zone removed from the wall whereby the collided streams become intermixed to atomize the fuel, a lid carried by the valve for movement over the opening to vary the size thereof, and means pivotally mounting the lid on the valve and a tool slot in the lid for engagement by a tool extended through the tubular member for shifting the angular position of the lid.
  • a carburetor comprising a tubular body member, a valve pivotally mounted in said member for movement (between an open position to allow maximum fluid flow therethrough and a closed position preventing fluid flow therethrough, means for admitting a stream of a rich fuel mixture through the Wall of the member downstream of the valve in its closed position, a single opening through the valve for passage of a stream of fluid therethrough, said opening and admitting means being oriented to direct the envelopes of the streams into an intersecting zone removed from the wall whereby the collided streams become intermixed to atomize the fuel, a tube secured to 9 one surface of the valve around the opening and a lid 1,884,359 carried by the other surface of the valve for movement 1,902,603 over the opening to vary the size thereof.

Description

B. WALKER Nov. 12, 1968 CARBURETQR 2 Sheets-Sheet 1 Filed April 21, 1966 Nov. 12, 1968 B. WALKER 3,410,539-
CARBURETOR Filed April 21, 1966 2 Sheets-Sheet 2 United States Patent 3,410,539 CARBURETOR Brooks Walker, 1280 Columbus Ave., San Francisco, Calif. 94133 Filed Apr. 21, 1966, Ser. No. 544,246 Claims. (Cl. 26141) ABSTRACT OF THE DISCLOSURE A carburetor for improving combustion of an internal combustion engine during closed throttle operation. An orifice is formed in the throttle valve for passing idling air when the throttle valve is closed. In one form of the invention the orifice for passing the idling air and the orifice for admitting rich fuel mixture are oriented such that the envelopes of idling air and rich fuel mixture are collided in a zone removed from the wall of the carburetor to produce proper atomizing of the fuel. In other forms of the invention the envelopes are collided in a mixing conduit and the mixture is guided to a zone adjacent the center of the flow passage through the carburetor. Adjusting means is usually provided for adjusting the orifices to regulate the flow of air and rich fuel to adjust the idling speed of the engine. The adjustment for the orifice through the valve is arranged to be made by the use of a tool inserted through the carburetor throat.
While not necessarily limited to such application, the present invention concerns improvements in the operation and effectiveness of carburetors for internal combustion engines having socalled butterfly valves. More particularly, the invention concerns the idling phase of such devices or analogous phases, e.g. rapid deceleration and slowspeed cruises.
Conventional arrangements of this kind require that the butterfly valve be cracked open for purposes of idling so that a volume of air deemed sufficient be allowed to enter all along the edges of the butterfly valve into a chamber below, where it is to be combined with a rich mixture of fuel and air entering in the form of a jet. The air so admitted around the butterfly valve is serving two indispensible functions. It provides the oxygen necessary for the combustion of the fuel. It also serves as the vehicle for the fuel on its way to the cylinders in which the combustion takes place. However, for the effective operation of the engine, it is not only necessary to provide oxygen and fuel in sufficient quantities, that is in a proper ratio of fuel to air, but the fuel must be uniformly distributed throughout the mixture and divided to a proper degree of fineness. Moreover, in engines having several cylinders which are all supplied off a common intake manifold which in turn is supplied by one or several carburetors, it is desirable to supply all cylinders uniformly, lest the engine run rOugh. Such rough running is uneconomical because, in order to provide the minimum condition for one cylinder, others must be over-supplied. It also results in excessive incidence of Waste products, on account of the incomplete combustion by overas well as under-supply of some of the cylinders,'which of late have become a matter of public concern, as they contribute to air pollution in the form of smog.
