US3072113A - Fuel feed device for explosion engines - Google Patents
Fuel feed device for explosion engines Download PDFInfo
- Publication number
- US3072113A US3072113A US72111A US7211160A US3072113A US 3072113 A US3072113 A US 3072113A US 72111 A US72111 A US 72111A US 7211160 A US7211160 A US 7211160A US 3072113 A US3072113 A US 3072113A
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- fuel
- tube
- feed device
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- chamber
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
Definitions
- An auxiliary device is used in this case for the starting and the idling speed of the engine and both feed devices are connected in parallel with a single feed manifold.
- An injection device enables the fuel to be injected into the vaporization chamber of the main feed device by means of a pump of the cylinder and piston type.
- the object of the present application is to provide modications and improvements for this device, said rnodications and improvements aiming more particularly at enabling the main feed device to be used when the engine is being run at idling speed, the auxiliary device being only employed for the starting of the engine.
- the auxiliary feed device is provided with a carburetor of conventional design including a conventional lioat chamber supplying in the usual fashion the normal jet and the idling jet and which also supplies a well feeding in turn the vaporization chamber of the main device.
- the auxiliary feed device merely comprises an auxiliary self-starting carburetor of small capacity and of a generally known type currently used for the starting of engines.
- the vaporization chamber of the main feed device is comprised by a coil tube located inside a heating chamber, said coil tube being fed by a pulsatingdiaphragm pump of conventional design, said coil tube ending by a tubular member extending into the engine air suction pipe, upstream of the throttle disc.
- FIG. l is a perspective View of an illustrative embodiment of an explosion engine provided with the improved feed device, in accordance with the invention.
- FIG. 2 is a diagrammatic showing of this device.
- FIG. 3 is a sectional view of a detail showing an alternative embodiment of one part of the invention.
- the invention is applied to an explosion engine of the fourcylinder type, including a suction tube 1, an inlet conduit 1a and a gas-exhaust manifold 2, said engine being fed by a pulsating-diaphragm pump 3 of a known construction and communicating through a pipe 4 with the fuel tank (not shown).
- This pump discharges fuel under pressure into a line 5 which is subdivided in two branches 5a and 5b adapted to feed the main feed device 6 and the auxiliary starting device 7, respectively.
- the latter device is mounted on the auxiliary self-starting carburetor 5i which may be of any well-known device including an outer lever Sa for controlling said auxiliary carburetor, and having an air inlet 8b and an air-fuel mixture outlet 8c.
- the main feed device 6 comprises a chamber 9 (FIG. 2) interposed on the hot-gas exhaust manifold 2, said chamber being preferably heat-insulated by means of an insulating wall 1G.
- a coil tube 11 surrounding a hollow body member 9a secured along the axis of hot-gas stream and adapted to promote the heat radiation on the tube coil.
- This tube coil 11 is connected through a preferably-insulated conduit 1?. with a tubular member 13 housed within the air-induction duct 1, and extending substantially into the axis of the neck portion of the venturi 2b, 1b thereof upstream of the throttle disc 14.
- the latter is connected through a double lever 1S, on the one hand, with a linkage 16 controllable by the accelerator pedal 17 (FIG. 1) and, on the other hand, by a linkage 18 with a control means 19 for the liquid-fuel input into the coil tube 11.
- the conduit 17 includes a by-pass provided with a tube 21 extending into the inlet circuit 1 downstream of the throttle disc, this tube or nozzle 21 acting thus as an idling jet which, as will be seen, is further fed from the main feed device 6.
- the control means 19 of liquid-fuel admission into the tube coil comprises a hollow body 22 connected, on the one hand, at 23 on the fuel inter conduit 5a and, on the other hand, at 2d on the end of the tube coil.
- An insulating sleeve 25 is interposed between the tube coil and the hollow body 22 to prevent heat convection therebetween.
