US1323415A - Gasolene system eor engines - Google Patents

Gasolene system eor engines Download PDF

Info

Publication number
US1323415A
US1323415A US1323415DA US1323415A US 1323415 A US1323415 A US 1323415A US 1323415D A US1323415D A US 1323415DA US 1323415 A US1323415 A US 1323415A
Authority
US
United States
Prior art keywords
chamber
fuel
engines
gasolene
conduit
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
Application number
Publication date
Application granted granted Critical
Publication of US1323415A publication Critical patent/US1323415A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • F02M1/00Carburettors with means for facilitating engine's starting or its idling below operational temperatures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B17/00Pumps characterised by combination with, or adaptation to, specific driving engines or motors
    • F04B17/03Pumps characterised by combination with, or adaptation to, specific driving engines or motors driven by electric motors
    • F04B17/04Pumps characterised by combination with, or adaptation to, specific driving engines or motors driven by electric motors using solenoids
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S261/00Gas and liquid contact apparatus
    • Y10S261/37Modern pumps diaphragm
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/8593Systems
    • Y10T137/85978With pump
    • Y10T137/86035Combined with fluid receiver
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/8593Systems
    • Y10T137/85978With pump
    • Y10T137/86083Vacuum pump

Definitions

  • the present invention relating as indicated to a. fuel supply system for engines, is more particularly concerned with a systern of the type commonly known as a vacuum system, and is intended to avoid the difiiculties which have been met with the systems of this type which are now in use.
  • a further object of the invention is the simplification of such asystem involving the use of fewer parts than the systems now in use, and avoiding the complicated mechanisms which are liable-to get out of order and which do not at all times operate successfully.
  • FIG. 1 is a side elevation partially in section. and showing more or less diagrammatically the parts and connections of my improved system; and Fig. 2 is a longitudi; nal section through a modification of one part of the apparatus.
  • a reservoir or .tank 1 adapted to be filled with liquid fuel and connected by means of a conduit 2 with a constant level chamber 3.
  • This chamber 3 is closed to the atmosphere and is provided with an internal rising to a predetermined height therein and separating the chamber into two chambers 5 and 6.
  • the part 6 is of course in the form of an open receptacle andthe conduit 2 enters the same below the top of the partition 4. From the bottom of the chamber 5 there in the chamber 6.
  • the partition thus serves to fix the maximum depth of fuel which can be maintained Extending from the bureter.
  • the partition 1 de-- termines the maximum fuel depth in the chamber 6 and means are also provided for maintaining this maximum depth therein, thus renderingthe chamber 6 capable of operating as does the float chamber of the ordinary carbureter and supplying fuel to the nozzle 8 connected thereto under a constant head.
  • This means just referred to may take any of several forms, and I have shown in Figs. 1 and 2 two constructions adapted to maintain a constant supply of fuel in the chamber 6 by liftingthe same from the tank 1 through the conduit 2.
  • Fig. 1 there is shown an intermediate 'chamber 10 into the bottom of which the conduit 2 extends, where there is mounted a check valve 11 adapted to permit valve 13 is mounted in the tube 12 at about.
  • this valve also .serving to permit the flow of fuel in the direction of the tank 3 only and not in the reverse direction.
  • a conduit 14 Connected to the top of the chamber 10 is a conduit 14; extending toany suitable pulsating means, such as as shown in Fig. 2, a diaphragm 16, the diaphragm being operated by the pulsations in the engine cylinder, to which it is connected on one side by means of a conduit 17.
  • this pulsating means is to produce intermittent variations in the pressure existing in the chamber 10 on the liquid therein.
  • this pressure is lowered, as it is on every outward stroke of the piston 18 in .the pump, fuel is drawn through theconduit 2 into the chamber 10, but is not forced into the tube 12 on this stroke of the pump.
  • the fuel in the chamber 10 is forced upwardly through the tube 12 and conduit 2 and into the chamber 3.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Description

