CA1047860A - Fuel induction system - Google Patents

Fuel induction system

Info

Publication number
CA1047860A
CA1047860A CA272,421A CA272421A CA1047860A CA 1047860 A CA1047860 A CA 1047860A CA 272421 A CA272421 A CA 272421A CA 1047860 A CA1047860 A CA 1047860A
Authority
CA
Canada
Prior art keywords
engine
wall
container
fuel
passage means
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
Application number
CA272,421A
Other languages
French (fr)
Inventor
Frederick J. Marsee
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Ethyl Corp
Original Assignee
Ethyl Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Ethyl Corp filed Critical Ethyl Corp
Priority to CA272,421A priority Critical patent/CA1047860A/en
Application granted granted Critical
Publication of CA1047860A publication Critical patent/CA1047860A/en
Expired legal-status Critical Current

Links

Landscapes

  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)

Abstract

FUEL INDUCTION SYSTEM
ABSTRACT OF THE DISCLOSURE
This invention relates to an improvement in the induction system of an internal combustion engine. More particularly, the invention comprises an improved com-bination with or addition to an induction system wherein the primary barrel of a carburetor releases a fuel-air mixture to an intermediate conditioning chamber, which in turn is connected to deliver the conditioned fuel-air mixture to the usual intake passage or manifold.

Of recent years there has been a trend toward operating spark-ignited internal combustion engines at leaner air/fuel ratios in order to decrease the amount of hydrocarbon and carbon monoxide in the exhaust. One limiting factor in going towards leaner operation is gasoline maldistribution from cylinder-to-cylinder. The induced air/fuel ratio must be kept lean enough such that the cylinder supplied with the leanest mixture will still fire, otherwise exhaust hydrocarbon and carbon monoxide emission will increase rather than decrease.

In our earlier Canadian applications Serial No.
218,950 and Serial No. 218,951, we have described fuel in-duction systems for and in combination with multicylinder engines in which fuel maldistribution is substantially lowered. In said system a container is provided in the exhaust gas flow path. The carburetor barrel, or venturi, delivers an air/fuel mixture directly into this container in which it is heated and subjected to great turbulence forming a uniform air/fuel mixture. This uniform air/
fuel mixture is then conducted into the intake manifold and thence into the individual cylinders.

Description

¦ Significant reductions in exhaust hydrocarbon and carbon monoxide are obtained using the above-described turbulent ¦ flow system. According to the present invention, still further ¦ improvement in overall performance is achieved by installing ¦ a liquid trap on -the inside wall of the conduit leading from ¦ the primary carburetor barrel, or barrels, into the container.
¦ During cold start of the engine liquid gasoline tends to ~mpinge ¦ on the inside surface of the carburetor barrel and drain down .
. ¦ in-to the container, which impedes engine start. The trap ¦ provided by the present invention collects this liquid ¦ gasoline before it reaches the container and conducts it ¦ directly into the intake manifold, thus allowing this small ¦ amount of liquid to by-pass the container. After start-up, ¦ substantially all of the air/fuel mixture still passes into the ¦ turbulent mixing container prior to entering the intake manifold ¦

I DESCRIPTION OF THE DRAWINGS
I ., .
¦ Figure 1 is a schematic cross-section of the inYention ¦ installed in an in-line engine.
. ¦ Figure 2 is a cross-section taken at AA of Figure 1.
¦ Flgure 3 is a schematic cross-section of the invention ¦ installed in a V-type engine.
_ ¦ Figure 4 is a cross-section of an induction system ¦ of this invention using liQuid engine coolant to heat the ¦ container. `

l DESCRIPTION OF THE PREFERRED EMBODIMENTS
¦ . A preferred embodiment of this invention is a spark-ignited multicylinder internal combustion engine having improved cylinder-to-cylinder fuel distribution and cold starting ability, said engine comprising means for atomizing gaSotine . #

