CA1036441A - Carburetor cranking fuel flow rate control - Google Patents

Carburetor cranking fuel flow rate control

Info

Publication number
CA1036441A
CA1036441A CA216,274A CA216274A CA1036441A CA 1036441 A CA1036441 A CA 1036441A CA 216274 A CA216274 A CA 216274A CA 1036441 A CA1036441 A CA 1036441A
Authority
CA
Canada
Prior art keywords
fuel
passage
flow
cranking
valve
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA216,274A
Other languages
French (fr)
Other versions
CA216274S (en
Inventor
Robert S. Harrison
Alvin P. Nowroski
John D. Medrick
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Ford Motor Company of Canada Ltd
Original Assignee
Ford Motor Company of Canada Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Ford Motor Company of Canada Ltd filed Critical Ford Motor Company of Canada Ltd
Application granted granted Critical
Publication of CA1036441A publication Critical patent/CA1036441A/en
Expired legal-status Critical Current

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Classifications

    • 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

Landscapes

  • 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)
  • Means For Warming Up And Starting Carburetors (AREA)

Abstract

ABSTRACT OF THE DISCLOSURE
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 dosing 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

1036~41 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 ~Y~

103644~
throctle valve is closed, such as during engine idling speeds and starting. For starting in cold weather below say 25F, 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 wi~hdrawn from fuel jets to simultan-eously 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.
In accordance with the present invention, there is provided an engine cranking fuel supply system comprising, a carburetor having an induction passage ; ~0 connected to Presh 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 tempera~ure from a predetermined level, the dual fuel supply means including ~irst 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 pre-¦ determined level, a flow-noflow valve in the second passage variably movable to a flow position in response to an engine .

~036~1 cranking operation to permit Llow through the second passage and variably movable to a non-flow position in response to the engine attaining a running condition whereby fuel flow for eold engine operation is supplied in varying amounts to the ~- 3 ' .
, ,,. ~;

3~;~4~
fuel port from both passages below the predetermined tempera-ture level during engine cranking, and from only the first passage after the engine has attained a running condition.
In this way, a fuel cranking system is provided that is operative below a predetermined temperature to supply quantities of fuel to the carburetor that are in addition to fuel inducted in the normal manner.
The invention is described further, by way of illustration, wi~h reference to the accompanying drawings, in which:
- Figure 1 is a plan view of a portion of a variable area venturi type carburetor embodying the invention;
Figure 2 is a side elavational view taken on a plane indicated by and viewed in the direction of the arrows
2-2 of Figure l;
Figure 3 is a cross sectional view taken on a plane indicated by and viewed in the direction of the arrows .3~3 of F~gure l;
Figures 4 and 5 are enlarged cross sectional views taken on planes indicated by and viewed in the direction of the arrows 4-4 and 5-5 of Figure l;
Figure 6 is a cross sectional view taken on a plane indicated by and viewed in the direction of the arrows 6-6 of Figure l;
Figure 7 is a bottom view taken on a plane indicated by and viewed in the direction of the arrows 7-7 of Figure 6, and looking up at the underside portion of the air horn portion of the carburetor and appears on the same sheet of drawings as Figures 9 and 10.
30 . Figure 8 is a cross sectional ~iew taken on a plane indicated by and viewed in the direction of the arrows r~ 3 A

36~41 8-8 of Figure 6 and looking down on the main or central body portion of the carburetor; and, Figures 9 and 10 are cross sectional views taken on planes indicated and viewed in the direction of the arrows 9-9 and 10-10 of Figure 8.
Figure 1, which is essentially to scale, i5 a plan view of a variable area venturi carburetor of the down-draft 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 (Figure 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 induction passages.

.

'` - 3b -~ !

~ 3~i441 1 As seen more clearly ln Figure 3, movahle walls 12 2 are plvotally mounted at 15 on a statlonary pln. The pin
3 actually i~ rlxed to a ~trut, not shown, that depends ~rom
4 a sectlon o~ the upper body of the carburetor. Pivotally attached to each Or the wall bodles i3 a fuel metering rod 6 16 that cooperates wlth a maln fuel meterlng Jet 18. The 7 needles have a controlled taper to provlde a rlcher alr/fuel 8 mixture at the lower and hi~her ends of the venturl opening 9 range~ Each ~et is located ln an aperture inside wall 14 at approximately the throat or mo~t constrlcted ~ectlon of 11 venturi 13. A fuel float bowl or reservolr 20 has a palr 12 of identlcal passages 22 conducting ~uel to the main metering 13 Jets 18. Downstream of the venturis, the carburetor throttle 14 body portlon 23 rotatably mounts a sha~t 24 on which are rixed a pair (only one shown) Or conventional throttle plates 16 25 that aontrol the rlow Or alr and fuel through induction passages 10.
18 The size Or venturis 13 and the movement of walls 19 12 ls controlled in thls case by a spring returned, control vacuum actuated, diaphra~m type servo 26. The servo consl~ts 21 or a hollow two-piece casting dlvlded into two chambers 28 22 and 30 by an annular flexlble diaphragm 32. The dlaphragm is 23 sealingly mounted along it~ edge in the casting. Chamber 28 24 18 an alr chamber, connected to amblent or atmospherlc pressure through a passage 34 (lndlcated also ln Flgures 1, 6 and 26 8). Chamber 30 ls a vacuum chamber connected to inductlon 27 pa8sage8 10 at a point below the throat but stlll ln the 28 venturl 13. This subJects chamber 30 to changes in a control 29 vacuum that varies wlth alrflow but at a rate that is sllghtly dlfferent than true venturi vacuum. The exact 31 location o~ the tap of cour3e is a matter of choice. Chamber 32 3 also ls connected to be actuated by ported intake manifold ~ 3644~L

