US1289716A - Fuel-pump for internal-combustion engines. - Google Patents
Fuel-pump for internal-combustion engines. Download PDFInfo
- Publication number
- US1289716A US1289716A US24052718A US24052718A US1289716A US 1289716 A US1289716 A US 1289716A US 24052718 A US24052718 A US 24052718A US 24052718 A US24052718 A US 24052718A US 1289716 A US1289716 A US 1289716A
- Authority
- US
- United States
- Prior art keywords
- pump
- fuel
- plunger
- stroke
- port
- 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
- 238000002485 combustion reaction Methods 0.000 title description 5
- 239000000446 fuel Substances 0.000 description 25
- 239000007788 liquid Substances 0.000 description 4
- 238000010276 construction Methods 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007717 exclusion Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000005507 spraying 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
- F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
- F02M59/20—Varying fuel delivery in quantity or timing
- F02M59/24—Varying fuel delivery in quantity or timing with constant-length-stroke pistons having variable effective portion of stroke
- F02M59/26—Varying fuel delivery in quantity or timing with constant-length-stroke pistons having variable effective portion of stroke caused by movements of pistons relative to their cylinders
Definitions
- This invention relates to n improved con struction of fuel pump for internal combustion engines of the kind employing ignition on Diesel lines and especially engines in which the fuel is sprayed into the cylinder mechanically without the aid of an air injector, the chief object of the invention being to provide simple means by which a pump plunger having no valve attachment may deliver varying quantities of fuel without altering the time at which injection begins.
- the pump plunger is formed with a fuel relief passage which at a variable predetermined point in the delivery stroke registers with a relief port in the pump casing and thus makes communication between the pump chamber and the said port, so that the pressure in the chamber is relieved and the delivery of fuel to the engine stopped.
- the amount of fuel supplied to the engine will therefore vary according to the point in the pump stroke at which release of the fuel occurs and in the construction preferred the plunger is rotatable by means of connections from the engine governor or regulator and the pump casing is formed with a relief port, preferably leading to the suction side of the pump, the-rear edge of which poi-t is inclined along the axis of the pump so that the moment at which the fuel pressure is relieved varies according to the angular adjustment of the plunger.
- Fig. 2 is a detail view illustrating the operation of the pump.
- A is the pump casing, within which works I J the plunger B provided with the relief passage b.
- C is the suction valve and D the delivery valve of the pump.
- E is a cam operating the pump through the intermediate member F havin the cam roller
- the suction stroke 0 the plunger B 1s effected by means of the spring G mounted on the end of the plunger extension 6' which passes through the casing A. This spring G keeps the opposite end of the plunger up against the member F, maintaining the cam roller f against the cam E.
- the cam E Assuming the pump chamber a to be filled with fuel at the end of the suction stroke of the pump, the cam E as it turns to meet the roller f drives in the plunger B against the pressure of the spring G, causing the annular shoulder bof the pump plunger to compress the fuel in the pump chamber a and to force it at high pressure through the delivery valve D, from which it passes to a suitable spraying nozzle or atomizer in the engine cylinder.
- the delivery of the fuel continues until the outer end I) of the relief passage 6 reaches the relief outlet a in the casing A, when the pressure on the fuel is instantly relieved, permitting. the delivery valve D to close, while the fuel during the remainder of the compression stroke escapes through the outlet port a, whence it may pass to the suction side of the pump.
- FIG. 2 shows the form of therelief aperture or port a which permits the amount of fuel delivered by the pump to be regulated by rotation of-the plunger B through its regulating arm I)".
- a pump casing provided with a fuel relief port, a plunger moving in the said casing havin a passage adapted to make communication etween the said port and the pump chamber and means for varying the point m the plunger stroke at which such communication is made.
- a pump casing provided with a fuel relief port in its wall, which port is formed with a slanting edge, a plunger having a passa e adapted during the delivery stroke to ma e communication between the said port and the pumpchamber and-means for angularly adjustin the plunger to vary the point in the stroke at which such communication is made.
