US2764961A - Intake manifold structure - Google Patents
Intake manifold structure Download PDFInfo
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- US2764961A US2764961A US445225A US44522554A US2764961A US 2764961 A US2764961 A US 2764961A US 445225 A US445225 A US 445225A US 44522554 A US44522554 A US 44522554A US 2764961 A US2764961 A US 2764961A
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- riser
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- manifold
- conduit
- cylinders
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- 239000000446 fuel Substances 0.000 description 52
- 239000000543 intermediate Substances 0.000 description 40
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 39
- 238000010438 heat treatment Methods 0.000 description 12
- 238000009826 distribution Methods 0.000 description 6
- 238000010304 firing Methods 0.000 description 6
- 230000009977 dual effect Effects 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 230000010349 pulsation Effects 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000002411 adverse Effects 0.000 description 2
- 239000002826 coolant Substances 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 241001052209 Cylinder Species 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000005057 refrigeration Methods 0.000 description 1
- 210000000707 wrist Anatomy 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B27/00—Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues
- F02B27/005—Oscillating pipes with charging achieved by arrangement, dimensions or shapes of intakes pipes or chambers; Ram air pipes
- F02B27/006—Oscillating pipes with charging achieved by arrangement, dimensions or shapes of intakes pipes or chambers; Ram air pipes of intake runners
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B27/00—Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
- F02B75/18—Multi-cylinder engines
- F02B75/22—Multi-cylinder engines with cylinders in V, fan, or star arrangement
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
- F02B75/18—Multi-cylinder engines
- F02B2075/1804—Number of cylinders
- F02B2075/1832—Number of cylinders eight
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
- F02B2275/34—Lateral camshaft position
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- This invention relates to intake manifold structures for engines of the type having a pair of cylinder banks arranged at an angle to each other and especially for V engines.
- My invention has particular application to improved intake manifolding for V8 engines wherein two inner cylinders of one bank of the engine and two outer or end cylinders of the other bank of the engine are fed from a common supply of air fuel mixture.
- the principal object of my invention is therefore to provide engines of the foregoing type with an intake manifold system providing good mid-speed torque output.
- Still another object is to provide engines of the foregoing type with an intake manifold system providing optimum torque in the speed range of 2000-3200 R. P. M.
- a further object is to provide an engine of the fore- 2,764,961 Patented Oct. 2, 1956 2 going type with an intake manifold system utilizing a pair of spaced single barrel carburetors and whose firing order provides the widest possible separation between suction impulses on the two carburetors.
- a further object is to provide such engines with an intake manifold system using a pair of single barrel carburetors arranged with the widest possible spacing and utilizing large air cleaners.
- the metering control means may be constituted of a single or plurality of conduits whose total area is somewhat critical in that if too large, the value of a firing order producing a wide separation in suction impulses may be somewhat lost with consequent loss of torque. No fixed formula for this area appears possible and hence it is recommended that several sizes be tried to find that which provides the best mixture control and best torque. In general an area of less than /2 sq. in. is preferred. An area of 0.3 sq. in. appears satisfactory for a 331 cu. in. V-8 engine using standard single barrel carburetors, for instance Ball & Ball BBS975S carburetors.
- a further object is to provide a manifold system as aforesaid wherein pulsation damping or mixture metering control means are provided between the intake riser passages of the manifold.
- heating of the intake riser passages for normal operation may advantageously be provided by water heating.
- water heating In the present manifold it is simpler to provide than exhaust gas heating and is practical in the case of truck engines or industrial use because in these operations the operator can take more time for warm up.
- water taps are readily available in the cylinderheads.
- Water heating the refrigeration effect of the air fuel mixture on the water is obtained and this thereby reduces the heat rejection of the coolant water necessary at the radiator.
- Still another object of my invention is to provide an intake manifold system as aforesaid in which the intake riser passages are water heated for normal operation and for reducing the heat rejection of the coolant system at the radiator.