E. H. SHERBONDY.
GASOLENE SYSTEM FOR ENGINES.
APPLICATION FILED APR. 23. 1917.
E 1s 0 W I I IV VE/V foa Patented Dec. 2, 1919.
UNITED STATES PATENT OFFICE.
EARL H. SHERBONDY, OF CLEVELAND, OHIO, ASSIGNOR 0F ONE-HALFTO ROBERT B. ABBOTT, 0F CLEVELAND, OHIO.
GASOLENE SYSTEM FOR ENGINES.
Specification of Letters Patent, Patented Dec, 2, 1919,
Application filed April 23, 1917. Serial N0. 163,772.
To all whom it may concern:
Be it known that I, EARL H. SHERBoNnr, a citizen of the United States, and a res1- dent of Cleveland, county of C-uyahoga, and State of Ohio, have invented a new and useful Improvement in Gasolene Systems for Engines, of which the following is a specification, the principle herein explained and the best mode in which I have contemplated applying that principle, so as to distinguish it from other inventions. p p
The present invention, relating as indicated to a. fuel supply system for engines, is more particularly concerned with a systern of the type commonly known as a vacuum system, and is intended to avoid the difiiculties which have been met with the systems of this type which are now in use. A further object of the invention is the simplification of such asystem involving the use of fewer parts than the systems now in use, and avoiding the complicated mechanisms which are liable-to get out of order and which do not at all times operate successfully. To the accomplishment of the foregoing and related ends, said invention,
.then. consists of the means hereinafter fully described and particularly pointed out in the claim.
The annexed drawing and the following description set forth in detail certain mechanism embodying the invention, such disclosed means constituting, however, but one of various mechanical forms in which the principle of the invention may be used.
In said annexed drawing Figure 1 is a side elevation partially in section. and showing more or less diagrammatically the parts and connections of my improved system; and Fig. 2 is a longitudi; nal section through a modification of one part of the apparatus.
Referring now to Fig. 1, there is shown a reservoir or .tank 1 adapted to be filled with liquid fuel and connected by means of a conduit 2 with a constant level chamber 3.
. This chamber 3 is closed to the atmosphere and is provided with an internal rising to a predetermined height therein and separating the chamber into two chambers 5 and 6. The part 6 is of course in the form of an open receptacle andthe conduit 2 enters the same below the top of the partition 4. From the bottom of the chamber 5 there in the chamber 6.
chamber 3 out of the portion 6 thereof and of the invention being a pump 15, or,
partition 4;
is a returnconduit 7 leading to the reservoir 1 and serving to return to the reservoir any fuel which overflows the partition -1. The partition thus serves to fix the maximum depth of fuel which can be maintained Extending from the bureter.
As already explained the partition 1 de-- termines the maximum fuel depth in the chamber 6 and means are also provided for maintaining this maximum depth therein, thus renderingthe chamber 6 capable of operating as does the float chamber of the ordinary carbureter and supplying fuel to the nozzle 8 connected thereto under a constant head. This means just referred to may take any of several forms, and I have shown in Figs. 1 and 2 two constructions adapted to maintain a constant supply of fuel in the chamber 6 by liftingthe same from the tank 1 through the conduit 2. Thus in Fig. 1 there is shown an intermediate 'chamber 10 into the bottom of which the conduit 2 extends, where there is mounted a check valve 11 adapted to permit valve 13 is mounted in the tube 12 at about.
the level of the top of the chamber 10, this valve also .serving to permit the flow of fuel in the direction of the tank 3 only and not in the reverse direction. Connected to the top of the chamber 10 is a conduit 14; extending toany suitable pulsating means, such as as shown in Fig. 2, a diaphragm 16, the diaphragm being operated by the pulsations in the engine cylinder, to which it is connected on one side by means of a conduit 17.
The function of this pulsating means is to produce intermittent variations in the pressure existing in the chamber 10 on the liquid therein. When this pressure is lowered, as it is on every outward stroke of the piston 18 in .the pump, fuel is drawn through theconduit 2 into the chamber 10, but is not forced into the tube 12 on this stroke of the pump. Upon every increase in the pressure existing in the chamber 10, (caused by the inward stroke of the piston 18) the fuel in the chamber 10 is forced upwardly through the tube 12 and conduit 2 and into the chamber 3.
It is a matter of indifi'erence as to whether the chamber 3 is filled at a higher rate of speed than necessary as the excess fuel drawn into the chamber merely overflows into the chamber 5 and is returned through the line 7 to the reservoir 1. A constant supply of fuel is thus maintained in the chamber 6 and this fuel is therefore supplied to the nozzle 8 under a constant head,
while a very small pump will produce sufii-' cient quantity of ,fuel to maintain the chamber 6 in a filled condition, and, if desired, the pump can be replaced by mechanism such as is shown in Fig. 2, which is operated directly from the engine cylinder. present system is not only extremely simple in its construction, but it avoids the use of any float in the chamber 6, which replaces the float chamber of thecarbureter and thus The - valves disposed in said conduits permitting flow away from said reservoir and toward said chamber only, an intermediate chamber of appreciable size disposed about the ends of said conduits, and means-adapted to alternately increase and decrease the pressure in said intermediate chamber, thereby alternately drawing fuel thereinto and then forcing it into said conduit leading to said fuel reservoir.
Signed by me, this 20 day of April, 1917 EARL H. SHERBONDY.
US1323415D Gasolene system eor engines Expired - Lifetime US1323415A (en)