For reasons developed later in this paper, the conventional arrangements are not fully effective in delivering to the intake manifold a mixture of fuel and air which has optimum characteristics. The shortcoming is inherent in the design of conventional arrangements which peculiarly fail to maximize the potential of the two moving principles-the rich fuel-air mixture jetting into the air passing the butterfly valve-for the purpose of achieving the ideal mixture of air and fuel or at least its practicable Patented Nov. 12, 1968 ice approximation. In mechanical terms, conventional devices are inadequate because the special requirements of carburetion in the idle phase are served only by provisions for the special delivery of the rich fuel mixture, while the air is admitted in the same manner as for full speed operation, by admitting it all around the butterfly valve which is opened for this purpose.
In contrast with such conventional devices, the arrangement according to the invention provides for a butterfly valve which is completely closed in the idling operation so that substantially no air is passing along its edges. One or more ports are provided in the body of the butterfly valve through which the necessary air is admitted in such a way that substantially all incoming air collides with all of the incoming rich fuel mixture. This results first in a better atomization of the incoming fuel. A second advantage is the more uniform distribution of the fuel in the air. Since the mixture resulting from the collision will move in a direction determined by the directional and kinetic characteristics if the two colliding streams, it is possible to control its movement by appropriate manipulation of the colliding streams. While these advantages further purely technical desiderata of automotive design, they are especially significant in the context of air pollution, as they improve the operation of motor vehicles especially in the large cities where most of the driving consists of idling, low-speed, or rapid deceleration within the familiar pattern of stop-and-go.
It is one object of the invention to provide a carburetor especially adapted to the requirements of idling, lowspeed, and rapid deceleration.
It is another object of the invention to provide a carburetor which will allow a more accurate management of the air passing through the butterfly valve.
It is a further object of the invention to provide a carburetor in which air and fuel are more effectively mixed.
It is a fourth object of the invention to provide a carburetor in which the mixing of air and fuel can be more effectively controlled.
It is a fifth object of the invention to provide a carburetor which will deliver a uniform mixture of air and fuel to a predetermined point in the intake manifold.
It is a sixth object of the invention to provide a carburetor which will reduce the incidence of waste products which contribute to air pollution in the form of smog.
It is a seventh object of the invention to provide a carburetor in which the motive power in the' air stream passing the butterfly valve and the rich fuel mixture jet passing the idle adjustment screw are utilized to achieve a better mixing of the air and fuel required for the idle, lowspeed, and analogous operations.
It is an eighth object of the invention to provide ways and means whereby the other objects of the invention can be economically achieved in newly manufactured as well as in present carburetors.
These and other objectives of the invention are described below in connection with certain specific embodiments of the invention and illustrated in the drawings in which:
FIG. 1 shows a cross-section through part of a conventional carburetor along the line 1-1 in FIG. 2;
FIG. 2 shows a plan'view of a section through a conventional carburetor; (such, as in FIG. 1);
FIG. 3 shows selected details of FIG. 1 to illustrate the mixing process in conventional carburetors;
FIG. 4 shows selected details of FIG. 2 to illustrate other aspects of the mixing process in conventional carburetors;
FIG. 5 shows the basic concept of the invention applied to the conventional arrangement shown in FIG. 1, some of the details conforming to a cross-section taken along the line 88 in FIG. 9;
FIG. 6 shows a special embodiment of the invention in application to the butterfly valve shown in FIG.
FIG. 7 shows a further embodiment of the invention, generally conforming to the disclosure of FIG. 5;
FIG. 8 shows a further embodiment of the invention, partially in cross-section taken along the line 88 in FIG. 9;
FIG. 9 shows a top view of the butterfly valve according to the invention;
FIG.- 10 shows further details of the concept disclosed in FIG. 5 in combination with elements of the embodiment of FIG. 8;
FIG. 11 ShOWs further details of the concept disclosed in FIG. 7 in combination with elements of FIG. 8;
FIG. 12 shows a practical modification of existing parts for the purpose of practicing the invention according to FIG. 8;
FIGS. l3, l4 and show further possibilities of practicable embodiments of the invention, partly in section.
