US2004178A - Automatic fuel regulator - Google Patents
Automatic fuel regulator Download PDFInfo
- Publication number
- US2004178A US2004178A US147250A US14725026A US2004178A US 2004178 A US2004178 A US 2004178A US 147250 A US147250 A US 147250A US 14725026 A US14725026 A US 14725026A US 2004178 A US2004178 A US 2004178A
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- orifices
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- liquid fuel
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- 239000000446 fuel Substances 0.000 title description 25
- 239000007788 liquid Substances 0.000 description 24
- 230000001276 controlling effect Effects 0.000 description 7
- 238000002485 combustion reaction Methods 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 230000001133 acceleration Effects 0.000 description 4
- 230000033001 locomotion Effects 0.000 description 4
- 238000010276 construction Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000037452 priming Effects 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
- F02M7/00—Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
- F02M7/23—Fuel aerating devices
- F02M7/24—Controlling flow of aerating air
- F02M7/28—Controlling flow of aerating air dependent on temperature or pressure
-
- 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
- F02M1/00—Carburettors with means for facilitating engine's starting or its idling below operational temperatures
- F02M1/04—Carburettors with means for facilitating engine's starting or its idling below operational temperatures the means to facilitate starting or idling being auxiliary carburetting apparatus able to be put into, and out of, operation, e.g. having automatically-operated disc valves
- F02M1/046—Auxiliary carburetting apparatus controlled by piston valves
-
- 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
- F02M3/00—Idling devices for carburettors
- F02M3/08—Other details of idling devices
Definitions
- My invention relates to improvements in automatic fuel regulation for internal combustion engines.
- Another object of my invention is to provide asimple, cheap and eicient carburetor having a minimum of moving parts.
- Fig. 1 is a vertical sectional view of my carburetor with my improvements incorporated therein.
- Fig. 2 is a view showing my invention attached to an internal combustion engine.
- Fig. 3 is a sectional view showing the mecha.-
- Fig. 4 is a transverse sectional view of part of Fig. 2.
- Fig. 5 is a sectional view of part of Fig. 4.
- Fig. 6 is an alternative construction for part of Fig. 4.
- Fig. 7 is 'an alternative construction for part of Figs. 1 and 3.
- Fig. 8 is an enlargedfragmentary sectional view of the discharge nozzle.
- An internal combustion engine I has the usual exhaust pipe 2 and intake pipe 3, to which latter is attached a carburetor 4 having an air inlet 5 connected by a hot air pipe 6 to a stove 1 surrounding exhaust pipe 2.
- a metal block 8 extends from exhaust pipe 2 and has mounted thereon a bi-metallic thermostat 9 adapted to operate through suitable mechanism I8 for controlling the action of carburetor 4.
- Carburetor 4 is fed by any suitable system with liquid fuel through a pipe II and comprises a mixing chamber I2 containing a large venturi I3 and a small venturi I4 adapted to discharge at the throat of large venturi I3.
- Liquid fuel through pipe I I passes into a liquid reservoir I5, maintained substantially at a constant level X--X, containing a iloat I6 operating in a well known manner a valve (not shown) for controlling the inlet of liquid fuel through pipe I I.
- Reservoir I5 is closed by a cover I1 and is open to atmosphere through a port I8.
- Liquid fuel passes through a passage I9 to the lower part of a well 20 which latter is divided into an upper and lower section by a plug 2I supporting a tube 22. 'Ihe lower part of well 20 is closed by a plug 23 containing a passage 24 and supporting a tube 25 and passage 24 leads to a passage 26 and a nozzle 21.
- a second nozzle 28 surrounds nozzle 21 and is adapted to register through a passage 29 with the upper part of well 20.
- a small orifice 38 is drilled in nozzle 21 for permitting liquid fuel, in restricted quantity, to ow from the upper part of well 20 to the interior of tube 25.
- Tube 25 has ceremoniess 3
- Air is supplied to well 20 through an airiadjusting valve 32.
- a throttle 33 controls the discharge of liquid fuel and air from carburetor 4 to the cylinders of engine I, responsive to the vacuum therein.
- valve 36 which in turn controls the passage of liquid fuel and air through the valve 36 by way of a restricted tone 31 as will presently appear.
- a disc 38 On the outer end of valve 36 is mounted a disc 38.
- Valve 36 contains a plurality of liquid fuel orifices 39 and a plurality of air orifices 40, the fuel orifices 39 being adapted to register at times with the upper discharge of tube 25 and the air orifices 48 being adapted to register at times with atmosphere through the regulating valve 4I.
