US3897765A - Carburetor cranking fuel flow rate control - Google Patents

Carburetor cranking fuel flow rate control Download PDF

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US3897765A
US3897765A US430819A US43081974A US3897765A US 3897765 A US3897765 A US 3897765A US 430819 A US430819 A US 430819A US 43081974 A US43081974 A US 43081974A US 3897765 A US3897765 A US 3897765A
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fuel
passage
flow
cranking
valve
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US430819A
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Robert S Harrison
John D Medrick
Alvin P Nowroski
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Ford Motor Co
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Ford Motor Co
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Priority claimed from AU76457/74A external-priority patent/AU479388B2/en
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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
    • F02M1/00Carburettors with means for facilitating engine's starting or its idling below operational temperatures
    • F02M1/04Carburettors 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
    • F02M1/046Auxiliary carburetting apparatus controlled by piston valves
    • 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
    • F02M1/00Carburettors with means for facilitating engine's starting or its idling below operational temperatures
    • F02M1/08Carburettors with means for facilitating engine's starting or its idling below operational temperatures the means to facilitate starting or idling becoming operative or inoperative automatically
    • F02M1/10Carburettors with means for facilitating engine's starting or its idling below operational temperatures the means to facilitate starting or idling becoming operative or inoperative automatically dependent on engine temperature, e.g. having thermostat
    • 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
    • F02M9/00Carburettors having air or fuel-air mixture passage throttling valves other than of butterfly type; Carburettors having fuel-air mixing chambers of variable shape or position
    • F02M9/10Carburettors having air or fuel-air mixture passage throttling valves other than of butterfly type; Carburettors having fuel-air mixing chambers of variable shape or position having valves, or like controls, of elastic-wall type for controlling the passage, or for varying cross-sectional area, of fuel-air mixing chambers or of the entry passage
    • F02M9/106Pneumatic or hydraulic control

Abstract

A carburetor has a supplemental fuel supply system for adding extra fuel to the carburetor during cold engine cranking to satisfy the richness requirement at this time. The extra fuel is supplied by a connection to a fuel reservoir past first, a flow rate control valve, and second, past a solenoid controlled valve that opens in response to closing of the engine starter relay to permit the induction of the extra fuel during engine cranking. A temperature responsive member is included to break the circuit above say 125*F., for example, to the solenoid. The flow rate control valve is moved by a temperature responsive element to progressively restrict or unblock the fuel passage entrance, thereby varying the rate of flow with temperature changes.

