US1739563A - Carburetor - Google Patents
Carburetor Download PDFInfo
- Publication number
- US1739563A US1739563A US634354A US63435423A US1739563A US 1739563 A US1739563 A US 1739563A US 634354 A US634354 A US 634354A US 63435423 A US63435423 A US 63435423A US 1739563 A US1739563 A US 1739563A
- Authority
- US
- United States
- Prior art keywords
- fuel
- air
- admission
- carburetor
- heater
- 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 - Lifetime
Links
- 239000000446 fuel Substances 0.000 description 29
- 239000007788 liquid Substances 0.000 description 17
- 230000008016 vaporization Effects 0.000 description 5
- 239000006200 vaporizer Substances 0.000 description 5
- 239000007789 gas Substances 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 210000003462 vein Anatomy 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000004880 explosion Methods 0.000 description 2
- 238000009834 vaporization Methods 0.000 description 2
- 239000002360 explosive Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Images
Classifications
-
- 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
- F02M31/00—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture
- F02M31/02—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating
- F02M31/04—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating combustion-air or fuel-air mixture
- F02M31/06—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating combustion-air or fuel-air mixture by hot gases, e.g. by mixing cold and hot air
- F02M31/08—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating combustion-air or fuel-air mixture by hot gases, e.g. by mixing cold and hot air the gases being exhaust gases
- F02M31/087—Heat-exchange arrangements between the air intake and exhaust gas passages, e.g. by means of contact between the passages
- F02M31/093—Air intake passage surrounding the exhaust gas passage; Exhaust gas passage surrounding the air intake passage
-
- 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
- F02M23/00—Apparatus for adding secondary air to fuel-air mixture
- F02M23/14—Apparatus for adding secondary air to fuel-air mixture characterised by adding hot secondary air
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the present invention relates to carburetors for explosion or internal combustion engines fed with light and heavy liquid fuels and in which the liquid fuel is wholly vaporized' by means of a small stream of very hot air, the resulting gaseous mass being afterwards mixed with the cold air with the object of forming a lukewarm, powerful explosive mixture.
- the object of the invention is to provide a device of particular4 construction by means of which the complete and instantaneous vaporization of the combustible liquid is obtained by the stream of very hot air proceeding from a suitable heater, the said vaporizing device being conveniently branched on a carburetor of any desired form and construction and provided with an admission duct for the cold air flowing to the heater,
- the vaporizer for the liquid fuel comprises a central duet through which flows the liquid fuel fed in regulable amounts through the corresponding admission of the carburetor, said duct ending in shape of a bell mouthiinto which penetrates concentrically an elongated solid ao member in such a manner that the liquid fuel is flattened into the shape of a thin conical sheet and in such condition exposed to the stream of hot air proceeding from a concentric outer duct and flattened into the shape .35 of a conical sheet striking the sheet of fuel,
- the gaseous mass thus formed being forwarded to the admission valves of the motor, where it is mixed with the cold air current to be carbureted.
- the figure is an axial section through the carburetor with the engine indicated in partial plan and the heater element of the engine with which the carburetor cooperates shown in section.
- the air heater shown serves at the same time as an exhaust manifold for the engine. It is formed of three tubes 1, 2, 3, arranged concentrically within each other. The exhaust gases enter through openings 10, 11,
- the apparatus comprises two admissions 27, 31, 32 and 28, 33, 34 for liquid fuel, but if more than-two grades or kinds of liquid fuel are to be disposed of and utilized simultaneously or successively in the same engine, the carburetor may have more than two admissions.
- the fluid inlets are controlled by valves 32 and 34 operated from the rod 31-33 simultaneously with the operation of the air admission port.
- the shaft 37 is held exactly in the axis of the apparatus by means of guides 40 and a stufling box 41, 42, 43.
- Said stufling box must f be completely liquid tight to avoid possible losses of liquid fuel.
- the fuel or fuels admitted through the admission or admissions enters the apparatus through the pipe 30, in which apparatus heat is exchanged between said fuel or fuels and the vein of hot air.