- .,~ , , , , , -: , , ~ 1047860 ¦¦ ~ o a carburetor barrel, ln~ake p~s6aee means for delivering ¦
air/fuel mixture to each of said multicylinders, an enclosed container having an inlet and an outlet, first passage means connecting said carburetor barrel to said inlet, second passage means connecting said outlet to said intake passage means, liquid fuel trap means inside said first passage means adapted to trap liquid fuel running down the inside wall of said first .
passage means, said first passage means having at least one small opening in said inside wall, said small opening forming a passage from said trap means into said intake passage means whereby liquid fuel passes directly from said trap means into said intake passage means by-passing said container. Pre~erably means are provided to heat the container.
Referring to the embodiment shown in Figure 1, the system comprises carburetor 1 having a primary barrel 2 and secondary barrel 3. Air/fuel mixtures ~re formed in the car-buretor by primary venturi 4 and secondary venturi 5. Throt-tle ~alve 6 controls the volume of air/fuel mixture flowing through . the primary barrel, and secondary throttle valve 7 controls the volume of air/fuel mixture flowing thraugh the secondary barrel.
. Exhaust gas leaving exhaust port 10 of engine 11 flows through exhaust manifold 12 into unit 13 having a main exhaust passage 14 and a by-pass exhaust passage 15. Valve 16 controls the flow of hot engine exhaust. Exhaust leaves unit 13 through exhaust pipe 17. :
Located inside exhaust passage 14 is container 20 which has inlet 21 and outlet 22. First conduit 23 connects primary barrel 2 to inlet 21. Secondary conduit 24 connects outlet 22 to intake manifold 25 which forms a passage to the intake port 26 of each cylinder.
,, . ,.
. 4 - - ~ , -Located inside first conduit 23 is tubular member 30 which is spaccd apart (appx. 2 to 5 mm) from the inside wail of first conduit 23 and is sealably engaged to the inside wall by bottom closure ring 31 forming an annular reservoir 32 betwee tubular member 30 and the inside wall of first conduit 23.
Located around the circumference of first conduit 23 are a series of small openings 33 (appx. 3 to 8 mm dia. or
2 x 6 mm slots) proximate to the bottom of reservoir 32 which form a passage into inta~e manifold 25.
In operation, starting with a cold engine, cranking the engine initially causes liquid gasoline to run into primary barrel 2 at about a 1:1 air/fuel ratio. Much of this initial gasoline is deflected by throttle valve 6 against the side wall of the primary barrel. This liquid flows down the inside wall of first conduit 23 and into reservoir 32. From here, it is lnducted directly into intake manifold 25 through openings 33 and thence to the intake port of each cylinder, allowing the engine to start rapidly under cold operating conditions.
Once the engine starts, the ~olume of air inducted through primary barrel 2 increases sharply causing better atomization and increased velocity and turbulence of air/fuel mixture flowing through the primary barrel and consequently very little of the atomized gasoline forms a liquid film on the irJside wall of first conduit 23. Under these operating conditio s substantially all of the air/fuel mixture now passes through flrst conduit 23 and inlet 21 into container 20 wherein extreme turbulence forms a uniform air/fuel mixture. This resultant air/fuel mixture flows thraugh outlet 22 and second conduit 24 into intake manifold 25 and thence to the intake port 26 of each of the multicylinders. -..

Another factor contributing to,the uniformity of the air/fuel mixture formed in container 20 is the length of first conduit 23. This conduit has a length of about 2'to 5 times its diameter~ which provides a longer than normal flow path for the primary air/fuel mixture and affords more opportunity for the mix-ture to form a uniform mixture than in a conventional induction system. .
Under high load, secondary throttle valve I opens inducting a secondary air/fuel mixture through secondary barrel 3 directly into intake manifold 25 at a location about opposite the location at which secondary conduit 24 opens into intake manifold 25. This feature is quite important because any air leaking past valve 7 during idle or low load operation is uniformly mixed with all of the primary air/fuel mix-ture prior to being distributed to each of the multicylinders, thus providing a uniform air/fuel ratio during idle and low load operating conditions.
Figure 3 shows the improved induction system installed in a V-type engine. Carburetor 40 has a primary barrel 41 including venturi 42 and throttle valve 43. Exhaust cross-over 44 connects an exhaust port 45 on one bank of cylinders with an . exhaust port 46 on the other bank of cylinders. The one bank of cylinders exhausts through exhaust manifold 47. The other ~ank of cylinders exhausts through exhaust manifold 48. Exhaust control valve 49 controls the relative proportion of exhaust flow through exhaust pipe 50 and exhaust cross-over'44. ' Mounted within exhaust cross-over 44 is container 51 .
having inlet 52 and outlets 53 and 54. The intake manifold is comprised of intake runners 55 and 56. Runner 55 supplies . 6 -, . . ~;