- the fuel arrives into an inner recess 26 communicating with the inner duct of the tube coil 11, and said communication is regulated by a needle valve 27 controlling the cross-sectional opening of a calibrated port 28, said needle valve being slidable in the block Z2 and being connected at 29, by the end thereof exterior of this block, with a bell-crank lever 313 pivotable at 31 and pivotally connected at 32 with the linkage 1S.
- the branch line 5b of the conduit S extends into a chamber 33 of the auxiliary device 7, a conduit 39 establishing a communication between this chamber and the auxiliary self-starting carburetor d.
- This self-starting carburetor S may be of any known design and is adapted to provide communication between the chamber 33 with the inner space of the inlet conduit 1a downstream of the throttle 14, said communication being effected through a pipe 34 where the auxiliary self-starting carburetor is controlled through its arm Sa, which arm is connected in a known manner through a rod 35 to any type of manual control member, such as a pull-button 36 (FEiG. 1).
- a needle valve or any other plugging member 37 to control the opening or the closing of a calibrated orifice 21S which, through a conduit 39, establishes communication between the charnber 33 and the instant-starting carburetor, which carburetor upon being actuated, brings into direct communication said conduit 3% with the conduit 3d.
- the needle valve is pivotally connected with a lever itl pivotable at 41 and whose end 42 is articulated on a rod 43 which is in turn pivotally mounted on the arm 8a of the carburetor 8.
- the improved device disciosed in the present addition is operated as follows:
- This tube coil is further heated by the radiating heat from the wall of chamber 9 and from the hollow body 9a.
- This fuel which is by then vaporized, is induced by the tube 1 (arrow Fd) and flows into the duct where it is mixed with air arriving in the direction iid', the inlet aoc/arie being regulated by the throttle as known per se, by means of the rod lo which is operated by the accelerator pedal simultaneously with the rod ld, whereby the supply into the coil tube ll and the gaseous fuel input to the tube i3 are always eiiected simultaneously.
- the main feed device cannot be used for the self-starting since the chamber 9 is at ambient temperature.
- the starting is eilected by means of the auxiliary device 7 which is fed under the pressure supplied by the diaphragm pump 3, which pressure is sui- .cient for the fuel to be injected into the conduit 39 when the auxiliary self-starting carburetor S is operated, whereupon the rotation of the arm 3a and hence of the lever it? causes the needle valve 37 to open.
- the liquid fuel is iniected through the auxiliary carburetor by the tube 34 into the iniection conduit, as shown by the arrow F6.
- the arm 8a may be returned to its normal operative position and the engine is running under normal conditions being fed from the device 6.
- the flow-rate control member which is embodied in FIG. 2 by the needle valve 27, can be of a dierent type, such as for example a spool with'a variable section port.
- FIG. 3 is shown a specific alternative embodiment wherein the control inember is comprised by a spool l5 consisting of a rod having a groove lli-6 formed therein, whose cross-section is increasing such that a rightwardly shift of the rod 45 gradually increases the cross-sectional passage of the liquid fuel (arrow F7) towards the tube coil l1 (arrow F8).
- a running carburetor for running an explosion engine at normal speeds and idling speed comprising: a vaporization chamber adapted to be so mounted on the engine as to be traversed bythe ilow of the exhaust gases of said engine, a coil tube in said chamber, axed heat-radiating body surrounded byY the coils of said coil tube in said vaporization chamber, and tube connecting means for connecting said coil tube to a fuel feed conduit and to a vapor feed conduit.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of The Air-Fuel Ratio Of Carburetors (AREA)
Description
M. CHAMP FUEL FEED DEVICE FOR EXPLOSION ENGINES 2 Sheets-Sheet l Jan. 8, 1963 Filed NOV. 28, 1960 Jan. 8, 1963 M. CHAMP FUEL FEED DEVICE EOE EXPLOSION ENGINES 2 Sheets-Sheet 2 Filed NOV. 28, 1960 I. 'll
MAQCEE Cmq/np rraQA/fys @fpm Jene enemies aan. e, rees 3,072,113 i FUEL FEED DEVICE FR EXPLSEN ENGENES Marcel Champ, Route de Tinchebray, Vire, Calvados, France Filed Nov. 28, 1966, Ser. No. 72,111 Claims priority, appiication France dan. 2t), 1960 1 Claim. (Cl. 12S-133) In the U.S.A. patent SN. 702,130 of December 1l, 1957, now Patent No. 2,895,462, granted July 21, 1959, there is disclosed an improved feed device for an explosion engine allowing a considerable fuel economy, said device comprising in particular a main feed device of the fuel prevaporization type by the heat of the exhaust gas, for operation at normal running speeds of the engine.
