US2711162A - Ignition control - Google Patents
Ignition control Download PDFInfo
- Publication number
- US2711162A US2711162A US330340A US33034053A US2711162A US 2711162 A US2711162 A US 2711162A US 330340 A US330340 A US 330340A US 33034053 A US33034053 A US 33034053A US 2711162 A US2711162 A US 2711162A
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- Prior art keywords
- venturi
- throttle
- restriction
- stage
- passage
- 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.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02P—IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
- F02P5/00—Advancing or retarding ignition; Control therefor
- F02P5/04—Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions
- F02P5/05—Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions using mechanical means
- F02P5/10—Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions using mechanical means dependent on fluid pressure in engine, e.g. combustion-air pressure
- F02P5/103—Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions using mechanical means dependent on fluid pressure in engine, e.g. combustion-air pressure dependent on the combustion-air pressure in engine
Definitions
- the object of this invention is to advance the ignition of an internal combustion engine with: (a) the air flow through the venturi; (b) the air pressure at the upstream lip of the butterfly throttle. By this means the centrifugal weights are not needed.
- One problem has arisen due to the re-introduction of the two-stage carburetor. When the second stage becomes operative, the spark must not become unduly retarded, because the secondary venturi robs air from the primary venturi.
- Figure 1 shows diagramatically the preferred form of my invention where only a one-stage carburetor is involved.
- Figure 2 is also a diagrammatic representation of a two-stage carburetor incorporating my invention.
- Figure 3 shows an alternative construction for a onestage carburetor.
- Figure 4 shows a modification applicable specifically to the first stage of the two-stage carburetor shown in Figure 2.
- venturi 20 is the pipe leading from venturi 20 to 24 which is an air chamber.
- 26 is a diaphragm connected to 28 a link which advances the throttle.
- Atent O 14 is the restricted opening in the wall of the throat 18 is the primary throttle (manual).
- Throttle 38 is slightly offset so that manifold suction keeps the secondary throttle 38 shut until it is time for it to open.
- the throttle 40 is a restricted opening in the Wall of the mixture outlet 42 of the primary stage of the carburetor, and becomes operative when the throttle is somewhere between 40 and 70, preferably to the horizontal.
- restriction 44 is a common passage from restriction 36 and 40 and leading to an air chamber 46.
- 60 is a booster venturi corresponding to booster venturi 20 of Figure 1.
- this booster venturi 60 is a passage from the throat of this booster venturi 60 to an air chamber 64 which has a diaphragm 66 connected to a link 68 which advances a circuit breaker '70 in a well-known manner.
- the restriction in the walls of the mixture outlet 42 is at 77 just a little upstream of the upstream lip of the butterfly throttle 18.
- a booster venturi 76 (#68:0.031" diam.)
- Passage 78 leads to a diaphragm chamber and the suction in 78 advances the spark.
- An ignition control system for an'internaI combustion engine having a carburetor having an air entrance, a mixture outlet and a butterfly throttle in said mixture outlet, and a restriction in the wall of said outlet so located as to be subjected to the suction downstream of the upstream lip of said butterfly throttle the moment it is moved away from its idle position, a passage leading to said restriction from the atmosphere, a booster venturi in said passage, an air chamber, a moving wall therein, a connection from said moving wall to advance the spark of said engine, a connection from said chamber to the throat of said booster venturi.
- An ignition control system for an internal combustion engine having a two-stage carburetor comprising a first stage, which is normally in operation, and a second stage which is automatically activated after the first throttte has been opened at least one-half way, comprising a venturi air entrance to each stage, a butterfly throttle in the mixture'outlet from the first stage, a restriction in the wall of the primary mixture outlet located so as to be subjected to the suction downstream of the upstream lip of said primary throttle the moment it is opened from its idling position, a venturi in the air entrance to the first stage, a restriction in the wall of the venturi, a common passage connecting the two restrictions together, an air entrance to this common passage, a booster venturi therein, a second venturi in the air entrance to the second stage carburetor, a restriction in the wallzof the throat of said second stage venturi, a passage connecting said restriction andsaid common passage, a check valve in said passage so that the suction in the second stage venturi only becomes active when the su
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- 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)
- Control Of The Air-Fuel Ratio Of Carburetors (AREA)
Description
June 21, 1955 D. T. ROBERTS IGNITION CONTROL Filed Jan, 8, 1953 IN V EN TOR.
