US1857004A - Apparatus for feeding liquid fuel to internal combustion engines - Google Patents
Apparatus for feeding liquid fuel to internal combustion engines Download PDFInfo
- Publication number
- US1857004A US1857004A US290722A US29072228A US1857004A US 1857004 A US1857004 A US 1857004A US 290722 A US290722 A US 290722A US 29072228 A US29072228 A US 29072228A US 1857004 A US1857004 A US 1857004A
- Authority
- US
- United States
- Prior art keywords
- fuel
- tank
- constant level
- conduit
- internal combustion
- 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
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
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/02—Feeding by means of suction apparatus, e.g. by air flow through carburettors
- F02M37/025—Feeding by means of a liquid fuel-driven jet pump
-
- 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
- F02M17/00—Carburettors having pertinent characteristics not provided for in, or of interest apart from, the apparatus of preceding main groups F02M1/00 - F02M15/00
- F02M17/02—Floatless carburettors
- F02M17/06—Floatless carburettors having overflow chamber determining constant fuel level
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/85978—With pump
- Y10T137/86075—And jet-aspiration type pump
Definitions
- the object of the invention is to provide in a fuel supply system having a constant level fuel tank feeding a fuel delivery pump supplying fuel to the delivery conduit of the system, a device for maintaining a constant level in said constant level tank.
- the invention consists in the provision of amain fuel reservoir below the constant level tank, a supplementary fuel feed conduit tapm ping from the fuel delivery conduit, an overflow conduit from the constant level tank to the main fuel reservoir, an uptake conduit leading from the bottom of the said main fuel tank, and delivering to the constant level tank ejector nozzles at the delivery end of said supplementary fuel feed conduit issuing to the delivery end of the uptake conduit and forming therewith an ejector delivering to the constant level tank.
- FIG. 1 designates a constant level fuel tank delivering by a pipe 2 to the inlet of a centrifugal pump 4 driven off an internal combustion engine 3 by transmission gear 5.
- the discharge 6 of said pump being connected to its inlet by a pipe 7 which forms a circuit to which is connected a pipe 9 having at its discharge end a nozzle 10 from which'the fuel is injected by the pump into the induction conduit 11 of the engine. It is desired to keep the liquid in tank 1 level with the outlet orifice of the jet 10, such level being indicated at 8-8.
- a mainreservoir 13 Disposed below the constant level tank 1, and communicating with the latter by an overflow pipe 12 is a mainreservoir 13.
- To the bottom of the reservoir 13 is connected an uptake pipe 14 which at its upper end discharges into the tank 1.
- a supplementary fuel feed pipe 15 is connected to the delivery pipe 6 of the pump so that it taps said pipe 6, and the disc arge end of said pipe 15 is provided with nozzles 16, 16 which are disposed inside the delivery end of the pipe 14, the latter and the nozzles 16, 16 constituting an ejector whereby liquid is drawn up the pipe 14 and discharged into the tank 1 in proportion to the amount of liquid withdrawn from said tank 1.
- tie level of the liquid in tank 1 is constantly maintained. 17 designates a fuel control valve in the pipe 9.
- a device for maintaining constant level in the constant level tank comprising a main fuel reservoir below the constant level tank, a supplementary fuel feed conduit tapping from the fuel delivery conduit, an overflow conduit from the constant level tank to the -main fuel reservoir, an uptake conduit leading from the bottom of the said main fuel tank and delivering to the constant level tank, ejector nozzles on delivery end of said supplementary fuel feed conduit issuing to the delivery end of the uptake conduit and forming therewith an ejector, delivering to said constant level tank.
- a device for maintaining constant level in the constant level tank comprising a main fuel reservoir below the constant level tank, a supplementary fuel feed conduit tapping from the fuel delivery conduit, an overflow conduit from the con.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Jet Pumps And Other Pumps (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Description
May 3, 1932. M. J. A. REBILLET 1,857,004
APPARATUS FOR FEEDING LIQUID FUEL T0 INTERNAL COMBUSTION ENGINES Filed July 6, 1928 Patented May 3, 1932 PATENT OFFICE mCEL JOSEPH AGHILLE REBILLE'I, OF LYON, FRANCE APPARATUS FOR FEEDING LIQUID FUEL T INTERIKAL OOMIBUSTION' ENGINES Application filed July 6, 1928, Serial No. 290,722, and in France July 11, 19 27.
