US2378165A - Fuel injection device - Google Patents
Fuel injection device Download PDFInfo
- Publication number
- US2378165A US2378165A US476977A US47697743A US2378165A US 2378165 A US2378165 A US 2378165A US 476977 A US476977 A US 476977A US 47697743 A US47697743 A US 47697743A US 2378165 A US2378165 A US 2378165A
- Authority
- US
- United States
- Prior art keywords
- fuel
- space
- plunger
- delivery
- pump
- 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 title description 19
- 238000002347 injection Methods 0.000 title description 12
- 239000007924 injection Substances 0.000 title description 12
- 238000002485 combustion reaction Methods 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 238000004939 coking Methods 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 238000003825 pressing Methods 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
- F02M57/00—Fuel-injectors combined or associated with other devices
- F02M57/02—Injectors structurally combined with fuel-injection pumps
-
- 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
- F02M2700/00—Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
- F02M2700/07—Nozzles and injectors with controllable fuel supply
- F02M2700/078—Injectors combined with fuel injection 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
- F02M2700/00—Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
- F02M2700/13—Special devices for making an explosive mixture; Fuel pumps
- F02M2700/1317—Fuel pumpo for internal combustion engines
- F02M2700/1335—Fuel pump combined with the fuel injector
Definitions
- the invention consists in that the fuel delivered by the pump in excess passes from the delivery space of thepump through any air bubbles that may be present. In this way troubles occurring to the injection in consequence of coking of the fuel or from the presence of air are prevented.
- the injection pump plunger is provided with a peripheral recess which is defined in part by an oblique edge, which controls the return flow of the fuel delivered in excess through the nozzle space. It is recommended to construct the return flow member in such a way that the excess of fuel passes through the nozzle space before the injection period.
- the pump plunger 1 is driven through a roller guide 2 by-the cam 3 of the camshaft 4.
- the cylinder 5 of the fuel pump is connected to the fuel tank 6 through a delivery pipe 1 and a return pipe 8. Part of the fuel delivered by the pump reaches the nozzle chamber l0 through the passage 9 and is then injected through the nozzle I l into the combustion space l2.
- the fuel is forced by the feed pump l3 through the pipe I past the valve ll into the delivery chamber lb of the pump.
- the delivery stroke of the plunger I fuel flows through the delivery valve 18 and the passage 9 into the nozzle chamber l0.
- a delivery conduit for conducting oil to the delivery chamber, a-passage for oil from the delivery chamber to the nozzle chamber, means for preventing return flow-of oil through said passage, a pump cylinder, a pump plunger reciprocable in said cylinder, said plunger having a forward end portion filling said cylinder, the delivery end of said cylinder communicating with said delivery chamber, the pump plunger having a peripheral recess rearwardly of said forward outer end portion providing a space between the plunger and the cylinder, an oil passage-from-the nozzle chamber, through the cylinder, to said space, and an oil, passage from said space, the
- plunger having a control edge defining a portion of said space and shaped to cut off flow of oil from said space to the oil passage leading therefrom at a predetermined position of the plunger during the advance thereof, to control the point during the advance of the plunger at which further forward movement thereof begins applying pressure on the oil in the nozzle chamber to cause injection.
- An oil injection device as set forth in claim 1 having means to vary the -position 'at which the device as set forth in claim
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Description
June 12,1945. 'WAEBER I 2,378,155
- FUEL INJECTION DEVICE F'iled Feb. 24, 1943 INVENTOR 01m mmae/ ATTORNEYS Patented June 12, 194
FUEL INJECTION DEVICE Erwin Waeber, Winterthur, Switzerland, assignor to Sulzer Freres, SocitAnonyme, Winterthur, Switzerland Application February 24, 1943, Serial No. 476,977 In Switzerland February "I, 1942 r 3 Claims. (Cl. 299-94012) The invention relates toa fuel injection device,
whose injection pump delivers fuel in excess of what is required. The invention consists in that the fuel delivered by the pump in excess passes from the delivery space of thepump through any air bubbles that may be present. In this way troubles occurring to the injection in consequence of coking of the fuel or from the presence of air are prevented.
the nozzle space to a member controlling the Preferably the injection pump plunger is provided with a peripheral recess which is defined in part by an oblique edge, which controls the return flow of the fuel delivered in excess through the nozzle space. It is recommended to construct the return flow member in such a way that the excess of fuel passes through the nozzle space before the injection period.
The single figure of the drawing shows one embodiment of the invention.
The pump plunger 1 is driven through a roller guide 2 by-the cam 3 of the camshaft 4. The cylinder 5 of the fuel pump is connected to the fuel tank 6 through a delivery pipe 1 and a return pipe 8. Part of the fuel delivered by the pump reaches the nozzle chamber l0 through the passage 9 and is then injected through the nozzle I l into the combustion space l2.