United States IGNITION CONTROL The object of this invention is to advance the ignition of an internal combustion engine with: (a) the air flow through the venturi; (b) the air pressure at the upstream lip of the butterfly throttle. By this means the centrifugal weights are not needed. One problem has arisen due to the re-introduction of the two-stage carburetor. When the second stage becomes operative, the spark must not become unduly retarded, because the secondary venturi robs air from the primary venturi.
In the figures:
Figure 1 shows diagramatically the preferred form of my invention where only a one-stage carburetor is involved.
Figure 2 is also a diagrammatic representation of a two-stage carburetor incorporating my invention.
Figure 3 shows an alternative construction for a onestage carburetor.
Figure 4 shows a modification applicable specifically to the first stage of the two-stage carburetor shown in Figure 2.
In Figure 1:
is the air entrance.
12 is the venturi.
14 is a restriction in the wall of the throat.
16 is a restriction in the walls of the mixture outlet 42 just a little upstream of the upstream lip of throttle 18 when throttle 18 is closed to its idling position.
20 is the throat of a small booster venturi subjected to the flow of air from restriction 14 to restriction 16, and vice-versa.
22 is the pipe leading from venturi 20 to 24 which is an air chamber.
26 is a diaphragm connected to 28 a link which advances the throttle.
In Figure 2:
10 is again the primary air entrance.
12 is the primary venturi.
atent O 14 is the restricted opening in the wall of the throat 18 is the primary throttle (manual).
16 is a restricted opening just upstream of the upstream lip of the throttle 18 when in its idling position.
30 is the secondary air entrance.
32 is the secondary venturi.
34 is a restriction in the wall of the throat of 32.
36 is a second restricted opening in the wall of 32 and is used to keep the secondary throttle 38 opening at the right moment after it has started to open.
Throttle 38 is slightly offset so that manifold suction keeps the secondary throttle 38 shut until it is time for it to open.
40 is a restricted opening in the Wall of the mixture outlet 42 of the primary stage of the carburetor, and becomes operative when the throttle is somewhere between 40 and 70, preferably to the horizontal.
44 is a common passage from restriction 36 and 40 and leading to an air chamber 46.
48 is a diaphragm connected to a link 50 which opens the secondary throttle 38 when the suction in air chamber 46 is powerful enough to overcome the manifold suction in manifold 52, which tends to hold the secondary throttle 38 shut.
This is the subject of a co-pending patent application Serial No. 330,328, filed January 8, 1953 by Marion L. Smitley and Melvin F. Sterner jointly.
Resuming the description of my own invention:
54 is a check valve raised by the suction in the opening 34.
Below the valve 54 is a restricted passage 16.
60 is a booster venturi corresponding to booster venturi 20 of Figure 1.
62 is a passage from the throat of this booster venturi 60 to an air chamber 64 which has a diaphragm 66 connected to a link 68 which advances a circuit breaker '70 in a well-known manner.
In Figure 3 (the single stage):
10 is the air entrance.
18 is the throttle.
The restriction in the walls of the mixture outlet 42 is at 77 just a little upstream of the upstream lip of the butterfly throttle 18.
A booster venturi 76 (#68:0.031" diam.)
78 is a passage leading from the throat.
80 is a restriction (#74=0.0225 diam.)
77 is a restriction (#38=O.1015 diam.)
A second restriction 82 (#56=0.0465" diam.) bleeds air from the atmosphere past spring loaded check valve 84.
In Figure 4:
In place of one opening 16, I substitute two openings 72 and 74. Otherwise, everything is the same as in Figure 2.
Figures 2 and 4:
Combining Figure 4 with Figure 2, the following dimensions have been found to be satisfactory:
72=#65 (0.035" diam.)
74=#46 (0.081" diam.)
14=#51 (0.067 diam.)
60=venturi throat=#47 (0.0785" diam.) 54= /s" nylon ball 34=#20 (0.161" diam.)
OPERATION Figure 1 By varying the three restrictions 14, 16 and 20, the spark advance characteristics can be varied to meet the customers most exacting demands. At top speeds either an increase, a decrease or a uniform spark advance can be obtained from part throttle advance which advances the spark to a more or less constant degree over a wide range of air flows.
F igure 4 The two restrictions 72 and 74. are substituted for one restriction 16 of Figure 2. The advance of the spark is thus made gradually so that a fast idle for example, will not call for an unduly high spark. The sudden advances in ignition inherent in constructions shown in Figures 1, 2 and 3 are not always desirable 'during the period when first opening the primary throttle from its idle position. i
What I claim is:
1. An ignition control system for an'internaI combustion engine having a carburetor having an air entrance, a mixture outlet and a butterfly throttle in said mixture outlet, and a restriction in the wall of said outlet so located as to be subjected to the suction downstream of the upstream lip of said butterfly throttle the moment it is moved away from its idle position, a passage leading to said restriction from the atmosphere, a booster venturi in said passage, an air chamber, a moving wall therein, a connection from said moving wall to advance the spark of said engine, a connection from said chamber to the throat of said booster venturi.
