US1883980A - Fuel pump - Google Patents
Fuel pump Download PDFInfo
- Publication number
- US1883980A US1883980A US156959A US15695926A US1883980A US 1883980 A US1883980 A US 1883980A US 156959 A US156959 A US 156959A US 15695926 A US15695926 A US 15695926A US 1883980 A US1883980 A US 1883980A
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- US
- United States
- Prior art keywords
- piston
- cylinder
- sleeve
- pump
- fuel
- 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
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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
- F02M59/02—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type
-
- 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
-
- 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
- F02M2700/1388—Fuel pump with control of the piston relative to a fixed cylinder
Definitions
- This invention relates to a fuelpuinp to be used' in connection with oil motors operating such that the delivery pipe relieving edge serves also for shifting the injection end and serves, therefore, also for regulating the amount to be delivered. rlhe respective arrangement and combination of parts is very simple and allows of an easy assembly. 1t is illustrated diagrammatically and by way of example on the accompanying drawing on which is shown an axial section through the same.
- 'lhe pump casing consists of a small member 1 and a large member 2, and where these members join one another there they form bearings for a shaft 3 provided with a cam 4 by which the piston 5 is intermittently lifted. This is effected by the intermediary of a roller 8 inserted into a separate enlarged foot of the piston.
- the roller 6 is constantly pressed against the cam 4 by a helical spring l rlhe piston is guided in an axial bore 8 of a ysleeve 9, and the free end of said bore is closed by a cover 10 holding a spring-actuated valve 11.
- rlhe cover 10 and the spring are kept in place by a V4threaded plug l,12, from the centre portion of which extends a pipe '14 to the injection nozzle 13.
- the fuel is supplied to the pump through a pipe terminating in a threaded plug 16 screwed into the pump casing 2.
- the sleeve 9 is provided with a longitudinal channel 19 communicatingl at its upper end by a lateral bore 17 with the pipe 15, and at its lower end with a shallow, but comparatively long circumferential groove 18of the piston 5.
- the bore 17 extends through the wall of the cylinder into the bore 8, of the same, where its orifice is -controlled-by the oblique upper end surface 22 of the piston 5. Also one ofV the piston Aedges at the groove 18, viz. the
- Another channel 21 of the sleeve 9 terminates opposite the upper portion of the piston (at least in the position shown in the ligure) and communicates at its upper end with the fuel delivery pipe, as shown. 1n a certain position of the lifted piston the channel 21 communicates also with the groove 18, and, therefore, with the channel 19, too, as well as with the fuel supply pipe 15, the pipes 15 and 14 being then alsolin communication with each other.
- y' lhe piston 5 can be turned by means hereinafter described, and the position of the sloping edges and 22 relatively to the inner ends of the passages 17 and 21 can, therefore be varied, that is to say, they will vbe opened and closed earlier or later according -to the degree of turning of the piston, and
- the supply of the fuel to the nozzle can be controlled in thisway. 1n the position of the piston as shown in the figure the amount of fuel supplied tothe nozzle will be the largest possible.
- the piston 5 carries near its lower end a cross-pin 26, which projects at both ends and engages slots 25 of a rotatory sleeve 24 enclosing the stationary sleeve 9 and being encompassed by the helical spring 7.
- the piston and said rotatory sleeve are coupled with each other by said pin 26, irrespective of whether the piston is lifted or not, andas the sleeve 24 can be turned more or .less by a lever 23 firmly connected with it, it follows that also the piston can be turned more or less by said lever. 4
- the shaft of the valve 11 entends into the bore 8 so that the valve is opened positively near the end of the delivery stroke whereby a reliable ventilation and evacuation of the pump cylinder is warranted.
- the cam 4 is so designed and arranged that the suction stroke of the piston continues a little when the control edge 22 has already fully opened the bore 17.
