GB2109866A - Compound carburettor for i.c. engines - Google Patents

Compound carburettor for i.c. engines Download PDF

Info

Publication number
GB2109866A
GB2109866A GB08134502A GB8134502A GB2109866A GB 2109866 A GB2109866 A GB 2109866A GB 08134502 A GB08134502 A GB 08134502A GB 8134502 A GB8134502 A GB 8134502A GB 2109866 A GB2109866 A GB 2109866A
Authority
GB
United Kingdom
Prior art keywords
running
carburettor
compound
slow
cylinders
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.)
Granted
Application number
GB08134502A
Other versions
GB2109866B (en
Inventor
Hiroshi Yokoyama
Tokuzi Ishida
Kunio Kikuchi
Kazuaki Zama
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.)
Mikuni Corp
Suzuki Motor Corp
Original Assignee
Mikuni Corp
Suzuki Motor 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 Mikuni Corp, Suzuki Motor Corp filed Critical Mikuni Corp
Priority to GB08134502A priority Critical patent/GB2109866B/en
Publication of GB2109866A publication Critical patent/GB2109866A/en
Application granted granted Critical
Publication of GB2109866B publication Critical patent/GB2109866B/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02M13/00Arrangements of two or more separate carburettors; Carburettors using more than one fuel
    • F02M13/02Separate carburettors
    • F02M13/04Separate carburettors structurally united
    • F02M13/046Separate carburettors structurally united arranged in parallel, e.g. initial and main carburettor

Abstract

The secondary carburettor bore 4 has outlet passages 4a containing a respective secondary throttle valve 6 for each engine cylinder and the primary bore 3 has a throttle valve 3 upstream of the passages for the respective cylinders. Individual transition mixture systems 7, 8, 9, 13, separately connected to the float chamber 14, have outlets 7 exposed on initial secondary throttle valve opening and are associated one with each or one with each pair of the secondary throttle valves 6. Portions of the transition mixture systems are formed by short resin pipes (10), Figures 2 to 4 (not shown), extending between the float chamber defining body 1a and the downstream end of the manifold body 1b. <IMAGE>