FIGS. 1 and 2 show, for reference only, a conventional carburetor, generally indicated at 1, attached to an intake manifold 2 above a hole 2a by means of screws 3, 3a, 3b and 30. A butterfly valve 4, on a shaft 5 and fastened by means of screws 6, divides a vertical air passage formed by a wall 13 into an upper chamber 7 and a lower chamber 8. An arm 9 is attached to the shaft 5 and controlled by a rod 10 whereby the shaft 5 and thus the butterfly valve 4 may be moved to various positions by the driver of the vehicle during the acceleration and cruising phases. Conventional means (not shown) are provided, commonly in the form of a fine thread adjustment screw, to define some preferred position of the butterfly valve 4 in the idling operation in which it is not subject. to the control of the driver, necessary adjustments being made before the vehicle is put to its normal use. Occasionally, special arrangements are made which allow the driver to make adjustments by means of a choke lever even during normal operation. It is the typical feature of conventional arrangements that for the purpose of the idle adjustment the butterfly valve is opened slightly, so that a suflicient quantity of air may pass between the cylindrical wall 13 and the-upper edge 11, and the lower edge 12 of the butterfly valve 4. For purposes of illustration, the space made available for the passage of air in FIG. 1 has been vastly exaggerated. In practical terms, the butterfly valve 4 is barely cracked open.
As-is generally known in the art, the intake manifold 2 (FIG. 1) communicates with the pistons of the engine (not shown) through valves, in such a manner that the receding pistons will create a suction effect by causing lower-than-ambient air pressure in the intake manifold 2. This suction will operate through a hole 2a in the intake manifold 2 to draw air all along the edges 11 and 12 of the butterfly valve 4, so that it passes from the upper chamber .7 intothe lower chamber 8.
The conventional arrangement also provides for a supply of fuel which enters the lower chamber 8 by virtue of the same suction which draws air past the butterfly valve 4, as explained above. The fuel is drawn from a reservoir (not shown) through a duct 14, past ports 15 and 16 which are at this time operative to allow the aspiration of some air from the upper chamber 7 into the fuel moving in the duct 14, and further past an idle adjustment screw 18 in the form of a needle valve which controls the volume of what now constitutes a rich mixture of fuel and air, to a port 17 from which the rich mixture emerges in the form of a jet aimed to traverse the lower chamber -8. The duct system provided for the delivery of the rich fuel mixture to the chamber 8, commonly in the form of holes cored or drilled in the wall of the car-buretor, is generally so arranged that fuel will not enter the lower chamber 8 by gravitational flow, nor syphon into it, but must be drawn in by the positive force of suction. However, such arrangements are well known in the art and need not be explained here.
Proceeding in the following discussion from the fact that the suction caused by the pistons of the engine causes the simultaneous entry of air around the butterfly valve 4 and of a rich fuel mixture through port 17, it is important to examine the mechanics of the collision between these two streams in the lower chamber 8. The air passing the butterfly valve 4 will enter in the form of two crescentshaped streams between the sections 13a and 13b of the wall 13 on the one and the upper edge 11, and lower edge 12 of the butterfly valve 4 on the other hand, as shown in FIG. 4. These two streams of air will fan out somewhat as they pass below the butterfly valve 4, as shown in FIG. 3. The jet of the rich fuel mixture will also spread upon entry into the chamber 8. Since the reasons for such spreading are generally known, they shall not be detailed here.
Examination of FIGS. 3 and 4 shows that the jet of the rich fuel mixture, bounded by line 19, will encounter a relatively small portion of the first air sheet which is shown as bounded by the wall section 13a and the line 11a. It has been established that the jet of the rich fuel mixture is not broken up in this collision. Most of it survives and traverses the space below the butterfly valve 4, as shown in FIG. 3.
Depending upon the arrangement, all or part of the surviving jet may then strike the butterfly valve 4. Such collision of the massive jet of relatively raw fuel with a solid body results in a consolidation of the course fuel particles on the butterfly valve 4 in the form of droplets which run to the edge 12 and pass into the second air sheet bounded by the line 12a and the Wall section 13b. If the surviving jet does not strike the butterfly valve 4, it collides once more with a relatively small part of the second air sheet and, not being completely dissipated in the air, strikes the wall section 131:. The consequences of striking this solid body are the same as described above. Runs of fuel droplets are formed which pass along the wall downward.
