US960057A - Means for feeding fluid fuel. - Google Patents
Means for feeding fluid fuel. Download PDFInfo
- Publication number
- US960057A US960057A US54082210A US1910540822A US960057A US 960057 A US960057 A US 960057A US 54082210 A US54082210 A US 54082210A US 1910540822 A US1910540822 A US 1910540822A US 960057 A US960057 A US 960057A
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- Prior art keywords
- fuel
- piston
- cylinder
- air
- chamber
- 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 28
- 239000012530 fluid Substances 0.000 title description 9
- 230000006835 compression Effects 0.000 description 11
- 238000007906 compression Methods 0.000 description 11
- 230000001105 regulatory effect Effects 0.000 description 4
- 239000002360 explosive Substances 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 230000001276 controlling effect Effects 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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
- F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
- F02M69/08—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by the fuel being carried by compressed air into main stream of combustion-air
Definitions
- the object of my invention is to provide an improved device. of this character by means of which fuel in regulated quantities and at proper intervals may be injected into the combustion chamber of the engine, the motive power for injecting the fluid into such 'chamber being derived from a pump operated by the engine.
- the numeral 2 designates the cylinder of a gas engine of the two-cycle type; 3 the usual water jacket therefor, 4 the engine piston, 5 the crank shaft, and 6 the sparker or igniterl.
- .15 is a fuel discharge plug, which is threaded into the end of the enlarged portion 14 of the discharge port.
- the shell 9 is 4provided with an interior chamber 18, into which is screwed a plug 19.
- the plug is also formed with a chamber or passage to receive a needle valve 20 threaded therein, the inner end portion of the needle valve being of less' diameter than the diameter of the chamber lor passage in the plug,
- the plug 19 has an annular groove 22 opposite the inner end of the fuel feed pipe 10, an( the bottom of this groove communicates with the interior space 21a of the plug by means o f a plurality of ports 23.
- the needle valve controls the discharge of fuel from the space 21El into theV port 13, and can be set so as to regulate the quantity of'discharge, being held in the desired adjustment by means of a lock or jam nut 24.
- Theinner end portion of the plug 20 is of reduced diameter, providing an air space into which the air pipe ll-discharges.
- the plug 19 can be screwed in or out so as to control the amount of air which willbe discharged from the chamber 18 into the port 13 with the fuel, being held in the desired adjustment by means -of a lock or jam nut 25.
- the air supply pipe 11 is connected at its other end to a cylinder 26 having therein ⁇ a piston valve 27 which controls the outlet from the cylinder to the pipe 11, and also having therein a piston 28.
- the piston valve 27 has a stem 29 which extends outwardly through the head 30 of the cylinder 26, where it is secured by a nut 31, or by other suitable means.
- a spring 29a is seated around said stem between tie valve and the inner wall of the head 30.
- the piston 28 has a rod 32 projecting through the opposite head 33 of the cylinder 26, and carries at its outer end a roller 33a, which engages a cam 34 on the crank shaft 5.
- the piston rod 32 is provided with a threaded portion 32a carrying a nut 35 exteriorly of the cylinder, a spring 36 being seated around the rod between this nut andthe out-er side of the cylinder head 33.
- the cam 34.- actuates the piston 28 on its compression stroke and the s ring 36 returns the piston after the comp etion of its compression stroke.
- the cylinder 26 is provided with air inlet ports or openings 37, which are arranged to be uncovered by the piston 28 on its return stroke and to be closed by said piston at an early point in its compression stroke.
- the operation is as follows :-The cam 34 is so set that the piston 28 will commence its compression stroke a short time before the engine piston 4 has completed its power stroke.
- the continued forward movement of the piston 28 effects a compression of air within the cylinder 26, admitted through the ports or openings 37, until a degree of compression is reached sufficient to overcome the pressure on the pistonvalve 27 exerted by the spring 32, and which pressure can be regulated to the desired extent by means of the nut 31.
- the piston valve 27 is then moved backwardly to expose the entrance to the air supply pipe 11, and the compressed air in the cylinder 26 is discharged through said pipe into the chamber 18 of the injector.
- the fluid fuel such as gasolene
- the fluid fuel which enters thel injector through the pipe 10 fills the groove or depression 22 and flows through the ports 23 into the chamber 21a, in which the needle valve is placed.
- the pressure discharged into the chamber 18 ⁇ through the pipe 11 meets the fuel discharged past the needle valve, and blows said fuel through port 13 and plug 15 into the engine cylinder, the pressure of the air being sufficient to unseat the ball valve 16. This operation will be repeated on each alternate stroke of the engine piston 4:.