Publications (1)

Publication Number Publication Date
US1323415A true US1323415A (en) 1919-12-02

Family

ID=3390869

Family Applications (1)

Application Number Title Priority Date Filing Date
US1323415D Expired - Lifetime US1323415A (en) Gasolene system eor engines

Country Status (1)

Country Link
US (1) US1323415A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3208738A (en) * 1960-01-15 1965-09-28 Acf Ind Inc Carburetor
US3208739A (en) * 1962-05-17 1965-09-28 Tillotson Mfg Co Charge forming apparatus
US4044744A (en) * 1976-07-09 1977-08-30 Keefer James J Internal combustion engine fuel economizer system
US4168687A (en) * 1977-11-04 1979-09-25 Toyota Jidosha Kogyo Kabushiki Kaisha Fuel pump for an internal combustion engine having a carburetor
US5010867A (en) * 1980-06-05 1991-04-30 S.O.F.O. Engineering & Distributing Co. Fuel economizer
US5074758A (en) * 1988-11-25 1991-12-24 Mcintyre Glover C Slurry pump

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3208738A (en) * 1960-01-15 1965-09-28 Acf Ind Inc Carburetor
US3208739A (en) * 1962-05-17 1965-09-28 Tillotson Mfg Co Charge forming apparatus
US4044744A (en) * 1976-07-09 1977-08-30 Keefer James J Internal combustion engine fuel economizer system
US4168687A (en) * 1977-11-04 1979-09-25 Toyota Jidosha Kogyo Kabushiki Kaisha Fuel pump for an internal combustion engine having a carburetor
US5010867A (en) * 1980-06-05 1991-04-30 S.O.F.O. Engineering & Distributing Co. Fuel economizer
US5074758A (en) * 1988-11-25 1991-12-24 Mcintyre Glover C Slurry pump

Similar Documents

Publication Publication Date Title
US4381741A (en) Mechanical fuel pressure operated device for supplying a fuel/oil mixture
US1323415A (en) Gasolene system eor engines
US2242582A (en) Fuel pump
US1330919A (en) Hydrocarbon-motor
US2444628A (en) Internal-combustion engine
US2389159A (en) Fuel pump for internal-combustion engines
US1025814A (en) Fuel-supply system for explosive-engines.
US2267570A (en) Accelerating pump
US1515981A (en) Ginia
US3065784A (en) Engine driven submerged fuel pump
US1729723A (en) Fuel-feed system
US1293804A (en) Priming device for internal-combustion engines.
US1860688A (en) Combined vacuum tank and pressure pump
US1751456A (en) Liquid-reserve tank
US1911950A (en) Fuel pump for internal combustion engines
US1582212A (en) Fuel-feeding system
US1690565A (en) Fuel-feeding device for internal-combustion engines
US984032A (en) Carbureter.
US1353949A (en) Fuel-feed system
US1649190A (en) Liquid-feeding apparatus
US1322674A (en) Engine-peimeh
US1637591A (en) Fuel economizer
US1420886A (en) Carburetor and ptjel peed
US2136079A (en) Device for feeding fluid to the motor portions of internal combustion engines
US1270446A (en) Engine-fuel-supply system.