US1066939A - Feeding means for internal-combustion engines. - Google Patents
Feeding means for internal-combustion engines. Download PDFInfo
- Publication number
- US1066939A US1066939A US48820409A US1909488204A US1066939A US 1066939 A US1066939 A US 1066939A US 48820409 A US48820409 A US 48820409A US 1909488204 A US1909488204 A US 1909488204A US 1066939 A US1066939 A US 1066939A
- Authority
- US
- United States
- Prior art keywords
- piston
- fuel
- conduit
- pistons
- feeding
- 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 16
- 239000000446 fuel Substances 0.000 description 37
- 230000035611 feeding Effects 0.000 description 17
- 238000004880 explosion Methods 0.000 description 9
- 238000012840 feeding operation Methods 0.000 description 7
- 239000007788 liquid Substances 0.000 description 7
- 230000000694 effects Effects 0.000 description 5
- 230000001105 regulatory effect Effects 0.000 description 5
- 238000001704 evaporation Methods 0.000 description 4
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000001276 controlling effect Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 241000370685 Arge Species 0.000 description 1
- 241001052209 Cylinder Species 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 230000000266 injurious effect Effects 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000003534 oscillatory effect Effects 0.000 description 1
- 239000002699 waste material Substances 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
- F02M47/00—Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure
- F02M47/02—Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure of accumulator-injector type, i.e. having fuel pressure of accumulator tending to open, and fuel pressure in other chamber tending to close, injection valves and having means for periodically releasing that closing pressure
- F02M47/027—Electrically actuated valves draining the chamber to release the closing pressure
Definitions
- This invention relates to means for feeding the fuel into internal combustion engines, and the object of the invention is to procure a great pressure for forcing the fi el into the engine and to facilitate the eva porating of the fuel so that it is effected with great rapidity.
- the said means are so arranged, that the said great pressure is rapidly reduced at the same moment as the feeding of the quantity of fuel, adapted for the piston stroke. has been effected, so that no injurious after-feeding operation can take place.
- This is attained by the providing of a special piston in addition to the pump piston in such manner, that the piston last mentioned forces the fuel into the conduit, leading-to the working cylinder or to the explosion chamber, and the piston first-- mentioned. effects the feeding operation proper.
- the said pistons may be advanced either simultaneously or alternately, or a differential piston maybe used, which, when moved in one direction, effects one of the said operations, and when moved in the opposite direction effects theother operation.
- a device is provided for regulating the fuel quantity fed into the engine at each stroke of the pistons.
- Figure 1 in the accompanying drawings is a section of the feeding means and the evaporating device, the pistons being so arranged that they runtogether.
- Fig. 2 is a section of the feeding means so arranged that the pistons are advanced alternately.
- Fig. 3 shows in the same manner the feed ing means last mentioned but combined with a device for regulating the quantity of fuel fed into the engine.
- Fig. 4 shows a modification of the said regulating device.
- Fig. 5 is asection of the feeding means provided with one piston only.
- Fig. 1 are two differential pistons or plungers, working in cylinders 3 and 4 respectively.
- the liquid fuel is drawn into the cylinder 3 from a tank (not shown), by
- the said fuel is then forced by the advanced piston through the spring actuated valve 6 and through the passage 7 into the cylinder 4, from which leads the passage 9, which may be considered a continuation of the passage 7, to the explosion chamber 10, which is in free ui11nii11ication with the working cyl inder 11.
- the said .pistons 1 and 2 are firmly connected by a cross head 12 and are reciprocated in the ordinary manner by a cam disk or the like, not shown in the drawings.
- the piston 2 is wider than the piston 1, and the cylinder 4, in which the piston 2 operates, communicates with the chamber 10 through the passage 9.
- the pistons 1 and 2 are forced forward rapidly immediately before the end of the compression stroke of the working piston in the cylinder 11, so that the quantity of fuel, drawn into the cylinder 3 by the piston 1 during its previous suction stroke, is forced therefrom by way of the conduit formed of passages 7 and 9, and cylinder 4. At the same time the capacity of the said conduit is reduced by the advanced piston 2 which has a greater area than the piston l, the fuel being thus forced into the chamber 10, subjected to a very high pressure.
- the pistons or plungers 1 and 2 may be advanced, alternately, as illustrated in Fig.