Description

SPECIFICATION Compound carburettor Background of the disclosure a) Field of the invention This invention relates to improvements in a compound carburettor to be used for an internal combustion engine of a plurality of cylinders.
b) Description of the prior art In a compound carburettor to be used for an engine of a plurality of cylinders, a primary air-fuel mixture passes through one throttle valve and is then distributed to be respective cylinders, a secondary air-fuel mixture is fed to the respective cylinders through secondary throttle valves arranged for the respective cylinders and a secondary slow-running fuel system for controlling the air-fuel ratio at the beginning of opening the secondary throttle valve is provided to smooth the transit from the primary side to the secondary side.However, in this type of conventional compound carburettor, generally, there have been defects that, as one secondary slow-running fuel system is distributed to the secondary throttle valves of the respective cylinders, due to the fluctuation of the opening of the secondary throttle valve for each cylinder, the fluctuation of the opening area of the secondary bypass hole, the difference in the length and bend of the secondary slow-running mixture path and the air locking phenomenon in the coarse of the secondary slow-running mixture path likely to occur at a high temperature which are all difficult to technically solve, the air-fuel ratio of the mixture for each cylinder will fluctuate in the course of the transit from the primary side to the secondary side and the transit will be no ionger smooth.Further, generally, the carburettor body is sectioned into a carburettor portion, a manifold portion and a throttle body portion and is formed by combining them. However, the above mentioned secondary slow-running fuel system or particularly the secondary slow-running mixture path is formed within these respective portions, is therefore comparatively long in the total length and can not help having many bends. Not only this will be likely to cause an air locking phenomenon when the engine temperature rises as described above but also it will increase the flow resistance to cause the delay of the transit from the primary side to the secondary side and the unstable jet of the mixture.Therefore, in order to shorten the total length of the secondary slowrunning mixture path and to decrease the bends, it has been already attempted to arrange the carburettor portion and throttle body portion in the same plane. However, there have been defects that this arrangement will not only increase the useless thickness of the component parts but also require a large space and cause a leakage due to different strains of the respective portion by heat.
Summary of the invention Therefore, a primary object of the present invention is to provide a compound carburettor for internal combustion engines wherein the transit from the primary side bore to the secondary side will be smoothly made and the air-fuel ratio of a mixture fed to each cylinder will not fluctuate.
According to the present invention, this object is attained by providing an independent secondary slow-running fuel system for one cylinder or each of two cylinders.
According to a preferred formation of the present invention, the mixture path of the secondary slow-running fuel system includes a pipe airtightly fitted between one part and the other part of the carburettor body. Thereby, the length of the mixture path of the secondary slowrunning fuel system can be made shortest and the above described problems can be solved. The pipe is fitted with an O-ring made of an elastic sealing material or has a rib formed at each end and is made preferably of such adiabatic material as a phenol resin.
Brief description of the drawings Fig. 1 is a partly sectioned plan view of an embodiment of a compound carburettor according to the present invention; Fig. 2 is a side view of the compound carburettor shown in Fig. 1; Fig. 3 is a sectional view showing an example of a pipe forming a part of a mixture path of a secondary slow-running fuel system; and Fig. 4 is a sectional view showing another example of a pipe forming a part of a mixture path of a secondary slow-running fuel system.
Description of the preferred embodiments With reference to Figs. 1 and 2, the reference numeral 1 indicates a carburettor body consisting of a carburettor portion 1 a, manifold portion 1 b and throttle body portion 1 c, 2 indicates a primary bore and 3 indicates a primary throttle valve provided on the downstream side of a venturi portion not illustrated. The primary bore 2 is branched on the downstream side of the primary throttle valve 3 and is connected to each cylinder.
The reference numeral 4 indicates a secondary bore which is branched on the downstream side of the venturi portion not illustrated and is connected to each cylinder. The reference numeral 5 indicates a secondary throttle shaft passing through each branched path 4a of the secondary bore 4 in the direction intersecting at right angles with the center line of the branched path 4a and 6 indicates a secondary throttle valve secured to the secondary throttle shaft 5 within each branched path 4a. The reference numeral 7 indicates a secondary bypass hole provided in the inner wall of each branched path 4a and 8 indicates a secondary slow-running jet connected to each secondary bypass hole 7 through each secondary slow-running mixture path 9.A pipe 10 fitted at one end to the carburettor portion 1 a and at the other end to the manifold portion 1 b is set in the course of each secondary slow-running mixture path 9, that is, between the part positioned in the carburettor portion 1 a of the path 9 and the part positioned in the manifold portion 1 b so as to make the length of the mixture path 9 shortest. By the way, in connecting such many holes, the pitch and size of the holes will be likely to fluctuate and problems will be likely to arise in the concentricity and sealability. However, in the case of this embodiment, as shown in Fig.
3, O-rings 11 made of an elastic sealing material are fitted on the outer peripheral portions at both ends of the pipe 10 so as to solve such problems.
Also, as different from it, as shown in Fig. 4, the pipe 10 itself may be molded of an elastic sealing material to have ribs 1 0a integrally formed on the outer peripheral portions at both ends. Further, if such adiabatic material as a phenol resin is used for the material of the pipe 10, the pipe will be thermally excellent. The reference numeral 12 indicates a secondary slow-running air jet connected to each secondary slow-running jet 8 and 1 3 indicates a secondary slow-running fuel path connecting each secondary slow-running air jet 12 with a float chamber 14. The part from the secondary bypass hole 7 to the secondary slowrunning fuel path 13 forms a secondary slowrunning fuel system and each secondary slowrunning jet 8 can have its size freely selected.
The operation of the above described compound carburettor shall be explained in the following.
During the operation of the engine, if a pedal not illustrated is trodden down for the acceleration, first the primary throttle valve will open and then the secondary throttle valve will open to gradually feed a large amount of a thick air-fuel mixture to each cylinder. In this case, in the course of the transit from the primary side to the secondary side1 at the beginning of opening the secondary throttle valve 6, each secondary slowrunning fuel system will act independently on each cylinder.Therefore, even if the opening of the secondary throttle valve 6 for each cylinder and the opening area of the secondary bypass hole 7 fluctuate and the length and bend of the secondary slow-running mixture path are different, by individually adjusting the size of each secondary slow-running jet 8, the fluctuation of the -air-fuel ratio for each cylinder in the coarse of the above mentioned transit will be able to be reduced. Further, as the secondary slow-running fuel systems for the respective cylinders are independent so as not to interfere with each other, the size of the secondary slow-running jet 8 for each cylinder can be freely selected and, as a result, the air-fuel ratio for each cylinder in the course of the above mentioned transit can be made optimum by taking the thermal factors and vibration conditions into consideration.From the above, according to the compound carburettor of the present invention, the transit from the primary side to the secondary side can be made very smooth. Further, the length of the secondary slow-running mixture path 9 is so short that substantially no air locking phenomenon will be generated by the temperature rise or the like.
Therefore, the total volume of the secondary slow-running fuel systems can be made so small and the number of bends of the secondary slowrunning mixture path 9 can be made so few that the passage resistance will reduce, the transit delay and unstable jetting of the mixture will be eliminated and, as a result, the response characteristic will improve. Further, as the secondary slow-running mixture path 9 is connected through the pipe 10 in the course, the freedom of the equipment will increase.
In the above mentioned embodiment, the secondary slow-running fuel systems are provided independently for the respective cylinders.
However, even if one secondary slow-running fuel system is provided independently for two cylinders so as to serve the two cylinders, the same effect will be able to be obtained. This formation is very advantageous to the cost.