The consolidation of fuel particles at any stage of the process of carburetion is obviously opposed to the functional assignment of the carburetor. It results at least in an insufficient division of the fuel but certainly also in an uneven distribution of the fuel in the air. In the now common multi-cylinder engines, it is furthermore detrimental to have an undue concentration of fuel anywhere near the circumference of the hole 2a, as the action of the various pistons sets off suction trains in various directions which will draw primarily air near the lower edge of the hole 2a. Heavily concentrated mixture or droplets which routinely occur at a particular location may thus result in feeding an unduly rich, yet ill divided mixture of air and fuel to particular cylinders.
The shortcomings of the conventional arrangement may be summarized as follows. Only a fraction of the atomizing effect of the air passing the butterfly valve 4 is utilized. The fuel is not evenly distributed in the chamber 8. The consolidation of fuel particles defeats the purpose of the carburetor.
The inventive concept is shown in FIG. 5 in its fundamental application. A butterfly valve 4, substantially identical with that of FIGS. 1, 2, 3 and 4, is provided on the shaft 5 and controlled as explained above by a rod 9 and arm 10 (these parts are not detailed in FIG. 5 for the sake of simplicity). The slightly inclined position of the butterfly valve 4 is desirable to avoid a binding of its edges 11 and 12 against the wall 13 of the large air passage. The contact of the edges 11 and 12 is ideally utilized to define the idle position of the butterfly valve 4 in relation to the air passage and also to insure a relatively airtight seal all around the circumference of the butterfly valve 4.. It is intended that all air admitted into the lower chamber 8 from the upper chamber 7 shall pass through a port 21 which is so located that the air will emerge from it in the form of a jet or envelope bounded by a line 20 and intercepting the jet or envelope of the rich fuel mixture which is indicated by the line 19. This collision will have an atomizing effect upon the jet of the rich fuel mixture, resulting in a new mixture which will depart the site of the collision in a direction generally indicated by the arrow a. The actual direction of the new mixture depends upon the direction of air stream passing the port 21 (hereafter designated as stream 20) and the direction of the rich fuel jet (hereafter designated as jet 19). It is also affected by the quantities of air and fuel passing in the two streams 19 and 20 and is therefore subject to variation which may be controlled by adjustment by means of the adjustment screw 18 and special control means provided for the port 21. Such control means may take the form of a lid or valve 22 (FIGS. 5 and 9) which is rotatable about and arrestable by a screw 23 and may be set to reduce the cross-section of the port 21. Such setting may be accomplished by tapping the lid 22 into a desired position. However, a slot 24 has been found useful for this purpose. If the working end of a screwdriver is inserted into slot 24, the setting operation can be accomplished with greater ease and accuracy. A further means to control the collision of the stream 20 with the jet 19 is shown in FIG. 6. The place of the port 21 is taken here by a slot 28 while the port 21 is located in a slide 29 which may be set under the guidance of screws and 30a, which also serve to arrest it in a preferred position, so that the port 21 occupies various positions in the slot 28. Such manipulation of the point of origin of the stream 20 will affect the collision with the jet 19 and the lid 22 affords thereafter further possibilities of adjustment, in the manner described. It will be observed that elongated slots 31 and 31a embrace the screws 30 and 30a to allow the setting of the slide 29. Since the slide 29 is longer than the distance between the shaft 5 and the edge 11 of the butterfly valve 4, it is necessary to remove part of the shaft 5. This is entirely within conventional construction and causes no difficulty.
The arrangement according to the invention, as described so far, is effective, by means of the various adjustments, to bring substantially all air in the stream 20 into collision with substantially all of the rich fuel mixture in the jet 19. By manipulation of the stream 20 and the jet 19, the quality of the mixture leaving the site of the collision and the direction of the departure may be controlled. The arrangement disclosed in FIGS. 5 and 6 may thus be utilized to deliver a mixture of fuel and air which conforms to a preferred standard of quality to be center of the hole 2a in the intake manifold 2 where it will be available for further transport to the various cylinders.
