US2477481A - Antidetonating device - Google Patents

Antidetonating device Download PDF

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Publication number
US2477481A
US2477481A US591126A US59112645A US2477481A US 2477481 A US2477481 A US 2477481A US 591126 A US591126 A US 591126A US 59112645 A US59112645 A US 59112645A US 2477481 A US2477481 A US 2477481A
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throttle
mixture
conduit
fuel
engine
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US591126A
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George R Ericson
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Carter Carburetor Corp
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Carter Carburetor Corp
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M7/00Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
    • F02M7/12Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves
    • F02M7/18Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves with means for controlling cross-sectional area of fuel-metering orifice

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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

G. R. ERICSON ANTIDETONATING' DEVICE July 26, 1949.
3 Sheets-Sheet JL Filed April 30, 1945 INVENTOR.
INVENTOR.
July 26, 1949. G. R. ERlcsoN ANTIDETONATING DEVICE Filed April 30., 1945 ratings than is otherwise practical.
Patented July 26, 1949 UNITED STATES PATENT OFFICE AN TIDETONATING DEVICE George R. Ericson, Kirkwood, Mo., assignor to Carter Carburetor Corporation, St. Louis, Mo., a corporation of Delaware Application April 30, 1945, Serial No.`591,126
. Claims. 1
This invention relates to a fuel control device for internal combustion engines and consists in novel means for elimination of objectionable detonation under certain conditions as. for instance, when operating at low speed with the throttle in open position.
One of the main advantages of the invention is that it permits the use of higher cylinder head compression ratios and fuelswith lower octane The invention will be betterunderstood upon consideration of the following specification and accompanying drawing, referring to which Figure l is a diagram illustrating the relative position of the fuel control device mounted on an internal combustion engine.
Figure 2 is a sectional view of the device showing the mechanism for accomplishing the purpose of the present invention.
Figures 3 and 4 are similar to Figure 2, but show the parts in different operating positions, Fig. 3 illustrating the positions of the parts under high speed full-open throttle operation of the engine, and Fig. 4 showing the positions occupied by the parts when the engine is operated at low speed with the throttle open.
Figure 5 shows a modified form of the invention. y
Figure 6 is similar to Figure 5, but shows the parts in different operating positions.
The engine represented in Fig. 1 comprises a cylinder head I, block 2 on the side of which is mounted the usual intake manifold 3 and the exhaust manifold 4. A carburetor 5 is mounted in the usual manner on the hot spot 6 of the manifolds 3 and 4. Fuel is supplied tothe device through conduit 1 from any suitable source of supply, and the device is manually controlled through rod 8 and throttle arm 9 connected to the throttle valve I5.
Figs. 2, 3, and 4 show a device in which a downdraft mixture conduit includes an air horn II, venturis I2, and outlet portion I3, flanged at I4 for attachment to the intake manifold 3 of an associated internal combustion engine. A throttle valve l5 is pivotally mounted in the outlet portion of the mixture conduit and is controlled by the throttle arm 3.
Adjacent the mixture conduit is a bowl I-6 within which fuel is maintained at a substantially constant level .r-- by needle valve mechanism I1 controlled by float I3. i Fuel is supplied to the mixture conduit through a main nozzle I9 opening into the throat portion of the smallest venturl I2 and communicating with the fuel bowl 55 through a calibrated metering orifice member 20. Fuel for idling and low speed operation is supplied through a passage shown at 2|, opening into the mixture conduit through a port 22 adjacent the edge of the throttle valve when closed. Formed in the wall of the mixture conduit is a cylinder or chamber 23 communicating through a passage 24 with opening 25 into the mixture conduit posterior to the throttle valve. Slidable within chamber 23 is a piston 26 having an elongated rod 21 projecting thereabove through cover 28 of the fuel bowl and having at its upper portion a laterally offset arm 29 pinned as at 30 to a metering rod 3| having a stepped lower portion 32 extending into metering orifice member 2li for varying the effective cross-sectional area thereof.
A spring 36 in the suction chamber constantly urges piston 26 upwardly and may be calibrated to move the smallest portion of the metering pin into operative relationship with orifice member 2G to provide an extra rich mixture when the suction posterior to the throttle drops below a predetermined value, say, three inches-of mercury. At other times, the metering pin will be drawn down so as to bring a larger portion thereof into the metering orifice to provide an economical mixture for normal, part throttle operation. l
