US2473412A - Fuel injection pump - Google Patents
Fuel injection pump Download PDFInfo
- Publication number
- US2473412A US2473412A US593308A US59330845A US2473412A US 2473412 A US2473412 A US 2473412A US 593308 A US593308 A US 593308A US 59330845 A US59330845 A US 59330845A US 2473412 A US2473412 A US 2473412A
- Authority
- US
- United States
- Prior art keywords
- ports
- cylinder
- plunger
- port
- piston
- 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
- F02M41/00—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor
- F02M41/02—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor being spaced from pumping elements
- F02M41/06—Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor being spaced from pumping elements the distributor rotating
-
- 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
-
- 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
Definitions
- This invention relates to an injector system for liquid fuel engines and is characterized by a single fuel injecting pump for a multiplicity of cylinders, the piston oi the pump having a constant stroke irrespective of the speed of and load on the engine, such variable being provided for by variation in the period of the piston stroke during which fuel is injected into the engine cylinders.
- FIG. 1 is a plain view of an injector unit embodying my invention
- Figure 2 is a similar view thereof with the cover plate removed;
- Figure 3 is a, vertical section on line 3-3 of Figure 1;
- Figure 9 is an elevation of the pump plunger
- Figures 10 and 11 are a section and a plan respectively, of the plunger spring abutment ring.
- the injector case consists of a box base A having an opening in its top closed by the flange b on the lower end of the pump cylinder casting B.
- D is the motor shaft of the engine (or some shaft driven thereby) which projects into the base A and has keyed thereon the channelled cam wheel D-l (to be described in detail later) and the bevelled gear wheel d.
- the pump cylinder casting has a vertical bore in which is contained a sleeve E and the plunger F, the latter within the former.
- the cylinder has equally horizontally spaced near its upper end iuel ejection ports b corresponding in number to the number of the engine cylinders to be served (see Figures 2 and 4) and below the ejection ports a single induction port b displaced angularly in respect to two of the ejection ports and having its inner end bifurcated so that such induction port communicates with the bore at two points, one above the other (see Figure 3).
- Check valves 11 are provided at each ejection portion in the feed line to the corresponding engine cylinder.
- the induction port is of course connected to a proper source of liquid fuel supplied.
- the pinion e is driven with the same angular velocity as the shaft D through the pinion it (see Figure 2), shaft h and bevelled gear h from the bevelled gear d
- the pinions e and h are con tained in recesses formed in the head of the pump cylinder, which are provided with the cover plate M.
- the shaft it has its bearings in the casting B.
- the sleeve has two ports e e through the wall thereof (see Figure 3), the ports e and e being in pairs, the one above the other. These ports register with the corresponding branches of the fuel inlet port 17
- the sleeve is also provided with a series of ports e while the hub of the pinion e is provided with a single fuel outlet port e (see Figures 3 and 4) adapted on rotation of the hub to register in succession with the fuel ejection ports b in the casting and e in the sleeve.
- the inlet ports b in the cylinder are so angularly displaced in respect to the ejection ports b therein as to be between two of the latter ports, while the outlet ports e9 in the sleeve have the same angular displacement in respect to the'inlet ports e and e therein.
- the ends of the several ports in the cylinder may be widened where they communicate with the bore or such widening may be given to the ports in the sleeve to increase-the period during the rotation of the hub that such ports are in communication. Such a widening is indicated at e in Figure 4. 4
- the piston or plunger J has an axial bore j opening on the upper end of the plunger and communicating with a cut away portion a" on one side of the plunger.
- This cutaway portion is diamond shaped in contour with its major l the walls of the cup are cut away on one side.
- an abutment ring k on which the lower end of the spring g abuts.
- a triangular lug k or cam follower projects downwardly from the lower surface of the cup into the channel d of the cam wheel d.
- rollers d corresponding in numbers to the cylinders to be served.
- Compression within the cylinder is controlled by adjusting a screw end in the head of the sleeve.
- the amount of fuel delivered on each stroke of the plunger to an engine cylinder is determined by the angular position of the plunger within the sleeve, this being due to the shape of the cutaway portion 7' such position being controlled through the rack L.