1 vacuum, for cold weather operation, as wlll be described in 2 more detail later.
3 Completlng the construction, servo 26 has fixed 4 to one side of diaphragm 32, by a retainer 35, a plunger or actuator 36. The plunger is plvotally connected to a ~haft 37 interconnecting cast portions o~ the movable walls 12.
7 Flxed to the other side of diaphragm 32 is a retalner 38 8 against whlch is seated a sprlng 39. The other end of the 9 sprlng bears agalnst a seat 40 axially ad~ustable to vary the sprlng preload.
11 Figure 3 indlcates schematically ln dotted llnes a 12 passage "p" between chamber 30 and lnductlon passages 10.
13 In actuality, as best seen ln Figures 5, 8, 9 and 10, servo 1l~ chamber 30 is connected by a restricted line 41 (Flgure 8) to an lntersectln~ passage 42 (Flgures 8-10). Passage 42 16 lntersects wlth a vertlcally downwardly extendln~ pa~age 44 17 (Flgure 10) containlng a flow restrlctor or orlflce 46 and 18 termlnatln~ ln a chamber 48. Chamber 48 ls connected by a 19 port 50 to lnductlon passage 10 at a polnt below the edge of throttle valve 25 when it ls in lt~ closed positlon shown.
21 In the posltlon shown, therefore, as the throttle valve 18 22 rotated to an open posltion, port 50 ls progresslvely sub~ected 23 to the lncreased pressure above the throttle valve to bleed 24 the vacuum in passage 42.
Passage 42 also intersects with a ri~ht angled 26 passage 52 (Figures 8, 9 and 5) that connects to a passa~e 27 54 (Flgure 5). The latter passe~ vertlcally through the main 28 body portlon of the carburetor lnto a horlzontal passage 56 29 ~ locat~d ln the carburetor alr horn sectlon. Pas~age 56 in turn is connected by a palr of passages 58 and 60 to the well 31 62 (Flgure ~) ln which is arcuately movable one of the mountlng 32 members 70 (Fi~ure 3) for movable wall 12. While not shown, 4~
l the well 62 in Figure 8 and the adJacent lnduction passage 2 10 are lnterconnected by a depressed porklon of the main 3 body between the two so that the openlng 63 shown ln Flgure 5 4 sen~es the control or venturl-llke vacuum connected by the passa~es named to servo chamber 30.