Rocker arm 33 is pivotally mounted on stanchion 39 above the fuel bowl cover 28 and is moved in xed relation to the throttle valve by arm 40, link 4I and throttle arm 42 on the throttle shaft 43. A lip extending from rocker arm 38 is so positioned as to extend under a laterally offset lip 46 formed on the upper portion of the elongated piston rod 21 for limiting the downward movement of metering rod 3| in accordance with a predetermined positioning of throttle Valve I5 to provide a proper fuel mixture.
Formed in the wall of the mixture conduit is a second cylinder or chamber 48 communicating through passage 49 with opening 50 into the throat ol the smallest venturi I2. Slidable within the chamber 48 is a piston 5I having an elonpath of lip 4E on piston rod 21. A spring 55 in the suction chamber v43 constantly urges piston 5l upwardly and may be calibrated so that the piston is moved downwardly when the suction in the small venturi I2 exceeds a predetermined value.
objectionable detonation occurs in an engine 3 when it is operated with a low manifold vacuum, as in hill climbing or-at low speeds, for instance, 'up to 40 M. P. H.; and I have found that this objectionable detonation can be eliminated by enorder to obtain these special advantages, I increase the compression ratio of the engine to a point substantially higher than that which could be used without detonation with a fuel mixture of richness corresponding to the optimum for maximum power. It will be understood by those skilled in the art that the maximum economy richness is much leaner than that required for maximum power, so that the engine is normally operated with a fuel mixture leaned out for best economy. This mixture is stepped up to a richness corresponding to the optimum for maximum power, but, according to my invention, the maximum power mixture issupplemented by a further increment of fuel for anti-detonating eiect when the engine speed and throttle position are such as to cause the introduction of a full charge of fuel into the cylinders which would cause objectionable detonation except for the provision of special means to prevent it.
In order to achieve maximum economy and also maximum power, I increase the compression ratio of the engine cylinders beyond that which would be usable with ordinary methods of fuel supply, supply an optimum economy mixture for normal operating conditions, an optimum power mixture for high speed operating conditions, and
an optimum anti-detonating mixture for maxirdegree of suction in the smallest venturi and that in the mixture passage posterior to the throttle are such as to permit the springs 55 and 36 to locate the respective pistons 5| and 26 in about the positions shown in Fig. 3, wherein with the throttle substantially full-open to position the rocker arm 38 as shown, the off-set arm .53 may be in Contact with the lip 46 of rod 21,
and lip 4 6 in engagement with the rocker arm lip 45. Thus the metering rod 3| will be related to the orifice 20 as appears in this figure.
In Fig. 4, the metering rod 3| is shown in the position for delivery of the extra amount of fuel to the mixture conduit with the throttle in a partially opened position and when the vacuum in the venturi I2 is comparatively low as when the engine is operated at speeds below 4U M. P. H. with the throttle more than half way open. With the throttle in a substantially open position during low speeds, the required suction in the mixture conduit to hold the pistons 26 and 5| down is lost. Pistons 26 and 5I and their associated rods are thus allowed to move under the influence of the springs 36 and 55 respectively to their uppermost vpositions whereby the metering rod 3| is positioned as shown in Figure 4. As the acceleration of the engine increases, suction in the small venturi l2 increases to a predetermined value suiiicient to lower piston 5| and rod 52 which in turn forces rod 21 and piston 26 down sufficiently to position metering rod 3| in the a metering orifice member 20 for normal economical high speed operation of the engine as indicated in Fig. 3. y
Fig. 5 illustrates a simplified form of the invention wherein the structure generally is in conformity with the structure of Fig. 2 and bears the same reference numerals on the corresponding parts. However, one important difference in the simplified form is that the piston 5|, rod 52, and passage 49 in the embodiment of Fig. 2 are here omitted. In this form, the only other difference is that the spring 36 as employed in the arrangement of Fig. 2, is here replaced by a spring 36a which must be very delicately calibrated and, when so calibrated, gives very satisfactory results. Thus in the operation of the modified arrangement, when the engine is running at a relatively low speed with the throttle more than half way vopen or full open as indicated in Fig. 5, and such that the suction in the mixture passage posterior 'to the throttle is less than a predetermined value,
say three inches of mercury, the spring 36a then is effective to locate the piston 26 in its uppermost position (Fig. 5). metering rod 3| will be thereby disposed as shown, wherein the smallest step of the rod portion 32 is in the orifice 20, thereby affording an extra rich mixture which will serve to prevent detonation.
Further with regard to the modified arrangement, as the engine speed increases under the foregoing condition of near or full open throttle, the piston 26 will lower against spring 36a in .response to the resulting rise in the mixture pasnormal speed operation of the engine.