FIG. 7 shows a further application of the concept of a collision of substantially all air admitted through the butterfly valve with substantially all of the rich fuel mixture entering through port 17. A second part 21:! is provided in the butterfly valve 4 and controllable by a lid 22a with a screw 23a. The stream of air admitted through the port 21a is designated as 20b and it may be manipulated in the same manner as the stream 20 discussed in connection with FIG. 5. Thus, it would be possible to allot equal shares of air to streams 20 and 20b, or to favor one over the other, or to shut either off completely, e.g. to have stream 20b serve the entire function of stream 20 in FIG. 5. One function intended for stream 20b is to effect a collision of fresh air with the mixture which resulted from the first collision which then moves in the direction 20a. This second collision serves to further atomize the fuel and to impart to the mixture'leaving the site of the second collision a direction of movement which is generally parallel to the center of the air passage formed by the wall 13, as indicated by the arrow 20a. It is obvious that the provision of a second port 210 augments the disclosure of FIGS. 5 and 6 when it is used to handle all air being ad mitted through the butterfly valve 4. If the port 21a is used in conjunction with the port 21, it supplements the disclosure of FIGS. 5 and 6.
FIG. 8 shows essentially the concept of FIG. 5, but subjected to the regimen of a guide tube 25 which receives the air passing from the port 21 with its upper end 25a. The collision of the air with the jet of rich fuel mixture is confined to the center part of the guide tube 25 and the resultant mixture departs through the lower end 25b. The inventor has found this to be an effective arrangement. The guide tube 25 is attached by means of a solder deposit 2612 to an upright tab extending from a ring 26 which is imbedded in the wall 13 of the carburetor throat. However, any conventional method of maintaining the guide tube 25 in the position shown would suffice.
An approach to the conversion of existing carburetors for the utilization of the arrangement of FIG. 8 is shown in FIG. 12. The Guide tube 25 is attached to a tab 26a extending from a ring 26 which forms an integral part of a gasket plate 27. While it would be generally desirable to have the ring 26 imbedded in the wall 13, its insertion in a throat which has not been modified would be acceptable since the arrangement according to FIG. 8 delivers the idle mixture to the center of the chamber 8 so that the edge of the ring 26 would not impair its flow. The theoretical impairment of the massive flow in the full-speed operation may be disregarded as negligible in practical terms. The same observation can be made for the presence of the guide tube 25 in the path of the mixture of fuel and air passing in the full-speed operation.
FIG. 10 shows a modified application of the principle disclosed in FIG. 8. The upper end 25a of the guide tube 25 is integrally attached to the underside of the butterfly valve 4 and moves with it. In the idle phase, it serves as a guide means for the stream of air passing from the port 21, delivering it in compact form to the site of the collision with the jet of the rich fuel mixture coming from the port 17. A lower lip 25c is provided substantially in the geometric path of the rich fuel mixture to delimit its movement in the mixing chamber in any event and to guide the mixture resulting from the collision to a predetermined area within the mixing chamber with somewhat Fore freedom than is allowed by the guide tube 25 in FIG. 11 shows the principle disclosed in FIG. 8 in combination with that of FIG. 7. A guide tube 25 is provided as in FIG. 8. However, the upper end 25a is cut at an angle, so that it does not make a close contact with the butterfly valve 4, a gap being left on the inside through which a stream of air 20d bypasses the collision in the guide tube 25 in order to combine later with the prodnot of the collision, which then moves in the direction 20a, in a less violent manner, but essentially on the same theory as disclosed in connection with FIG. 7.
FIG. 12, showing a practical application of the invent1ve concept with emphasis on cost reduction and ease of installation, has been discussed above.