Description

United States Patent Harrison et a1.
CARBURETOR CRANKING FUEL FLOW RATE CONTROL inventors: Robert S. Harrison, Grosse lle; John D. Medrick, Plymouth; Alvin P. Nowroski, Livonia, all of Mich.
Assignee: Ford Motor Company, Dearborn,
Mich,
Filed: Jan. 4, 1974 Appl. No.: 430,819
[52] US. Cl 123/179 G; 261/39 D; 261/44 R [51] Int. Cl. F02M 17/00 [58) Field of Search 123/179 G, 187.5 R; 261/39 D [56] References Cited UNITED STATES PATENTS 2,905,165 9/1959 Hall 123/179 G 2,940,436 6/1960 DeClaire et al.... 261/39 D 3,587,553 6/1971 Sutton 123/179 G 'nmu mm Aug. 5, 1975 [57] ABSTRACT A carburetor has a supplemental fuel supply system for adding extra fuel to the carburetor during cold engine cranking to satisfy the richness requirement at this time. The extra fuel is supplied by a connection to a fuel reservoir past first, a flow rate control valve, and second, past a solenoid controlled valve that opens in response to closing of the engine starter relay to permit the induction of the extra fuel during engine cranking. A temperature responsive member is included to break the circuit above say 125F., for example, to the solenoid. The flow rate control valve is moved by a temperature responsive element to pro gressively restrict or unblock the fuel passage entrance, thereby varying the rate of flow with temperature changes.
5 Claims, 10 Drawing Figures FICLQL SHEET i' ATEF-ITEU AUG 1975 SHEET PATENTED AUG 5 I975 SHEU PATENTEDAUB 5|975 PIC 2.3
SHEET PATENTEI] AUG 51975 PATENTEDMJB 1975 1 F'IG.6
CARBURETOR CRANKING FUEL FLOW RATE CONTROL This invention relates to a motor vehicle carburetor and more particularly to a system for supplying cranking fuel to the engine.
A conventional downdraft carburetor has an idle speed channel that bypasses the induction passage around the throttle valve to permit a supply of fuel and air when the throttle valve is closed, such as during engine idling speeds and starting. For starting in cold weather below say 125F., a choke valve is rotated towards a closed position as a function of temperature changes to restrict the air inlet and thereby draw in the richer mixture necessary for cranking at these temperatures.
This invention relates to a variable area venturi carburetor in which at least one wall of the venturi is moved to enlarge the venturi. Tapered fuel metering rods attached to the movable wall are withdrawn from fuel jets to simultaneously change fuel flow. The engine cranking position and idle speed position of the venturi are the same, and this type of carburetor has no choke valve. However, it is still necessary during cold engine operation, to supply the carburetor with extra fuel and in amounts that increase as the temperature drops.
Therefore, it is an object of this invention to provide a cranking fuel system for a carburetor that is operative below a predetermined temperature to supply quantities of fuel to the carburetor that are in addition to whatever fuel may be inducted in the normal manner.
Another object of the invention is to provide a carburetor cold weather operating cranking fuel system that is operative when the engine ignition is turned to an engine start position below a predetermined temperature to energize a solenoid to unblock a fuel passage and permit the induction of additional quantities of fuel to the engine, the rate of supply being controlled by means of a tapered valve move as a function of temperature changes.
Other objects, features and advantages of the invention will become more apparent upon reference to the succeeding detailed description thereof, and to the drawings illustrating the preferred embodiments thereof, wherein;
FIG. 1 is a plan view of a portion of a variable area venturi type carburetor embodying the invention;
FIG. 2 is a side elevational view taken on a plane indicated by and viewed in the direction of the arrows 22 of FIG. 1;
FIG. 3 is a cross sectional view taken on a plane indicated by and viewed in the direction of the arrows 3-3 of FIG. 1;
FIGS. 4 and 5 are enlarged cross sectional views taken on planes indicated by and viewed in the direction of the arrows 44 and 55 of FIG 1;
FIG. 6 is a cross sectional view taken on a plane indicated by and viewed in the direction of the arrows 6-6 of FIG. 1;
FIG. 7 is a bottom view taken on a plane indicated by and viewed in the direction of the arrows 7-7 of FIG. 6, and looking up at the underside portion of the air horn portion of the carburetor;
FIG. 8 is a cross sectional view taken on a plane indicated by and viewed in the direction of the arrows 8-8 of FIG. 6 and looking down on the main or central body portion of the carburetor; and,
FIGS. 9 and 10 are cross sectional views taken on planes indicated and viewed in the direction of the arrows 99 and 10-10 of FIG. 8.
FIG. I, which is essentially to scale, is a plan view of a variable area venturi carburetor of the downdraft type. It has a pair of rectangularly shaped induction passages 10, each having one end wall 12 which is pivotally movable and has the profile (FIG. 3) of one-half of a venturi 13. Each opposite fixed cooperating wall 14 is formed with the mating profile of a portion of a venturi. The airflow capacity, therefore, varies in proportion to the opening movements of walls 12 of the in duction passages.
As seen more clearly in FIG. 3, movable walls 12 are pivotally mounted at 15 on a stationary pin. The pin ac tually is fixed to a strut, not shown, that depends from a section of the upper body of the carburetor. Pivotally attached to each of the wall bodies is a fuel metering rod 16 that cooperates with a main fuel metering jet 18. The needles have a controlled taper to provide a richer air/fuel mixture at the lower and higher ends of the venturi opening range. Each jet is located in an aperture inside wall 14 at approximately the throat or most constricted section ofventuri 13. A fuel float bowl or reservoir 20 has a pair of identical passages 22 conducting fuel to the main metering jets I8. Downstream of the venturis, the carburetor throttle body portion 23 rotatably mounts a shaft 24 on which are fixed a pair (only one shown) of conventional throttle plates 25 that control the flow of air and fuel through induction passages 10.
The size of venturis l3 and the movement of walls 12 is controlled in this case by a spring returned, control vacuum actuated, diaphragm type servo 26. The servo consists of a hollow two-piece casting divided into two chambers 28 and 30 by an annular flexible diaphragm 32. The diaphragm is sealingly mounted along its edge in the casting. Chamber 28 is an air chamber, connected to ambient or atmospheric pressure through a passage 34 (indicated also in FIGS. I, 6 and 8). Chamber 30 is a vacuum chamber connected to induction passages 10 at a point below the throat but still in the venturi 13. This subjects chamber 30 to changes in a control vacuum that varies with airflow but at a rate that is slightly different than true venturi vacuum. The exact location of the tap of course is a matter of choice. Chamber 30 also is connected to be actuated by ported intake manifold vacuum, for cold weather operation, as will be described in more detail later.
Completing the construction, servo 26 has fixed to one side of diaphragm 32, by a retainer 35, a plunger or actuator 36. The plunger is pivotally connected to a shaft 37 interconnecting cast portions of the movable walls 12. Fixed to the other side of diaphragm 32 is a retainer 38 against which is seated a spring 39. The other end of the spring bears against a seat 40 axially adjustable to vary the spring preload.