- the relative quantities of gas and fuel admitted at each operation may be regulated, as may be desired. Any excessive pressure between the piston 28 and the piston valve 27 caused by the admission of a less volume of air into the engine cylinder with the fuel than the volume which is compressed between the piston 28 and the piston valve 27, is taken care of by the further backward movement of the piston valve against the action of its spring 29a.
- my invention is equally applicable to four cycle engines, by causing the piston rod 32 to be actuated from a half speed shaft instead of directly from the main shaft of the engine.
- the cylinder 26 may be variously arranged, and its piston may be actuated by any desired timed connection with a moving part ofthe engine, the arranvement shown in the drawing being intendad simply to illustrate a simple arrangement for actuating the air compressing piston.
- the engine can be provided with governing mechanism of any usual or desired character.
- Various changes may also be made in the construction and arrangement of the injector parts without departing from my invention.
- the apparatus described forms a reliable and efficient means for feeding fuel to explosive engines, or for other purposes.
- the air compressor is of a simple and eiiicient type, no valves being required, except the piston valve 27, the piston 28 acting itself as a valve to control the admission to the compressor cylinder.
- an injector comprising a casin or shell having a chamber therein provlded with a discharge port leading from its inner end, a valve seatin backwardly to close said port, a pluga justably seated within the chamber of the shell or casing, an air supply pipe communicating with said chamber, a fuel discharge in said plug, an adjustable valve for controlling said passage, the plug having fuel ports communicating with a fuel supply, and means for periodically admitting a volume of compressed air to said chamber; substantially as described.
- a fluid fuel injector comprising a plug or casing having a chamber therein, and a port leading from the inner end of said chamber, said port having a backwardly seating valve, an air supply pipe communicating with said chamber, means for periodically admitting a volume of compressed air through said pipe, a plug adjustably seated in said chamber and having a reduced Vinner end portion acting as a valve.
- said plug also having-fan annular groove or depression therein communicating with a fuel supply, with ports leading from said depression into an interior fchamber in the plug, and a needle valve adjustably seated in said plug and controlling the outlet from said chamber, the outlet from said chamber being in line with the said .discharge port; substantially as described.
- Means for feeding fluid fuel comprising an injector'having a fuel supply, and an air supplly,
- a fuel feeding I injector having a Afuel supply and an air supply, an air compressing cylinder to which the air su ply is connected, and means for periodica y delivering ⁇ a volume of compressed ar from said cylinder into the air supply land thence into the inj ectojr, together with t
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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
T. TURNBULL., JR. MEANS FOREBEDING FLUID FUEL.
APPLICATION FILED JAN. 29, 1910.
Patented May 31, 1910.
2 SHEETS-SHEET 1.
INVENTOR WITNESSES T. TURNBULL, JR. MEANS FOR FEEDING FLUID FUEL.
APPLICATION FILED JAN. 29, 1M
2 gxnglT'sTsnnmj z.
l Patented May 31,
Z7 IIIIIIIIIII WITNESSES www.
THOMAS TURNBLL, JR., OF PITTSBURG, PENNSYLVANIA.
MEANS FOR` FEEDING FLUID FUEL.
I Specication of Letters Patent. y Patented luay 31, 1910.
Application led January 29, 1910. Serial N o. 540,822.
To all lwhom 'it may concern:
Be it known that l, THOMAS TURNBULL, Jr., of Pittsburg, Allegheny county, Penn- Sylvania, have invented a new and useful Means for Feeding Fluid Fuel, of which the following is a full, clear, and exact description, reference being had to the accompanying drawings, forming part of this speci signed to provide fuel-feeding means for use with explosive engines.
The object of my invention is to provide an improved device. of this character by means of which fuel in regulated quantities and at proper intervals may be injected into the combustion chamber of the engine, the motive power for injecting the fluid into such 'chamber being derived from a pump operated by the engine.
The precise nature of my invention will be best understood by reference to the accompanying drawings, in whichl have shown the preferred embodiment thereof, and which will now be described, it being premised, however, that various changes may be iliade in the details of construction and arrangement of the several parts, by those skilled in the art, without departing from the spirit and scope. of my invention as defined in the appended claims.
ln these drawings, the numeral 2 designates the cylinder of a gas engine of the two-cycle type; 3 the usual water jacket therefor, 4 the engine piston, 5 the crank shaft, and 6 the sparker or igniterl.
7 designates the exhaust openings, and 8 an airadmission, which is arranged opposite the exhaust opening 7 and into which air enters under compression from the cranky ease chamber as is usual in two-cycle enguies.