6 Looklng now at Fl~ure 5, the openlilg 63 to the 7 control vacuum ln this case is adapted to be alternately 8 restricted or progressively opened by a needle type valve 72.
9 me valve is movable into and out of the seat 63 ln response to a temperature sensltlve element, in a manner that wlll ll be described more clearly later. Suffice it to say at thls 12 polnt~ that durlng normal englne operatlng temperatures, 13 the needle valve 72 is completely wlthdrawn from opening 63 14 thcreby permlttln~ venturl-like vacuum to be sensed through passa~es 60, 58, 56, 54, 52, 42 and 40 to chamber 30 Or the 16 servo, the ported manlfold vacuum ~lmultaneously beln~ sensed 17 through port 50, chamber 48, line 42 to llne 41 and ~ervo 18 chamber 30.
l9 It should be noted that the slze of the venturi-like vacuum pasBages 60~ 58, 56, 54 and 52 are conslderably 21 larger than that of the ported manifold vacuum passage 44, 22 coupled wlth the oriflce 46, so that when the needle valve 23 72 is in the up posltion, the manifold vacuum is bled to the 24 level of the venturl-like or control vacuum and, therefore, has e~sentlally no effect on the movement of ~ervo 26. The 26 manifold vacuum ls used during cold weather operatlons to 27 modulate the venturi-like or control vacuum to schedule the 28 opening o~ the venturi 13 to regulate the richness of the 29 fuel/air mixture. When the needle valve 72 is in the closed or nearly closed position, the venturl vacuum flow will be 31 es~entlally blocked and manifold vacllum will be the prlme force 32 acting on servo ~hamber 30. This will cause the movable ~03~
l venturi wall3 12 to be moved to a larger area venturl pulllng 2 the fuel meterlng rods 16 out further.
3 As thus ~ar described~ durlng norMal engine operating 4 temperatures, the operation ~s as follows. The rotatlve movement of throttle valves 25 controls total airflow through 6 both passages lO to lncrease as the throttle valves are moved 7 from thelr closed positlon. An increase ln alr~low provldes 8 e~sentially a proportional lncrease in the control vacuum in 9 chamber 30 from port 63 until the dlaphragm 32 1~ moved towards the cup 40. This moves both walls 12 to open inductlon 11 passages lO and increase the area of venturls 13 whlle 12 simultaneously retractlng the fuel meterlng rods 16 to increase 13 fuel flow. Thus, the total airflow and ~uel flow vary wlth 14 changes in throttle valve settlng up to a maxlmum.
Returnlng now to the general construction shown 16 ln Figure l, durlng cold englne operatlon, as stated prevlously, 17 it is de~lrable to provlde an addltional supply of fuel to 18 the lndu¢t~on passages to assure sufriclent fuel vapor both l9 ror startlng the engine as well as a dlfferent schedule Or addltlonal fuel for runnlng the cold englne prlor to its 21 reachlng normal operatlng temperature level. The~e requlrements 22 are sati~fled by providing a comblnatlon fuel enrlchment system, 23 a cranking fuel enrlchment system embodylng the lnventlon~
24 as well as a throttle plate posltloner devlce to crack open the throttle plates an addltlonal amount durlng cold starting 26 operations.
27 More speclflcally, Flgures 5J 6 and 8 show portions 28 Or both the cold running enrlchment system as well as the 29 cold start cranking fuel system. The body portlon of the carburetor 15 cast with a ~uel bowl 20 containlng fuel 31 dellvered thereto past a conventlonal inlet needle valve 80 32 from a supply llne 82. The needle valve 80 is moved vertlcally ~364~
1 ln a bore 84 by the tab 86 secured to a float member B8 2 plvotally mounted at 90 on a depending portlon of the air 3 horn ~ectlon o~ the carburetor.
4 ~ The lnlet valve 80 operates in a known manner.
Movement Or float 88 downwardly as a result of lowering of 6 the liquid ruel level causes the needle 80 to drop. This 7 permlts ~uel under pres~ure to enter the reservolr from 8 llne 82 to rlll it agaln to the deslred level. Raising of 9 the rloat rai~es the inlet valve agalnst the conlcal seat shown to 3hut orf the upply when the desired level ha~ been reached.
11 The lower portion of fuel bowl 20 contains a needle 12 like cranking fuel supply valve 100 (Flgure 5). The latter 13 has a conical ~alve portlon 102 that cooperates wlth the 14 upper edges 104 o~ a ~uel well 106. Valve 100 is connected to a temperature respon~ive device to be moved lnto and out 16 Or the wall wlth changes ln temperature, ln a manner to be 17 descrlbed, to control the rate of rlow Or ruel rrom reservolr 18 20 lnto ~uel well 106. Well 106 13 connected to an intersecting 19 passage 112 tFlgure 8) that connect~ wlth a cross passage 114 to rlow ruel into another pas~age 116 past a solenold controlled 21 valve unlt 118.
22 As best seen ln Flgure 69 unlt 118 conslsts 23 esRentlally o~ a valve 120 ~ormed on the end o~ the armature 24 of a solenold 122. A sprlng not shown normally blases valve 120 to close communlcatlon between pas3ages 114 and 116.
26 The solenold normaliy would be powered from the starter relay 27 Or the motor vehlcle lgnltlon system so that the solenold ls 28 - rendered operatlve only durlng en~ine startlng conditions.
.
29 That is, when the lgnltlon key ls turned to the st~rt positlon, the solenold 118 would be energized and cause valve 120 to 31 be retracted rlghtwardly to open communlcatlon between pa~sa~es 32 114 and 116. A rlow Or startlng ~uel would then be permltted .

~1~36~
1 rrom ~uel bowl 20 into passage 116.
2 As soon as the englne attained runnlng condltion, 3 return o~ the lgnltion switch to the on positlon would 4 de-energize solenold 122 and again block pa~sage 114 rrom con~unlcating wlth passage 116. The solenold unit could ~6 lnclude a manlrold vacuum swltch so the solenold ls not 7 energized above a vacuum level o~ say 2"Hg., for example.
8 It also could oontain a thermal swltch to prevent operation 9 above 120~F., ~or example, when extra cranklng fuel usually ls no* needed.
11 From passage 116 the ruel passes upwardly through 12 the carburetor main body passage 124 (Flgure 6) where it 13 flows into a plenum 126, shown also ln Flgure 7. From the 14 plenum, the ~uel ls divided equally to be lnducted out through passages 128 into each Or the induction passages 10 at a 16 location adJacent the venturi but spaced from the fuel ~ets 17 18. Thu~, lt wlll be seen that ~or startlng operations, 18 energlzatlon o~ the solenold by turnlng Or the vehlcle lgnltlon 19 swltch cause~ addltlonal ~uel to be added at times to the lnductlon passages, ror startlng purposes.
2~ The quantlty Or cranklng fuel to be added to the 22 inductlon passages, or, on the other hand, the positlon of 23 crankln~ valve 100, 19 controlled by the connectlon o~ valve 24 100 to the lower end o~ a needle valve 140 (Flgure 5). The needlo Yalve rorms a portlon Or the engine running fuel 26 enrlc}lment system. More speclflcally, needle valve 140 is 27 tapered a~ lts lower end as shown at 142, ror a purpose to 28 be descrlbed, and ha~ a unlversal connectlon 144 to the 29 plastlc con~cal valve 100. The latter defines a varlable ~low srea 145 between the Yalve and wall Or well 106 that varies 31 ~n slze as a ~unction of the vertlcal movement o~ valve 100.
32 Thererore~ vertical movement Or valve 100 modulates the rate .