An auxiliary device is used in this case for the starting and the idling speed of the engine and both feed devices are connected in parallel with a single feed manifold. An injection device enables the fuel to be injected into the vaporization chamber of the main feed device by means of a pump of the cylinder and piston type.
The object of the present application is to provide modications and improvements for this device, said rnodications and improvements aiming more particularly at enabling the main feed device to be used when the engine is being run at idling speed, the auxiliary device being only employed for the starting of the engine. In the known device, the auxiliary feed device is provided with a carburetor of conventional design including a conventional lioat chamber supplying in the usual fashion the normal jet and the idling jet and which also supplies a well feeding in turn the vaporization chamber of the main device.
ln the device designed in accordance with the present invention, the auxiliary feed device merely comprises an auxiliary self-starting carburetor of small capacity and of a generally known type currently used for the starting of engines. The vaporization chamber of the main feed device is comprised by a coil tube located inside a heating chamber, said coil tube being fed by a pulsatingdiaphragm pump of conventional design, said coil tube ending by a tubular member extending into the engine air suction pipe, upstream of the throttle disc.
Further features of the invention will become apparent from the ensuing description when read in connection with the accompanying drawings, in which:
FIG. l is a perspective View of an illustrative embodiment of an explosion engine provided with the improved feed device, in accordance with the invention;
FIG. 2 is a diagrammatic showing of this device; and
FIG. 3 is a sectional view of a detail showing an alternative embodiment of one part of the invention.
The illustrative embodiment shown in FIG. 1, the invention is applied to an explosion engine of the fourcylinder type, including a suction tube 1, an inlet conduit 1a and a gas-exhaust manifold 2, said engine being fed by a pulsating-diaphragm pump 3 of a known construction and communicating through a pipe 4 with the fuel tank (not shown). This pump discharges fuel under pressure into a line 5 which is subdivided in two branches 5a and 5b adapted to feed the main feed device 6 and the auxiliary starting device 7, respectively. The latter device is mounted on the auxiliary self-starting carburetor 5i which may be of any well-known device including an outer lever Sa for controlling said auxiliary carburetor, and having an air inlet 8b and an air-fuel mixture outlet 8c.
` The main feed device 6 comprises a chamber 9 (FIG. 2) interposed on the hot-gas exhaust manifold 2, said chamber being preferably heat-insulated by means of an insulating wall 1G. Within this chamber is located a coil tube 11 surrounding a hollow body member 9a secured along the axis of hot-gas stream and adapted to promote the heat radiation on the tube coil. This tube coil 11 is connected through a preferably-insulated conduit 1?. with a tubular member 13 housed within the air-induction duct 1, and extending substantially into the axis of the neck portion of the venturi 2b, 1b thereof upstream of the throttle disc 14. The latter is connected through a double lever 1S, on the one hand, with a linkage 16 controllable by the accelerator pedal 17 (FIG. 1) and, on the other hand, by a linkage 18 with a control means 19 for the liquid-fuel input into the coil tube 11.
The conduit 17; includes a by-pass provided with a tube 21 extending into the inlet circuit 1 downstream of the throttle disc, this tube or nozzle 21 acting thus as an idling jet which, as will be seen, is further fed from the main feed device 6.
