US2353430A - Fuel and air regulating means for engines - Google Patents
Fuel and air regulating means for engines Download PDFInfo
- Publication number
- US2353430A US2353430A US432711A US43271142A US2353430A US 2353430 A US2353430 A US 2353430A US 432711 A US432711 A US 432711A US 43271142 A US43271142 A US 43271142A US 2353430 A US2353430 A US 2353430A
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- US
- United States
- Prior art keywords
- valve
- fuel
- air
- ports
- regulating means
- 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 18
- 230000001105 regulatory effect Effects 0.000 title description 8
- 238000002485 combustion reaction Methods 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 238000010276 construction Methods 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/34—Ultra-small engines, e.g. for driving models
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D9/00—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2700/00—Mechanical control of speed or power of a single cylinder piston engine
- F02D2700/02—Controlling by changing the air or fuel supply
- F02D2700/0217—Controlling by changing the air or fuel supply for mixture compressing engines using liquid fuel
- F02D2700/0225—Control of air or mixture supply
- F02D2700/0228—Engines without compressor
- F02D2700/023—Engines without compressor by means of one throttle device
Definitions
- This invention relates to means for controlling the admission of fuel and combustion supporting air to internal combustion engines, and has particular reference to means for this purpose as disclosed in my prior application, Serial No. 278,772, filed June 12, 1939, now Patent No. 2,274,644 dated March 3, 1942, of which the present application is a division.
- the object of the present invention is to provide asimple, practical Valve means to enable a wide range in regulation of the proportionate amounts of fuel and air to be obtained to facilitate engine starting and'high engine operating efficiency at variou different speeds.
- Figure 1 is a central, longitudinal section through a portion of an internal combustion engine equipped with a fuel and air admission regulating means constructed in accordance with one practical embodiment of the invention.
- Figure 2 is a central cross section through the structure shown in Fig. 1;
- Figures 3 and 4 are cross sections through the repective air inlet port portions of the regulating means.
- l designates a portion of the crank case of an internal combustion engine
- l4 designates the crank shaft of the engine journaled in the front wall of said crank case
- 33 designates a longitudinal bore in the crank shaft I 4 opening through the inner end of said crank shaft into said crank case
- 34 designates a lateral port in said crank shaft to provide communication at predetermined times between the bore 33 and a fuel and air supply I duct 35 in the front wall of the crank case
- crank case Ill designates an elongated, cylindrical valve chamber in the bottom portion of the crank case Ill communicating at one end with the duct 35.
- valve chamber 36 In the valve chamber 36 is rotatably mounted a hollow, cylindrical valve 3! which closely fits said chamber and which is open at its end adjacent the duct 35 to afford communication between the interior thereof and said duct. At its other end said valve is closed and provided with a'suitable handle 38 for use in manually, rotatably adjusting the same.
- a hollow, cylindrical valve 3! which closely fits said chamber and which is open at its end adjacent the duct 35 to afford communication between the interior thereof and said duct.
- said valve At its other end said valve is closed and provided with a'suitable handle 38 for use in manually, rotatably adjusting the same.
- said valve In said valve,.media1ly thereof, is a .circumferentially. extending slot .39'
- a fuel nozzle 42 which is threaded into an opening in the .wall defining the chamber 38 and which maybe .connected with any suitable source of fuel supply.
- the valve thus is held in said chamber by said nozzle 4!), the latter serving at the same time, as an abutment engageable by the walls defining the ends of the slot'39 to limit rotative adjust.- ments of the valve.
- the wall defining the chamber In the wall defining the chamber are two air inlet ports .4! and 42, While in the side wallof the valve 37 are two .air inlet ports at and M for cooperation, respectively, with the ports .41! and 42.
- the ports M, 43 are disposed inwardl with respect to the nozzle Mi; that is to say, between said nozzle and the duct 35.
- the ports 42, 44 are disposed outwardly with respect to the nozzle 40; that is to say, to the side of said nozzle remote from the duct 35.
- valve 31 is rotatable through an angle of approximately and the ports M, 43 and 42, M are of such circumferential lengths that when said valve is at its limit of rotation in one direction both ports 4! and 42 are closed, while when said valve is at its limit of rotation in the other direction both ports 43 and 44 are alined with the ports 4i and 62, respectively, and air is free to enter the valve through both pairs of ports.
- the port 45 is longer than the port 43 and is disposed so that it begins to uncover the port 42 immediately upon rotation of the valve from its first mentioned position toward its second mentioned position and thereafter maintains said port 32 open during such rotation of the valve.
- the shorter-length port 43 is disposed relative to the port 43 to begin to open the port 3!
- valve chamber 36 is disposed at the bottom of the crank case H1, asshown, although it may be disposed elsewhere if desired.
- the described arrangement affords .a simple, practical means especially suited for miniature engine use to enable a wide range of fuel and air mixing regulation.