- Valve 36 has an annular groove 42 cut therein .with a tapered portion 43 adapted to control at times the supply of air to the upper portion of well 20 through passages 44 and 45.
- ⁇ end of valve 36 is squared to work through a guide 46 so that the positions of orifices 39 and 40 will always remain the same and a spring 41 encircles the outer end of valve 36 for limiting its movement in one direction, disc 38 limiting its movement in the other direction.
- Disc 38 is adapted to work in an enlarged extension 50 which is open to atmosphere through ports 48, suitable clearance being allowed between disc 38 The outer and casing 50.
- An orifice 49 is provided for suitably locking valve 36 in any predetermined position by means of a pin, or otherwise, if so desired.
- Casing 50 is adapted to contain ay rod 5I having a head 54 thereon and ⁇ a member 52 rests against thermostat 9 and contains a spring 53 working against head 54 to the end that the motion of thermostat 9 will be conveyed through spring 53 and rod 5
- Block 8 is adapted to contain valve 60 threaded into member 521 and adapted to work in an enlarged passage 6I for closing port 59 at times, the exhaust gases passing through port 59 are arranged to impinge on thermostat 9.
- spring 53 forms a substantially universal joint betweenmember 52 and rod 5I and in the alternative shown in Fig. 6.
- stem of valve 69 is adapted to move freelyin member 52 and. has a disc 62 provided on the end ofvalve 611 for fiexibly seating valve 6D.
- Tube 22 is provided with a plurality of 'liquid feed orifices 63, some of which are above and some below the liquid level X-X.
- a groove 64 is out in valve 36 and adapted to register at times with atmosphere through a passage 65 and groove 64 is connected with the interior of valve 36 through orifices 39.
- the upper ends of tubes 22 and 25 fit snugly in the metal of carburetor 4, the upper end of tube 22 being spaced a desired amount.
- valve 36 from the valve 36 to form a reservoir 66 of any desired content.
- valve 36 will be in the position shown in Fig. 3 due to the action of spring 41 and thus a plurality of the orifices 39 will be in registry with the upper discharge of tube 25 for raising liquid fuel and discharging the same in large volume through orifice 31 for priming the engine, it being noted at this time that only one, or perhaps none, of the orifices 49 is in connection with atmosphere through valve 4l.
- valve 36 At this time more of the .air orifices 40 will permit passage of atmosphere to the interior of valve 36, thus reducing the vacuum applied for raising liquid fuel through the remaining orifices 39 and groove 64 will also be open to atmosphere thus minimizing any tendency of the engine vacuum to draw liquid fuel between valve 36 and casing 35. Also at this time, the upper part of well will be in connection with atmosphere through port 45, groove 42 and passage 44. Thermostat 9, being in its fully contracted position, will thus not exert any influence on valve 36 and consequently, upon opening throttle 33 wide for sudden acceleration, valve 36 will be drawn by spring 41 to its outermost position as shown ⁇ in Fig.
- valve 36 is tapered at 34 on its inner end to form a projection in the air stream in chamber I 2 whereby a portion of the air, due to its velocity, impinges on said projection 34 and is diverted through orifices 31 and 39 to the interior of tube 25, this diversion being accentuated by the difference in vacuum on the engine side of throttle 33 and the throat of venturi I4.
- FIG. '1 A modification of this construction is shown in Fig. '1 wherein a deflecto'r 61 is provided in place of projection 34.
- thermostat 9 will expand to bring spring 53 and rod 5I gradually in contact with disc 38 whereby, when optimum engine operating temperatures are reached, valve 36 will be at its innermost position whereby when throttle 33 is closed at idling speeds, only one of the orifices 39 will register with the discharge from tube 25 for providing an idling mixture.
- orifices 63 and 39 can be determined only -by trial and may vary as to size depending on the engine to which they supply liquid fuel.
- a regulating valve 32 controls the vdischarge from orifices 63 at optimum temperatures and thereafter valve 36 automatically controls the degree of vacuum applied through nozzle 28 to the upper portion of well 20 for rais"- ing a column of liquid fuel therein and varying then head under which the same discharges throughorifices 63.
- v two wells are plying liquid fuel and air to engine I in the proper mixture proportions under all conditions of load, speed and temperature, one well comprising the provided for supvarying amounts of air bled into the wells with varying degrees of .vacuum on either side of throttle 33,y whereby these two compensating wells take care of engine operation under all conditions.
- valve 36 may be permitted certain movement only for operating under optimum ternperature conditions, as' described, and this can be accomplished by changing the position of disc 38 along valve 36, so that the outermost position of valve 36 may be limited as required for a given effect.