open throttle positions, with correspondingly sage suction posterior to the throttle, thereby lowering the metering rod 3| from the raised position thereof as shown in Fig. 5, ultimately to the position illustrated in Fig. 6. In the latter position, as limited by the full open position of the throttle through abutment' of vi-the piston rod element46 with the throttle positioned rocker arm lip (Fig. 6), the next larger step of the metering rod stepped portion 3 2 will be eiective in the orifice 20, llo-determine the mixture for At part lowered positions of the lip.45, increased suctionwill cause further lowering of the metering rod to bring larger diameter portions of the rod Astepped end 32 into coaction with the orifice 20, such as to effect adjustments of the mixture-in accordance with part throttle operation of the engine.
I claim:
1. In a fuel control device for an internal combustion engine, means forming a mixing conduit, a throttle valve in said conduit, operating means for said throttle valve, a fuel supply chamber, a fuel control device for regulating the supply of fuel from said chamber to said conduit, pressure operated means for adjusting said fuel control device in response to suction posterior to said throttle, means operably connecting said throttle and fuel control device to open the latter in accordance with throttle position and regardless of said pressure operated means, said last named means operating to limit the closing movement of said control device when the latter is actuated independent of said throttle, and means including a iluid responsive device for limiting the opening movement of said control device in response to pressure anterior to saidbustion engines comprising means forming a mixiiow through said conduit, a fuel supply cham- In such piston position, the
ber, a passageway connecting said supplycham-` v way, iluid motor means for operating said metering pin tosupply a fuel mixture of optimum rich ness for economy whenthethrottle is in slightly open position and when the vacuum posterior to said throttle is high, a member controlled by the movement of said throttle for adjusting said metering pin to regulate the mixture to the optimum for maximum power when the throttle is moved to fully open position, and an additional fluid operated motor, responsive to mixing conduit vacuum anterior to said throttle, said motors cooperating to adjust said metering pin for en- `riching the mixture beyond the optimum richl ness for maximum -power when the vacuum in "tion in said conduit for affecting said stop means so as to limit enriching movement of said valve to a normal, power mixture.
4. A charge forming device for an internal combustion engine comprising a mixture conduit, a fuel supply chamber, a fuel supply system connecting said chamber and said conduit, a metering valve in said system, means for varying the position of said valve between positions for supplying normal and abnormally rich mixtures, stop means for limiting movement of said valve in the enriching direction, and means operable responsive topredetermined suction in said conduit for shifting said stop means, at least in part,
so as to limit enriching movement of said valve to its normal mixture position.
5. A' charge forming device for an internal combustion engine comprising a mixture conduit, a `throttle valve therein, a fuel supply chamber, a fuel supply system connecting said chamber and said conduit, a metering valve in said system, means including a spring andan element responsive to suction in said conduit posterior to said throttle for varying the position of said valve between its normal and abnormally rich'mixture supplying positions, stop means for limiting movement of said valve, and means operable responsive to predetermined suction in said conduit anterior to said throttle for affecting said stop means so as to limit enriching movement pf said valve to anormal mixture position.
` GEORGE R. ERICSON.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,103,689 Mullen, Jr. Dec. 28, 1937 2,156,115 Gistucci et al. Apr. 25, 1939 2,191,905 Cioedy et al. Feb. 27, 1940 2,295,656 V Hersey et al Sept. 15, 1942 Udale Apr. 13, 1943
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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2611594A (en) * 1948-10-27 1952-09-23 Thompson Prod Inc Supplementary fluid feed device with automatic tandem metering valves
US2611592A (en) * 1948-10-27 1952-09-23 Thompson Prod Inc Dual carburetor
US2616404A (en) * 1948-10-07 1952-11-04 Ethyl Corp Method and apparatus for supplying auxiliary fuel or antiknock fluid to internal-combustion engines
US2616405A (en) * 1948-11-20 1952-11-04 Ethyl Corp Enrichment device and method of controlling the same
US2624558A (en) * 1948-10-27 1953-01-06 Thompson Prod Inc Supplementary fuel feed device
US2657913A (en) * 1948-08-06 1953-11-03 Thompson Prod Inc Supplementary feed device for internal-combustion engines
US2661196A (en) * 1949-05-13 1953-12-01 Chrysler Corp Carburetor
US2664871A (en) * 1949-07-30 1954-01-05 Thompson Prod Inc Supplemental fuel feed device
US2699326A (en) * 1951-05-31 1955-01-11 Thompson Prod Inc Collar mounted dual actuated fuel feed device
US2711885A (en) * 1952-10-20 1955-06-28 Carter Carburetor Corp Carburetor metering control
US2717149A (en) * 1951-10-09 1955-09-06 Thompson Prod Inc Fluid feed device
US2791995A (en) * 1954-02-15 1957-05-14 Gen Motors Corp Anti-detonation device for a carburetor
US2808245A (en) * 1950-11-20 1957-10-01 Anna M Grover Fuel feed devices for internal combustion engines
US6394426B1 (en) * 2000-07-07 2002-05-28 Walbro Corporation Engine dual fuel supply apparatus