- control edges for the commencement and the termination of the' injection have been drawn as straight lines located obliquely with respect rto the pump axis, and also in the claims pertaining to this speciication the control edges have been stated to extend obliquely with respect to' said axis.
- I claim 1 In a fuel pump having a piston and an intake passage and a discharge passage, a discharge valve controlling said discharge passage, and means providing a'coinmunication between the discharge side of the discharge valve and said intake passage, said piston formed to provide valve means controlling said intake passage and such communication.
- a discharge valve controlling said discharge passage
- means providing a communication between the discharge side of the discharge valve and said intake passage
- said piston formed to provide valve means controlling sa1d intake passage and such communication, and means for adjusting the position of said piston to control the time of operation of such valve means.
- a fuel pu'mp. having a piston, a discharge valve, an lnjection nozzle, a conduit connecting said discharve valve and said injection nozzle, said .piston iormedV to provide an overflow valve connected to said conduit between the discharge valve and said nozzle, said overflow valve operable to periodically relieve the pressure in said conduit, and means for adjusting said piston by rotation only to control the time of operation of said overflow valve.
- a pump piston In a fuel pump for internal combustion engines, a pump piston, an intake port, a discharge valve7 an injection nozzle, a pressure conduit connecting said discharge valve and said injection nozzle, a second conduit communicating with said pressure conduit and adapted to relieve the pressure therein, said piston having inclined edges and adapted to open and close said intake port and said second conduit, and means for rotating said piston about its axis lto control the point of opening and closing of said intake port and said second conduit.
- a fuel injection pump comprising a cylinder, a piston plunger slidable therein and extending outwardly therefrom, said piston covering and uncovering a port in the cylinder at a time dependent upon the angular position of the piston with respect to the cylinder, a sleeve rotatably mou'nted on'thecylinder and extending,axially'heyond the end of the cylinder and a non-rotatable but slidable connection between the extension of vsaid sleeve and said plunger comprising a pin in one of said parts and a longitudinal slot in the .other of said parts, wherebyA angular adjustment of said sleeve produces a corresponding change in the angular positionI of the piston plunger with respect to the cylinder.
- a fuel injection pump comprising a casing, a cylinder within said casing having its upper end rigidly secured to the upper part of the casing and its lower end spaced apart from the inner walls of said casing, a piston plunger in said cylinder adapted to cover and uncover a port in the cylinder at a time dependent upon the angular position of the piston with respect to the cylinder, a cam shaft rotatably mounted in the lower part of the casing, a tappet roller engaging the cam on said shaft, a housing for said roller slidably mounted in said casing and operatively connected to said piston plunger, a sleeve rotatably mounted on the"lower end of the cylinder and a non-rotatable but axially slidable connection between the lower part of said sleeve and the piston plunger located between the lower end of said cylinder and said housing whereby angular adjustment of said sleeve produces a corresponding change in the angular position of the piston plunger with respectto the cylinder.
- a fuel injection pump comprising a, cylindersa piston plunger slidable therein and extending outwardly therefrom said piston covering 'and uncovering a port in the cylinder at a ⁇ time dependent upon the angular lll position of the piston vwith respect to the cyl# inder, a sleeve rotatably mounted on the cylinder and extending axially beyond the end of the cylinder, a non-rotatable but slidable I connection" between the extension of said sleeve and said plungenwhereby angular adjustment of said sleeve produces a corre sponding change 1n the angular position of the piston plunger with respect to the cylinder, a helical spring surrounding said rotary sleeve, one end of said sprin g pressing against a collar on said sleeve to prevent longitudinal displacement of said sleeve, and the other end of said spring engaging said piston plunger and serving to drive said plunger"J on its suo-
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Description
F. LANG FUEL PUMP Filed Deo'.
Oct. 25, 1932.
gril. .fill
9W? 7W im@ Patented Oct. 25, 1932 UNITED STATES PArENr g oi-FicjE FRANZ LANG, F MUNICH-NYMPHENBURG, GERMANY, ASSIGNOR TO ROBERT BOSCH AKTIENGESELLSCHAFT, OF STUTTGART, GERMANY FUEL PUMP .Application filed Beeember 24, 1926, Serial No. 156,959, and in Germansr January 2, 1926.