The object of the invention is to provide in a fuel supply system having a constant level fuel tank feeding a fuel delivery pump supplying fuel to the delivery conduit of the system, a device for maintaining a constant level in said constant level tank.
The invention consists in the provision of amain fuel reservoir below the constant level tank, a supplementary fuel feed conduit tapm ping from the fuel delivery conduit, an overflow conduit from the constant level tank to the main fuel reservoir, an uptake conduit leading from the bottom of the said main fuel tank, and delivering to the constant level tank ejector nozzles at the delivery end of said supplementary fuel feed conduit issuing to the delivery end of the uptake conduit and forming therewith an ejector delivering to the constant level tank.
The invention is illustrated diagrammatically in the accompanying drawings showing the device applied by way of example to the fuel supply tank of an internal combustion.
engine. Referring to the drawing 1 designates a constant level fuel tank delivering by a pipe 2 to the inlet of a centrifugal pump 4 driven off an internal combustion engine 3 by transmission gear 5. the discharge 6 of said pump being connected to its inlet by a pipe 7 which forms a circuit to which is connected a pipe 9 having at its discharge end a nozzle 10 from which'the fuel is injected by the pump into the induction conduit 11 of the engine. It is desired to keep the liquid in tank 1 level with the outlet orifice of the jet 10, such level being indicated at 8-8. Disposed below the constant level tank 1, and communicating with the latter by an overflow pipe 12 is a mainreservoir 13. To the bottom of the reservoir 13 is connected an uptake pipe 14 which at its upper end discharges into the tank 1. A supplementary fuel feed pipe 15 is connected to the delivery pipe 6 of the pump so that it taps said pipe 6, and the disc arge end of said pipe 15 is provided with nozzles 16, 16 which are disposed inside the delivery end of the pipe 14, the latter and the nozzles 16, 16 constituting an ejector whereby liquid is drawn up the pipe 14 and discharged into the tank 1 in proportion to the amount of liquid withdrawn from said tank 1. By this means tie level of the liquid in tank 1 is constantly maintained. 17 designates a fuel control valve in the pipe 9.
It will be understood that although the in- 5 5 vention has been described in connection with a fuel supply system for an internal combustion engine, its application is not limited thereto, but may be applied to an fuel feeding system in which a constant uel level is desirable.
What I claim as my invention and desireto secure by Letters Patent of .the United States is 1. In a fuel supply system having a con- 5 stant'level fuel tank and a fuel delivery pump supplying fuel to the delivery conduit of the "system, a device for maintaining constant level in the constant level tank comprising a main fuel reservoir below the constant level tank, a supplementary fuel feed conduit tapping from the fuel delivery conduit, an overflow conduit from the constant level tank to the -main fuel reservoir, an uptake conduit leading from the bottom of the said main fuel tank and delivering to the constant level tank, ejector nozzles on delivery end of said supplementary fuel feed conduit issuing to the delivery end of the uptake conduit and forming therewith an ejector, delivering to said constant level tank.
2. In a fuel supply system having a constant level fuel tank and a centrifugal fuel delivery pump supplying fuel to'the delivery conduit of the system, a device for maintaining constant level in the constant level tank comprising a main fuel reservoir below the constant level tank, a supplementary fuel feed conduit tapping from the fuel delivery conduit, an overflow conduit from the con.