1 1047860 .
¦ air/fuel mixture to one-half of the multicylinders and runner 56 ¦ supplies the other half of the multicylinders in a conventional ¦ manner.
¦ First conduit 57 forms an elongated passage from ¦ primary barrel 42 into container 51. Secondary conduit 58 forms ¦ a passage from the outlet 53 of container 51 into runner 55.
¦ Secondary conduit 59 forms a passage from the outlet 54 of ¦ container 51 into.runner 56.
¦ Located inside first conduit 57 is a liquid trap ¦ formed by concentric tubular member 60 spaced a small distance ¦ (appx. 2 to 5 mm) fr~m the inside wall of conduit 57. The ¦ bottom of member 60 is sealed to the inside wall of fir~t ¦ conduit 57 by bottom closure ring 61 forming annular reservoir ¦ 62. A series of small openings (appx. 3 ta 8 mm dia. or 2 x 6 ¦ mm slots) in the side waIl of first conduit 57 at the bottom of ¦ reservoir 62 form a passage to runner 55 (openings 65) and with ¦ runner 56 (openings 66).
¦ In operation, starting with a cold engine, cranking ¦ the engine inducts air an~ liquid gasoline into primary barrel 2~ ¦ 41. Throttle valve 4~ deflects much of the gasoline against ¦ the side wall of primary barrel 41 and first conduit 57. The ¦ liquid gasoline runs down the inside wall of first conduit 57 ¦ into reservoir 62 and is inducted directly into intake runners 55 and 56 through openin~s 65 and 66 causing rapid firing of the engine.
Once the engine starts, the volume of air induc-ted through primary barrel 41 increases sharply forming a large volume of primary air/fuel mixture which is now inducted directly through first conduit 57 and inlet 52 into container 51. The ' .
.

7 .

, . , , , . . ~ , .
.

primary air/fuel mixture encounters extreme turbulence in passing through first conduit 57 and container 51 forming a uniform primary air/fuel mixture.
Part of this mixture passes through outlet 53 and second conduit 58 into intake runners 55. Another part of this uniform mixture passes through outlet 54 and secondary conduit 5~
into intake runner 56. Intake runners 55 and 56 then supply .
the multicylinders with a uniform primary air/fuel mixture.
While the engine is cold, exhaust control valve 49 is closed forcing exhaust from the left bank of cylinders to flow through exhaust cross-o-ver 44 to be exhausted through exhaust mani~old 48. . This provides heat to the surface of container 51 which further improves engine performance. Once _ the engine attains operating temperature exhaust control valve 49 opens allowing exhaust from the left cylinder bank to exit through exhaust pipe 50.
Figure 4 shows the turbulent flow system using liquid engine coolant to heat the container. It includes primary . barrel 70, choke valve 71, throttle valve 72, first conduit 73, - 20 liquid trap 74, opening 75 in the side wall of first conduit 73, container 76 having inlet 77 and outlet 78, second conduit 79, . and intake manifold 80. Secondary barrel 81 connects to intake manifold 80 at a location opposite the place where secondary conduit 79 connects. Jacket 82 surrounds part of container 76 and is connected to the liquid cooling system of the engine (not shown) such that hot liquid coolant circulates through ~acket 82. , Operation is the same as in the previously-described embodiments. During the cranking period liquid gasoline runs 10478bO
down the side of first passage 73 and collects in the reservoir of liquid trap 74. From here, it is inducted di~ctly into intakc manifold 80 through openings 75. After the engine starts, the atomized primary air/fuel mixture passes through container 76 and then into the intake manifold 80.
Improved engine operation is achieved even without heating the contalner. Preferably, the container is heated.
Hot exhaust gas and liquid engine coolant have been shown.
Other equivalent heating means can be used, such as electrical resistance heaters.
The liquid trap~ in the first conduit can be any structure that will trap liquid gasoline running down the side wall of the first conduit to prevent it from running into the container. Any barrier extending inwardly from the side wall and having liquid retention means can be used. For example, any inwardly extending flange around the circumference of the first conduit will work as long as the inner diameter of the flange has a raised barrier or is higher than the outer diameter of the flange.
Engines fitted with the turbulent flow system as described herein when properly ad~usted attain hydrocarbon and carbon monoxide exhaust levels which satisfy the 1975 for-ty-nine state Federal standards while operating on a commercial leaded gasoline. ~
. . ' '' .
. . . , . .