This invention relates to a fuelpuinp to be used' in connection with oil motors operating such that the delivery pipe relieving edge serves also for shifting the injection end and serves, therefore, also for regulating the amount to be delivered. rlhe respective arrangement and combination of parts is very simple and allows of an easy assembly. 1t is illustrated diagrammatically and by way of example on the accompanying drawing on which is shown an axial section through the same.
'lhe pump casing consists of a small member 1 and a large member 2, and where these members join one another there they form bearings for a shaft 3 provided with a cam 4 by which the piston 5 is intermittently lifted. This is effected by the intermediary of a roller 8 inserted into a separate enlarged foot of the piston. The roller 6 is constantly pressed against the cam 4 by a helical spring l rlhe piston is guided in an axial bore 8 of a ysleeve 9, and the free end of said bore is closed by a cover 10 holding a spring-actuated valve 11. rlhe cover 10 and the spring are kept in place by a V4threaded plug l,12, from the centre portion of which extends a pipe '14 to the injection nozzle 13.
The fuel is supplied to the pump through a pipe terminating in a threaded plug 16 screwed into the pump casing 2. The sleeve 9 is provided with a longitudinal channel 19 communicatingl at its upper end by a lateral bore 17 with the pipe 15, and at its lower end with a shallow, but comparatively long circumferential groove 18of the piston 5.`
The bore 17 extends through the wall of the cylinder into the bore 8, of the same, where its orifice is -controlled-by the oblique upper end surface 22 of the piston 5. Also one ofV the piston Aedges at the groove 18, viz. the
upper edge 20, is oblique, its slope corresponding to that of the upper end surface 22, or to the edge of this surface respectively. Another channel 21 of the sleeve 9 terminates opposite the upper portion of the piston (at least in the position shown in the ligure) and communicates at its upper end with the fuel delivery pipe, as shown. 1n a certain position of the lifted piston the channel 21 communicates also with the groove 18, and, therefore, with the channel 19, too, as well as with the fuel supply pipe 15, the pipes 15 and 14 being then alsolin communication with each other. As long as thisI communication exists, the fuel pressed by the piston through the valve 11 into the pipe 14 will flow back on the way 21 18 19 17 16 .15, and the pipe la will be relieved so that the nozzle 13 can be closed quickly and tightly by its appertaining spring. i
y' lhe piston 5 can be turned by means hereinafter described, and the position of the sloping edges and 22 relatively to the inner ends of the passages 17 and 21 can, therefore be varied, that is to say, they will vbe opened and closed earlier or later according -to the degree of turning of the piston, and
the supply of the fuel to the nozzle can be controlled in thisway. 1n the position of the piston as shown in the figure the amount of fuel supplied tothe nozzle will be the largest possible.
The piston 5 carries near its lower end a cross-pin 26, which projects at both ends and engages slots 25 of a rotatory sleeve 24 enclosing the stationary sleeve 9 and being encompassed by the helical spring 7. The piston and said rotatory sleeve are coupled with each other by said pin 26, irrespective of whether the piston is lifted or not, andas the sleeve 24 can be turned more or .less by a lever 23 firmly connected with it, it follows that also the piston can be turned more or less by said lever. 4
The shaft of the valve 11 entends into the bore 8 so that the valve is opened positively near the end of the delivery stroke whereby a reliable ventilation and evacuation of the pump cylinder is warranted.
|The places where the channels 19 and 21 communicate with the groove 18 are so located that this groove when having been filled with fuel from the pipe 14e cannot run empty. In this way a simple and reliable tightening of the delivery space of the pump is attained, especially as regards the prevention 'of air entering along the piston wall.