FIG. 13 shows another low cost approach in practicing the invention. An interponent 28 is sandwiched between the carburetor 1 and the intake manifold 2. It is contemplated that this solution would be particularly economical even though it requires two gaskets 27 instead of the one in the conventional arrangement. Gaskets are inexpensive and since they are identical, no stocking problem arises. The interponent 28 may be inexpensively die cast for use without reworking or special adaptation. An 0 ring may be provided as shown to take up any tolerances which cannot be controlled in mass production. The function of the interponent is described as follows. An upright member 29, which extends from the body of the interponent 28, contains a duct 32 which guides the air passing through the port 21 in the butterfly valve 4 into a horizontal passage 31 which receives the rich fuel mixture from the port 17 and conducts the mixture resulting from the collision between the fresh air and the rich fuel mixture to a discharge passage 33 which is aimed at some preferred part of the mixing chamber, for example the center. While it would be possible, and might in many cases be desirable, to provide passages in the upright member 29 which follow the operative principle of the guide tube 25, the
inventor has found it advantageous in certain cases to conduct the mixture resulting from the collision of the fresh air with the rich fuel mixture horizontally and to discharge it after such horizontal movement through a flared or funnel-shaped discharge passage.
FIG. 14 deals further with the problem of possible practical applications of the invention to existing devices but also to newly manufactured carburetors. The substantially horizontal passage 31 in FIG. 13 is now designated as 36 and oriented in the general direction of the flow indicated at 2001 in FIG. 5. A flared terminal passage 33 is provided as in FIG. 13 to allow expansion of the mixture of air and fuel being delivered to the intake manifold. However, a special tubular port 37 is provided which extends into the passage 36 to forestall the possibility of back pressure into the port 17 in cases in which extreme conditions require a favoring of the fresh air flow in the adjustment of the mixing ratio which has been referred to earlier. By way of further illustration of the practical aspects, a space 29a is shown between the upright member 29 and the wall 13. Such a space may be the result of unintended tolerance in the parts. It may also be intentionally provided to manufacture and assemble less costly. The O ring 30 insures that the rich fuel mixture coming from the port 17 reaches the site of the collision with the fresh air undiminished by leakage.
FIG. 15 shows the structure of FIG. 14 with provisions for a choking effect upon the mixture without impairment of the ratio of fuel to air. A choke valve 38 in the form of a conventional needle valve is provided in the interponent 28 into which a hole 43 has been drilled and tapped for this purpose. The choke valve 38 is settable against the pressure of a spring 41 from a first position in which its point 42 is substantially retracted from the passage 33 to another position in which is provides maximum obstruction in the passage 33. The point of maximum obstruction is defined by an end 40 on the interponent 28 which stops the screw when its shoulder 39 comes in contact with it. While such setting for the maximum obstruction may define some preferred setting for minimum admission of the mixture of fuel and air, which otherwise, and especially in view of manufacture for various, differing conditions may be provided by adjusting the cross-section (in a plane perpendicular to the section shown in FIG. 15) of the passage 33 with respect to that of the point 42, it also serves to prevent that excessive advance of the throttle valve 38 result in damage to the delicate wall section 33a. In general terms, FIG. 15 is merely illustrative of the principle of providing a throttle down stream from the site of the collision of the rich fuel mixvention in various forms and in its application to certain embodiments. However, to those skilled in the art many variations and other applications to widely differing embodiments will suggest themselves entirely within the con-- cept of the invention and without departure from its spirit and scope. All such applicaions and uses are intended to be claimed below, description and drawings being intended as mere illustrations which do not limit the invention to particular uses within the devices to which it is applied nor to the art of carburetors generally.
It will be especially obvious to the skilled in the art that elements of the invention shown as incorporated in separate parts of the arrangement might advantageously be incorporated in common parts, especially when the invention is applied to carburetors newly manufactured according to the die casting in similar methods whereby it is possible to produce complicated parts.
I claim as my invention:
1. A carburetor comprising a tubular body member, a valve pivotally mounted in said member for movement between an open position to allow maximum fluid flow therethrough and a closed position preventing fluid flow therethrough, means for admitting a stream of a rich fuel mixture through the wall of the member downstream of the valve in its closed position, a single opening through the valve for passage of a stream of fluid therethrough, said opening and admitting means being oriented to direct the envelopes of the streams into an intersecting zone removed from the wall whereby the collided streams become intermixed to atomize the fuel, a conduit secured to the member and having one end thereof adjacent the opening in the valve, another end adjacent the center area of the member, and a passage between the ends of the conduit connecting the admitting means to the conduit whereby the streams intersect in the conduit and the mixture is exhausted in the center area of the member.