- the engine partially illustrated is of the twostroke-cycle type in which the fuel and air is admitted to the crank case In under the co ntrol of the .valve means comprisedby the port. 34 in the crank shaft I4 in cooperation with the bore ;33 in said crank shaft and the duct 35 in the crank case, and from, the .crank case I0 .is deliveredto the combustion chamber of the; engine .in any well known or desired manner.. It is to be.understood,however, that thepresent fuel and air admission regulating means is not restricted'ito use with two-stroke-cycle engines and is.
- valve having a circumferentially lextendingslot, and a fuel nozzle carried by said crank case and extending into said slot, thereby holding said valve against longitudinal movement in said bore, said crankcase and valve having airiadmission Iports disposed, longitudinally withrespect to said valve, at opposite sides of said nozzle, respectively, for cooperation by rotatiorr of said vvalvetoregulate admission ofair into said yalve.
- Iports disposed, longitudinally withrespect to said valve, at opposite sides of said nozzle, respectively, for cooperation by rotatiorr of said vvalvetoregulate admission ofair into said yalve.
- valve-accommodating bore .andlaufuelsupply' duct .fonthe engine leading from saidlbore ahollow cylindrical valve open at one end and closedeat its other end and'rotatably mounted insaid bore and havingits interior in communication through its openendwith said duct, and a nozzle disposed. torsupply fuel intosaid valve at apoint intermediate its ends, said. crank case and valve having cooperating pairs, of air inlet ports disposed, longitudinally with respect .to said valve, at opposite sides. of said nozzle, respectively, to regulate supply of air and fuel to the interior of said' valve responsive to rotatableadjustment. of said valve. 7 f
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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
' July 11, 1944. I T, R, A DEN 2,353,430
FUEL AND AIR REGULATING MEANS FOR ENGINES Original Filed June 12, 1959 Patented July 11, 1944 FUEL AND AIR REGULATING MEANS FOR ENGINES Thomas R. Arden, Danbury, Conn.
Original application June 12, 1939, Serial No. 278,772. Divided and this application February 27, 1942, Serial No. 432,711
2 Claims.
This invention relates to means for controlling the admission of fuel and combustion supporting air to internal combustion engines, and has particular reference to means for this purpose as disclosed in my prior application, Serial No. 278,772, filed June 12, 1939, now Patent No. 2,274,644 dated March 3, 1942, of which the present application is a division.
Generally speaking, the object of the present invention is to provide asimple, practical Valve means to enable a wide range in regulation of the proportionate amounts of fuel and air to be obtained to facilitate engine starting and'high engine operating efficiency at variou different speeds.
With the foregoing general object and various other objects in View, which will become more fully apparent as the nature of the invention is better understood, the same consists in a fuel and air admission regulating means embodying the novel features of construction, combination and arrangement of parts as will be hereinafter more fully described, illustrated in the accompanying drawing and defined in the appended claims.
In the accompanying drawing, wherein like characters of reference denote corresponding parts in the different views:
Figure 1 is a central, longitudinal section through a portion of an internal combustion engine equipped with a fuel and air admission regulating means constructed in accordance with one practical embodiment of the invention.
Figure 2 is a central cross section through the structure shown in Fig. 1; and
Figures 3 and 4 are cross sections through the repective air inlet port portions of the regulating means.
Referring to the drawing in detail, l designates a portion of the crank case of an internal combustion engine, l4 designates the crank shaft of the engine journaled in the front wall of said crank case, 33 designates a longitudinal bore in the crank shaft I 4 opening through the inner end of said crank shaft into said crank case, 34 designates a lateral port in said crank shaft to provide communication at predetermined times between the bore 33 and a fuel and air supply I duct 35 in the front wall of the crank case, and
36 designates an elongated, cylindrical valve chamber in the bottom portion of the crank case Ill communicating at one end with the duct 35.
In the valve chamber 36 is rotatably mounted a hollow, cylindrical valve 3! which closely fits said chamber and which is open at its end adjacent the duct 35 to afford communication between the interior thereof and said duct. At its other end said valve is closed and provided with a'suitable handle 38 for use in manually, rotatably adjusting the same. In said valve,.media1ly thereof, is a .circumferentially. extending slot .39'
in which is disposed the inner end of a fuel nozzle 42 which is threaded into an opening in the .wall defining the chamber 38 and which maybe .connected with any suitable source of fuel supply. The valve thus is held in said chamber by said nozzle 4!), the latter serving at the same time, as an abutment engageable by the walls defining the ends of the slot'39 to limit rotative adjust.- ments of the valve.
In the wall defining the chamber are two air inlet ports .4! and 42, While in the side wallof the valve 37 are two .air inlet ports at and M for cooperation, respectively, with the ports .41! and 42. The ports M, 43 are disposed inwardl with respect to the nozzle Mi; that is to say, between said nozzle and the duct 35. On the other hand, the ports 42, 44 are disposed outwardly with respect to the nozzle 40; that is to say, to the side of said nozzle remote from the duct 35.