IIn order to fill the pump cylinder securely also when the pump is running quickly, the cam 4 is so designed and arranged that the suction stroke of the piston continues a little when the control edge 22 has already fully opened the bore 17.
With the constructional form shown by way of example the control edges for the commencement and the termination of the' injection have been drawn as straight lines located obliquely with respect rto the pump axis, and also in the claims pertaining to this speciication the control edges have been stated to extend obliquely with respect to' said axis.
' It is, however, a matter of course 'thatfthey may have a curved configuration and I wish it to be understood that I consider such constructional forms as falling within the scope of my claims. There may be conditions of service necessitating curved control4 edges; these latter are no departure from this invention.
Besides, although I have shown the two control edges located at the piston, this arrangement is .not indispensably necessary in that it is as well possible to provide any" one of said edges, or even both., in the wall of the cylinder or in an intermediate sleeve.
If the two control 'edges are provided at two members of the pump instead of at one and the same, as in the drawing, it isrendered possible to adjust the commencement of the injection perfectly independent of the termination of the same. This is, however, impossible, if said edges are located at one member.
I claim 1. In a fuel pump having a piston and an intake passage and a discharge passage, a discharge valve controlling said discharge passage, and means providing a'coinmunication between the discharge side of the discharge valve and said intake passage, said piston formed to provide valve means controlling said intake passage and such communication.
2. In a fuel pump having a piston and an intake passage and a discharge passage, 'a discharge valve controlling said discharge passage, means providing a communication between the discharge side of the discharge valve and said intake passage, said piston formed to provide valve means controlling sa1d intake passage and such communication, and means for adjusting the position of said piston to control the time of operation of such valve means.
3. In an internal combustion engine, a fuel pu'mp. having a piston, a discharge valve, an lnjection nozzle, a conduit connecting said discharve valve and said injection nozzle, said .piston iormedV to provide an overflow valve connected to said conduit between the discharge valve and said nozzle, said overflow valve operable to periodically relieve the pressure in said conduit, and means for adjusting said piston by rotation only to control the time of operation of said overflow valve.
4. In a fuel pump for internal combustion engines, a pump piston, an intake port, a discharge valve7 an injection nozzle, a pressure conduit connecting said discharge valve and said injection nozzle, a second conduit communicating with said pressure conduit and adapted to relieve the pressure therein, said piston having inclined edges and adapted to open and close said intake port and said second conduit, and means for rotating said piston about its axis lto control the point of opening and closing of said intake port and said second conduit.
5. A fuel injection pump comprising a cylinder, a piston plunger slidable therein and extending outwardly therefrom, said piston covering and uncovering a port in the cylinder at a time dependent upon the angular position of the piston with respect to the cylinder, a sleeve rotatably mou'nted on'thecylinder and extending,axially'heyond the end of the cylinder and a non-rotatable but slidable connection between the extension of vsaid sleeve and said plunger comprising a pin in one of said parts and a longitudinal slot in the .other of said parts, wherebyA angular adjustment of said sleeve produces a corresponding change in the angular positionI of the piston plunger with respect to the cylinder.
6. A fuel injection pump comprising a casing, a cylinder within said casing having its upper end rigidly secured to the upper part of the casing and its lower end spaced apart from the inner walls of said casing, a piston plunger in said cylinder adapted to cover and uncover a port in the cylinder at a time dependent upon the angular position of the piston with respect to the cylinder, a cam shaft rotatably mounted in the lower part of the casing, a tappet roller engaging the cam on said shaft, a housing for said roller slidably mounted in said casing and operatively connected to said piston plunger, a sleeve rotatably mounted on the"lower end of the cylinder and a non-rotatable but axially slidable connection between the lower part of said sleeve and the piston plunger located between the lower end of said cylinder and said housing whereby angular adjustment of said sleeve produces a corresponding change in the angular position of the piston plunger with respectto the cylinder.