~q~369~

1 O~ ~low Or ruel rrom reservoir 20 lnto well 106 when solenold 2 valve 120 i~ opened. The needle valve 140 moves upwardly and 3 downwardly wlth changes in temperature, as will now be descrlbed.
4 The needle valve 140, ln thi3 case, ls vertlcally movable ln a well 146 in the upper body portlon. It ls axially 6 aligned by a seal 148 and a valve seat 150 with whlch it cooperates to meter fuei. The seal and seat deflne a chamber a 152 ~hlch is c~nnected by an angled passage 154 to the end 156 9 of a worm-like passage 158 best seen in Flgure 7. The opposite end 1~0 of pas~age 158 connect3 wlth a vertlcal passage 162 11 (Flgure 6) that lnter~ects an angled passage 164 leadln~ to 12 the plenum 126. As stated previously, plenum 126 also receives 13 ~uel from ths cranking fuel passage 124. Together then, 14 the ~uel passes into each lnductlon passage 10 through the slde passage3 128. It wlll be seen then that, dependlng upon 16 the vertlcal position o~ needle valve 140, a quantity of fuel ~7 will rlow past the tapered portlon 142 of the needle valve 18 lnto tlle varlous passages lnto lnduction passages 10 to supply 19 addltional ruel durlng cold runnlng operation of the engine.
The vertlaal movement of needle valve 140 1~ controlled 21 by a temperature sensltlve element that moves the needle 22 valve 14Q upwardly to increase ruel rlow a3 the temperature 23 decreases below the normal operating level, and moves the 24 needle valve 140 to a downward position to shut orf the fuel enrlchment when the temperature reaches the normal operatlng 26 level. Concurrently9 the downward movement Or needle valve 27 140 as the temperature lncreases will move the cranklng fuel 28 valve 100 downwardly in proportlon to the temperature lncrea~e.
29 There~ore, when the normal operating level is reached? cranklng Yalve 100 wlll provide a maximum restrictlon to flow through the 31 area 145, and Yery llttle addltional ruel will then be added 32 during startin~ of the englne.
33 The upper end o~ needle valve l4n 19 plvotally 34 connected to the end Or a lever 16~. The lever ls pivotally . .

~1113~
1 mounted on a pln 168 proJecting through an aperture ln a boss 2 170 proJecting from the carburetor upper body. The opposlte 3 end of lever 166 ls pivotally connected to an ad~ustable nut 172 4 on the upper end o~ a dependlng llnk 174. The lln~ 174 is adapted to be connected to a thermo~tatically responsive movable 6 elemen~ to be dç~crlbed. Ad~ustlng the upper en~l 172 of course 7 wlll vary the operating characteristics o~ the system. Downward 8 movement of lin~ 174 is limlted by abutment Or the nut 172 9 agalnst a stop washer 176. Pro~ecting horlzontally or laterally from link 174 18 a connector 178 plvotally engaging the threaded 11 upper end 180 of needle valve 72. The upper end 180 contains a 12 yoke member 182 adJustably threaded to the end of needle valve 13 72 as ~hown to determine the upward and downward llmits o~
14 movement Or the needle valve.
Ac thus far descrlbed, therefore, wlth respect to the 16 runnln~ ~ue~ enrlchm2n~ ~ystem, wi'h the 'hrc~tle plate~ ln the 17 ldle speed positlons, when link 174 1~ ln the po~ltion shown 18 indiaatlng that the temperature is at the lowest below normal 19 englne operating level, the needle val~e 140 will ha~e been ~0 moved to lt~ upwardmo~t posltlon to provide maxlmum rate of 21 ~uel ~low. Needle valve 72 also wlll have moved to its downward-22 mo3t positlon re~tricting the port or outlet 63 to the lnductlon 23 passage ~hown in Figure 8. Thu8, ported mr~rilfold vacuum in 24 port 50 (Fl~ure 10) wlll act ln servo chamber 30 to move walls 12 to enlarge the venturl areas, w~lch decreases the ~uel 26 meterlng slgnal actlng on both outlet passages 128 and Jet 18.
27 ~h18 leana the mixture a~ compared to the cranking mlxture and 28 what lt would be under accelerative condltlon3.
29 Slmultaneously, maxlmum addltlonal ruel quantlty wlll rlow ~rom the fuel enrichment well 152 lnto the lnductlon 31 passage~ 10 through the lnterconnectlng~outlet passages 128.
32 As soon as the temperature lncreases rrom its lowest settlng, 33 the llnk 174 wlll move vertlcally upwardly from the posltlon 34 ~hown. Thl~ will ~radually and progressl~ely ralse the venturi-") `
` ` ~036~