- Figure l is an end elevational view partly in section of an 8-cylinder V-type overhead valve engine embodying the intake manifold system of my invention, the section through the manifold being taken approximately at ZZ of Figure 2;
- Figures 1A and 1B are schematic views of the two preferred two plane crank pin arrangements for an 8-cylinder V engine utilizing my invention, the Roman numerals in the figures indicating the positioning of the crank throws counting from the front or fan end of the engine and the numerals in the brackets indicating cylin der numbers whose pistons are connected with the engine throw;
- Figure 2 is a plan view of the manifold of my invention and schematically showing the banks of cylinders in relation thereto;
- Figure 2A is a schematic showing of the air-fuel passages of the manifold of Figure 2;
- Figure 3 is a side elevational view of the manifold of Figure 2 showing the carburetors and air cleaners in position thereon;
- Figure 4 is a sectional development taken in elevation at A'A of Figure 2 through a pair of conduits connecting with one manifold riser passage and showing a portion of the throttle passage of a carburetor feeding the same;
- Figure 5 is a sectional development taken in elevation at BB of Figure 2 through a second pair of conduits connecting with the same riser;
- Figure 6. is, a sectional development taken in elevation at C'C of Figure 2 through a pair of conduits connecting with the other manifold riser;
- Figure 7 is a sectional development taken in elevation at D'-'D of Figure 2 through a second pair of conduits connecting with the same riser passage as the conduits of Figure 6 and showing the throttle passage portion of the carburetor feeding the same;
- Figure 8 is a sectional elevation taken at E-E of Figure 2 through the riser passages and longitudinal water heating conduit;
- Figure 9 is a sectional elevation taken at FF of Figure 2 through one transverse water heating passage
- I Figure 10 is a sectional elevation taken at GG of Figure 2 through a second transverse water heating passage
- Figure 11 is a plan view of a portion of the manifold of Figure 2 showing a modification providing metering means between the carburetor riser passages;
- Figure 12 is a sectional elevationof portions of the riser passages of the manifold of Figure 11 taken at thereof showing the manner of providing metering means therebetween.
- the engine has two banks 9 and 9a of cylinders 10, four in each bank, arranged at 90 in a cylinder block 11, to which cylinder heads 12 and 1221 are secured and provided with hemispherical typecombustion chambers 13 immediately above each cylinder 10.
- the cylinders of each bank are aligned longitudinally of the axis of the engine and the cylinders of the opposite banks are offset longitudinally relative to each other.
- the cylinders of the lefthand cylinder bank which is to the left looking forward from the flywheel end of the engine are numbered 1, 3, 5, and 7 respectively, starting such numbering at the fan end of the engine, and those of the right-hand cylinder bank are numbered 2, 4, 6, and 8 respectively, these numbers appearing internally of the cylinder representations in Figure 2.
- crankshaft 15 may be of any of the conventional types but preferably as seen in Figures 1A and 1B is an inherently balanced shaft, for example, a two-plane crankshaft wherein the double crank throws identified by the Roman numerals I, II, III, and IV are arranged 90 apart, with throws I and II being respectively opposite throws IV and III.
- Throw No. I of Figures 1A and 13 connects with the pistons of cylinders l and 2, throw II with the pistons of cylinders 3 and 4, throw No. III with the pistons of cylinders 5 and 6, and throw No.
- throw No. III will follow throw, No. I by 90 of crank rotation counting clockwise in that figure and by interchanging throws II and III as in Figure 1B, throw No. II may be arranged 90 of clockwise rotation from throw No. I.
- firing orders are possible for the two described crank arrangements while affording preferred feeding intervals in the intake manifold of Figure 2.
- firing orders are possible for the two described crank arrangements while affording preferred feeding intervals in the intake manifold of Figure 2.
- firing orders :
- crank arrangement of Figure 1B may be used with the crank arrangement of Figure 1B.
- the hemispherical combustion chambers 13 of the cylinders 10 are by preference each provided with a single inlet opening or port 18 closed by an inlet valve 19 and with a single smaller exhaust outlet or port 20 closed by an exhaust valve 21, these valves being arranged transversely of the longitudinal axis 22 of the engine and at a substantial angle, for instance, 60 to each other, and preferably on a great arc of the spherical segment forming the combustion chamber 13.