In the present instance the valve 31 is rotatable through an angle of approximately and the ports M, 43 and 42, M are of such circumferential lengths that when said valve is at its limit of rotation in one direction both ports 4! and 42 are closed, while when said valve is at its limit of rotation in the other direction both ports 43 and 44 are alined with the ports 4i and 62, respectively, and air is free to enter the valve through both pairs of ports. The port 45 is longer than the port 43 and is disposed so that it begins to uncover the port 42 immediately upon rotation of the valve from its first mentioned position toward its second mentioned position and thereafter maintains said port 32 open during such rotation of the valve. On the other hand, the shorter-length port 43 is disposed relative to the port 43 to begin to open the port 3! only after the port 42 has been fully opened by rotation of the valve 31 from its first mentioned position toward its second mentioned position. Because of this arrangement, initial rotation of the valve from its first mentioned position toward its second mentioned position results in opening of the port 42 and maintenance of the port it closed. Air then is drawn only through the ports 42, 44, and since air drawn through these ports is required to flow over the fuel nozzle iii in order to reach the duct 35, an effective mixing of fuel and air results. If a rich mixture is desired the valve 31 is rotated to aline greater or lesser areas of the ports 42, 44, depending upon the mixture richness desired. In any event, the valve is not rotated so far as they aline, or partly aline, the ports 4|, 43. On the other hand, if a lean mixture is desired the valve is further rotated to aline the ports Al, 43 to a greater or lesser extent, depending upon the mixture leanness desired. Air entering the valve through the'po'rts 4|, 43 does not flow over the nozzle 40 and, therefore, as lean a mixture as desired may be obtained. a 7
Preferably the valve chamber 36 is disposed at the bottom of the crank case H1, asshown, although it may be disposed elsewhere if desired. In any event, the described arrangement affords .a simple, practical means especially suited for miniature engine use to enable a wide range of fuel and air mixing regulation. I v
The engine partially illustrated is of the twostroke-cycle type in which the fuel and air is admitted to the crank case In under the co ntrol of the .valve means comprisedby the port. 34 in the crank shaft I4 in cooperation with the bore ;33 in said crank shaft and the duct 35 in the crank case, and from, the .crank case I0 .is deliveredto the combustion chamber of the; engine .in any well known or desired manner.. It is to be.understood,however, that thepresent fuel and air admission regulating means is not restricted'ito use with two-stroke-cycle engines and is. not necessarily embodied in orassociated with an engine in the manner specifically illustrated in the drawing but, on the'contrary, may be used on four-or-more-stroke-cycle.engines and may be operatively associated with any given engine in any suitable manner otherthan the specific manner illustrated in the drawing. Furthermore, it is to be understood that the. regulating means itself is not necessarily of the specific said duct, said valve having a circumferentially lextendingslot, and a fuel nozzle carried by said crank case and extending into said slot, thereby holding said valve against longitudinal movement in said bore, said crankcase and valve having airiadmission Iports disposed, longitudinally withrespect to said valve, at opposite sides of said nozzle, respectively, for cooperation by rotatiorr of said vvalvetoregulate admission ofair into said yalve. .Inaninternal.Vcombustionengine a crank case havingtherein a. valve-accommodating bore .andlaufuelsupply' duct .fonthe engine leading from saidlbore, ahollow cylindrical valve open at one end and closedeat its other end and'rotatably mounted insaid bore and havingits interior in communication through its openendwith said duct, and a nozzle disposed. torsupply fuel intosaid valve at apoint intermediate its ends, said. crank case and valve having cooperating pairs, of air inlet ports disposed, longitudinally with respect .to said valve, at opposite sides. of said nozzle, respectively, to regulate supply of air and fuel to the interior of said' valve responsive to rotatableadjustment. of said valve. 7 f
' THOMAS R. ARDEN;
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US432711A US2353430A (en) | 1939-06-12 | 1942-02-27 | Fuel and air regulating means for engines |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US278772A US2274644A (en) | 1939-06-12 | 1939-06-12 | Internal combustion engine and adjuncts therefor |
| US432711A US2353430A (en) | 1939-06-12 | 1942-02-27 | Fuel and air regulating means for engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2353430A true US2353430A (en) | 1944-07-11 |
Family
ID=26959268
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US432711A Expired - Lifetime US2353430A (en) | 1939-06-12 | 1942-02-27 | Fuel and air regulating means for engines |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2353430A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2658489A (en) * | 1952-03-14 | 1953-11-10 | Putt J Lewis | Internal-combustion engine |
-
1942
- 1942-02-27 US US432711A patent/US2353430A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2658489A (en) * | 1952-03-14 | 1953-11-10 | Putt J Lewis | Internal-combustion engine |
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