1 llke vacuum control needle ~alve 72 and lower progre~slvely the 2 needle valve 140. Thus, the venturi-like control vacuum 3 be~ln~ to bleed lnto passage 60. The vacuum force acting Oll 4 serYo chamber 30 will progresslvely decrease to permit servo sprlng 3g to ~lowly close the venturl towards the normal engine 6 ldle ~peed posltion. The addltlonal ~uel nrlc~ant will 7 decrease as the tapered port~on 142 o~ needle valve 140 closes 8 the openin~ to the ruel bowl.
9 Turnlng now to the teMperature re~ponsive control of the movement Or llnk 174 and the throttle valve positioner, 11 F~gures 1, 2 and 4 show the same more clearly. As best seen 12 ln Figure 4, the lower end of link 174 is plvotally connected 13 to one end o~ a lever 216 that ls fixed on a shaft 218. T~,e 14 ot~er end Or lever 216 ad~u~tably supports a screw 220 that bears agalnst the end 222 of an essentially conventlonal fast 16 ldle cam 224. The cam 18 rotatably mounted on sha~t 218 and 17 ha3 a wei~hted lower end 223. The end has a peripheral edge 18 portion ~ormed with a serie~ Or clrcumferentially contl~uous 19 steps 224, 226 and 228 and a hlg~ cam step 230. Each 3tep progre8~ively in the order named ls o~ greater radial extent 21 than the pre~ious. ~ -22 Cooperating with fast idle cam 224 to locate or 23 posltlon the throttl~ plàtes 25 ls a lever or throttle stop 24 232 ~ormed at lts outer end with a cur~ed engaging portion 234. Le~er 232 is rotatably mounted on throttle shaft 24. ~-~
26 It has a dependlng tang portion 236 engaged by the end of 27 an adJu~tably mounted screw 238 carrled by a lln~age 240 rlxed 28 to the throttle ~ha~t 24. A throttle return coll sprlng 29 242 has one end 244 ancnored under a pln 246 exten~lng ,. from a ~lxed portion of the car~uretor throttle flange.
31 The opposlte end of the sprlnæ ~ears agalnst an angled tane 32 250 of linka~e 240 thereby blasing the linka~e and screw ~38 , . . , , . .... . . ... . ~ . , .. ~

! !
6~

l ln a clockwise directlon against the tab end 236 Or lever 2 232. The le~er 232 thus i3 constantly biased in a clockwlse 3 directlon towards the edge surrace of fast idle cam 224.
4 The cam steps thererore c~nstitute abutment means or stops ln the path o~ movement Or lever 232 to determine the idle 6 speed positlon o~ throttle plate~ 25.
7 Insertable at tlmes between the end 234 of lever ~8 232 and the ed~e of fast idle cam 224 is the ~lnger portion 9 252 Or an arcuately movable link 254. The latter 15 plvotally connected at 256 to the end Or a lever 258 rotatably mounted ll on shart 218. Lever 258 ls connected at its upper end at 12 260 to an actuatlng llnk 262. The opposlte end o~ link 13 262 ls connected to one end of a bell crank lever 264 plvotally 14 mounted at 266 on the ears of an extension of a servo houslng 268.
16 The servo hou~in~ is hollow and divideu into tWG
17 chambers 270 and 272 by an edge mounted annular flexlble 18 diaphragm 274. Chamber 270 1B an alr chamber communicating l9 to the atmosphere through an openlng 276. Chamber 272 is a ~acuum chamber communlcating by a passage not shown with 21 ~he lnductlon passages at a loca~ion below the throttle valves 22 25. A plunger 278 ls rlveted at one end 280 to a hat shaped 23 spri~g retalner 282, and pro~ects through a stop 284 ~or 24 connection to the opposIte end 286 of bell crank le~er 264.
A oompresslon sprlng 288 normally blases the plunger 278 26 upwardly to move bell crank 264, llnk 262, lever 258 and 27 ~lnger portion 254 in a clockwise dlrection.
28 Appllcatlon o~ engine vacuum to the servo chamber 29 272 when the englne ls runnlng is suf~iclent to counteract the ~orce Or spring 288 and cause the plunger 278 to move 31 ~ertlcally downwardly. Thls moves lever 258 and flnger portlon 32 254 in a counterclockwise dlrectlon to withdraw or retract 33 the finger portlon rrom between the lever end 234 and the fast l ldle cam steps. ~ ~ 4 2 Thus, lt will be seen that when the ~n~ine 15 o~f 3 preparato~ to starting operatlon, depresslon o~ the vehlcle 4 accelerator pedal wlll rotate throttle shaft 24 and lever 232 ln a GounterclockwIse dlrectlon away from the end 252 6 of fin~er portlon 254. Slnce there ls no manl~old va¢uum in 7 chamber 272 of servo 269, ~pring 288 wlll posltion the ~inger 8 portion 254 to the positlon shown 80 that upon relea~e Or 9 the accelarator pedal, coil spring 242 will cause a clockwise return movement of the throttle valve lever 232 untll lt 11 engage~ the arcuate portion 290 Or the end 252 of the rlnger 12 portlon 254, whl~h ln turn abuts the edge of the fast idle 13 cam 2240 14 Once the englne has attalned runnlng operatlon beyond cranking vacuum level, then openlng o~ the throttle 16 valves 25 by depresslon of the a¢celerator pedal, pivot3 lever 17 232 downwardly and permits retraction or movement of finger 18 portion 254 to an ~noperatlve positlon to the right by the l9 vacuum ln servo 268. Lever 232 then 18 permltted to engage the edge of the fast ldle cam directly and the positlon of the 21 throttle plates will be determlned strlctly by the rotatlve 22 posltion of the rast ldle cam 224.
23 The fast ldle cam i3 controlled ln its rotation 24 by a lever 292 flxed on shaft 218. The lever ls located '~
wlthln a hollow cup-shaped houslng 294 that ls cast integ,rally, 26 wlth the throttle body portlon 23. Lever 292 has an uptu~ne.d 27 slotted end 296 in whlch i8 located the outer end 297 of,.a 28 thermostatlcally re~ponslve blmetalllc sprln~ coll 298. The 29 lnner end Or the spring i~ flxed on a stub shaft 300 proJec~ing from an insulated cover 302. The cover is fastened by 31 screw~ to the houslng 294 with an lnsulating gasket 302 32 between. The gasket has an arcuate slot 304 along whloh th~