9 designates the outer shell or casing of a fuel injector having a fuel admission pipe 10 and an air admission pipe 11. This shell is provided with a screw-threaded extension 12 at one end, which is screwed into thecylinder wall, and through which extends the discharge port 13, said port being enlarged at 14.
.15 is a fuel discharge plug, which is threaded into the end of the enlarged portion 14 of the discharge port.
16 is' a ball valve, seated within the enlarged portion 14 of the port and normally holding the port 13 closed, by means of a spring 17 to prevent back-fiashng.
The shell 9 is 4provided with an interior chamber 18, into which is screwed a plug 19. The plug is also formed with a chamber or passage to receive a needle valve 20 threaded therein, the inner end portion of the needle valve being of less' diameter than the diameter of the chamber lor passage in the plug,
vas indicated at 21. The plug 19 has an annular groove 22 opposite the inner end of the fuel feed pipe 10, an( the bottom of this groove communicates with the interior space 21a of the plug by means o f a plurality of ports 23. The needle valve controls the discharge of fuel from the space 21El into theV port 13, and can be set so as to regulate the quantity of'discharge, being held in the desired adjustment by means of a lock or jam nut 24. Theinner end portion of the plug 20 is of reduced diameter, providing an air space into which the air pipe ll-discharges. The plug 19 can be screwed in or out so as to control the amount of air which willbe discharged from the chamber 18 into the port 13 with the fuel, being held in the desired adjustment by means -of a lock or jam nut 25.
The air supply pipe 11 is connected at its other end to a cylinder 26 having therein` a piston valve 27 which controls the outlet from the cylinder to the pipe 11, and also having therein a piston 28. The piston valve 27 has a stem 29 which extends outwardly through the head 30 of the cylinder 26, where it is secured by a nut 31, or by other suitable means. A spring 29a is seated around said stem between tie valve and the inner wall of the head 30. The piston 28 has a rod 32 projecting through the opposite head 33 of the cylinder 26, and carries at its outer end a roller 33a, which engages a cam 34 on the crank shaft 5. The piston rod 32 is provided with a threaded portion 32a carrying a nut 35 exteriorly of the cylinder, a spring 36 being seated around the rod between this nut andthe out-er side of the cylinder head 33. The cam 34.- actuates the piston 28 on its compression stroke and the s ring 36 returns the piston after the comp etion of its compression stroke.'
The cylinder 26 is provided with air inlet ports or openings 37, which are arranged to be uncovered by the piston 28 on its return stroke and to be closed by said piston at an early point in its compression stroke.
The operation is as follows :-The cam 34 is so set that the piston 28 will commence its compression stroke a short time before the engine piston 4 has completed its power stroke. The continued forward movement of the piston 28 effects a compression of air within the cylinder 26, admitted through the ports or openings 37, until a degree of compression is reached sufficient to overcome the pressure on the pistonvalve 27 exerted by the spring 32, and which pressure can be regulated to the desired extent by means of the nut 31. The piston valve 27 is then moved backwardly to expose the entrance to the air supply pipe 11, and the compressed air in the cylinder 26 is discharged through said pipe into the chamber 18 of the injector. The fluid fuel, such as gasolene, which enters thel injector through the pipe 10 fills the groove or depression 22 and flows through the ports 23 into the chamber 21a, in which the needle valve is placed. The pressure discharged into the chamber 18` through the pipe 11 meets the fuel discharged past the needle valve, and blows said fuel through port 13 and plug 15 into the engine cylinder, the pressure of the air being sufficient to unseat the ball valve 16. This operation will be repeated on each alternate stroke of the engine piston 4:.
As before stated, by adjusting the needle valve and the plug 19, the relative quantities of gas and fuel admitted at each operation may be regulated, as may be desired. Any excessive pressure between the piston 28 and the piston valve 27 caused by the admission of a less volume of air into the engine cylinder with the fuel than the volume which is compressed between the piston 28 and the piston valve 27, is taken care of by the further backward movement of the piston valve against the action of its spring 29a.
It will be readily understood that my invention is equally applicable to four cycle engines, by causing the piston rod 32 to be actuated from a half speed shaft instead of directly from the main shaft of the engine. In fact, the cylinder 26 may be variously arranged, and its piston may be actuated by any desired timed connection with a moving part ofthe engine, the arranvement shown in the drawing being intendad simply to illustrate a simple arrangement for actuating the air compressing piston.