- the pistons 1 and 2 are connected by a two armed lever 12 swinging on a stationary pin, the piston 2 being besides provided with a pendent extension adapted to be acted'upon by an eccentric, cam disk or the like not shown in the drawings. Owing to the fact that the pistons are each connected with an arm of the lever 12, they are advanced alternately in their respectivecylinders. As the piston 1 is moved forward, it forces the fuel through the valve 6 and into the conduit afforded by the passages 7 and 9 and the cylinder 4, the capacity of which is increased at the same time by the returning piston 2 in a higher degree, compared with the quantity of fuel fed into the said conduit. owing to the fact that the piston 2 is wider than the piston 1. The device may be modified in such manner.
- each of the pistons may evidently be actuated by an eccentric, cam-disk or the like, and the moment, during which the pistons are moved in opposite directions, may be confined to a greater or less part of the piston stroke.
- the piston 1 is connected with the lever 12 by a link 13 which is pivotally connected with the piston 1 and can be swung longitudinally along one arm of the lever 6, provided for that purpose with a slot 14, engaged by a pin 15 in the said link.
- the link 13 is adapted to be connected in suitable manner with the centrifugal governor of the engine, the link 16 being provided for that purpose.
- Thestroke of the piston and consequently the quantity of fuel fed into the engine is increased or decreased according as the link 13 is located farther from or nearer to the fulcrum of the lever 12:
- the fulcrum of the lever 12 is movable in a slot in the lever and fixed in a movable part, preferably a swingable arm 17 connected with the governor.
- Fig. 5 shows the feeding device provided with a double-acting piston 16.
- the fuel previously drawn into the cylinder through the valve 5 is forced from one end of the piston to the other through the valve 6, and as the piston 6 is moved in the opposite direction, the said fuel is forced into the chamber 10.
- surface of the piston which is employed for forcing the'fuel into the chamber 10 is given a greater area than the opposite surface which forces the charge through the passage 7, one end of the piston being of greater area than the other so as to insure the desired differential operation.
- the fuel pump is independent of the pressure in the conduit formed of passages 7 and 9 and cylinder 4, which is the case also in the form shown in Fig. 5. Consequently the said pressure during the combustion period may be of any high rate without interfering with the feeding operation.
- the feeding through the valve 6) is effected, while there is a low pressure in the conduit, the feeding operation'can readily be so regulated as to supply very small quantities of fuel, while the strokes of the piston, forcing the fuel into the engine remain constant.
- the evaporating device shown in Fig. 1 is characterized by the conduit 9 being provided with a conical enlargement 20 and by a conical body- 21 .being mounted in the conical part 20 of the conduit, which body is congruent to the said part and has a rather sharp tip.
- the liquid fuel passes, when forced into the chamber 10, between the surface of the body 21 and the inner side or wall of the conical enlargement 20 of the conduit.
- a great pressure is prevailing in the explosion chamber due to the operation of the piston in the working cylinder. as stated above, and the said pressure forces the conical body 21 as a valve body against the wall 20, serving as a valve seat, the liquid will be divided into a thin layer.
- the complete evaporation is, evidently, of great importance also for effecting rapid and complete combustion, as the combustion is dependent upon the intimate mixing of the fuel with the air necessar for the combustion and, the mixture is facilitated in the same degree as the fuel is finely divided and brought into a gaseous state as completely as possible upon its entry into the explosion chamber.
- the evaporator although shown only in Fig. 1, may, evidently, be used also in connection with the forms of the device shown in Figs. 2 to 5 inclusive or in modifications derived from the same.
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Description
0. OHLSSON. FEEDING MEANS ron INTERNAL COMBUSTION ENGINES. APPLICATION FILED APR. 6, 1909.
1,066,939. Patented July 8, 1913.
2 SHEETS-SHEET l.
W E'znesses Jim/auto?" pf. OZOfOIZZSSOIL NEW Attornqy 0 OHLSSON.
FEEDING MEANS FOR INTERNAL GbMBUSTION ENGINES. APPLICATION FILED APB.6, 1909.
Patented July 8, 1913.
2 SHEETS-SHEET 2.
Witnesses V7. CW (1m '63 fizveiztar Olaf 072 255071,
@Ttornqy OLOF OHLSSON, 0F soDERTELJE, SWEDEN.
FEEDING MEANS FOR INTERNAL-COMBUSTION ENGlINES.
Specification of Letters latent.
Patented July 8, 1913.