-1~36~4~
l end 296 moves wlth temperature changes. The gasket also has 2 a hole 306 through which pro~ectR the end 308 of a tube 3 connected by a pair of passages 309 and 310 to the lnductlon 4 passages lO at a locatlon ~not shown) below the throttle valves. For clarity, the cover 302 has been removed ln 6 Figurs 2, and Figure 4 show~ the outllne of the houslng ln 7 phantom, for orlentatlon purpose~. Completlng the constructlon, 8 ~he housing has a hot air lnlet tube 312 connected by a passage 9 314 to the lnterior of houslng 294 on the far ~ide of ga3ket 302. ~he tube would emanate from a known type Or exhaust ll mani~old heated stove ln whlch alr flowlng past the manlfold 2 18 warmed.
13 In operatlon, once the en~ine 18 operatlng, wlth 14 gasket 302 in place and cover 304 applied9 manlrold vacuum actlng ln pa~sages 309 and 310 oauses hot alr to Plow into 16 tube 312 to the far slde of gasket 302. The air is then drawn 17 throuKh the slot 306 and out through passages 309 and 310, 18 warmlng the coll 298 as it passes lt. Thus, the coll wlll l9 bo progre~slvely warmed as the englne temperature rlses, resultlng in a clrcumferentlal movement of the end 297 of 21 the ooll to rotate lever 292 in the same directlon. This 22 rota~es lever 216 away ~rom the ~aat idle cam and permlts the 23 ~ast ldle cam to rotate counterclockwlse by gravlty. Slmilarly, 24 upon englne shutdown, coollng of the coll wlll cause lt to rotate levers 292 and 216 in the opposlte dlrection. This 26 of course 31multaneously rotates the fast ldle cam 224 by 27 the screw 220~ so that, dependlng upon the temperature level, 28 one of the steps 225, 226, 228 or the hlgh cam atep 230 will 29 be presented opposite the end 234 of throttle lever 232.
Thus, the throttle plate ldle speed setting wlll be determined 31 by which step is engaged by lever 232, during runnlng operations 32 of the englne. Durlng cold start operations, as described ~364~
1 prev~ously, the rlnger portion 254 will be inserted between 2 the end 234 of lever 232 and whatever step or rota~ive cam 3 posi~lon the fast idle cam 224 has attained ~o that the 4 throttle plates are opened more for ~tartlng purposes th~n durin~ normal cold runnlng conditions.
6 It will be ~een, therefore, that regardless of 7 what po~ltlon the ~ast ldle cam 224 assumes because of the 8 prevaillng ambient temperature, the throttle plates wlll be 9 oponed an additlonal amount ror startlng purposes. The a~ditlonal amount will vary to agree wlth the amblent temper-11 ature le~el so that a ¢orrect startlng air/ruel mlxture 1~
12 obtalned. This is in contrast to the conventlonal constructlons 13 in which thare is only one rast ldle start posltlon, accomplished 14 only by po~itlonlng the slngle high step 230 agalnst the throttle lever end 234~ At the lnbetween temperature levels, 16 thls i8 too high and results ln too fast an idle speed, and 17 one that may provide undesirable emlsslons.
18 The overall operatlon of the carburetor ls belleved 19 to be clear ~rom the above descrlptlon and by reference to th~ drawlngs. Thererore, lt wlll be repeated now only briefly.
21 Aasume that the engine is Orr and the ambient temperature 22 18 ~ssentlally 0F. ~he colled bimetalllc sprin~ 2g8 will have 23 contraoted a maxlmum amount rotatlng lever 292 clockwlse ~rom 24 th~ posltlon shown in Figure 2 to posltlon the end 297 of 25 ` the le~er at the left end 316 of the slot 306. Thls wlll 26 rotate lever 216 to mo~e the rast ldle ¢am 224 clockwise to 27 locate the hlgh cam ~tep 230 opposlte the end 234 of throttle 28 lever 232. Simultaneously~ by openlng the throttle platesJ
29 lever 232 wlll move away from the fast ldle cam and permlt the s~rvo sprlng 288 to move the finger portion 254 between 31 the rast idle cam step 230 and lever 232. The throttle plates 32 now will be opened a maximum amount for the coldest start ~364~
1 posltions, The induction passage~ 10 at thls tlme are at 2 th~ir smallest cross section because the servo sprlng 39 ha~
3 moved wall~ 12 to thls po4itlon. This, therefore, exposes the 4 pa~sages to a larger cranklng vacuum slgnal 80 that the alrflow a~ro~s the ~uel metering Jets 18 ls lncreas~d.
6 Slmultaneously, the rotation of lever 216 moves link 7 174 downw~rdly to its extreme posltion untll the stop 172 8 shown ln Flgure 5 abut~ the washer 176. This plvot needle 9 valv~ 140 to its uppermost positlon allowlng a maximum amount or fuel from ~uel bowl 20 through the space between the ~eat 11 150 and the tapered lower portlon of valve 140. Thls upward 12 posltion also moves the cranking valve 100 upwardly to open 13 wlde the pas~age 145 to flow fuel to passage 112. ~lerefore, 14 whon the ignltlon swltch 1~ turned to an on or start posltlon, tho solenoid 118 will wlthdraw the valve 120 to permlt a maximum 16 rate Or fuel to Plow from passage 114 to 116.