- a pump casing provided with a fuel relief port, a plunger position of the plunger,- an
- a pump casing provided with a fuel relief port, a plunger having a fuel relief passage adapted to registerwith the said port at a predetermined point in the pump stroke, a. cam. effecting the delivery stroke of the plunger and a spring adapted to return the plunger on the suction stroke 5.
- a liquid fuel pump having a relief passage arranged to dischar e fluid from the pump chamber independent y of the regular delivery of the pump and t0 the exclusion thereof, and means whereby said relief passage may be brought into action at any one of a number of different predetermined points in the deliver stroke of the pump.
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
H. E. FENCHELLE.
FUEL PUMP FOR INTERNAL COMBUSTION ENGINES. APPLICATION FILED DEC-6.1917- RENEWED JUNE I7, I918,
11. 289;? 1 6 Patented Dec. 31, 191&
Inventor.
sir-are rarest @FFEQE.
HUGH EMILE FENCHELLE, OF GENOA, ITALY, ASSIGNOR T0 WILLIAM L. KANN,
TRUSTEE, OF PITTSBURGH, PENNSYLVANIA.
FUEL-PUMP FOR INTEBNAL-COMBUSTION ENGINES.
Specification of Letters Patent,
Patented Dec; 31*, 1918.
Application filed December 6, 1817, Serial No. 205,885. Renewed June 17, 1918. Serial No. 240,527.
To all whom it may concern:
Be it known that I, HUGH EMILE FEN- CHELLE, a British subject, residing at Via XX Settembre 34/4, Genoa, in the Kingdom of Italy, have invented certain new and useful Improvements in Fuel-Pumps for Internal-Combustion Engines, of which the following is a specification.
This invention relates to n improved con struction of fuel pump for internal combustion engines of the kind employing ignition on Diesel lines and especially engines in which the fuel is sprayed into the cylinder mechanically without the aid of an air injector, the chief object of the invention being to provide simple means by which a pump plunger having no valve attachment may deliver varying quantities of fuel without altering the time at which injection begins. I
According to this invention the pump plunger is formed with a fuel relief passage which at a variable predetermined point in the delivery stroke registers with a relief port in the pump casing and thus makes communication between the pump chamber and the said port, so that the pressure in the chamber is relieved and the delivery of fuel to the engine stopped. The amount of fuel supplied to the engine will therefore vary according to the point in the pump stroke at which release of the fuel occurs and in the construction preferred the plunger is rotatable by means of connections from the engine governor or regulator and the pump casing is formed with a relief port, preferably leading to the suction side of the pump, the-rear edge of which poi-t is inclined along the axis of the pump so that the moment at which the fuel pressure is relieved varies according to the angular adjustment of the plunger.
In order that-the said invention may be clearly understood and readily carried into effect I will describe the same more fully with reference to the accompanying drawings, in which Figure 1 is a longitudinal section of a pump constructed in accordance with this inventlon, showing also the cam mechanism for operating the pump; and
Fig. 2 is a detail view illustrating the operation of the pump.
' A is the pump casing, within which works I J the plunger B provided with the relief passage b. C is the suction valve and D the delivery valve of the pump. E is a cam operating the pump through the intermediate member F havin the cam roller The suction stroke 0 the plunger B 1s effected by means of the spring G mounted on the end of the plunger extension 6' which passes through the casing A. This spring G keeps the opposite end of the plunger up against the member F, maintaining the cam roller f against the cam E.
Assuming the pump chamber a to be filled with fuel at the end of the suction stroke of the pump, the cam E as it turns to meet the roller f drives in the plunger B against the pressure of the spring G, causing the annular shoulder bof the pump plunger to compress the fuel in the pump chamber a and to force it at high pressure through the delivery valve D, from which it passes to a suitable spraying nozzle or atomizer in the engine cylinder. The delivery of the fuel continues until the outer end I) of the relief passage 6 reaches the relief outlet a in the casing A, when the pressure on the fuel is instantly relieved, permitting. the delivery valve D to close, while the fuel during the remainder of the compression stroke escapes through the outlet port a, whence it may pass to the suction side of the pump.