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2103689A (en) * 1935-11-01 1937-12-28 Jr James F Mullen Carburetor
US2156115A (en) * 1935-08-09 1939-04-25 Carbureteurs Zenith Soc Gen De Carburetor
US2191905A (en) * 1933-03-20 1940-02-27 Carter Carburetor Corp Carburetor
US2295656A (en) * 1940-04-24 1942-09-15 United Aircraft Corp Fuel metering device
US2316300A (en) * 1940-08-23 1943-04-13 George M Holley Control for fuel supplies

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2191905A (en) * 1933-03-20 1940-02-27 Carter Carburetor Corp Carburetor
US2156115A (en) * 1935-08-09 1939-04-25 Carbureteurs Zenith Soc Gen De Carburetor
US2103689A (en) * 1935-11-01 1937-12-28 Jr James F Mullen Carburetor
US2295656A (en) * 1940-04-24 1942-09-15 United Aircraft Corp Fuel metering device
US2316300A (en) * 1940-08-23 1943-04-13 George M Holley Control for fuel supplies

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2657913A (en) * 1948-08-06 1953-11-03 Thompson Prod Inc Supplementary feed device for internal-combustion engines
US2616404A (en) * 1948-10-07 1952-11-04 Ethyl Corp Method and apparatus for supplying auxiliary fuel or antiknock fluid to internal-combustion engines
US2611594A (en) * 1948-10-27 1952-09-23 Thompson Prod Inc Supplementary fluid feed device with automatic tandem metering valves
US2611592A (en) * 1948-10-27 1952-09-23 Thompson Prod Inc Dual carburetor
US2624558A (en) * 1948-10-27 1953-01-06 Thompson Prod Inc Supplementary fuel feed device
US2616405A (en) * 1948-11-20 1952-11-04 Ethyl Corp Enrichment device and method of controlling the same
US2661196A (en) * 1949-05-13 1953-12-01 Chrysler Corp Carburetor
US2664871A (en) * 1949-07-30 1954-01-05 Thompson Prod Inc Supplemental fuel feed device
US2808245A (en) * 1950-11-20 1957-10-01 Anna M Grover Fuel feed devices for internal combustion engines
US2699326A (en) * 1951-05-31 1955-01-11 Thompson Prod Inc Collar mounted dual actuated fuel feed device
US2717149A (en) * 1951-10-09 1955-09-06 Thompson Prod Inc Fluid feed device
US2711885A (en) * 1952-10-20 1955-06-28 Carter Carburetor Corp Carburetor metering control
US2791995A (en) * 1954-02-15 1957-05-14 Gen Motors Corp Anti-detonation device for a carburetor
US6394426B1 (en) * 2000-07-07 2002-05-28 Walbro Corporation Engine dual fuel supply apparatus

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