7. A fuel injection pump comprising a, cylindersa piston plunger slidable therein and extending outwardly therefrom said piston covering 'and uncovering a port in the cylinder at a `time dependent upon the angular lll position of the piston vwith respect to the cyl# inder, a sleeve rotatably mounted on the cylinder and extending axially beyond the end of the cylinder, a non-rotatable but slidable I connection" between the extension of said sleeve and said plungenwhereby angular adjustment of said sleeve produces a corre sponding change 1n the angular position of the piston plunger with respect to the cylinder, a helical spring surrounding said rotary sleeve, one end of said sprin g pressing against a collar on said sleeve to prevent longitudinal displacement of said sleeve, and the other end of said spring engaging said piston plunger and serving to drive said plunger"J on its suo- 4 tion stroke. In testimony whereof I have hereunto faffixed my signature. A
' FRANZ LANG.'
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1883980X | 1926-01-02 |
Publications (1)
Publication Number | Publication Date |
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US1883980A true US1883980A (en) | 1932-10-25 |
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ID=7747516
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US156959A Expired - Lifetime US1883980A (en) | 1926-01-02 | 1926-12-24 | Fuel pump |
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US (1) | US1883980A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2421843A (en) * | 1943-07-23 | 1947-06-10 | United Aireraft Corp | Accumulator fuel injection system |
US2426319A (en) * | 1943-05-11 | 1947-08-26 | United Aircraft Corp | Injection system |
US2474419A (en) * | 1945-02-02 | 1949-06-28 | Jesse R Hale | Fuel injection apparatus |
US2502989A (en) * | 1945-03-05 | 1950-04-04 | Rathbun Jones Engineering Comp | Fuel injection device for diesel engines |
US2559364A (en) * | 1944-06-24 | 1951-07-03 | William H Mashinter | Fuel injector |
US2575955A (en) * | 1947-07-10 | 1951-11-20 | James W Hatch | Fuel injection pump |
US2602434A (en) * | 1947-03-29 | 1952-07-08 | Worthington Pump & Mach Corp | Hydraulic valve operating mechanism operable to vary valve lift and valve timing |
US2628570A (en) * | 1946-04-26 | 1953-02-17 | American Bosch Corp | Fuel injection device |
US2919685A (en) * | 1955-08-24 | 1960-01-05 | Joy Mfg Co | Apparatus for the stabilization of free-piston machines |
US3737258A (en) * | 1971-06-07 | 1973-06-05 | Caterpillar Tractor Co | Fuel injection pump with timing port |
-
1926
- 1926-12-24 US US156959A patent/US1883980A/en not_active Expired - Lifetime
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2426319A (en) * | 1943-05-11 | 1947-08-26 | United Aircraft Corp | Injection system |
US2421843A (en) * | 1943-07-23 | 1947-06-10 | United Aireraft Corp | Accumulator fuel injection system |
US2559364A (en) * | 1944-06-24 | 1951-07-03 | William H Mashinter | Fuel injector |
US2474419A (en) * | 1945-02-02 | 1949-06-28 | Jesse R Hale | Fuel injection apparatus |
US2502989A (en) * | 1945-03-05 | 1950-04-04 | Rathbun Jones Engineering Comp | Fuel injection device for diesel engines |
US2628570A (en) * | 1946-04-26 | 1953-02-17 | American Bosch Corp | Fuel injection device |
US2602434A (en) * | 1947-03-29 | 1952-07-08 | Worthington Pump & Mach Corp | Hydraulic valve operating mechanism operable to vary valve lift and valve timing |
US2575955A (en) * | 1947-07-10 | 1951-11-20 | James W Hatch | Fuel injection pump |
US2919685A (en) * | 1955-08-24 | 1960-01-05 | Joy Mfg Co | Apparatus for the stabilization of free-piston machines |
US3737258A (en) * | 1971-06-07 | 1973-06-05 | Caterpillar Tractor Co | Fuel injection pump with timing port |
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