FIG. 3 indicates schematically in dotted lines a passage p between chamber 30 and induction passages 10. In actuality, as best seen in FIGS. 5, 8, 9 and 10, servo chamber 30 is connected by a restricted line 41 (FIG. 8) to an intersecting passage 42 (FIGS. 810). Passage 42 intersects with a vertically downwardly extending passage 44 (FIG. 10) containing a flow restrictor or orifice 46 and terminating in a chamber 48. Chamber 48 is connected by a port 50 to induction passage I0 at a point below the edge of throttle valve 25 when it is in its closed position shown. In the position shown, therefore, as the throttle valve is rotated to an open position, port 50 is progressively subjected to the increased pres sure above the throttle valve to bleed the vacuum in passage 42.
Passage 42 also intersects with a right angled passage 52 (FIGS. 8, 9 and 5) that connects to a passage 54 (FIG. 5). The latter passes vertically through the main body portion of the carburetor into a horizontal passage 56 located in the carburetor air horn section. Passage 56 in turn is connected by a pair of passages 58 and 60 to the well 62 (FIG. 8) in which is arcuately movable one of the mounting members 70 (FIG. 3) for movable wall 12. While not shown, the well 62 in FIG. 8 and the adjacent induction passage 10 are interconnected by a depressed portion of the main body between the two so that the opening 63 shown in FIG. 5 senses the control or venturi-like vacuum connected by the passages named to servo chamber 30.
Looking now at FIG. 5, the opening 63 to the control vacuum in this case is adapted to be alternately restricted or progressively opened by a needle type valve 72. The valve is movable into and out of the seat 63 in response to a temperature sensitive element, in a manner that will be described more clearly later. Suffice it to say at this point, that during normal engine operating temperatures, the needle valve 72 is completely withdrawn from opening 63 thereby permitting venturi-like vacuum to be sensed through passages 60, 58, 56, 54, 52, 42 and 40 to chamber 30 of the servo, the ported manifold vacuum simultaneously being sensed through port 50, chamber 48, line 42 to line 41 and servo chamber 30.
It should be noted that the size of the venturi-like vacuum passages 60, 58, 56, 54 and 52 are considerably larger than that of the ported manifold vacuum passage 44, coupled with the orifice 46, so that when the needle valve 72 is in the up position, the manifold vacuum is bled to the level of the venturi-like or control vacuum and, therefore, has essentially no effect on the movement of servo 26. The manifold vacuum is used during cold weather operations to modulate the venturi-like or control vacuum to schedule the opening of the venturi 13 to regulate the richness of the fule/air mixture. When the needle valve 72 is in the closed or nearly closed position, the venturi vacuum flow will be essentially blocked and manifold vacuum will be the prime force acting on servo chamber 30. This will cause the movable venturi walls 12 to be moved to a larger area venturi pulling the fuel metering rods l6 out further.
As thus far described, during normal engine operating temperatures, the operation is as follows. The rotative movement of throttle valves 25 controls total airflow through both passages 10 to increase as the throttle valves are moved from their closed position. An increase in airflow provides essentially a proportional increase in the control vacuum in chamber 30 from port 63 until the diaphragm 32 is moved towards the cup 40. This moves both wall 12 to open induction passages 10 and increase the area of venturis 13 while simultaneously retracting the fuel metering rods 16 to increase fuel flow. Thus, the total airflow and fuel flow vary with changes in throttle valve setting up to a maximum.
Returning now to the general construction shown in FIG. 1, during cold engine operation, as stated previously, it is desirable to provide an additional supply of fuel to the induction passages to assure sufficient fuel vapor both for starting the engine as well as a different schedule of additional fuel for running the cold engine prior to its reaching normal operating temperature level. These requirements are satisfied by providing a combination fuel enrichment system, a cranking fuel enrichment system embodying the invention, as well as a throttle plate positioner device to crack open the throttle plates an additional amount during cold starting operations.
More specifically, FIGS. 5, 6 and 8 show portions of both the cold running enrichment system as well as the cold start cranking fuel system. The body portion of the carburetor is cast with a fuel bowl 20 containing fuel delivered thereto past a conventional inlet needle valve from a supply line 82. The needle valve 80 is moved vertically in a bore 84 by the tab 86 secured to a float member 88 pivotally mounted at 90 on a depending portion of the air horn section of the carburetor.
The inlet valve 80 operates in a known manner. Movement of float 88 downwardly as a result of lowering of the liquid fuel level causes the needle 80 to drop. This permits fuel under pressure to enter the reservoir from line 82 to fill it again to the desired level. Raising of the float raises the inlet valve against the conical seat shown to shut off the supply when the desired level has been reached.
The lower portion of fuel bowl 20 contains a needle like cranking fuel supply valve (FIG. 5). The latter has a conical valve portion 102 that cooperates with the upper edges 104 of a fuel well 106. Valve 100 is connected to a temperature responsive device to be moved into and out of the wall with changes in temperature, in a manner to be described, to control the rate of flow of fuel from reservoir 20 into fuel well 106. Well 106 is connected to an intersecting passage I12 (FIG. 8) that connects with a cross passage 114 to flow fuel into another passage 116 past a solenoid controlled valve unit 118.
As best seen in FIG. 6, unit 118 consists essentially of a valve 120 formed on the end of the armature of a solenoid 122. A spring not shown normally biases valve 120 to close communication between passages 114 and 116. The solenoid normally would be powered from the starter relay of the motor vehicle ignition system so that the solenoid is rendered operative only during engine starting conditions. That is, when the ignition key is turned to the start position, the solenoid l 18 would be energized and cause valve 120 to be retracted rightwardly to open communication between passages 114 and 116. A flow of starting fuel would then be permitted from fuel bowl 20 into passage I16.
As soon as the engine attained running condition, return of the ignition switch to the on position would deenergize solenoid 122 and again block passage 114 from communicating with passage 116. The solenoid unit could include a manifold vacuum switch so the solenoid is not energized above a vacuum level of say 2 inches Hg, for example. It also could contain a thermal switch to prevent operation above 120F., for example, when extra cracking fuel usually is not needed.
From passage 116 the fuel passes upwardly through the carburetor main body passage 124 (FIG. 6) where it flows into a plenum 126, shown also in FIG. 7. From the plenum, the fuel is divided equally to be inducted out through passages 128 into each of the induction passages 10 at a location adjacent the venturi but spaced from the fuel jets 18. Thus, it will be seen that for starting operations, energization of the solenoid by turning of the vehicle ignition switch causes additional fuel to be added at times to the induction passages, for starting purposes.