17 When the engine ls cranked ~or ~tartlng purposes, 18 th~ cranking vacuum slgnal 18 ~urrlclent actlng across the 19 inductlon passage outlets 128 (Flgure 7) ~o draw fuel up cranking fuel aircult passage 124 into plenum 126. Slmultan-21 eously~ fuel ls drawn past the engine runnlng ~uel circult 22 noedle ~alve 140 into the worm passage 158 (Figure 7) to 23 plenum chamber 126, where both clrcults combine and the fuel 24 lndusted to provide the necesAary startlng richness. On¢e the englne has been started, release Or t}~e lgnltlon switch 26 to tho englne runnln~ position de-energlze~ ~olenold 118 to 27 then agaln block the connection between the cranking supply 28 line 114 and the line 116. However, with the llnk 174 ln lts 29 downwardmost coldest positlon, the valve 72 will also be down os~ntially blocklng off port 63. Accordlngly, the higher 31 ported englne running manl~old vacuum will act ln servo chamber 32 3 and draw the wall~ 12 of the venturis to open or enlarge l the venturi area. ~3~44~
2 Wlth the throttle plates unmoved from the ~ast ldle 3 speed position, the openlng of the venturls wlll decrease 4 the alr velocity across the fuel ~et 18 to decrease the fuel metering slgnal while at the same time enlarglng the fuel 6 Jet orlfices. Simultaneously, the area of dlscharges 128 7 being constant, lowerlng the air velocity decreases the fuel 8 meterlng signal to decrease fuel output tllrough these passages.
9 This leans the overall mixture ~or the closed throttle position attained at that temperature level. At closed throttlel 11 the manifold vacuum is considerably higher than the cranking 12 vacuum. ~hls causes excess vaporlzatlon and would normally 13 lead to a richer than deslred mixture. However, the ported l~ manl~old vacuum control ln this case compensates ~or this by leaning the overall mixture to the desired level by openlng 16 the venturis.
17 Similarly, once the throttle plates are moved to 18 an o~f-ldle accelerative posltion, the mani~old vacuum level 19 i8 reduced so that there now iB less vaporizatlon. A slightly richer mixture, therefore, is desired to provide acceptable 21 englne operation. This ls accomplished by the throttle plates 22 traverslng the port 50 as they move off-idle, whlch progressively 23 sub~ects the chamber 48 to more and more control vacuum 24 exlsting above the throttle plates. The manifold vacuum signal acting on servo 30 therefore decays, and the venturl move~
26 towards a more closed posltlon to provide the richer setting 27 deslred. It is only a very short time, therefore~ berore 28 the throttle plates have completely traversed the port 50, 29 leaving control of movement o~ the venturl then strictly to the changes in venturl-llke control vacuum. Thus, a rlcher 31 than normal ldle but less than cranking mixture is provided 32 at this time by the main ~uel metering system as well as the ~L0369L4~
1 needle valve supplemental ~eed system.
2 Concurrent with the englne attalnlng a runnlng 3 conditlon, the manl~old vacuum established in servo chamber 4 272 wlll be suf~iclent, once throttle lever 232 i5 pivoted counterclockwise to relea~e ~lnger portio~ 254, to pivot the flnger portlon out from between the end 234 of lever 232 and 7 the ~ast ldle cam step lt abut3. l~ow the portlon 234 will 8 move to ~irect~y abut the step o~ the ld e cam 224 and thereby 9 clo~e down the throttle plates to less open ~ast idle speed po~l~ions~ Tbis reduces both the fuel flow and alr~low for 11 cold runn~ng operations~ whloh as stated above is deslred 12 because a less rich alr~uel mixture is requlred once the 13 engine has attalned its i~le speed horsepower.
14 As the temperature increaseR, the bimetallic oolled 1 15 sprlng 298 will rotate the lever 216 in a counterclockwise ;6 dire¢tion awa~ 4rom the 4a~t ldle cam. The cam then can 17 move in the s8me direction by gravity when the throttle 18 plates are opened beyond the rast idle position so that the 19 end o~ lever 234 graduall~ moves progresslvely clockwlse to permit the progresslve closur~ o~ t~le throttle plates to less 21 open ldle speed posltiorls. Simultaneously, the counterclock-22 wlse rotation o~ lever 216 efrects an upward movement of llnk 23 174 to progres3ively move the needle valve 140 downwardly and 24 thareby progre~sively clo~e Orr the addltional ruel flow past the Yalve. Thls movement also causes an upward movement o~
26 needle valve 72 so that the venturi-llk~ vacuum decays 27 whatever ported manlrold vacuum slgnal is acting ln servo 28 c}lamb~r 30.
29 Thus, ror closed throttle pla~e~po~itlons, the lowering ~acuum sl~nal in pre~ure chamber 30 will permlt 31 the venturl walls 12 to move to contract the venturl area 32 and move the meterlne rods 16 lnto the Jet 18. Eventually, ~ ~ .