- the latter enters at 25 connected by a pipe 25' to the tube 26 of the heater, whilst liquid fuel passes into the nozzle 24, at the end of which it will be expande'd to a thin circular film by the cone 22 arranged concentrically in the flaring mouth of the nozzle 24.
- the vein of hot air will also beexpanded to a conical film so that at 48 the two films of liquid fuel and hot air will cross each other and mix intimately with an instantaneous and complete exchange of heat, and an instantaneous vaporization of fuel will result.
- a l controlled primary cold air inlet In a carburetor for explosion engines, a l controlled primary cold air inlet, a heater connected to said inlet and by Which the primary air is heated, controlled liquid fuel inlets, a vaporizing chamber connected to said fuel inlets and to the heater, in Which the liquid fuels are vaporized by the heated primary air, a controlled secondary cold air inlet, leading directly to the engine, the vaporizing chamber opening into the stream of secondary cold air, and means whereby the primary air inlet, the liquid fuel inlets and the secondary air inlet are controlled simultaneously and proportionally.
- a primary cold air inlet a connection from said air inlet leading to a heater, 55 a valve for Controlling the passage of the air from the cold air inlet to the heater, a vaporizer, a heated air connection from the heater to the vaporizer, independent fuel admissions formed in the carburetor, a conduit common to said fuel admissions and leading to the vaporizer, valve mechanism for each of the fuel admissions lwhereby the admission of a particular fuel may be controlled,v a secondary air passage leading directly to the engine manifold, a conduit from the vaporizer leading into the secondary air passage adjacent the junction of the latter with the manifold, a valve controlling the admission of air to the secondary air passage, and a single member for siniultaneously Controlling all of said valves.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Spray-Type Burners (AREA)
Description
Dec. 17, 1929. F. v. A. THoMAs CARBURETOR Filed April- 24. 1925 Patented Dec. 17, 1929 PATENT OFFICE FBANCOIS VICTOR .ALBERT THOMAS, OF PARIS, FRANCE canal-:miron Application led April 24, 1923, Serial No. 634,354, and in France April 28, 1922.
The present invention relates to carburetors for explosion or internal combustion engines fed with light and heavy liquid fuels and in which the liquid fuel is wholly vaporized' by means of a small stream of very hot air, the resulting gaseous mass being afterwards mixed with the cold air with the object of forming a lukewarm, powerful explosive mixture.
The object of the invention is to provide a device of particular4 construction by means of which the complete and instantaneous vaporization of the combustible liquid is obtained by the stream of very hot air proceeding from a suitable heater, the said vaporizing device being conveniently branched on a carburetor of any desired form and construction and provided with an admission duct for the cold air flowing to the heater,
an admission for the cold air to be mixed with the vaporized fuel and an admission for the liquid' fuel.
According to the invention, the vaporizer for the liquid fuel comprises a central duet through which flows the liquid fuel fed in regulable amounts through the corresponding admission of the carburetor, said duct ending in shape of a bell mouthiinto which penetrates concentrically an elongated solid ao member in such a manner that the liquid fuel is flattened into the shape of a thin conical sheet and in such condition exposed to the stream of hot air proceeding from a concentric outer duct and flattened into the shape .35 of a conical sheet striking the sheet of fuel,
the gaseous mass thus formed being forwarded to the admission valves of the motor, where it is mixed with the cold air current to be carbureted.
40 The figure is an axial section through the carburetor with the engine indicated in partial plan and the heater element of the engine with which the carburetor cooperates shown in section.
The air heater shown serves at the same time as an exhaust manifold for the engine. It is formed of three tubes 1, 2, 3, arranged concentrically within each other. The exhaust gases enter through openings 10, 11,
12, 13, (the engine having four cylinders for instance) and escape through 8. Cold air entering at 6 passes through the space 14 between the tubes 1 and 2 and enters the central tube 3 through the bot'tom. Thus such cold air passes in two opposite directions, each time along a surface directly heated by eXhaust gases. It will be seen that in this arrangement the heat of exhaust gases may be utilized to a maximum.