- a liquid fuel injector the combination with a housing having an induction port and a series of eduction ports, of a tubular cylinder within the housing having an induction port registering with the induction port in the housing, and a plurality of eduction ports, a reciproeating piston in the cylinder opening and closing on its movement the induction port therein, a rotary member surrounding the head of the cylinder and having an eduction port, and means for reciprocating the piston and rotating the rotary member in synchronism with each other.
- a liquid fuel injector the combination with a housing having a bore therein and having an induction port and a series of eduction ports of a tubular cylinder within the bore of the housing, having a plurality of induction ports therein, the one above the other, and each connecting with the induction port in the housing, and a plurality of eduction ports, a reciprocating piston in the cylinder successively covering and uncovering in its reciprocation the two induction ports in the cylinder and having a lateral port in communication with its head, brought into registration with the lower induction port on the compressive stroke of the piston, a rotary member surrounding the head of the cylinder and havin an eduction port, and means for reciprocating the piston and rotating the rotary member in synchronism with each other.
- a liquid fuel injector such as defined in claim 2, in which the wall of the piston has 2. diamond-shaped depression surrounding its lateral opening, in combination with means for adjusting the piston around its longitudinal axis.
- a liquid fuel injector such as is defined in.
- a liquid fuel injector such as defined in a REFERENCES CITED
- the following referenlces are of record in the file of this patent:
Description
w. F. BRYANT 1 2,473,412
FUEL INJECTION PUMP Filed May 11, 1945 4 Sheets-Sheet 2 IN V EN TOR.
Mliiam deficit Bfyam la n, 149 W.'F. BRYANT 1 2,473,412
' FUEL INJECTION PUMP Filed May 11, 1945 4 Shee'ts-Sheet 3 -INVENTOR. MNiamflfdezfihk Bryan?" W l 1949. w. F. BRYANT FUEL INJECTION PUMP Filed May 11, 1945 4; SheetS-She'eo 4 IN TOR. we zym Z- mmdm WW8 Patented June 14, 1949 2,4?3Alll2 F UlElL MJECTEQN Fl] William Frederick ldryant, Chamblee, Ga. application May 11, E945, Serial No. 593,308
(Ell. 103-2) Elaims.
This invention relates to an injector system for liquid fuel engines and is characterized by a single fuel injecting pump for a multiplicity of cylinders, the piston oi the pump having a constant stroke irrespective of the speed of and load on the engine, such variable being provided for by variation in the period of the piston stroke during which fuel is injected into the engine cylinders.
To this end it involves a much simplified form of fuel injector, which is compact and easy to manufacture and it consists in the construction arrangement and combination of the several parts as will be hereinafter described and claimed.
Referring to the accompanying drawings in which corresponding parts are designated by corresponding marks of reference,
Figure 1 is a plain view of an injector unit embodying my invention;
Figure 2 is a similar view thereof with the cover plate removed;
Figure 3 is a, vertical section on line 3-3 of Figure 1;
pump plunger;
Figure 9 is an elevation of the pump plunger;
Figures 10 and 11 are a section and a plan respectively, of the plunger spring abutment ring.
The injector case consists of a box base A having an opening in its top closed by the flange b on the lower end of the pump cylinder casting B.
D is the motor shaft of the engine (or some shaft driven thereby) which projects into the base A and has keyed thereon the channelled cam wheel D-l (to be described in detail later) and the bevelled gear wheel d.
The pump cylinder casting has a vertical bore in which is contained a sleeve E and the plunger F, the latter within the former.
The cylinder has equally horizontally spaced near its upper end iuel ejection ports b corresponding in number to the number of the engine cylinders to be served (see Figures 2 and 4) and below the ejection ports a single induction port b displaced angularly in respect to two of the ejection ports and having its inner end bifurcated so that such induction port communicates with the bore at two points, one above the other (see Figure 3). Check valves 11 are provided at each ejection portion in the feed line to the corresponding engine cylinder. The induction port is of course connected to a proper source of liquid fuel supplied.