During the sucton stroke of the plunger I, the fuel is forced by the feed pump l3 through the pipe I past the valve ll into the delivery chamber lb of the pump. During the delivery stroke of the plunger I fuel flows through the delivery valve 18 and the passage 9 into the nozzle chamber l0.
As long as the return passage I! is in connection with the pipe 8 through the space formed by the recess l8 in the plunger I, the fuel delivered'inexcess flows again into the tank 6.
If the control edge 20 of the piston l breaks ofi the connection between the passage I1 and the pipe 8, the fuel delivered to the injection space I is subjected to pressure. In that way the fuel needle 2| is raised against theforce of the spring 22. The fuel can'then be injected through the I nozzle ll into the combustion space l2. After In order to prevent pressure waves forming in the delivery pipe after the beginning .of an injection stroke, and to lead away the fuel supplied in excess by the delivery pump it, a bypass having an overflow valve 24 loaded with the spring 23 is provided. The superfluous fuel then passes from the pipe 1, through the byby oil pressure in said chamber greater than the loading pressure thereon, an oil delivery chamber. a delivery conduit for conducting oil to the delivery chamber, a-passage for oil from the delivery chamber to the nozzle chamber, means for preventing return flow-of oil through said passage, a pump cylinder, a pump plunger reciprocable in said cylinder, said plunger having a forward end portion filling said cylinder, the delivery end of said cylinder communicating with said delivery chamber, the pump plunger having a peripheral recess rearwardly of said forward outer end portion providing a space between the plunger and the cylinder, an oil passage-from-the nozzle chamber, through the cylinder, to said space, and an oil, passage from said space, the
plunger having a control edge defining a portion of said space and shaped to cut off flow of oil from said space to the oil passage leading therefrom at a predetermined position of the plunger during the advance thereof, to control the point during the advance of the plunger at which further forward movement thereof begins applying pressure on the oil in the nozzle chamber to cause injection.
2. An oil injection device as set forth in claim 1 having means to vary the -position 'at which the device as set forth in claim
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH2378165X | 1942-02-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2378165A true US2378165A (en) | 1945-06-12 |
Family
ID=4568878
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US476977A Expired - Lifetime US2378165A (en) | 1942-02-07 | 1943-02-24 | Fuel injection device |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2378165A (en) |
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2547174A (en) * | 1946-07-03 | 1951-04-03 | Gardiner M Rogers | Fuel injector mechanism |
| US2552776A (en) * | 1947-05-14 | 1951-05-15 | Louis O French | Fuel injector |
| US2552778A (en) * | 1948-08-28 | 1951-05-15 | Louis O French | Fuel injector |
| US2555930A (en) * | 1948-05-17 | 1951-06-05 | Palumbo Giuseppe | Fuel injection pump for internal-combustion engines |
| US2585100A (en) * | 1947-06-02 | 1952-02-12 | William V Falcon | Fuel pump and nozzle for internalcombustion engines |
| US2590575A (en) * | 1945-08-02 | 1952-03-25 | Gardiner M Rogers | Fuel injector |
| US2628866A (en) * | 1950-04-25 | 1953-02-17 | Gen Motors Corp | Fuel injection pump |
| US2974599A (en) * | 1956-01-26 | 1961-03-14 | Gen Motors Corp | Pump |
| US3006556A (en) * | 1961-01-03 | 1961-10-31 | Gen Motors Corp | Unit fuel pump-injector |
| US3352245A (en) * | 1965-12-09 | 1967-11-14 | Allis Chalmers Mfg Co | Fuel injection system |
| US3628895A (en) * | 1968-11-15 | 1971-12-21 | Lucas Industries Ltd | Liquid fuel pumping apparatus |
| US3640466A (en) * | 1968-11-05 | 1972-02-08 | Sulzer Ag | Fuel injection system for an internal combustion piston engine |
| US3782864A (en) * | 1970-12-30 | 1974-01-01 | Cummins Engine Co Inc | Fuel injector |
| US4355961A (en) * | 1978-04-03 | 1982-10-26 | Ingersoll-Rand Company | Controlling means for a fuel valve |
| US4467963A (en) * | 1982-04-02 | 1984-08-28 | The Bendix Corporation | Single dump single solenoid fuel injector |
| US4565320A (en) * | 1982-03-15 | 1986-01-21 | Yanmar Diesel Engine Co. Ltd. | Unit injector of internal combustion engine |