Application filed April 6, 1909. Serial No. 488,204.
To all zc/zom 1' i may concern Be it known that I, OLoF ()HLSSON, a subject of the King of Sweden, and resident of Sodertelje, in the Kingdom of Sweden, have invented certain new and useful Improvements in Feeding Means for InternaLCombustion Engines, of which the following is a specification, reference being had therein to the accompanying drawings.
This invention relates to means for feeding the fuel into internal combustion engines, and the object of the invention is to procure a great pressure for forcing the fi el into the engine and to facilitate the eva porating of the fuel so that it is effected with great rapidity. The said means are so arranged, that the said great pressure is rapidly reduced at the same moment as the feeding of the quantity of fuel, adapted for the piston stroke. has been effected, so that no injurious after-feeding operation can take place. This is attained by the providing of a special piston in addition to the pump piston in such manner, that the piston last mentioned forces the fuel into the conduit, leading-to the working cylinder or to the explosion chamber, and the piston first-- mentioned. effects the feeding operation proper. The said pistons may be advanced either simultaneously or alternately, or a differential piston maybe used, which, when moved in one direction, effects one of the said operations, and when moved in the opposite direction effects theother operation. In combination with the said means, preferably when two pistons are used, a device is provided for regulating the fuel quantity fed into the engine at each stroke of the pistons.
Figure 1 in the accompanying drawings is a section of the feeding means and the evaporating device, the pistons being so arranged that they runtogether. Fig. 2 is a section of the feeding means so arranged that the pistons are advanced alternately.
Fig. 3 shows in the same manner the feed ing means last mentioned but combined with a device for regulating the quantity of fuel fed into the engine. Fig. 4 shows a modification of the said regulating device. Fig. 5 is asection of the feeding means provided with one piston only.
1 and 2, Fig. 1, are two differential pistons or plungers, working in cylinders 3 and 4 respectively. The liquid fuel is drawn into the cylinder 3 from a tank (not shown), by
way of a passage controlled by a valve The said fuel is then forced by the advanced piston through the spring actuated valve 6 and through the passage 7 into the cylinder 4, from which leads the passage 9, which may be considered a continuation of the passage 7, to the explosion chamber 10, which is in free ui11nii11ication with the working cyl inder 11. The said .pistons 1 and 2 are firmly connected by a cross head 12 and are reciprocated in the ordinary manner by a cam disk or the like, not shown in the drawings. The piston 2 is wider than the piston 1, and the cylinder 4, in which the piston 2 operates, communicates with the chamber 10 through the passage 9. The pistons 1 and 2 are forced forward rapidly immediately before the end of the compression stroke of the working piston in the cylinder 11, so that the quantity of fuel, drawn into the cylinder 3 by the piston 1 during its previous suction stroke, is forced therefrom by way of the conduit formed of passages 7 and 9, and cylinder 4. At the same time the capacity of the said conduit is reduced by the advanced piston 2 which has a greater area than the piston l, the fuel being thus forced into the chamber 10, subjected to a very high pressure. During the subsequent return stroke of the acting pistons the capacity of the said conduit is rapidly increased by the retraction of piston 2 in cylinder 4, so that a liquid fuel in passage 9 is subjected to a backward suction, whereby the feeding of the charge into the chamber 10 is instantaneoi'isly interrupted. Consequently the piston 2 effects an oscillatory movement of the charge forward and backward in the passage 9, or in other words, the operation of said piston 2 intensifies the variations in pressure in the feeding conduit over the variations which would be afforded if only the piston 1 were provided. In this manner the feeding of the fuel is more closely timed to the beginning of the feeding period as well as to the instantaneous interruption of the said period. Consequently, a feeding operation of shorter duration and a more sudden reduction of the pressure in the conduit respectively is effected than by means of one piston. The said feeding period can easily be so shortencd and timed, that it is equal to and coincides with that part of the stroke of the working piston, during which the combustion is effected in the most advantageous manner. In this manner a very nearly complete combustion can be effected during the short period, as the compression is at the maximum. Consequently, the after feeding operation and the after-combustion operation resulting from the same are obviated, which hitherto often take place in internal combustion engines and which cause a great waste of fuel to no useful purpose. Where my improvements are employed the temperature of the igniting means or of the chamber 10 may also be much higher than hitherto. since it is possible to accurately time the supply of the charge to said igniting means or to said chamber.