The quantity of cranking fuel to be added to the in' duction passages, or, on the other hand, the position of cranking valve 100, is controlled by the connection of valve 100 to the lower end of a needle valve 140 (FIG. 5). The needle valve forms a portion of the engine running fuel enrichment system. More specifically, needle valve 140 is tapered at its lower end as shown at 142, for a purpose to be described, and has a universal con' nection 144 to the plastic conical valve 100. The latter defines a variable flow area 145 between the valve and wall of well 106 that varies in size as a function of the vertical movement of valve 100. Therefore, vertical movement of valve 100 modulates the rate of flow of fuel from reservoir 20 into well 106 when solenoid valve 120 is opened. The needle valve 140 moves upwardly and downwardly with changes in temperature, as will now be described.
The needle valve 140, in this case, is vertically movable in a well 146 in the upper body portion. It is axially aligned by a seal 148 and a valve seat 150 with which it cooperates to meter fuel. The seal and seat define a chamber 152 which is connected by an angled passage 154 to the end 156 of a wormlike passage 158 best seen in FIG. 7. The opposite end 160 of passage 158 connects with a vertical passage 162 (FIG. 6) that intersects an angled passage 164 leading to the plenum 126. As stated previously, plenum 126 also receives fuel from the cranking fuel passage 124. Together then, the fuel passes into each induction passage through the side passages 128. It will be seen then that, depending upon the vertical position of needle valve 140, a quantity of fuel will flow past the tapered portion 142 of the needle valve into the various passages into induction passages 10 to supply additional fuel during cold running operation of the engine.
The vertical movement of needle valve 140 is controlled by a temperature sensitive element that moves the needle valve 140 upwardly to increase fuel flow as the temperature decreases below the normal operating level, and moves the needle valve 140 to a downward position to shut off the fuel enrichment when the temperature reaches the normal operating level. Concurrently, the downward movement of needle valve 140 as the temperature increases will move the cranking fuel valve 100 downwardly in proportion to the temperature increase. Threfore, when the normal operating level is reached, cranking valve 100 will provide a maximum restriction to flow through the area 145, and very little additional fuel will then be added during starting of the engine.
The upper end of needle valve 140 is pivotally connected to the end of a lever 166. The lever is pivotally mounted on a pin 168 projecting through an aperture in a boss 170 projecting from the carburetor upper body. The opposite end of lever 166 is pivotally connected to an adjustable nut 172 on the upper end of a depending link 174. The link 174 is adapted to be connected to a thermostatically responsive movable element to be described. Adjusting the upper end 172 of course will vary the operating characteristics of the system. Downward movement of link 174 is limited by abutment of the nut 172 against a stop washer 176.
Projecting horizontally or laterally from link 174 is a connector 178 pivotally engaging the threaded upper end 180 of needle valve 72. The upper end 180 contains a yoke member 182 adjustably threaded to the end of needle valve 72 as shown to determine the upward and downward limits of movement of the needle valve.
As thus far described, therefore, with respect to the running fuel enrichment system, with the throttle plates in the idle speed positions, when link 174 is in the position shown indicating that the temperature is at the lowest below normal engine operating level, the needle valve will have been moved to its upwardmost position to provide maximum rate of fuel flow. Needle valve 72 also will have moved to its downwardmost position restricting the port or outlet 63 to the induction passage shown in FIG. 8. Thus, ported manifold vacuum in port 50 (FIG. 10) will act in servo chamber 30 to move walls 12 to enlarge the venturi areas, which decreases the fuel metering signal acting on both outlet passages 128 and jet 18. This leans the mixture as compared to the cranking mixture and what it would be under accelerative conditions.
Simultaneously, maximum additional fuel quantity will flow from the fuel enrichment well 152 into the induction passages 10 through the interconnecting outlet passages 128. As soon as the temperature increases from its lowest setting, the link 174 will move vertically upwardly from the position shown. This will gradually and progressively raise the venturi-like vacuum control needle valve 72 and lower progressively the needle valve 140. Thus, the venturi-like control vacuum begins to bleed into passage 60. The vacuum force acting on servo chamber 30 will progressively decrease to permit servo spring 39 to slowly close the venturi towards the normal engine idle speed position. The additional fuel enrichment will decrease as the tapered portion 142 of needle valve 140 closes the opening to the fuel bowl.
Turning now to the temperature responsive control of the movement of link 174 and the throttle valve positioner, FIGS. 1, 2 and 4 show the same more clearly. As best seen in FIG. 4, the lower end of link 174 is pivotally connected to one end of a lever 216 that is fixed on a shaft 218. The other end of lever 216 adjustably supports a screw 220 that bears against the end 222 of an essentially conventional fast idle cam 224. The cam is rotatably mounted on shaft 218 and has a weighted lower end 223. The end has a peripheral edge portion formed with a series of circumferentially contiguous steps 224, 226 and 228 and a high cam step 230. Each step progressively in the order named is of greater radial extent than the previous.
Cooperating with fast idle cam 224 to locate or position the throttle plates 25 is a lever or throttle stop 232 formed at its outer end with a curved engaging portion 234. Lever 232 is rotatably mounted on throttle shaft 24. It has a depending tang portion 236 engaged by the end of an adjustably mounted screw 238 carried by a linkage 240 fixed to the throttle shaft 24. A throttle return coil spring 242 has one end 244 anchored under a pin 246 extending from a fixed portion of the carburetor throttle flange. The opposite end of the spring bears against an angled tang 250 of linkage 240 thereby biasing the linkage and screw 238 in a clockwise direction against the tab end 236 oflever 232. The lever 232 thus is constantly biased in a clockwise direction towards the edge surface of fast idle cam 224. The cam steps therefore constitute abutment means or stops in the path of movement of lever 232 to determine the idle speed position of throttle plates 25.
lnsertable at times between the end 234 of lever 232 and the edge of fast idle cam 224 is the finger portion 252 of an arcuately movable link 254. The latter is pivotally connected at 256 to the end of a lever 258 rotatably mounted on shaft 218. Lever 258 is connected at its upper end at 260 to an actuating link 262. The opposite end of link 262 is connected to one end of a bell crank lever 264 pivotally mounted at 266 on the ears of an extension of a servo housing 268.
The servo housing is hollow and divided into two chambers 270 and 272 by an edge mounted annular flexible diaphragm 274. Chamber 270 is an air chamber communicating to the atmosphere through an opening 276. Chamber 272 is a vacuum chamber communicating by a passage not shown with the induction passages at a location below the throttle valves 25. A plunger 278 is riveted at one end 280 to a hat shaped spring retainer 282, and projects through a stop 284 for connection to the opposite end 286 of bell crank lever 264. A compression spring 288 normally biases the plunger 278 upwardly to move bell crank 264, link 262, lever 258 and finger portion 254 in a clockwise direction.
Application of engine vacuum to the servo chamber 272 when the engine is running is sufficient to counteract the force of spring 288 and cause the plunger 278 to move vertically downwardly. This moves lever 258 and finger portion 254 in a counterclockwise direction to withdraw or retract the finger portion from between the lever end 234 and the fast idle cam steps.