2. In a device as set forth in claim 1 in which there striction in the wall of the venturi throat, a connection from said restriction to said booster venturi so that the booster venturi is connected on one side with the mixture outlet and on the other with the throat of said carburetor, which is its connection with the atmosphere.
3. An ignition control system for an internal combustion engine having a two-stage carburetor comprising a first stage, which is normally in operation, and a second stage which is automatically activated after the first throttte has been opened at least one-half way, comprising a venturi air entrance to each stage, a butterfly throttle in the mixture'outlet from the first stage, a restriction in the wall of the primary mixture outlet located so as to be subjected to the suction downstream of the upstream lip of said primary throttle the moment it is opened from its idling position, a venturi in the air entrance to the first stage, a restriction in the wall of the venturi, a common passage connecting the two restrictions together, an air entrance to this common passage, a booster venturi therein, a second venturi in the air entrance to the second stage carburetor, a restriction in the wallzof the throat of said second stage venturi, a passage connecting said restriction andsaid common passage, a check valve in said passage so that the suction in the second stage venturi only becomes active when the suction in the second stage venturi is greaterthan the suction in the common passage, an air chamber, a moving wall, a mechanical connection from said moving wall to advance the time of the ignition, a pipe connecting the air chamber with the throat of said booster venturi.
References Cited in the file of this patent UNITED STATES PATENTS
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US330340A US2711162A (en) | 1953-01-08 | 1953-01-08 | Ignition control |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US330340A US2711162A (en) | 1953-01-08 | 1953-01-08 | Ignition control |
Publications (1)
Publication Number | Publication Date |
---|---|
US2711162A true US2711162A (en) | 1955-06-21 |
Family
ID=23289326
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US330340A Expired - Lifetime US2711162A (en) | 1953-01-08 | 1953-01-08 | Ignition control |
Country Status (1)
Country | Link |
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US (1) | US2711162A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1216020B (en) * | 1963-04-09 | 1966-05-05 | Bosch Gmbh Robert | Distributor for internal combustion engines |
DE2754942A1 (en) * | 1976-12-13 | 1978-06-22 | Toyo Kogyo Co | END ADJUSTMENT DEVICE FOR COMBUSTION ENGINES WITH TWO-DUCT INTAKE SYSTEM |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2093524A (en) * | 1934-10-20 | 1937-09-21 | Harold W Meade | Automatic ignition control for internal combustion motors |
US2317885A (en) * | 1942-04-15 | 1943-04-27 | George M Holley | Ignition timing device |
US2361271A (en) * | 1943-07-05 | 1944-10-24 | George M Holley | Ignition timing device |
US2450834A (en) * | 1944-11-09 | 1948-10-05 | Niles Bement Pond Co | Control apparatus for internal combustion engines |
US2621482A (en) * | 1947-09-04 | 1952-12-16 | Harold W Meade | Pressure-operated mechanism for controlling fluid flow |
-
1953
- 1953-01-08 US US330340A patent/US2711162A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2093524A (en) * | 1934-10-20 | 1937-09-21 | Harold W Meade | Automatic ignition control for internal combustion motors |
US2317885A (en) * | 1942-04-15 | 1943-04-27 | George M Holley | Ignition timing device |
US2361271A (en) * | 1943-07-05 | 1944-10-24 | George M Holley | Ignition timing device |
US2450834A (en) * | 1944-11-09 | 1948-10-05 | Niles Bement Pond Co | Control apparatus for internal combustion engines |
US2621482A (en) * | 1947-09-04 | 1952-12-16 | Harold W Meade | Pressure-operated mechanism for controlling fluid flow |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1216020B (en) * | 1963-04-09 | 1966-05-05 | Bosch Gmbh Robert | Distributor for internal combustion engines |
DE2754942A1 (en) * | 1976-12-13 | 1978-06-22 | Toyo Kogyo Co | END ADJUSTMENT DEVICE FOR COMBUSTION ENGINES WITH TWO-DUCT INTAKE SYSTEM |
US4181105A (en) * | 1976-12-13 | 1980-01-01 | Toyo Kogyo Co., Ltd. | Ignition timing control for internal combustion engine having a dual induction type intake system |
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