The pistons or plungers 1 and 2 may be advanced, alternately, as illustrated in Fig.
2. In the said figure the pistons 1 and 2 are connected by a two armed lever 12 swinging on a stationary pin, the piston 2 being besides provided with a pendent extension adapted to be acted'upon by an eccentric, cam disk or the like not shown in the drawings. Owing to the fact that the pistons are each connected with an arm of the lever 12, they are advanced alternately in their respectivecylinders. As the piston 1 is moved forward, it forces the fuel through the valve 6 and into the conduit afforded by the passages 7 and 9 and the cylinder 4, the capacity of which is increased at the same time by the returning piston 2 in a higher degree, compared with the quantity of fuel fed into the said conduit. owing to the fact that the piston 2 is wider than the piston 1. The device may be modified in such manner. that the arms of the lever 12 are of unequal length, so that the stroke of the piston 2 is greater than thatof the piston 1. The piston 1 is then returned and the piston 2 advanced, causing the same quantity/of fuel to be forcibly passed into the chamber 10, which has previously been fed into the conduit formed of passages 7 and 9 and cylinder 4 by. the piston 1, the said conduit being now shut off from the piston 1 by the valve 6. Each of the pistons may evidently be actuated by an eccentric, cam-disk or the like, and the moment, during which the pistons are moved in opposite directions, may be confined to a greater or less part of the piston stroke.
In Fig. 3 the piston 1 is connected with the lever 12 by a link 13 which is pivotally connected with the piston 1 and can be swung longitudinally along one arm of the lever 6, provided for that purpose with a slot 14, engaged by a pin 15 in the said link. The link 13 is adapted to be connected in suitable manner with the centrifugal governor of the engine, the link 16 being provided for that purpose. Thestroke of the piston and consequently the quantity of fuel fed into the engine is increased or decreased according as the link 13 is located farther from or nearer to the fulcrum of the lever 12: In'Fig. 4 the fulcrum of the lever 12, is movable in a slot in the lever and fixed in a movable part, preferably a swingable arm 17 connected with the governor.
Fig. 5 shows the feeding device provided with a double-acting piston 16. As the said piston is moved in the direction indicated by the arrow, the fuel previously drawn into the cylinder through the valve 5 is forced from one end of the piston to the other through the valve 6, and as the piston 6 is moved in the opposite direction, the said fuel is forced into the chamber 10. In this construction that surface of the piston which is employed for forcing the'fuel into the chamber 10 is given a greater area than the opposite surface which forces the charge through the passage 7, one end of the piston being of greater area than the other so as to insure the desired differential operation.
In the constructions shown in Figs. 2 to 4 inclusive the fuel pump is independent of the pressure in the conduit formed of passages 7 and 9 and cylinder 4, which is the case also in the form shown in Fig. 5. Consequently the said pressure during the combustion period may be of any high rate without interfering with the feeding operation. Owing to the fact that the feeding (through the valve 6) is effected, while there is a low pressure in the conduit, the feeding operation'can readily be so regulated as to supply very small quantities of fuel, while the strokes of the piston, forcing the fuel into the engine remain constant.
The evaporating device shown in Fig. 1 is characterized by the conduit 9 being provided with a conical enlargement 20 and by a conical body- 21 .being mounted in the conical part 20 of the conduit, which body is congruent to the said part and has a rather sharp tip. The liquid fuel passes, when forced into the chamber 10, between the surface of the body 21 and the inner side or wall of the conical enlargement 20 of the conduit. As the forcin into the engine is effected w 'le a great pressure is prevailing in the explosion chamber due to the operation of the piston in the working cylinder. as stated above, and the said pressure forces the conical body 21 as a valve body against the wall 20, serving as a valve seat, the liquid will be divided into a thin layer. As the wide ends of the conical surfaces are directed toward the chamber 10 and the liquid is spread in the direction from the tip of the cone 2'. e. practically from one point, the liquid fuel 1s rapidly divided'around the hot conical of the fuel body 21, so that it is evaporated and conse ward the chamber 10, from which the cone receives its heat. By means of the said arrangement the disadvantage is removed, that the part, which operates as an evaporator, also serves as a receptacle for the fuel, from which the fuel in a liquid state enters the explosion chamber almost uninterruptedly. Owing to this fact a great quantity of fuel is saved. The complete evaporation is, evidently, of great importance also for effecting rapid and complete combustion, as the combustion is dependent upon the intimate mixing of the fuel with the air necessar for the combustion and, the mixture is facilitated in the same degree as the fuel is finely divided and brought into a gaseous state as completely as possible upon its entry into the explosion chamber. The evaporator although shown only in Fig. 1, may, evidently, be used also in connection with the forms of the device shown in Figs. 2 to 5 inclusive or in modifications derived from the same.