Thus, it will be seen that when the engine is off preparatory to starting operation, depression of the vehicle accelerator pedal will rotate throttle shaft 24 and lever 232 in a counterclockwise direction away from the end 252 of finger portion 254. Since there is no manifold vacuum in chamber 272 of servo 269, spring 288 will position the finger portion 254 to the position shown so that upon release of the accelerator pedal, coil spring 242 will cause a clockwise return movement of the throttle valve lever 232 until it engages the arcuate portion 290 of the end 252 of the finger portion 254, which in turn abuts the edge of the fast idle cam 224.
Once the engine has attained running operation beyond cranking vacuum level, then opening of the throttle valves 25 by depression of the accelerator pedal, pivots lever 232 downwardly and permits retraction or movement of finger portion 254 to an inoperative position to the right by the vacuum in servo 268. Lever 232 then is permitted to engage the edge of the fast idle cam directly and the position of the throttle plates will be determined strictly by the rotative position of the fast idle cam 224.
The fast idle cam is controlled in its rotation by a lever 292 fixed on shaft 218. The lever is located within a hollow cup-shaped housing 294 that is cast integrally with the throttle body portion '23. Lever 292 has an upturned slotted end 296 in which is located the outer end 297 of a thermostatically responsive bimetallic spring coil 298. The inner end of the spring is fixed on a stub shaft 300 projecting from an insulated cover 302. The cover is fastened by screws to the housing 294 with an insulating gasket 302 between. The gasket has an arcuate slot 304 along which the end 296 moves with tem perature changes. The gasket also has a hole 306 through which projects the end 308 of a tube connected by a pair of passages 309 and 310 to the induction passages 10 at a location (not shown) below the throttle valves. For clarity, the cover 302 has been removed in FIG. 2, and FIG. 4 shows the outline of the housing in phantom, for orientation purposes. Completing the construction, the housing has a hot air inlet tube 312 connected by a passage 314 to the interior of housing 294 on the far side of gasket 302. The tube would emanate from a known type of exhaust manifold heated stove in which air flowing past the manifold is warmed.
in operation, once the engine is operating, with gasket 302 in place and cover 304 applied, manifold vacuum acting in passages 309 and 310 causes hot air to flow into tube 312 to the far side of gasket 302. The air is then drawn through the slot 306 and out through passages 309 and 310, warming the coil 298 as it passes it. Thus, the coil will be progressively warmed as the engine temperature rises, resulting in a circumferential movement of the end 297 of the coil to rotate lever 292 in the same direction. This rotates lever 216 away from the fast idle cam and permits the fast idle cam to rotate counterclockwise by gravity. Similarly, upon engine shutdown, cooling of the coil will cause it to rotate levers 292 and 216 in the opposite direction. This of course simultaneously rotates the fast idle cam 224 by the screw 220, so that, depending upon the temperature level, one of the steps 225, 226, 228 or the high cam step 230 will be presented opposite the end 234 of throttle lever 232. Thus, the throttle plate idle speed setting will be determined by which step is engaged by lever 232, during running operations of the engine. During cold start operations, as described previously, the finger portion 254 will be inserted between the end 234 of lever 232 and whatever step or rotative cam position the fast idle cam 224 has attained so that the throttle plates are opened more for starting purposes than during normal cold running conditions.
It will be seen, therefore, that regardless of what position the fast idle cam 224 assumes because of the prevailing ambient temperature, the throttle plates will be opened an additional amount for starting purposes. The additional amount will vary to agree with the ambient temperature level so that a correct starting air/fuel mixture is obtained. This is in contrast to the conventional constructions in which there is only one fast idle start position, accomplished only by positioning the single high step 230 against the throttle lever end 234. At the inbetween temperature levels, this is too high and results in too fast an idle speed, and one that may provide undesirable emissions.
The overall operation of the carburetor is believed to be clear from the above description and by reference to the drawings. Therefore, it will be repeated now only briefly. Assume that the engine is off and the ambient temperature is essentially 0F. The coiled bimetallic spring 298 will have contracted a maximum amount rotating lever 292 clockwise from the position shown in FIG. 2 to position the end 297 of the lever at the left end 316 of the slot 306. This will rotate lever 216 to move the fast idle cam 224 clockwise to locate the high cam step 230 opposite the end 234 of throttle lever 232. Simultaneously, by opening the throttle plates, lever 232 will move away from the fast idle cam and permit the servo spring 288 to move the finger portion 254 between the fast idle cam step 230 and lever 232. The throttle plates now will be opened a maximum amount for the coldest start positions. The induction passages at this time are at their smallest cross section because the servo spring 39 has moved walls 12 to this position. This, therefore, exposes the passages to a larger cranking vacuum signal so that the airflow across the fuel metering jets 18 is increased Simultaneously, the rotation of lever 216 moves link 174 downwardly to its extreme position until the stop 172 shown in FIG. 5 abuts the washer 176. This pivots needle valve 140 to its uppermost position allowing a maximum amount of fuel from fuel bowl 20 through the space between the seat 150 and the tapered lower portion of valve 140. This upward position also moves the cranking valve 100 upwardly to open wide the passage 145 to flow fuel to passage 112. Therefore, when the ignition switch is turned to an on or start position, the solenoid 118 will withdraw the valve 120 to permit a maximum rate of fuel to flow from passage 114 to 116.
When the engine is cranked for starting purposes, the cranking vacuum signal is sufficient acting across the induction passage outlets 128 (FIG. 7) to draw fuel up cranking fuel circuit passage 124 into plenum 126. Simultaneously, fuel is drawn past the engine running fuel circuit needle valve 140 into the worm passage 158 (FIG. 7) to plenum chamber 126, where both circuits combine and the fuel inducted to provide the necessary starting richness. Once the engine has been started, release of the ignition switch to the engine running, posi tion deenergizes solenoid 118 to then again block the connection between the cranking supply line 114 and the line 116. However, with the link 174 in its downwardmost coldest position, the valve 72 will also be down essentially blocking off port 63. Accordingly, the higher ported engine running manifold vacuum will act in servo chamber 30 and draw the walls 12 of the ven turis to open or enlarge the venturi area.