The control means 19 of liquid-fuel admission into the tube coil comprises a hollow body 22 connected, on the one hand, at 23 on the fuel inter conduit 5a and, on the other hand, at 2d on the end of the tube coil. An insulating sleeve 25 is interposed between the tube coil and the hollow body 22 to prevent heat convection therebetween.
The fuel arrives into an inner recess 26 communicating with the inner duct of the tube coil 11, and said communication is regulated by a needle valve 27 controlling the cross-sectional opening of a calibrated port 28, said needle valve being slidable in the block Z2 and being connected at 29, by the end thereof exterior of this block, with a bell-crank lever 313 pivotable at 31 and pivotally connected at 32 with the linkage 1S.
The branch line 5b of the conduit S extends into a chamber 33 of the auxiliary device 7, a conduit 39 establishing a communication between this chamber and the auxiliary self-starting carburetor d. This self-starting carburetor S may be of any known design and is adapted to provide communication between the chamber 33 with the inner space of the inlet conduit 1a downstream of the throttle 14, said communication being effected through a pipe 34 where the auxiliary self-starting carburetor is controlled through its arm Sa, which arm is connected in a known manner through a rod 35 to any type of manual control member, such as a pull-button 36 (FEiG. 1).
To this end, provision is made of a needle valve or any other plugging member 37 to control the opening or the closing of a calibrated orifice 21S which, through a conduit 39, establishes communication between the charnber 33 and the seit-starting carburetor, which carburetor upon being actuated, brings into direct communication said conduit 3% with the conduit 3d.
lt will be obviously required that the opening of the port 38 and the operation of the self-starting carburetor take place simultaneousiy and7 to this end, the needle valve is pivotally connected with a lever itl pivotable at 41 and whose end 42 is articulated on a rod 43 which is in turn pivotally mounted on the arm 8a of the carburetor 8.
The improved device disciosed in the present addition is operated as follows:
Under normal running conditions, the liquid fuel arriving (F113. 2) in the direction shown by the arrow F1 (FiG. 2) into the conduit S, is fed through the branch 5e to the chamber and, should the needle vulve be operated by means of the accelerator pedal fuel penetrates into the tube coil 11, which coil is heated by corning into the Contact with hot gasses which flow through the exhaust duct in the direction of arrows F2 and 1:3. This tube coil is further heated by the radiating heat from the wall of chamber 9 and from the hollow body 9a. This fuel which is by then vaporized, is induced by the tube 1 (arrow Fd) and flows into the duct where it is mixed with air arriving in the direction iid', the inlet aoc/arie being regulated by the throttle as known per se, by means of the rod lo which is operated by the accelerator pedal simultaneously with the rod ld, whereby the supply into the coil tube ll and the gaseous fuel input to the tube i3 are always eiiected simultaneously.
With the engine idling and the throttle closed, the sole supply is effected through the idling jet 2l. lt is shown by experience that the use of gaseous fuel for feeding he engine during Slow-speed running ollers the advantage of eliminating the evolution of fumes and of unpleasant and noxious smells which are inherent to conventional internal combustion engines, when passing from normal to idling speed.
It will be clear that the main feed device cannot be used for the self-starting since the chamber 9 is at ambient temperature. The starting is eilected by means of the auxiliary device 7 which is fed under the pressure supplied by the diaphragm pump 3, which pressure is sui- .cient for the fuel to be injected into the conduit 39 when the auxiliary self-starting carburetor S is operated, whereupon the rotation of the arm 3a and hence of the lever it? causes the needle valve 37 to open. The liquid fuel is iniected through the auxiliary carburetor by the tube 34 into the iniection conduit, as shown by the arrow F6.