| US4650116A (en) * | 1983-08-31 | 1987-03-17 | L'orange Gmbh | Fuel-injection device |
| US5255845A (en) * | 1991-05-31 | 1993-10-26 | Robert Bosch Gmbh | Fuel injection device for internal combustion engines |
| US5624072A (en) * | 1994-05-13 | 1997-04-29 | Nippondenso Co., Ltd. | Fuel injection pump having reduced reflux pulsation effects |
-
1943
- 1943-02-24 US US476977A patent/US2378165A/en not_active Expired - Lifetime
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2590575A (en) * | 1945-08-02 | 1952-03-25 | Gardiner M Rogers | Fuel injector |
| US2547174A (en) * | 1946-07-03 | 1951-04-03 | Gardiner M Rogers | Fuel injector mechanism |
| US2552776A (en) * | 1947-05-14 | 1951-05-15 | Louis O French | Fuel injector |
| US2585100A (en) * | 1947-06-02 | 1952-02-12 | William V Falcon | Fuel pump and nozzle for internalcombustion engines |
| US2555930A (en) * | 1948-05-17 | 1951-06-05 | Palumbo Giuseppe | Fuel injection pump for internal-combustion engines |
| US2552778A (en) * | 1948-08-28 | 1951-05-15 | Louis O French | Fuel injector |
| US2628866A (en) * | 1950-04-25 | 1953-02-17 | Gen Motors Corp | Fuel injection pump |
| US2974599A (en) * | 1956-01-26 | 1961-03-14 | Gen Motors Corp | Pump |
| US3006556A (en) * | 1961-01-03 | 1961-10-31 | Gen Motors Corp | Unit fuel pump-injector |
| US3352245A (en) * | 1965-12-09 | 1967-11-14 | Allis Chalmers Mfg Co | Fuel injection system |
| US3640466A (en) * | 1968-11-05 | 1972-02-08 | Sulzer Ag | Fuel injection system for an internal combustion piston engine |
| US3628895A (en) * | 1968-11-15 | 1971-12-21 | Lucas Industries Ltd | Liquid fuel pumping apparatus |
| US3782864A (en) * | 1970-12-30 | 1974-01-01 | Cummins Engine Co Inc | Fuel injector |
| US4355961A (en) * | 1978-04-03 | 1982-10-26 | Ingersoll-Rand Company | Controlling means for a fuel valve |
| US4565320A (en) * | 1982-03-15 | 1986-01-21 | Yanmar Diesel Engine Co. Ltd. | Unit injector of internal combustion engine |
| US4467963A (en) * | 1982-04-02 | 1984-08-28 | The Bendix Corporation | Single dump single solenoid fuel injector |
| US4650116A (en) * | 1983-08-31 | 1987-03-17 | L'orange Gmbh | Fuel-injection device |
| US5255845A (en) * | 1991-05-31 | 1993-10-26 | Robert Bosch Gmbh | Fuel injection device for internal combustion engines |
| US5624072A (en) * | 1994-05-13 | 1997-04-29 | Nippondenso Co., Ltd. | Fuel injection pump having reduced reflux pulsation effects |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2378165A (en) | Fuel injection device | |
| US4211202A (en) | Pump nozzle for air-compressing injection internal combustion engine | |
| US4378774A (en) | Fuel injection system for internal combustion engines | |
| US4811899A (en) | Apparatus for generating pre-injections in unit fuel injectors | |
| ES546948A0 (en) | IMPROVEMENTS IN AN ELECTRICALLY GOVERNED FUEL PUMP FOR INTERNAL COMBUSTION ENGINES | |
| GB1390422A (en) | Fuel injection systems for internal combustion engines | |
| US5042718A (en) | Solenoid-valve-controlled fuel injection device, for an air-compressing internal combustion engine | |
| US2565681A (en) | Fuel injection for internal combustion engines | |
| US3392715A (en) | Device for controlling the pre-injection | |
| US3752136A (en) | Liquid fuel injection pumping apparatus | |
| US2890657A (en) | Unit injector pump with pilot injection | |
| GB1391326A (en) | Fuel injection devices for internal combustion engines | |
| US5533481A (en) | Fuel Injection system | |
| US4590903A (en) | Fuel injection apparatus for definite pilot injection and main injection in internal combustion engines | |
| GB1346501A (en) | Fuel injection valves for internal combustion engines | |
| ES318867A1 (en) | Improvements in the fuel injection system in an internal combustión engine of the type of injection of liquid fuel and ignition by compression. (Machine-translation by Google Translate, not legally binding) | |
| US3479999A (en) | Injection pump valve | |
| US2225019A (en) | Injection device for combustion engines | |
| US3465737A (en) | Fuel injection system | |
| US3427979A (en) | Liquid fuel pumping apparatus for supplying fuel to internal combustion engines | |
| US3104817A (en) | Fuel injector with pilot injection | |
| US2382000A (en) | Fuel injection pump | |
| US3510062A (en) | Delivery valve for engine fuel pump | |
| US2253454A (en) | Fuel injection apparatus for diesel and other internal combustion engines | |
| US2287702A (en) | Fuel injection device |