With the throttle plates unmoved from the fast idle speed position, the opening of the venturis will decrease the air velocity across the fuel jet 18 to decrease the fuel metering signal while at the same time enlarging the fuel jet orifices. Simultaneously, the area of discharges 128 being constant, lowering the air velocity decreases the fuel metering signal to decrease fuel output through these passages. This leans the overall mixture for the closed throttle position attained at that temperature level. At closed throttle, the manifold vacuum is considerably higher than the cranking vacuum. This causes excess vaporization and would normally lead to a richer than desired mixture. However, the ported manifold vacuum control in this case compensates for this by leaning the overall mixture to the desired level by opening the venturis.
Similarly, once the throttle plates are moved to an off-idle accelerative position, the manifold vacuum level is reduced so that there now is less vaporization. A slightly richer mixture, therefore, is desired to provide acceptable engine operation. This is accomplished by the throttle plates traversing the port 50 as they move off-idle, which progressively subjects the chamber 48 to more and more control vacuum existing above the throttle plates. The manifold vacuum signal acting on servo 30 therefore decays, and the venturi moves towards a more closed position to provide the richer setting desired. It is only a very short time, therefore, before the throttle plates have completely traversed the port 50, leaving control of movement of the venturi then strictly to the changes in venturi-like control vacuum. Thus, a richer than normal idle but less than cranking mixture is provided at this time by the main fuel metering system as well as the needle valve supplemental feed system.
Concurrent with the engine attaining a running condition, the manifold vacuum established in servo chamber 272 will be sufficient, once throttle lever 232 is pivoted counterclockwise to release finger portion 254, to pivot the finger portion out from between the end 234 of lever 232 and the fast idle cam step it abuts. Now the portion 234 will move to directly abut the step of the idle cam 224 and thereby close down the throttle plates to less open fast idle speed positions. This reduces both the fuel flow and airflow for cold running operations, which as stated above is desired because a less rich air/fuel mixture is required once the engine has attained its idle speed horsepower.
As the temperature increases, the bimetallic coiled spring 298 will rotate the lever 216 in a counterclockwise direction away from the fast idle cam. The cam then can move in the same direction by gravity when the throttle plates are opened beyond the fast idle position so that the end of lever 234 gradually moves progressively clockwise to permit the progressive closure of the throttle plates to less open idle speed positions. Simultaneously, the counterclockwise rotation of lever 216 effects an upward movement of link 174 to progressively move the needle valve 140 downwardly and thereby progressively close off the additional fuel flow past the valve. This movement also causes an upward movement of needle valve 72 so that the venturi-like vacuum decays whatever ported manifold vacuum signal is acting in servo chamber 30.
Thus, for closed throttle plate positions, the lowering vacuum signal in pressure chamber 30 will permit the venturi walls 12 to move to contract the venturi area and move the metering rods 16 into the jet 18. Eventually, therefore, the throttle plates will be returned to a normal closed idle speed position, the needle valve 72 will be drawn essentially completely out of port 63 so that movement of the venturi walls will be controlled solely by control or venturi-like vacuum changes, and the supplemental fuel needle valve 140 will be moved downwardly to shut off or essentially close off the supply of additional fuel to the system. At this time, the cranking valve will be at a minimum rate of flow position. The closing venturi increases the air velocity past the fuel jet 18. The fuel jet, threfore, will have a smaller flow area. The total fuel flow will be less because the throttle plates are now closed more completely and because no fuel is now being inducted from passages 128, but only that through the main jets 18.
While the invention has been shown and described in its preferred embodiment, it will be clear to those skilled in the arts to which it pertains that many changes and modifications may be made thereto without departing from the scope of the invention.
We claim:
1. An engine cranking fuel supply system comprising, a carburetor having an induction passage connected to fresh air at one end and adapted to be connected to the engine intake manifold at the other end, a fuel port opening into the passage, and dual fuel supply means connected to the port for the induction of varying amounts of cranking fuel to the port as a function of changes in temperature from a predetermined level, the dual fuel supply means including first and second fuel passages each connected at one end to the fuel port and at its other end to a source of fuel, the first passage containing a valve variably movable between flow and no flow positions, the second passage containing an on-off valve movable to block and unblock the second passage, the second passage also containing flow control means variably movable in the second passage for modulating the rate of flow of fuel through the second passage, means biasing the valves towards noflow positions blocking the first and second fuel passages, means responsive to an engine cranking operation to move the on-off valve to an on-flow position permitting the induction of cranking fuel through the port from the second passage, and temperature responsive means connected to both the first passage valve and the flow control means for modulating the rate of flow of fuel through both the passages as a function of changes in temperature from a predetermined level.
2. A cranking fuel system as in claim 1, including a fuel reservoir supplying fuel to the fuel passages, the second passage flow control means comprising a tapered valve movable into and out of the second passage to control the volume of fuel admitted to the second fuel passage, the temperature responsive means including a temperature responsive device operatively connected to the tapered valve for moving it in one direction.
3. A cranking fuel system as in claim 2, the means biasing the valves including spring means biasing the lapered valve to an open position permitting the free supply of fuel from the reservoir to the second fuel passage.
4. A cranking fuel system as in claim 2, wherein the temperature responsive device operatively engages the tapered valve at times and moves the tapered valve to positions progressively decreasing the quantity of fuel admitted from the reservoir to the second fuel passage as the temperature increases towards the predetermined level.
5. An engine cranking fuel supply system comprising, a carburetor having an induction passage connected to fresh air at one end and adapted to be connected to the engine intake manifold at the other end, a fuel port opening into the passage, and dual fuel supply means connected to the port for the induction of varying amounts of cranking fuel to the port as a function of changes in temperature from predetermined level, the dual fuel supply means including first and second fuel passages each containing a temperature responsive flow control means variably movable to decrease the cranking fuel flow as temperature increases towards a predetermined level, a flow-noflow valve in the second passage movable to a flow position in response to an engine cranking operation to permit flow through the second passage and movable to a non-flow position in response to the engine attaining a running condition whereby fuel flow for cold engine operation is supplied in varying amounts to the fuel port from both passages below the predetermined temperature level during engine cranking, and from only the first passage after the engine hs attained a running condition.