- all of the inlet openings 18 are in longitudinal alignment and all of the exhaust openings 20 are similarly arranged.
- the inlet and exhaust valves of both banks of the engine are operable from a single camshaft 24 located above the crankshaft 15, the camshaft actuating suitable tappet mechanism associated with the push rods 25 and 26 of the inlet and exhaust valve mechanisms respectively which in turn actuate respectively the inlet valve rocker arms 27 and exhaust valve rocker arms 28, these rocker arms actuating in turn the normally spring-held closed valves 19 and '21.
- the camshaft 24 is usually arranged to open the respective inlet valves 19 before top dead center position of the piston and to close the exhaust valves after top dead center position of the piston so as to maintain the intake valve open during a substantial portion of crank rotation and to maintain the exhaust valve open long enough to obtain an overlap between opening of the inlet valve and closing of the exhaust valve of each cylinder.
- the intake or induction manifold of my invention generally referred to by the numeral 29, comprises an integral structure having two systems of conduits or passages indicated diagrammatically and generally in Figure 2A by the reference numerals 30, 32.
- the system 30 comprises four air-fuel passages or conduits generally referred to by the numerals 34, 36, 38, and 40 communicating at one end with a manifold intake or riser passage 42 fed by the single barrel riser or the carburetor X (see Figure 3) and preferably located on the longitudinal axis 22 of the manifold and approximately on a transverse line midway the cylinders 1 and 4 and communicating at the opposite ends with the intake passages 43 leading to the intake ports 18 for the cylinders 1, 4, 6, and 7 respectively.
- the system 32 comprises four airfuel passages or conduits generally referred to by the numerals 44, 46, 48, and 50 communicating at one end with a manifold intake or riser passage 52 fed by the single barrel of the carburetor Y, preferably located on the longitudinal axis 22 and approximately on a transverse line midway the cylinders 5 and 8 and communicating at the opposite ends with the intake passages 43 leading to the intake ports 18 for the cylinders 2, 3, 5, and 8.
- the carburetors X and Y are mounted on raised pads or bases 54, 56 respectively of the manifold, defining the riser passages 42, 52, the latter being in vertical alignment with the barrels 58, 60 respectively, of the carburetors X and Y from which gas or air-fuel mixture may be delivered to the risers 42, 52 under control of bladed throttle members 62, 64 located in the barrels 58, 60 respectively, and adapted to assume any condition from fully open to fully closed throttle.
- These throttle members may be controlled in any suitable manner preferably conjointly.
- the pads 54, 56 are carried by the air-fuel conduits aforesaid, these in turn connecting with longitudinally extending manifold mounting portions or flanges 66, 68 provided with inclined finished under faces 70, 72 which are downwardly converging and which coincide with mounting faces 74, 74a of the cylinder heads 12, 12a when seating the manifold. It will be noted that these flanges are somewhat longitudinally offset with respect to each other and symmetrically arranged relative to the risers 42, 52.
- the manifold 29 is secured in position on the cylinder heads 12, 12a with intervening gaskets 75 by bolts (not shown) which pass through the mounting holes 76 of the flanges into threaded holes (not shown) of the cylinder heads.
- the riser passage 42 for the carburetor X is shorter than the riser passage 52 for the carburetor Y.
- the riser 42 comprises a cylindrical portion 42a and an enlarged base portion forming a distri bution chamber 77 into which the conduits 34, 36, 38, and 40 open.
- the riser passage 52 comprises a similar but somewhat longer cylindrical portion 52a and a base portion forming a chamber 78 into which the conduits 44, 46, 48 and 50 open in a lower plane or level than the conduits of the riser 42 open into the chamber 77.