After the engine has been running for some time and the chamber 9 has been brought to a sufficient temperature for the fuel vaporization to take place normally in the tube coil il, the arm 8a may be returned to its normal operative position and the engine is running under normal conditions being fed from the device 6.
ln the control device il?, the flow-rate control member which is embodied in FIG. 2 by the needle valve 27, can be of a dierent type, such as for example a spool with'a variable section port. in FIG. 3 is shown a specific alternative embodiment wherein the control inember is comprised by a spool l5 consisting of a rod having a groove lli-6 formed therein, whose cross-section is increasing such that a rightwardly shift of the rod 45 gradually increases the cross-sectional passage of the liquid fuel (arrow F7) towards the tube coil l1 (arrow F8).
lt was found that with certain type of engines and for certain operating conditions thereof, a gas build-up may take place in the tube coil 1l resulting in a phenom-V stricted to the embodiments thereof which have been shown and described merely by Way of examples, andV various modiiications can be made therein without falling outside the scope of the appended claim.
Having now described my invention what I claim as new and desire to secure-by Letters Patent is:
A running carburetor for running an explosion engine at normal speeds and idling speed, said running carburetor comprising: a vaporization chamber adapted to be so mounted on the engine as to be traversed bythe ilow of the exhaust gases of said engine, a coil tube in said chamber, axed heat-radiating body surrounded byY the coils of said coil tube in said vaporization chamber, and tube connecting means for connecting said coil tube to a fuel feed conduit and to a vapor feed conduit.
References Cited in the le of this patent UNITED STATES PATNTS 1,060,042 Wales Apr. 29, 1913 1,377,529 Trotter May 10, 1921 1,728,323 Bartley Y Sept; y17,1929 2,895,462 Champ v Iuly'2l, 1959
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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FR3072113X | 1960-01-20 |
Publications (1)
Publication Number | Publication Date |
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US3072113A true US3072113A (en) | 1963-01-08 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US72111A Expired - Lifetime US3072113A (en) | 1960-01-20 | 1960-11-28 | Fuel feed device for explosion engines |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3789817A (en) * | 1971-04-30 | 1974-02-05 | M Morel | Anti-pollution supply device for internal combustion engines |
US3948224A (en) * | 1970-04-22 | 1976-04-06 | Knapp Edward M | System to prevent pollution of atmosphere |
US4458653A (en) * | 1981-06-01 | 1984-07-10 | Geddes Harold L | Vapor fuel system for internal combustion engines |
US4506647A (en) * | 1981-06-01 | 1985-03-26 | Geddes Harold L | Vapor fuel system internal combustion engines |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1060042A (en) * | 1912-12-28 | 1913-04-29 | Nathaniel B Wales | Vaporizer for internal-combustion engines. |
US1377529A (en) * | 1921-05-10 | Carbureter for internal-combustion engines | ||
US1728323A (en) * | 1927-10-27 | 1929-09-17 | Gen Comb Company | Fuel-supply apparatus for internal-combustion engines |
US2895462A (en) * | 1956-12-17 | 1959-07-21 | Champ Marcel | Feed device for an internal combustion engine |
-
1960
- 1960-11-28 US US72111A patent/US3072113A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1377529A (en) * | 1921-05-10 | Carbureter for internal-combustion engines | ||
US1060042A (en) * | 1912-12-28 | 1913-04-29 | Nathaniel B Wales | Vaporizer for internal-combustion engines. |
US1728323A (en) * | 1927-10-27 | 1929-09-17 | Gen Comb Company | Fuel-supply apparatus for internal-combustion engines |
US2895462A (en) * | 1956-12-17 | 1959-07-21 | Champ Marcel | Feed device for an internal combustion engine |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3948224A (en) * | 1970-04-22 | 1976-04-06 | Knapp Edward M | System to prevent pollution of atmosphere |
US3789817A (en) * | 1971-04-30 | 1974-02-05 | M Morel | Anti-pollution supply device for internal combustion engines |
US4458653A (en) * | 1981-06-01 | 1984-07-10 | Geddes Harold L | Vapor fuel system for internal combustion engines |
US4506647A (en) * | 1981-06-01 | 1985-03-26 | Geddes Harold L | Vapor fuel system internal combustion engines |
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