Claims (5)

1. An engine cranking fuel supply system comprisiNg, a carburetor having an induction passage connected to fresh air at one end and adapted to be connected to the engine intake manifold at the other end, a fuel port opening into the passage, and dual fuel supply means connected to the port for the induction of varying amounts of cranking fuel to the port as a function of changes in temperature from a predetermined level, the dual fuel supply means including first and second fuel passages each connected at one end to the fuel port and at its other end to a source of fuel, the first passage containing a valve variably movable between flow and no flow positions, the second passage containing an on-off valve movable to block and unblock the second passage, the second passage also containing flow control means variably movable in the second passage for modulating the rate of flow of fuel through the second passage, means biasing the valves towards no-flow positions blocking the first and second fuel passages, means responsive to an engine cranking operation to move the on-off valve to an on-flow position permitting the induction of cranking fuel through the port from the second passage, and temperature responsive means connected to both the first passage valve and the flow control means for modulating the rate of flow of fuel through both the passages as a function of changes in temperature from a predetermined level.
2. A cranking fuel system as in claim 1, including a fuel reservoir supplying fuel to the fuel passages, the second passage flow control means comprising a tapered valve movable into and out of the second passage to control the volume of fuel admitted to the second fuel passage, the temperature responsive means including a temperature responsive device operatively connected to the tapered valve for moving it in one direction.
3. A cranking fuel system as in claim 2, the means biasing the valves including spring means biasing the tapered valve to an open position permitting the free supply of fuel from the reservoir to the second fuel passage.
4. A cranking fuel system as in claim 2, wherein the temperature responsive device operatively engages the tapered valve at times and moves the tapered valve to positions progressively decreasing the quantity of fuel admitted from the reservoir to the second fuel passage as the temperature increases towards the predetermined level.
5. An engine cranking fuel supply system comprising, a carburetor having an induction passage connected to fresh air at one end and adapted to be connected to the engine intake manifold at the other end, a fuel port opening into the passage, and dual fuel supply means connected to the port for the induction of varying amounts of cranking fuel to the port as a function of changes in temperature from predetermined level, the dual fuel supply means including first and second fuel passages each containing a temperature responsive flow control means variably movable to decrease the cranking fuel flow as temperature increases towards a predetermined level, a flow-noflow valve in the second passage movable to a flow position in response to an engine cranking operation to permit flow through the second passage and movable to a non-flow position in response to the engine attaining a running condition whereby fuel flow for cold engine operation is supplied in varying amounts to the fuel port from both passages below the predetermined temperature level during engine cranking, and from only the first passage after the engine hs attained a running condition.
US430819A 1974-01-04 1974-01-04 Carburetor cranking fuel flow rate control Expired - Lifetime US3897765A (en)