The central bore of the cylinder is restricted midway of its length by the annular shoulder Contained within the bore is the sleeve E having mounted on its upper end the pinion e and inter-=- inediate of its'length an external annular flange 8 which is spring-pressed upwardly against the lower surface of the shoulder 13 by the spring G. The pinion e is driven with the same angular velocity as the shaft D through the pinion it (see Figure 2), shaft h and bevelled gear h from the bevelled gear d The pinions e and h are con tained in recesses formed in the head of the pump cylinder, which are provided with the cover plate M. The shaft it has its bearings in the casting B.
The sleeve has two ports e e through the wall thereof (see Figure 3), the ports e and e being in pairs, the one above the other. These ports register with the corresponding branches of the fuel inlet port 17 The sleeve is also provided with a series of ports e while the hub of the pinion e is provided with a single fuel outlet port e (see Figures 3 and 4) adapted on rotation of the hub to register in succession with the fuel ejection ports b in the casting and e in the sleeve.
As stated, the inlet ports b in the cylinder are so angularly displaced in respect to the ejection ports b therein as to be between two of the latter ports, while the outlet ports e9 in the sleeve have the same angular displacement in respect to the'inlet ports e and e therein.
The ends of the several ports in the cylinder may be widened where they communicate with the bore or such widening may be given to the ports in the sleeve to increase-the period during the rotation of the hub that such ports are in communication. Such a widening is indicated at e in Figure 4. 4
The piston or plunger J has an axial bore j opening on the upper end of the plunger and communicating with a cut away portion a" on one side of the plunger. This cutaway portion is diamond shaped in contour with its major l the walls of the cup are cut away on one side.
Within the cup and resting on the collar of the piston is an abutment ring k on which the lower end of the spring g abuts.
A triangular lug k or cam follower projects downwardly from the lower surface of the cup into the channel d of the cam wheel d. In this channel are mounted rollers d corresponding in numbers to the cylinders to be served.
Compression within the cylinder is controlled by adjusting a screw end in the head of the sleeve.
It will be noted that:
1. The distribution of fuel to the several en gine cylinders is accomplished by the rotation of the distributing hub of the pinion e.
2. The amount of fuel delivered on each stroke of the plunger to an engine cylinder is determined by the angular position of the plunger within the sleeve, this being due to the shape of the cutaway portion 7' such position being controlled through the rack L.
3. The fuel charge is trapped in the cylinder only after the plunger has gained speed after passing its lower center.
Operation With the parts in the position as above described and shown in Figure 3, after the descent of the plunger under the influence of the spring G, communication is established between both branches of the fuel inlet port 11 and the head of the cylinder. When the plunger is raised by the cam wheel the upper inlet port in the sleeve will be closed by the plunger, but communication will continue between the inlet port and the head of the sleeve through the lower inlet port e and the lateral opening in the plunger until the latter has been moved sufiiciently to break the connection, the exact time this is broken and hence the amount of charge that will be delivered depending on the angular position of the plunger as determined by the rack L. Thereafter the continued up stroke of the plunger compresses the trapped charge which, when the single outlet port 2 in the distributin hub of the pinion e registers with one of the eduction ports b in the cylinder casting is delivered suddenly and with full pressure to the connected cylinder.
Having thus described my invention what I claim as new and desire to secure by United States Letters Patent is:
1. In a liquid fuel injector, the combination with a housing having an induction port and a series of eduction ports, of a tubular cylinder within the housing having an induction port registering with the induction port in the housing, and a plurality of eduction ports, a reciproeating piston in the cylinder opening and closing on its movement the induction port therein, a rotary member surrounding the head of the cylinder and having an eduction port, and means for reciprocating the piston and rotating the rotary member in synchronism with each other.
2. In a liquid fuel injector, the combination with a housing having a bore therein and having an induction port and a series of eduction ports of a tubular cylinder within the bore of the housing, having a plurality of induction ports therein, the one above the other, and each connecting with the induction port in the housing, and a plurality of eduction ports, a reciprocating piston in the cylinder successively covering and uncovering in its reciprocation the two induction ports in the cylinder and having a lateral port in communication with its head, brought into registration with the lower induction port on the compressive stroke of the piston, a rotary member surrounding the head of the cylinder and havin an eduction port, and means for reciprocating the piston and rotating the rotary member in synchronism with each other.