2. A carburetor as defined in claim 1, wherein the conduit is an an-gulated tube, the end of the conduit adjacent the valve lying in a plane making a small divergent angle with the valve.
3. A carburetor as defined in claim 1 further including means mounting the valve and end of the conduit in sealing engagement with each other when the valve is in the closed position.
4. A carburetor as defined in claim 3 wherein the conduit is an an-gulated tube and the means for securing the tube to the member comprises a ring in the member, a tab extending from the ring, and means welding the tube to the tab.
5. A carburetor as defined in claim 3 wherein the means securing the conduit comprises a ring secured to the body and the conduit comprises an extension integral with the ring and positioned adjacent the tubular wall of the member, and sealing means sealing the admitting means and passage against escape of fluid between the wall and extension.
6. A carburetor as defined in claim 5 wherein the discharge opening is flared and makes an angle with the axis of the tubular member.
7. A carburetor as defined in claim 5 wherein the discharge opening is flared and is normal to the axis of the tubular member.
8. A canburetor as defined in claim 7 further including means in the conduit for obstructing the flow of fluid from the discharge opening.
9. A carburetor comprising a tubular body member, a valve pivotally mounted in said member for movement between an open position to allow maximum fluid flow therethrough and a closed position preventing fiuid flow therethrough, means for admitting a stream of a rich fuel mixture through the wall of the member downstream of the valve in its closed position, a single opening through the valve for passage of a stream of fluid therethrough, said opening and admitting means being oriented to direct the envelopes of the streams into an intersecting zone removed from the wall whereby the collided streams become intermixed to atomize the fuel, a lid carried by the valve for movement over the opening to vary the size thereof, and means pivotally mounting the lid on the valve and a tool slot in the lid for engagement by a tool extended through the tubular member for shifting the angular position of the lid.
10. A carburetor comprising a tubular body member, a valve pivotally mounted in said member for movement (between an open position to allow maximum fluid flow therethrough and a closed position preventing fluid flow therethrough, means for admitting a stream of a rich fuel mixture through the Wall of the member downstream of the valve in its closed position, a single opening through the valve for passage of a stream of fluid therethrough, said opening and admitting means being oriented to direct the envelopes of the streams into an intersecting zone removed from the wall whereby the collided streams become intermixed to atomize the fuel, a tube secured to 9 one surface of the valve around the opening and a lid 1,884,359 carried by the other surface of the valve for movement 1,902,603 over the opening to vary the size thereof. 2,656,167 3,201,097 References Cited 5 UNITED STATES PATENTS 329,749 1,038,040 9/1912 Weiss 261-51 1,150,108 1,691,201 11/1928 Larkin. 1,819,706 8/1931 Geiger 261-65 X 1,833,863 11/1931 Schwier.
1 0 Sturm. Wilson. 10/ 1953 Phillips.
8/ 1965 Arndt.
FOREIGN PATENTS 11/ 1920 Germany.
7/1957 France.
HARRY B. THORNTON, Primary Examiner. 0 TIM R. MILES, Assistant Examiner.