- the air-fuel conduits of my invention on one side of the axis 22 are when viewed in plan symmetrical with those on the opposite side, that each is preferably of generally the latter on a line normal to the axis 22 and terminating in an opening 82 in the flange 66 coinciding with the entrance of the intake passage 43 for cylinder No. 1.
- the conduit 50 extends from its entrance opening 84 in the chamber 78 of the riser 52 and terminates in an opening 86 in the flange 68 coinciding with the entrance opening of the intake passage 43 of cylinder No. 8.
- the passages 34, 36, 38, and 40 emanating from the chamber 77 of the riser 42 may be termed the upper level air-fuel passages, these being in the uppermost conduit plane of the manifold, whereas the passages 44, 46, 48, and 50 emanating from the chamber 78 of the riser 52 may be termed the lower level air-fuel passages, these being in the intermediate conduit plane of the manifold,
- the upper level passages 36, 38 are in juxtaposition to each other where they emanate from the chamber 77 of the riser 42 and have adjacent rectangular entrance openings 88, 89 respectively.
- the conduit 36 as seen in Figure 2 is of a generally reverse curve shape. It extends obliquely from the riser 42 until past the conduit 44 and then dips down as seen in Figure 7 and terminates in an opening 90 coinciding with the entrance of the intake passage 43 of cylinder No. 4.
- the conduit 38 extends alongside the conduit 36 and over the conduit 44. It has a common vertical wall 91 with the conduit 36 until these conduits separate and diverge from each other at the point where the conduit 36 turns outwardly on a line normal to the axis 22 to meet the intake passage of cylinder No. 4.
- the conduit 38 continues on a line substantially parallel to the axis 22 and then turns outwardly generally normal to the axis 22 when abreast cylinder No. 6 and turns downwardly as seen in Figure 6 to terminate in an opening 92 coinciding with the entrance of the intake passage 43 for cylinder No. 6.
- the conduits 46, 48 extend between their risers 52 and mounting in a flange manner similar to that which the conduits 36, 38 extend between the chamber 78 of the riser 52 and mounting flange 66 but in an opposite direction and at the lower air-fuel passage level aforesaid, they being -below the air-fuel passage 40.
- These conduits 46, 48 have juxtaposed entrance openings 93, 94 in the chamber 77 of the riser 52 and terminal openings 95, 96 respectively in the flange 66 where they coincide with the entrances of the intake passages 43 for cylinders Nos. 3 and 5 respectively.
- the conduits 46, 48 have a common vertical wall 97 extending a portion of their length from the riser 52.
- the conduit 40 extends at the upper air-fuel level from its entrance opening 98 in the chamber 77 of the riser 42 along a path generally paralleling the axis 22 and over the conduit 46 crossing the conduit 48 and curving outwardly when past intermediate cylinders 5 and 7 and downwardly when past the conduit 48 to terminate in an opening 99 coinciding with the intake passage 43 for cylinder No. 7.
- the entrance opening 98 of the conduit 40 is juxtaposed the entrances 80 and 89 of the conduits 34 and 38 respectively; and that the entrance openings 80, 98, 89, and 88 are arranged one in juxtaposition to the next at the level of the chamber 77.
- the upper level conduit 40 has a common horizontal wall 100 with the lower level air-fuel conduits 46 and 48 where it is immediately above the same.
- the vertical wall 101 of the conduit 40 intersects at 102 with the vertical wall 103 of the conduit 38 to form a common vertical edge for the juxtaposed openings 98 and 89 of these conduits, that the vertical wall 1640f the conduit 40 intersects at 105 with the vertical wall 106 of the conduit 34 to define a common edge of the juxtaposedentrance openings 93 and 80 of these conduits and that the terminal end 99a of the common vertical wall 91 of the conduits 36, 38 provides a common edge for the juxtaposed entrance openings 88, 89 of these conduits in the chamber 77.
- the lower level air-fuel conduit 44 extends between its chamber 73 of the riser 52 and its mounting flange 68 in the same manner to that in which the conduit 40 extends from its riser 42 but below the conduits 36, 38. It has an entrance opening 107 in the chamber 78 of the riser 52 and a terminal opening 108 in the flange 68 where it coincides with the intake passage 43 of cylinder No. 2.