- Fig. 2 shows the form of therelief aperture or port a which permits the amount of fuel delivered by the pump to be regulated by rotation of-the plunger B through its regulating arm I)". As will be noted in Fig.
lar displacement of the pump plunger. which is free to turn in the casing. By turning the plunger through the lever arm I), operated automatically or otherwise through any suitable gear, the end of the effective stroke of the pump is timed in a very simple manner by bringing the end 6 of the passage 6 v in line with the desired point on the sloping port edge a When the cam has completed its delivery stroke the spring G returns the plunger and 4 fresh fuel is drawn throu h the suction valve G into the pump cham er a ready for the next delivery stroke.
What I claim and desire to secure by Letters Patent of the United States is 1. In a liquidtfuel pump, a pump casing provided with a fuel relief port, a plunger moving in the said casing havin a passage adapted to make communication etween the said port and the pump chamber and means for varying the point m the plunger stroke at which such communication is made.
2. In a liquid fuel pump, a pump casing provided with a fuel relief port in its wall, which port is formed with a slanting edge, a plunger having a passa e adapted during the delivery stroke to ma e communication between the said port and the pumpchamber and-means for angularly adjustin the plunger to vary the point in the stroke at which such communication is made.
3. In a liquid fuel pump, a pump casing provided with a fuel relief port, a plunger position of the plunger,- an
moving in the said casing having a passage adapted to make communication between the said port and the pump chamber at a point in the stroke dependir. on the angular means for angularly adjusting the plunger.
4. In a liquid fuel pump, a pump casing provided with a fuel relief port, a plunger having a fuel relief passage adapted to registerwith the said port at a predetermined point in the pump stroke, a. cam. effecting the delivery stroke of the plunger and a spring adapted to return the plunger on the suction stroke 5. A liquid fuel pump having a relief passage arranged to dischar e fluid from the pump chamber independent y of the regular delivery of the pump and t0 the exclusion thereof, and means whereby said relief passage may be brought into action at any one of a number of different predetermined points in the deliver stroke of the pump.
HUGH E ILE FENCHELLE.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US24052718A US1289716A (en) | 1918-06-17 | 1918-06-17 | Fuel-pump for internal-combustion engines. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US24052718A US1289716A (en) | 1918-06-17 | 1918-06-17 | Fuel-pump for internal-combustion engines. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1289716A true US1289716A (en) | 1918-12-31 |
Family
ID=3357279
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US24052718A Expired - Lifetime US1289716A (en) | 1918-06-17 | 1918-06-17 | Fuel-pump for internal-combustion engines. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1289716A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2421844A (en) * | 1944-01-28 | 1947-06-10 | United Aircraft Corp | Fuel injection system |
| US2441259A (en) * | 1943-12-06 | 1948-05-11 | William H Cook | Ratio control comprising a chamber for a first liquid passing therethrough and a member therein having a port for feeding a second liquid into the first liquid |
| US2482733A (en) * | 1946-07-13 | 1949-09-20 | Injector Company Aktiebolag | Fuel injection pump |
| US2540755A (en) * | 1947-06-25 | 1951-02-06 | United Aireraft Corp | Fuel injection system and apparatus |
-
1918
- 1918-06-17 US US24052718A patent/US1289716A/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2441259A (en) * | 1943-12-06 | 1948-05-11 | William H Cook | Ratio control comprising a chamber for a first liquid passing therethrough and a member therein having a port for feeding a second liquid into the first liquid |
| US2421844A (en) * | 1944-01-28 | 1947-06-10 | United Aircraft Corp | Fuel injection system |
| US2482733A (en) * | 1946-07-13 | 1949-09-20 | Injector Company Aktiebolag | Fuel injection pump |
| US2540755A (en) * | 1947-06-25 | 1951-02-06 | United Aireraft Corp | Fuel injection system and apparatus |
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