US544246A 1966-04-21 1966-04-21 Carburetor Expired - Lifetime US3410539A (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4153650A (en) * 1977-06-15 1979-05-08 Toyota Jidosha Kogyo Kabushiki Kaisha Idling fuel supplying system of a carburetor
US4241704A (en) * 1978-06-15 1980-12-30 Toyota Jidosha Kogyo Kabushiki Kaisha Intake system of an internal combustion engine
US4308837A (en) * 1978-05-22 1982-01-05 Toyota Jidosha Kogyo Kabushiki Kaisha Intake system of an internal combustion engine
US4344396A (en) * 1978-03-15 1982-08-17 Yamaha Hatsudoki Kabushiki Kaisha Induction system of multi-cylinder engine
US4377538A (en) * 1980-07-11 1983-03-22 Aisan Industry, Co., Ltd. Variable venturi type carburetor
US4768494A (en) * 1987-09-09 1988-09-06 Brunswick Corporation Idling system for multi-cylinder two-stroke engine
US5827335A (en) * 1995-11-07 1998-10-27 Pioneer/Eclipse Corporation Enhanced performance carburetor system
US20090007894A1 (en) * 2006-03-03 2009-01-08 Shinichi Wada Two-Cycle Engine

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US1038040A (en) * 1912-01-25 1912-09-10 Maxi Company Carbureter.
DE329749C (en) * 1919-03-20 1920-11-30 Philipp Lang Idle device for spray carburetor with an externally adjustable pin that fits into a section of the throttle device
US1691201A (en) * 1926-07-02 1928-11-13 Charles A Criqui Carburetor
US1819706A (en) * 1928-03-27 1931-08-18 Edward F Geiger Carburetor
US1833863A (en) * 1929-03-18 1931-11-24 Schwier William Carburetor
US1884359A (en) * 1927-03-29 1932-10-25 Bosch Robert Carburetor
US1902603A (en) * 1927-08-29 1933-03-21 Bendix Aviat Corp Automatic priming device
US2656167A (en) * 1950-02-06 1953-10-20 Tillotson Mfg Co Charge forming device
FR1150108A (en) * 1956-04-27 1958-01-08 Sibe Improvements made to fuel systems for internal combustion engines
US3201097A (en) * 1961-11-20 1965-08-17 Walbro Corp Carburetor fuel system

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US1038040A (en) * 1912-01-25 1912-09-10 Maxi Company Carbureter.
DE329749C (en) * 1919-03-20 1920-11-30 Philipp Lang Idle device for spray carburetor with an externally adjustable pin that fits into a section of the throttle device
US1691201A (en) * 1926-07-02 1928-11-13 Charles A Criqui Carburetor
US1884359A (en) * 1927-03-29 1932-10-25 Bosch Robert Carburetor
US1902603A (en) * 1927-08-29 1933-03-21 Bendix Aviat Corp Automatic priming device
US1819706A (en) * 1928-03-27 1931-08-18 Edward F Geiger Carburetor
US1833863A (en) * 1929-03-18 1931-11-24 Schwier William Carburetor
US2656167A (en) * 1950-02-06 1953-10-20 Tillotson Mfg Co Charge forming device
FR1150108A (en) * 1956-04-27 1958-01-08 Sibe Improvements made to fuel systems for internal combustion engines
US3201097A (en) * 1961-11-20 1965-08-17 Walbro Corp Carburetor fuel system

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4153650A (en) * 1977-06-15 1979-05-08 Toyota Jidosha Kogyo Kabushiki Kaisha Idling fuel supplying system of a carburetor
US4344396A (en) * 1978-03-15 1982-08-17 Yamaha Hatsudoki Kabushiki Kaisha Induction system of multi-cylinder engine
US4308837A (en) * 1978-05-22 1982-01-05 Toyota Jidosha Kogyo Kabushiki Kaisha Intake system of an internal combustion engine
US4241704A (en) * 1978-06-15 1980-12-30 Toyota Jidosha Kogyo Kabushiki Kaisha Intake system of an internal combustion engine
US4377538A (en) * 1980-07-11 1983-03-22 Aisan Industry, Co., Ltd. Variable venturi type carburetor
US4768494A (en) * 1987-09-09 1988-09-06 Brunswick Corporation Idling system for multi-cylinder two-stroke engine
US5827335A (en) * 1995-11-07 1998-10-27 Pioneer/Eclipse Corporation Enhanced performance carburetor system
US20090007894A1 (en) * 2006-03-03 2009-01-08 Shinichi Wada Two-Cycle Engine
US7658170B2 (en) * 2006-03-03 2010-02-09 Husqvarna Zenoah Co., Ltd. Two-cycle engine

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