3. A liquid fuel injector, such as defined in claim 2, in which the wall of the piston has 2. diamond-shaped depression surrounding its lateral opening, in combination with means for adjusting the piston around its longitudinal axis.
4. A liquid fuel injector, such as is defined in.
claim 1, in combination with a threaded head for the pump cylinder.
5. A liquid fuel injector, such as defined in a REFERENCES CITED The following referenlces are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,791,600 Onions Feb. 10, 1931 2,084,057 French June 15, 1937 2,353,188 Roosa July 11, 1944
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US593308A US2473412A (en) | 1945-05-11 | 1945-05-11 | Fuel injection pump |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US593308A US2473412A (en) | 1945-05-11 | 1945-05-11 | Fuel injection pump |
Publications (1)
Publication Number | Publication Date |
---|---|
US2473412A true US2473412A (en) | 1949-06-14 |
Family
ID=24374233
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US593308A Expired - Lifetime US2473412A (en) | 1945-05-11 | 1945-05-11 | Fuel injection pump |
Country Status (1)
Country | Link |
---|---|
US (1) | US2473412A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2661729A (en) * | 1948-06-02 | 1953-12-08 | Cummins Engine Co Inc | Fuel feeding apparatus |
US2910056A (en) * | 1956-09-27 | 1959-10-27 | Thompson Ramo Wooldridge Inc | Fuel injection pump |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1791600A (en) * | 1927-10-05 | 1931-02-10 | Ruston & Hornsby Ltd | Fuel-distributing pump for internal-combustion engines |
US2084057A (en) * | 1937-02-23 | 1937-06-15 | Ethel Quarles French | Fuel injector |
US2353188A (en) * | 1941-04-26 | 1944-07-11 | Ernest J Willson | Fuel pump |
-
1945
- 1945-05-11 US US593308A patent/US2473412A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1791600A (en) * | 1927-10-05 | 1931-02-10 | Ruston & Hornsby Ltd | Fuel-distributing pump for internal-combustion engines |
US2084057A (en) * | 1937-02-23 | 1937-06-15 | Ethel Quarles French | Fuel injector |
US2353188A (en) * | 1941-04-26 | 1944-07-11 | Ernest J Willson | Fuel pump |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2661729A (en) * | 1948-06-02 | 1953-12-08 | Cummins Engine Co Inc | Fuel feeding apparatus |
US2910056A (en) * | 1956-09-27 | 1959-10-27 | Thompson Ramo Wooldridge Inc | Fuel injection pump |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2667840A (en) | Fuel injection apparatus and control mechanism therefor | |
US2286928A (en) | Diesel fuel injector pump | |
US2393175A (en) | Pump | |
US2544561A (en) | Fuel injection pump | |
US2210067A (en) | Fuel feeding and distributing apparatus for oil burning engines | |
US2458294A (en) | Oil distributing system | |
US2165696A (en) | Fluid control mechanism | |
US2658486A (en) | Engine for transmitting forces developed therein | |
US2697007A (en) | Fuel injection device for internalcombustion engines | |
US3058425A (en) | Liquid fuel pumps for internal combustion engines | |
US2372559A (en) | Fuel injection pump | |
US2391174A (en) | Fluid feeding and distributing apparatus | |
US3385221A (en) | Multi-plunger engine fuel oil pump | |
US2473412A (en) | Fuel injection pump | |
US2052737A (en) | Fuel feed mechanism for internal combustion engines | |
US1816157A (en) | Injector | |
US2424943A (en) | Fuel pump | |
US1307282A (en) | Internal-combustion engine | |
US2319566A (en) | Fuel pump | |
US1668919A (en) | Fuel-oil pump | |
US2041422A (en) | Fuel pump for internal combustion engines | |
US3744465A (en) | Hydraulic shuttle vavle for fuel injection pumps | |
US2029941A (en) | Internal combustion engine "diesel" | |
US2019103A (en) | Pump | |
US2530507A (en) | Fuel injection apparatus and control |