Having now described my invention, what I claim as new and desire to secure by Letters Patent is:
1. In an internal combustion engine the combination of a working cylinder, an explosion chamber, an evaporator consisting of two congruent cones, one mounted in the other affording a passage between them, the inner cone being forced a inst the outer one b the pressure efl'ecte in the working cylin er during the com ression stroke and means for forcing the c arge between said cones to the explosion chamber.
2. In an internal combustion engine, the
combination of a working cylinder, an explosion chamber, a fuel supply conduit in communication with the chamber, a plurality of cylinders interposed in the conduit and in communication one with the other, means for controlling such communication between the cylinders, operatively connected pistons within the cylinders capable of operation in such a manner that the fuel is acted upon first by one of said pistons then by the other piston after the fuel has passed beyond the means for controlling the communication between the cylinders, a lever capable of operation to reciprocate the pistons and a regulating device for changing the length of the lever arm.
3. In an internal combustion engine, the combination of a working cylinder, an explosion chamber in communication with the said cylinder, a fuel supply conduit leading to the said chamber, cylinders interposed in the conduit, pistons mounted to reciprocate in such cylinders to force the fuel through the conduit into the combustion chamber, one of said pistons operating to effect forward and backward movement of the fuel in the conduit whereby a feeding operation of short duration and a sudden reduction of the pressure in the conduit are effected.
In witness whereof, I have hereunto signed my name in the presence of two subscribing witnesses.
OLOF OH LSSON.
\Vitnesses ANNA sonnnsrnom, ROBERT APELGREN.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US48820409A US1066939A (en) | 1909-04-06 | 1909-04-06 | Feeding means for internal-combustion engines. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US48820409A US1066939A (en) | 1909-04-06 | 1909-04-06 | Feeding means for internal-combustion engines. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1066939A true US1066939A (en) | 1913-07-08 |
Family
ID=3135182
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US48820409A Expired - Lifetime US1066939A (en) | 1909-04-06 | 1909-04-06 | Feeding means for internal-combustion engines. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1066939A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3913548A (en) * | 1974-06-11 | 1975-10-21 | Ora E Wilson | Fuel injection engine |
-
1909
- 1909-04-06 US US48820409A patent/US1066939A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3913548A (en) * | 1974-06-11 | 1975-10-21 | Ora E Wilson | Fuel injection engine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3699939A (en) | Fuel injection pump for internal combustion engines and method of fuel control | |
| US4083345A (en) | Fuel injection pump | |
| US2322606A (en) | Internal combustion engine | |
| US3104817A (en) | Fuel injector with pilot injection | |
| US2352267A (en) | Motor | |
| US2946292A (en) | Liquid fuel pumps for internal combustion engines | |
| US1698102A (en) | Construction and method of operating crankless internal combustion and explosion engines | |
| US1497258A (en) | Internal-combustion engine | |
| US1948047A (en) | Fuel pump | |
| US1139898A (en) | Internal-combustion engine. | |
| US2067997A (en) | Fuel injector for internal combustion engines | |
| US3403629A (en) | Fuel injection pump for internal combustion engines | |
| US1290374A (en) | Oil-feeding mechanism for internal-combustion engines. | |
| US1918076A (en) | Internal combustion engine | |
| US1683040A (en) | Working oil engine | |
| US1610997A (en) | Fuel pump for internal-combustion engines | |
| US923054A (en) | Combustion-engine. | |
| US3079862A (en) | Piston pumps, in particular for the injection of fuel into internal combustion engines | |
| US998463A (en) | Internal-combustion engine. | |
| US1019563A (en) | Gas-engine. | |
| US3097607A (en) | Liquid fuel pumps | |
| US1677202A (en) | Means for introducing oil or liquid-fuel charges into internal-combustion engines | |
| US2195037A (en) | Fuel metering and injecting device for internal combustion engines | |
| US920989A (en) | Combustion-engine. | |
| US3016835A (en) | Self-regulating reciprocating action pumps |