~036441 1 therefore~ the throttle plates will be returned to a normal 2 closed idle ~peed posltion, the needle valve 72 wlll be drawn 3 essentially completely out of port 63 so that movement of 4 the venturi walls wlll be controlled solely by control or venturi-like vacu~n charlges, and the supplemental fuel needle 6 valve 140 will be moved downwardly to shut o~ or es~entially 7 close off the supply o~ additlonal fuel to the system. At 8 thls time, the cranklng valve 100 wlll ~e at a mlnlmum rate 9 of flow posltion. The closlng venturi increases the alr velocity past the fuel ~et 18. The fuel ~et, therefore, wlll 11 ha~e a smaller flow area, The total fuel ~low will be less 12 because the throttle plates are now closed more completely 13 and because no fuel is now belng lnducted ~rom ~assages 128, 14 but only that through the main Jets 18, While the lnvention has been shown and descrlbed 16 ln its pre~erred embodlment, lt wlll be clear to those skllled 17 in the arts to which lt pertaln~ that many changes and modlflca-18 tlons may be made thereto without depar~lng from the scope of 19 t}~e invention,

Claims (5)

The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:
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 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 variably movable to a flow position in response to an engine cranking operation to permit flow through the second passage and variably 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 has attained a running condition.
2. 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 predeter-mined 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 and second passage each containing a temperature responsive flow control means variably movable to decrease the cranking fuel flow as the temperature increases towards a predetermined level, the temperature responsive means in the first passage being in the form of a valve variably movable between flow and no flow positions, the second passage containing an on-off valve movable to block flow and unblock flow through the second passage, means biasing the valves towards no-flow positions blocking flow through 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 on-off valve for modulating the rate of flow of fuel through both the passages as a function of changes in temperature to permit fuel flow for cold engine operation to be supplied in varying amounts to the fuel port from both passages below the predetermined temperature level and to move the on-off valve to a no-flow position in response to the engine attaining a running condition so that fuel flow occurs through the first passage only after the engine has attained a running condition.
3. The cranking fuel system of claim 2, including a fuel reservoir supplying fuel to the fuel passages and wherein the second passage flow control means comprises a tapered valve movable into and out of the second passage to control the volume of fuel admitted to the second fuel passage, and the temperature responsive means includes a temperature responsive device operatively connected to the tapered valve for moving it in one direction.
4. The cranking fuel system of claim 3 wherein the means biasing the valves includes spring means biasing the tapered valve to an open position permitting the free supply of fuel from the reservoir to the second fuel passage.
5. The cranking fuel system of claim 3, 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.
CA216,274A 1974-01-04 1974-12-16 Carburetor cranking fuel flow rate control Expired CA1036441A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US430819A US3897765A (en) 1974-01-04 1974-01-04 Carburetor cranking fuel flow rate control

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Publication Number Publication Date
CA1036441A true CA1036441A (en) 1978-08-15

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US (1) US3897765A (en)
JP (1) JPS5834664B2 (en)
CA (1) CA1036441A (en)
DE (1) DE2461277A1 (en)
GB (1) GB1475008A (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5496631A (en) * 1978-01-13 1979-07-31 Yamaha Motor Co Ltd Controlling system for starter carburetter
EP0008499B1 (en) * 1978-08-19 1983-01-12 Ford Motor Company Limited Down-draft carburettor
GB2033481B (en) * 1978-10-19 1983-02-09 Nissan Motor Carburettor with automatic choking and acceleration device
JPS5756648A (en) * 1980-09-19 1982-04-05 Hitachi Ltd Carburettor with switch valve for preventing fuel vapor generation
FR2610995B1 (en) * 1987-02-13 1989-11-10 Campos Jean Louis FUEL DEVICE WITH VARIABLE ELASTIC VENTURI AND ELECTRONIC MANAGEMENT FOR EXPLOSION ENGINES
EP3033512A2 (en) 2013-08-15 2016-06-22 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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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

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AU7645774A (en) 1976-06-17
JPS5834664B2 (en) 1983-07-28
US3897765A (en) 1975-08-05
GB1475008A (en) 1977-06-01
JPS5097738A (en) 1975-08-04
DE2461277A1 (en) 1975-07-10

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