- Block 8 may be an integral part of exhaust pipe 2 and, as preferred, comprising a considerable block of metal capable of forming a reservoir for heat to the end that after engine I has been stopped for some time, thermostat 9 will be contracted more or less in proportion to the loss of heat from the engine itself, but passage 58 and'port 59 provide that thermostat 9 will be reactive in proportion asthe engine warms up and in this manner the control of carburetor 4 is assured for giving the eiects already described.
- a carburetor having an intake passage, a liquid fuel reservoir, a throttle in said passage, a well between the reservoir and said passage and connected to each, and deecting means in said passage for circulating air from the passage through the well and past said throttle.l
- a carburetor having a mixing chamber, a
- liquid fuel reservoir a throttle controlling the outlet from the mixing chamber, two wells between the reservoir and mixing chamber and connected to each and means responsive to temperature and vacuum for controlling the admission of air to both wells and detlecting means on the posterior side of said throttle for circulating air through the well and past said throttle.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of The Air-Fuel Ratio Of Carburetors (AREA)
Description
June 11, 1935. c. L. sToKEs 2,004,178
- I AUTOMATIC FUEL REGULATOR Filed Nov. 9, 192s Z INVENTOR Patented June 11, 1935 UNITED STATES PATENT OFFICE AUTOMATIC FUEL REGULATOR Charles L. Stokes, Los Angeles, Calif., assignor, by mesne assignments, to Lynn A. Williams, Evanston, Ill., and Clifford C. Bradbury, Glencoe, Ill., as successor trustees Application November 9, 1926, Serial No. 147,250
3 Claims.
My invention relates to improvements in automatic fuel regulation for internal combustion engines.
' an internal combustion engine by means of which to the engine.
Another object of my invention is to provide asimple, cheap and eicient carburetor having a minimum of moving parts.
Referring to the drawing in which the same numbers indicate like parts:
Fig. 1 is a vertical sectional view of my carburetor with my improvements incorporated therein.
Fig. 2 is a view showing my invention attached to an internal combustion engine.
Fig. 3 is a sectional view showing the mecha.-
nism of Fig. 1 in another position.
Fig. 4 is a transverse sectional view of part of Fig. 2.
Fig. 5 is a sectional view of part of Fig. 4. Fig. 6 is an alternative construction for part of Fig. 4.
Fig. 7 is 'an alternative construction for part of Figs. 1 and 3.
Fig. 8 is an enlargedfragmentary sectional view of the discharge nozzle.
The invention disclosed in this application is an improvement over that disclosed in my copending application Serial Number 106,012, iiled May 1st, 1926, and copending application, Serial N0. 142,761, filed October 19, 1926.
An internal combustion engine I has the usual exhaust pipe 2 and intake pipe 3, to which latter is attached a carburetor 4 having an air inlet 5 connected by a hot air pipe 6 to a stove 1 surrounding exhaust pipe 2. A metal block 8 extends from exhaust pipe 2 and has mounted thereon a bi-metallic thermostat 9 adapted to operate through suitable mechanism I8 for controlling the action of carburetor 4.
Carburetor 4 is fed by any suitable system with liquid fuel through a pipe II and comprises a mixing chamber I2 containing a large venturi I3 and a small venturi I4 adapted to discharge at the throat of large venturi I3.
Liquid fuel through pipe I I passes into a liquid reservoir I5, maintained substantially at a constant level X--X, containing a iloat I6 operating in a well known manner a valve (not shown) for controlling the inlet of liquid fuel through pipe I I. Reservoir I5 is closed by a cover I1 and is open to atmosphere through a port I8.
Liquid fuel passes through a passage I9 to the lower part of a well 20 which latter is divided into an upper and lower section by a plug 2I supporting a tube 22. 'Ihe lower part of well 20 is closed by a plug 23 containing a passage 24 and supporting a tube 25 and passage 24 leads to a passage 26 and a nozzle 21. A second nozzle 28 surrounds nozzle 21 and is adapted to register through a passage 29 with the upper part of well 20. A small orifice 38 is drilled in nozzle 21 for permitting liquid fuel, in restricted quantity, to ow from the upper part of well 20 to the interior of tube 25. Tube 25 has orices 3|, the lower one of which is relatively large compared with the upper orice and the upper orice is located just below the liquid level X-X.
Air is supplied to well 20 through an airiadjusting valve 32. A throttle 33 controls the discharge of liquid fuel and air from carburetor 4 to the cylinders of engine I, responsive to the vacuum therein.