Claims (9)

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A spark-ignited multicylinder internal combustion engine having improved cylinder-to-cylinder fuel distribution and cold starting ability, said engine comprising means for atomizing gasoline into a carburetor barrel, intake passage means for delivering air/fuel mixture to each of said multi-cylinders, an enclosed container having an inlet and an outlet, first passage means connecting said carburetor barrel to said inlet, second passage means connecting said outlet to said intake passage means, liquid fuel trap means inside said first passage means adapted to trap liquid fuel running down the inside wall of said first passage means, said first passage means having at least one small opening in said inside wall, said small opening forming a passage from said trap means into said intake passage means whereby liquid fuel passes directly, without passing through heating means, from said trap means into said intake passage means by-passing said container.
2. An engine of Claim 1 further characterized by including means for heating said container.
3. An engine of Claim 2 wherein said heating means comprises a jacket around said container and means for circu-lating hot liquid engine coolant through said jacket.
4. An engine of Claim 2 wherein said heating means comprises an exhaust passage means, said container being in heat exchange contact with exhaust gas passing through said exhaust passage.
5. An engine of Claim 2 wherein said trap means comprises a wall inside said first passage means spaced apart from said inside wall of said first passage means, said wall and said side wall forming a reservoir which is open at the top to receive and trap liquid fuel running down said inside wall and closed at the bottom to prevent liquid fuel from draining into said container, said small opening in said inside wall being located proximate to the bottom of said reservoir.
6. An engine of Claim 3 wherein said trap means comprises a wall inside said first passage means spaced apart from said inside wall of said first passage means, said wall and said side wall forming a reservoir which is open at the top to receive and trap liquid fuel running down said inside wall and closed at the bottom to prevent liquid fuel from draining into said container, said small opening in said inside wall being located proximate to the bottom of said reservoir.
7. An engine of Claim 4 wherein said trap means comprises a wall inside said first passage means spaced apart from said inside wall of said first passage means, said wall and said side wall forming a reservoir which is open at the top to receive and trap liquid fuel running down said inside wall and closed at the bottom to prevent liquid fuel from draining into said container, said small opening in said inside wall being located proximate to the bottom of said reservoir.
8. An engine of Claim 7 wherein said reservoir is formed by a cylindrical wall concentric with said first passage means and spaced apart from said inside wall and a bottom closure between said cylindrical wall and said inside wall forming an annular reservoir.
9. An engine of Claim 8 having a plurality of said small openings in said inside wall proximate to the bottom of said reservoir.
CA272,421A 1977-02-23 1977-02-23 Fuel induction system Expired CA1047860A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA272,421A CA1047860A (en) 1977-02-23 1977-02-23 Fuel induction system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA272,421A CA1047860A (en) 1977-02-23 1977-02-23 Fuel induction system

Publications (1)

Publication Number Publication Date
CA1047860A true CA1047860A (en) 1979-02-06

Family

ID=4108001

Family Applications (1)

Application Number Title Priority Date Filing Date
CA272,421A Expired CA1047860A (en) 1977-02-23 1977-02-23 Fuel induction system

Country Status (1)

Country Link
CA (1) CA1047860A (en)

Similar Documents

Publication Publication Date Title
US4257384A (en) Intake control apparatus of engine
US3444846A (en) Engine exhaust recirculation
US4167166A (en) Hot air vaporization system for an internal combustion engine
US4276864A (en) Fuel-vaporizing system for internal-combustion engine and method of operating same
US6067971A (en) Heated assembly for vaporization of fuel in an internal combustion engine
JPS5813748B2 (en) fuel supply device
US4510913A (en) Vaporizing fuel system for internal combustion engine
US4016845A (en) Fuel induction system
US3972324A (en) Fuel induction system
US4188928A (en) Fuel vaporizing apparatus for internal combustion engines
CA1047860A (en) Fuel induction system
US3580232A (en) Engine exhaust recirculation
US3587541A (en) Engine exhaust recirculation
US3626913A (en) Exhaust velocity control of exhaust recycling
US4086892A (en) Fuel induction system
US4479470A (en) Intake passage structure for internal combustion engines
JPH0343464B2 (en)
US4355622A (en) Air/fuel mixture heating device for internal combustion engine
US3996907A (en) Fuel induction system
EP0012533A1 (en) System for increasing the temperature of an air/fuel mixture delivered to an internal combustion engine
GB1423098A (en) Fuel vapourizer for an internal combustion engine
US3971352A (en) Fuel induction system
GB1432916A (en) Internal combustion engine intake manifold
US20050022783A1 (en) Fuel supply system for internal combustion engine
US4478198A (en) Fuel treating apparatus for internal combustion engines