15 designates the inlet of cold air from the 00 atmosphere towards the admission 16-17. Air thus admitted in varying volumes and at varying rates of speed according to the running and load of the engine, passes into the heater, wherein the vein of hot air is formed. To this end the mechanical admission 16-17 is connected to the heaterv by means of a pipe 18' connected at 18 and 6. The apparatus comprises two admissions 27, 31, 32 and 28, 33, 34 for liquid fuel, but if more than-two grades or kinds of liquid fuel are to be disposed of and utilized simultaneously or successively in the same engine, the carburetor may have more than two admissions. The fluid inlets are controlled by valves 32 and 34 operated from the rod 31-33 simultaneously with the operation of the air admission port.
The shaft 37 is held exactly in the axis of the apparatus by means of guides 40 and a stufling box 41, 42, 43. Said stufling box must f be completely liquid tight to avoid possible losses of liquid fuel.
It is obvious that instead of two or more liquid fuel admissions, a single admission may be used in cases where a single fuel is used at a time.
The fuel or fuels admitted through the admission or admissions enters the apparatus through the pipe 30, in which apparatus heat is exchanged between said fuel or fuels and the vein of hot air. The latter enters at 25 connected by a pipe 25' to the tube 26 of the heater, whilst liquid fuel passes into the nozzle 24, at the end of which it will be expande'd to a thin circular film by the cone 22 arranged concentrically in the flaring mouth of the nozzle 24. Owing to the bulging portion 23 the vein of hot air will also beexpanded to a conical film so that at 48 the two films of liquid fuel and hot air will cross each other and mix intimately with an instantaneous and complete exchange of heat, and an instantaneous vaporization of fuel will result. 'The -mixing is assisted by the deflecting action of the reversed cone 21 and the Wall 23, F' which have a tendency to defiect the current of hottair incompletely utilized in the direction of the movement of fuel. The combustible mixture produced passes through the conduit 44 to the cylinder or cylinders of the engine, but before reaching the latter it meets with cold air arriving from the admission 35, 37 through the pipe 45.V Having now fully described my said invention, what I claim and desire to secure l by Letters Patent, is: 1. In a carburetor for explosion engines, a l controlled primary cold air inlet, a heater connected to said inlet and by Which the primary air is heated, controlled liquid fuel inlets, a vaporizing chamber connected to said fuel inlets and to the heater, in Which the liquid fuels are vaporized by the heated primary air, a controlled secondary cold air inlet, leading directly to the engine, the vaporizing chamber opening into the stream of secondary cold air, and means whereby the primary air inlet, the liquid fuel inlets and the secondary air inlet are controlled simultaneously and proportionally.
2. In a carburetor for internal combustion engines, a primary cold air inlet, a connection from said air inlet leading to a heater, 55 a valve for Controlling the passage of the air from the cold air inlet to the heater, a vaporizer, a heated air connection from the heater to the vaporizer, independent fuel admissions formed in the carburetor, a conduit common to said fuel admissions and leading to the vaporizer, valve mechanism for each of the fuel admissions lwhereby the admission of a particular fuel may be controlled,v a secondary air passage leading directly to the engine manifold, a conduit from the vaporizer leading into the secondary air passage adjacent the junction of the latter with the manifold, a valve controlling the admission of air to the secondary air passage, and a single member for siniultaneously Controlling all of said valves.
In testimony Whereof I have hereunto set my hand. 4
FRANCOIS VICTOR ALBERT THOMS.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1739563X | 1922-04-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1739563A true US1739563A (en) | 1929-12-17 |
Family
ID=9680638
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US634354A Expired - Lifetime US1739563A (en) | 1922-04-28 | 1923-04-24 | Carburetor |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1739563A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2946575A (en) * | 1958-10-27 | 1960-07-26 | Gen Motors Corp | Carburetor air heating device |
| US4305350A (en) * | 1980-02-04 | 1981-12-15 | Brown Michael H | Dual fuel system |
-
1923
- 1923-04-24 US US634354A patent/US1739563A/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2946575A (en) * | 1958-10-27 | 1960-07-26 | Gen Motors Corp | Carburetor air heating device |
| US4305350A (en) * | 1980-02-04 | 1981-12-15 | Brown Michael H | Dual fuel system |
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