The engine vacuum, on the engine side of throttle 33 is applied to the interior of a casing 35, forming an extension of carburetor 4, for operating a valve 36 which in turn controls the passage of liquid fuel and air through the valve 36 by way of a restricted orice 31 as will presently appear. On the outer end of valve 36 is mounted a disc 38. Valve 36 contains a plurality of liquid fuel orifices 39 and a plurality of air orifices 40, the fuel orifices 39 being adapted to register at times with the upper discharge of tube 25 and the air orifices 48 being adapted to register at times with atmosphere through the regulating valve 4I.
Valve 36 has an annular groove 42 cut therein .with a tapered portion 43 adapted to control at times the supply of air to the upper portion of well 20 through passages 44 and 45. `end of valve 36 is squared to work through a guide 46 so that the positions of orifices 39 and 40 will always remain the same and a spring 41 encircles the outer end of valve 36 for limiting its movement in one direction, disc 38 limiting its movement in the other direction. Disc 38 is adapted to work in an enlarged extension 50 which is open to atmosphere through ports 48, suitable clearance being allowed between disc 38 The outer and casing 50. An orifice 49 is provided for suitably locking valve 36 in any predetermined position by means of a pin, or otherwise, if so desired.
Engine exhaust gases pass through pipe 2 to atmosphere and on their way 'come in contact with a bevelled face of block 8, a portion thereof being thus diverted to pass through a passage 5B and a port 59 to atmosphere. Block 8 is adapted to contain valve 60 threaded into member 521 and adapted to work in an enlarged passage 6I for closing port 59 at times, the exhaust gases passing through port 59 are arranged to impinge on thermostat 9. It will be seen that spring 53 forms a substantially universal joint betweenmember 52 and rod 5I and in the alternative shown in Fig. 6. It will be noted that the stem of valve 69 is adapted to move freelyin member 52 and. has a disc 62 provided on the end ofvalve 611 for fiexibly seating valve 6D.
Tube 22 is provided with a plurality of 'liquid feed orifices 63, some of which are above and some below the liquid level X-X. A groove 64 is out in valve 36 and adapted to register at times with atmosphere through a passage 65 and groove 64 is connected with the interior of valve 36 through orifices 39. The upper ends of tubes 22 and 25 fit snugly in the metal of carburetor 4, the upper end of tube 22 being spaced a desired amount.
from the valve 36 to form a reservoir 66 of any desired content.
The operation of the device is as follows:
If it be assumed that engine I is very cold, throttle 33 will be closed, as shown in Fig. 1, and engine I will be cranked. A partial vacuum is thus applied to mixing chamber I2, which partial vacuum is very low due to the low cranking speed and therefore valve 36 will be in the position shown in Fig. 3 due to the action of spring 41 and thus a plurality of the orifices 39 will be in registry with the upper discharge of tube 25 for raising liquid fuel and discharging the same in large volume through orifice 31 for priming the engine, it being noted at this time that only one, or perhaps none, of the orifices 49 is in connection with atmosphere through valve 4l.
After a period of cranking, su'icient liquid fuel will have been drawn in the engine, together with a limited amount of air past throttle 33, and the mixture is fired in the cylinders of engine I, whereupon a sudden jump in vacuum occurs whereby valve 36 'advances to the position as shown in Fig. 1 thus closing some of the orifices 39 and suddenly reducing the supply of liquid fuel to the engine. The number of orlces thus cut off will be determined by the particular engine to which carburetor 4 is applied. At this time more of the .air orifices 40 will permit passage of atmosphere to the interior of valve 36, thus reducing the vacuum applied for raising liquid fuel through the remaining orifices 39 and groove 64 will also be open to atmosphere thus minimizing any tendency of the engine vacuum to draw liquid fuel between valve 36 and casing 35. Also at this time, the upper part of well will be in connection with atmosphere through port 45, groove 42 and passage 44. Thermostat 9, being in its fully contracted position, will thus not exert any influence on valve 36 and consequently, upon opening throttle 33 wide for sudden acceleration, valve 36 will be drawn by spring 41 to its outermost position as shown` in Fig. 3 whereby passage 44 will be closed to atmosphere thus throwing the full suction at the throat of venturi I4 upon nozzles 21 and 28 and thus upon orifices 63. Said suction will be also applied when the engine is cold in greater strength to orifices 3| because groove 64 will be shrouded and only a limited amount of air may pass through orifices 40 and 39 to the interior of tube 29, but this amount of air is sufficient to permit the drop of the column of liquid fuel in tube for quick accelerating discharge through nozzle 21 and thereafter permitting as before stated, an enhanced application of the engine vacuum to orifices 3l, the result of all which is to increase the richness of the mixture supplied to the engine at low temperatures.