stant level tank to the main fuel reservoir, an
uptake conduit leading from the bottom of the said main fuel tank and delivering to the constant level tank,- ejector nozzles on deliv- 5 ery end of said sup lementary fuel feed conduit issuing to the delivery end of the uptake conduit and forming therewith an ejector, delivering to said constant level tank. 7
In witness whereof I have signed this specification;
ARCH. JOSEPH ACHILLE REBlLLl-IT.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1857004X | 1927-07-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
US1857004A true US1857004A (en) | 1932-05-03 |
Family
ID=9681712
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US290722A Expired - Lifetime US1857004A (en) | 1927-07-11 | 1928-07-06 | Apparatus for feeding liquid fuel to internal combustion engines |
Country Status (1)
Country | Link |
---|---|
US (1) | US1857004A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2418231A (en) * | 1944-01-24 | 1947-04-01 | Curtis Pump Co | Booster pump and tank assembly |
US3013665A (en) * | 1959-10-21 | 1961-12-19 | Elgin Sweeper Co | Eductor with auxiliary pump-out arrangement |
US3077836A (en) * | 1960-02-01 | 1963-02-19 | Kobe Inc | High speed triplex pump |
US3194174A (en) * | 1960-02-01 | 1965-07-13 | Kobe Inc | High speed triplex pump |
US3223140A (en) * | 1964-01-16 | 1965-12-14 | Oliver R Jones | Self-controlled fuel system |
US3726310A (en) * | 1971-02-18 | 1973-04-10 | Bendix Corp | Fluid amplified auxiliary reservoir |
US4339917A (en) * | 1979-06-13 | 1982-07-20 | The Garrett Corporation | Fuel delivery system and method |
US4874013A (en) * | 1987-10-22 | 1989-10-17 | Hack Jr J Roy | Emergency fuel system apparatus |
US20030024577A1 (en) * | 2001-07-17 | 2003-02-06 | Siemens Aktiengesellschaft | Fuel tank for a motor vehicle |
CN110067652A (en) * | 2018-01-23 | 2019-07-30 | 中国航发商用航空发动机有限责任公司 | A kind of aero-engine oil supply system and oil-feeding control method |
-
1928
- 1928-07-06 US US290722A patent/US1857004A/en not_active Expired - Lifetime
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2418231A (en) * | 1944-01-24 | 1947-04-01 | Curtis Pump Co | Booster pump and tank assembly |
US3013665A (en) * | 1959-10-21 | 1961-12-19 | Elgin Sweeper Co | Eductor with auxiliary pump-out arrangement |
US3077836A (en) * | 1960-02-01 | 1963-02-19 | Kobe Inc | High speed triplex pump |
US3194174A (en) * | 1960-02-01 | 1965-07-13 | Kobe Inc | High speed triplex pump |
US3223140A (en) * | 1964-01-16 | 1965-12-14 | Oliver R Jones | Self-controlled fuel system |
US3726310A (en) * | 1971-02-18 | 1973-04-10 | Bendix Corp | Fluid amplified auxiliary reservoir |
US4339917A (en) * | 1979-06-13 | 1982-07-20 | The Garrett Corporation | Fuel delivery system and method |
US4874013A (en) * | 1987-10-22 | 1989-10-17 | Hack Jr J Roy | Emergency fuel system apparatus |
US20030024577A1 (en) * | 2001-07-17 | 2003-02-06 | Siemens Aktiengesellschaft | Fuel tank for a motor vehicle |
US6810908B2 (en) * | 2001-07-17 | 2004-11-02 | Siemens Aktiengesellschaft | Fuel tank for a motor vehicle |
CN110067652A (en) * | 2018-01-23 | 2019-07-30 | 中国航发商用航空发动机有限责任公司 | A kind of aero-engine oil supply system and oil-feeding control method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US1857004A (en) | Apparatus for feeding liquid fuel to internal combustion engines | |
US2017867A (en) | Mixing device | |
US3840183A (en) | Burner | |
US3736072A (en) | Systems for the supply of liquid fuel to gas-turbine engines | |
US3196926A (en) | Fuel supply systems | |
US3611717A (en) | Device for programming the throughput of fuel supplied to a combustion chamber during an ignition or reignition phase | |
US2355882A (en) | Cleaning installation | |
US2432641A (en) | Dispensing nozzle or faucet | |
GB694371A (en) | Control system for a rocket motor | |
US2444628A (en) | Internal-combustion engine | |
US1453662A (en) | Firing boilers by means of fuel oils | |
US2445479A (en) | Automatic metering water injector for engines | |
US1506229A (en) | Carburetor | |
GB647344A (en) | Improvements in or relating to combustion apparatus | |
US1854994A (en) | Sand trap | |
US1778745A (en) | Injector | |
GB610248A (en) | Improvements relating to liquid fuel supply systems for internal combustion engines | |
US1732531A (en) | Carburetor | |
US1008871A (en) | Means for increasing energy of stored compressed air or other gas capable of supporting combustion. | |
US2632672A (en) | Steam generator | |
US2445104A (en) | Fuel carbureting means | |
US1484057A (en) | Carburetor for internal-combustion engines | |
US1754546A (en) | Fluid-fuel combustion | |
US1750766A (en) | Method and means for regulating fuel | |
US1660954A (en) | Fuel-consumption system |