Claims (8)

Claims
1. A compound carburettor comprising a primary bore provided therein with a primary throttle valve and branched in the downstream part of said primary throttle valve to be respectively connected to a plurality of cylinders of an engine to be used, a secondary bore arranged adjacently to said primary bore and branched in the downstream part to be respectively connected to said plurality of cylinders through secondary throttle valves arranged respectively for said plurality of cylinders, and a plurality of secondary slowrunning fuel systems set respectively independently for said plurality of cylinders and cooperating respectively with said respective secondary throttle valves.
2. A compound carburettor comprising a primary bore provided therein with a primary throttle valve and branched in the downstream part of said primary throttle valve to be respectively connected to a plurality of cylinders of an engine to be used, a secondary bore arranged adjacently to said primary bore and branched in the downstream part to be respectively connected to said plurality of cylinder though secondary throttle valves arranged respectively connected to said plurality of cylinders through secondary throttle valves arranged set respectively independently for a pair of cylinders among said plurality of cylinders and cooperating respectively with said respective secondary throttle valves.
3. A compound carburettor according to claim 1 or 2 wherein said secondary slow-running fuel system comprises a secondary slow-running fuel path, a secondary slow-running jet set in said secondary slow-running fuel path, a secondary slow-running air jet set in connection with said secondary slow-running jet, and a secondary slow-running mixture path communicating with said secondary slow-running jet and secondary slow-running air jet and opened within said cylinder adjacently to said secondary throttle valve.
4. A compound carburettor according to claim 3 wherein said secondary slow-running mixture path includes a pipe airtightly fitted at one end to one part of the carburettor body and at the other end to the other part.
5. A compound carburettor according to claim 4 wherein said pipe includes O-rings made of an elastic sealing material and fitted respectively to both ends.
6. A compound carburettor according to claim 4 wherein said pipe is made of an elastic sealing material and has ribs respectively at both ends.
7. A compound carburettor according to claim 4 wherein said pipe is made of an adiabatic material.
8. A compound carburettor substantially as herein described with reference to the accompanying drawings.
GB08134502A 1981-11-16 1981-11-16 Compound carburettor for i c engines Expired GB2109866B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08134502A GB2109866B (en) 1981-11-16 1981-11-16 Compound carburettor for i c engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08134502A GB2109866B (en) 1981-11-16 1981-11-16 Compound carburettor for i c engines

Publications (2)

Publication Number Publication Date
GB2109866A true GB2109866A (en) 1983-06-08
GB2109866B GB2109866B (en) 1985-04-03

Family

ID=10525919

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08134502A Expired GB2109866B (en) 1981-11-16 1981-11-16 Compound carburettor for i c engines

Country Status (1)

Country Link
GB (1) GB2109866B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2517371A1 (en) * 1981-11-30 1983-06-03 Suzuki Motor Co Compound carburettor for IC engine - has independent secondary slow-running fuel system for each cylinder

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2517371A1 (en) * 1981-11-30 1983-06-03 Suzuki Motor Co Compound carburettor for IC engine - has independent secondary slow-running fuel system for each cylinder

Also Published As

Publication number Publication date
GB2109866B (en) 1985-04-03

Similar Documents

Publication Publication Date Title
US4411226A (en) Intake system for an internal combustion engine
US4492207A (en) Dual fuel system
GB2073316A (en) Fuel injection installation for preventing vapour lock
EP0281771B1 (en) Temperature compensated fluid flow metering system
US5341772A (en) Intake manifold for an internal combustion engine having a cylinder head
US4476838A (en) Exhaust gas suppressor
GB2054786A (en) Preventing access to adjuster screws
US4702209A (en) Device for adjusting the idling rpm
US4379096A (en) Compound carburetor
US1933380A (en) Carburetor
US3684257A (en) Carburetters
CA1145214A (en) Fuel enrichment apparatus for gaseous fuel mixers
US4064850A (en) Internal combustion engine with main and auxiliary combustion chambers
US4191140A (en) Induction flow guide device for internal combustion engine intake manifold
US3809032A (en) Internal combustion engine manifold
GB2109866A (en) Compound carburettor for i.c. engines
US3235237A (en) De-popper valve
US2827269A (en) Idle control system
CA1166099A (en) Compound carburetor
US5076218A (en) Constant velocity intake manifold
CA1299350C (en) Method of making a carburetor
US3903211A (en) Control mechanism and method for dual carburetors
US4038950A (en) Intake manifold of the internal combustion engine
EP0096842B2 (en) Fuel injector body assembly
JPS629743B2 (en)

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19941116