'Ihe sudden opening of throttle 33 also increases the speed at which the contents of tube 25 are discharged through nozzle 21 because valve 36 is tapered at 34 on its inner end to form a projection in the air stream in chamber I 2 whereby a portion of the air, due to its velocity, impinges on said projection 34 and is diverted through orifices 31 and 39 to the interior of tube 25, this diversion being accentuated by the difference in vacuum on the engine side of throttle 33 and the throat of venturi I4.
A modification of this construction is shown in Fig. '1 wherein a deflecto'r 61 is provided in place of projection 34.
During the period of operation described, exhaust gases will have passed through passage 58 in block 8 to impinge on thermostat 9 and also to heat block 8 for heat transmission to thermostat 9 and thus thermostat 9 will expand to bring spring 53 and rod 5I gradually in contact with disc 38 whereby, when optimum engine operating temperatures are reached, valve 36 will be at its innermost position whereby when throttle 33 is closed at idling speeds, only one of the orifices 39 will register with the discharge from tube 25 for providing an idling mixture. Thereafter under such optimum conditions, upon suddenly opening throttle 33 wide for acceleration, or for opening the same for slow acceleration, the compression of spring 41 is sufficiently greater than the tension of thermostat 9 to permit the reces-l sion of valve 36 only to the extent of maintaining groove 64 in registry with both port 65 and the upper discharge from tube 25 and at the same time permitting passage 44 to be only partially closed. Thus acceleration is provided for under all conditions and an economical mixture is provided at optimum engine temperatures.
'Ihe actual position of orifices 63 and 39 can be determined only -by trial and may vary as to size depending on the engine to which they supply liquid fuel. A regulating valve 32 controls the vdischarge from orifices 63 at optimum temperatures and thereafter valve 36 automatically controls the degree of vacuum applied through nozzle 28 to the upper portion of well 20 for rais"- ing a column of liquid fuel therein and varying then head under which the same discharges throughorifices 63.
Thus, in effect,v two wells are plying liquid fuel and air to engine I in the proper mixture proportions under all conditions of load, speed and temperature, one well comprising the provided for supvarying amounts of air bled into the wells with varying degrees of .vacuum on either side of throttle 33,y whereby these two compensating wells take care of engine operation under all conditions.
The various orifices, well sizes, etc., may be determined only by trial for a particular engine but, thereafter require no adjustment. Valves 32 and 4I may even be replaced by set orices. If desired to operate without thermostatic control, valve 36 may be permitted certain movement only for operating under optimum ternperature conditions, as' described, and this can be accomplished by changing the position of disc 38 along valve 36, so that the outermost position of valve 36 may be limited as required for a given effect.
I claim:
1. A carburetor having an intake passage, a liquid fuel reservoir, a throttle in said passage, a well between the reservoir and said passage and connected to each, and deecting means in said passage for circulating air from the passage through the well and past said throttle.l
2. A carburetor having a mixing chamber, a
liquid fuel reservoir, a throttle controlling the outlet from the mixing chamber, two wells between the reservoir and mixing chamber and connected to each and means responsive to temperature and vacuum for controlling the admission of air to both wells and detlecting means on the posterior side of said throttle for circulating air through the well and past said throttle.
3. The combination with an internal combustion engine of a carburetor having a mixing chamber, a liquid fuel reservoir, a throttle controlling the outlet from the mixing chamber, a well between the reservoir and mixing chamber and connected to each, and means jointly controlled by the engine vacuum and temperature for controlling the circulation of air from the mixing chamber through the well and past said throttle. 1
- CHARLES L. STOKES.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US147250A US2004178A (en) | 1926-11-09 | 1926-11-09 | Automatic fuel regulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US147250A US2004178A (en) | 1926-11-09 | 1926-11-09 | Automatic fuel regulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2004178A true US2004178A (en) | 1935-06-11 |
Family
ID=22520837
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US147250A Expired - Lifetime US2004178A (en) | 1926-11-09 | 1926-11-09 | Automatic fuel regulator |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2004178A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2981245A (en) * | 1959-04-07 | 1961-04-25 | Chrysler Corp | Carburetor idle fuel control means |
-
1926
- 1926-11-09 US US147250A patent/US2004178A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2981245A (en) * | 1959-04-07 | 1961-04-25 | Chrysler Corp | Carburetor idle fuel control means |
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