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US430819A US3897765A (en) 1974-01-04 1974-01-04 Carburetor cranking fuel flow rate control
CA216,274A CA1036441A (en) 1974-01-04 1974-12-16 Carburetor cranking fuel flow rate control
AU76457/74A AU479388B2 (en) 1974-01-04 1974-12-16 Carburetor cranking fuel flow rate control
GB5530474A GB1475008A (en) 1974-01-04 1974-12-20 Carburetor cranking fuel system
DE19742461277 DE2461277A1 (en) 1974-01-04 1974-12-23 EQUIPMENT ON A CARBURETOR FOR MOTOR VEHICLES TO ACHIEVE A RICHER AIR-FUEL MIXTURE
JP49149078A JPS5834664B2 (en) 1974-01-04 1974-12-27

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WO1980000470A1 (en) * 1978-08-19 1980-03-20 Ford Motor Co Down-draft carburetor
US4205641A (en) * 1978-01-13 1980-06-03 Yamaha Hatsudoki Kabushiki Kaisha Start control means for internal combustion engine
US4276238A (en) * 1978-10-19 1981-06-30 Nissan Motor Company, Limited Carburetor with automatic choking and acceleration device
US9464588B2 (en) 2013-08-15 2016-10-11 Kohler Co. Systems and methods for electronically controlling fuel-to-air ratio for an internal combustion engine
US10054081B2 (en) 2014-10-17 2018-08-21 Kohler Co. Automatic starting system

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Publication number Priority date Publication date Assignee Title
JPS644067B2 (en) * 1980-09-19 1989-01-24 Hitachi Ltd
FR2610995B1 (en) * 1987-02-13 1989-11-10 Campos Jean Louis FUEL DEVICE WITH VARIABLE ELASTIC VENTURI AND ELECTRONIC MANAGEMENT FOR EXPLOSION ENGINES

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US2905165A (en) * 1957-05-21 1959-09-22 Thompson Ramo Wooldridge Inc Fuel enrichment device
US2940436A (en) * 1956-03-26 1960-06-14 Holley Carburetor Co Fuel control for an internal combustion engine
US3587553A (en) * 1969-07-24 1971-06-28 Bendix Corp Carburetor priming system

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US2940436A (en) * 1956-03-26 1960-06-14 Holley Carburetor Co Fuel control for an internal combustion engine
US2905165A (en) * 1957-05-21 1959-09-22 Thompson Ramo Wooldridge Inc Fuel enrichment device
US3587553A (en) * 1969-07-24 1971-06-28 Bendix Corp Carburetor priming system

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4205641A (en) * 1978-01-13 1980-06-03 Yamaha Hatsudoki Kabushiki Kaisha Start control means for internal combustion engine
WO1980000470A1 (en) * 1978-08-19 1980-03-20 Ford Motor Co Down-draft carburetor
US4404151A (en) * 1978-08-19 1983-09-13 Ford Motor Company Down-draft carburetor
US4276238A (en) * 1978-10-19 1981-06-30 Nissan Motor Company, Limited Carburetor with automatic choking and acceleration device
US9464588B2 (en) 2013-08-15 2016-10-11 Kohler Co. Systems and methods for electronically controlling fuel-to-air ratio for an internal combustion engine
US10240543B2 (en) 2013-08-15 2019-03-26 Kohler Co. Integrated ignition and electronic auto-choke module for an internal combustion engine
US10794313B2 (en) 2013-08-15 2020-10-06 Kohler Co. Integrated ignition and electronic auto-choke module for an internal combustion engine
US10054081B2 (en) 2014-10-17 2018-08-21 Kohler Co. Automatic starting system

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JPS5097738A (en) 1975-08-04
GB1475008A (en) 1977-06-01
AU7645774A (en) 1976-06-17
CA1036441A (en) 1978-08-15
DE2461277A1 (en) 1975-07-10
JPS5834664B2 (en) 1983-07-28

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