Various fuels require different degrees of compression in the engine cylinder, and hence should be supplied to the cylinder at different pressure and at diii'erenttimes in the compression stroke. This can be readily and accurately regulated by adjusting the tension of the spring 29a to thereby vary the degree of compression in the cylinder 26 which will be reached before the piston valve 27 will be moved to uncover thev entrance to the pipe 11. It is obvious that the greater the tenslon given the sprin 29a, the greater will be the compression e ected in the cylinder 26, and the later will the charge be injected into the engine cylinder. Therefore the fuel charge can be injected into the engine cylinder at any point in thecompression stroke of the engine piston. The volume of air which enters the engine cylinder will, of course remain constant with all adjustments of the spring 29a.
The engine can be provided with governing mechanism of any usual or desired character. Various changes may also be made in the construction and arrangement of the injector parts without departing from my invention.
The apparatus described forms a reliable and efficient means for feeding fuel to explosive engines, or for other purposes.
It will be noted that the air compressor is of a simple and eiiicient type, no valves being required, except the piston valve 27, the piston 28 acting itself as a valve to control the admission to the compressor cylinder.
What I claim is 1. In apparatus of the character described, an injector comprising a casin or shell having a chamber therein provlded with a discharge port leading from its inner end, a valve seatin backwardly to close said port, a pluga justably seated within the chamber of the shell or casing, an air supply pipe communicating with said chamber, a fuel discharge in said plug, an adjustable valve for controlling said passage, the plug having fuel ports communicating with a fuel supply, and means for periodically admitting a volume of compressed air to said chamber; substantially as described.
2. In apparatus of the character described, a fluid fuel injector comprising a plug or casing having a chamber therein, and a port leading from the inner end of said chamber, said port having a backwardly seating valve, an air supply pipe communicating with said chamber, means for periodically admitting a volume of compressed air through said pipe, a plug adjustably seated in said chamber and having a reduced Vinner end portion acting as a valve. for the discharge port, said plug also having-fan annular groove or depression therein communicating with a fuel supply, with ports leading from said depression into an interior fchamber in the plug, and a needle valve adjustably seated in said plug and controlling the outlet from said chamber, the outlet from said chamber being in line with the said .discharge port; substantially as described.
3. Means for feeding fluid fuel, comprising an injector'having a fuel supply, and an air supplly,
an air com ressin' g cylinder to which t e .air sulppl ips connected, and means for periodica y elivering avolume of compressed air from said cylinder into the air supply, and thence into the injector, together with means for varyin the pressure of said air; substantially as described.
4. In an explosive engine, a fuel feeding I injector having a Afuel supply and an air supply, an air compressing cylinder to which the air su ply is connected, and means for periodica y delivering `a volume of compressed ar from said cylinder into the air supply land thence into the inj ectojr, together with t In testimony whereof, I have hereunto y set my hand. l THOMAS "IURNBULL, JIL
Witnesses: I' A 'l GEO. H. Panmimnn, H. M. -Conwnn
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US54082210A US960057A (en) | 1910-01-29 | 1910-01-29 | Means for feeding fluid fuel. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US54082210A US960057A (en) | 1910-01-29 | 1910-01-29 | Means for feeding fluid fuel. |
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US960057A true US960057A (en) | 1910-05-31 |
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US54082210A Expired - Lifetime US960057A (en) | 1910-01-29 | 1910-01-29 | Means for feeding fluid fuel. |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2482864A (en) * | 1944-12-01 | 1949-09-27 | Margaret Nemnich | Liquid fuel carburetor |
US2720845A (en) * | 1951-12-14 | 1955-10-18 | Automatic Pump & Softener Corp | Ejector nozzle |
US4408574A (en) * | 1978-10-25 | 1983-10-11 | Josef Schaich | Method and apparatus for forming fuel-air mixture in an internal combustion engine |
US4836453A (en) * | 1988-02-22 | 1989-06-06 | Outboard Marine Corporation | Fuel injector with continuous air flow |
-
1910
- 1910-01-29 US US54082210A patent/US960057A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2482864A (en) * | 1944-12-01 | 1949-09-27 | Margaret Nemnich | Liquid fuel carburetor |
US2720845A (en) * | 1951-12-14 | 1955-10-18 | Automatic Pump & Softener Corp | Ejector nozzle |
US4408574A (en) * | 1978-10-25 | 1983-10-11 | Josef Schaich | Method and apparatus for forming fuel-air mixture in an internal combustion engine |
US4836453A (en) * | 1988-02-22 | 1989-06-06 | Outboard Marine Corporation | Fuel injector with continuous air flow |
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