- the entrance openings 84, 107, 93, and 94 to the chamber 78 of riser passage 52 are at the same level and one juxtaposed the other.
- the entrance 197 is juxtaposed the entrance 84 and has a common vertical edge 110 formed by the intersection of the vertical wall 112 of the conduit 44 with a vertical wall 114 of the conduit 50;
- the entrance 107 is also juxtaposed the entrance 93 and these have a common vertical edge 116 formed by intersection of the vertical wall 118 of the conduit 44 and the vertical wall 129 of conduit 46 and the entrance 93 of conduit 46 is juxtaposed the entrance 94 of conduit 48 and these have a common terminal edge 122 determined by their common vertical wall 97.
- the lower level air-fuel conduit 44 crosses the upper conduit 36 and substantially coincides part way with the upper level conduit 38 so as to have in part a common horizontal wall 124 with the conduits 36, 38.
- the manifold of this invention lends itself particularly to water heating of the carburetor riser hot spot and although exhaust gas heating may be used therefor, water heating is preferred since it avoids the need of a pair of exhaust gas crossover passages in the cylinder head of each bank.
- water heating is preferred since it avoids the need of a pair of exhaust gas crossover passages in the cylinder head of each bank.
- I provide intermediate each of the end pairs of cylinders of each bank in the cylinder heads thereof, suitable water outlet passages 129 which conduct water to suitable passages to be described of the manifold 29 and provided adjacent the risers 42, 52 thereof and from which the water is returned to the radiator of the vehicle.
- water may enter the manifold structure 29 through openings 130 and 132 in the mounting flange 66 of the left hand cylinder bank and through openings 131 and 133 in the mounting flange 68 of the right hand cylinder bank.
- the openings 130, 131 communicate with a cross conduit or passage 135 of rectangular shape seen best in Figures 2 and 10 which passes immediately below and in joinder with the chamber 78.
- This passage 135 has a common horizontal wall 137 with the chamber 78 of the riser 52 by which to communicate heat to the passage riser.
- the level of the cross passage 135 is below that of these air-fuel passages 44, 46, 48, and 60 and may be designated the lowermost or bottom conduit plane of the manifold 29. Due to the offset between the cylinders of the opposite banks of the engine the cross passage 135 as seen in Figure 2, has its portions or branches on the opposite side of the axis 22 offset somewhat from each other. As also seen in Figure 2, the cross passage 135 extends intermediate the cylinders Nos. and 7 of the left hand bank, and cylinders Nos.
- the second pair of water inlet apertures 1 32 and 133 are, as seen in Figure 2, located in the mounting flanges 66 and68 respectively, intermediate the cylinders Nos. 1 and 3 of the left hand bank, and the cylinders Nos. 2 and 4 of the right hand bank. These apertures are connected by a cross passage 138 which, as seen in Figures 2 and 9 and by reference to Figure 10, extends transversely from the aperture 133 to just past the axis 22 of the manifold and at the same level as the water passage extends across the manifold.
- This portion or branch of the water passage 138 identified by the numeral 140, has its top horizontal wall 142 in the same plane common with the bottom wall 144 of the conduit 44.
- the vertical portion 146 of the water passage has a vertical Wall 150 common with a vertical wall of the conduit 44 and has a horizontal wall 152 common with the floor of the chamber 77 of the riser 42 by which to directly communicate heat thereto.
- Connecting the two cross water passages 135 and 138 is a central longitudinal water passage or chamber 154 in the plane of the passage 135 and which is defined by side Walls 156 and 157 seen in Figure 2 and bottom wall 158, and a top wall 160 seen in Figure '8, the latter wall lying intermediate the longitudinally directed air-fuel passages 38, 4t 44, and 46 of Figure 2.
- the portions 175, 176 of the bore 174 are somewhat larger than the remaining portions 177, 178 and larger than the tubes 170, 172. Such facilitates easy assembly of the tubes in the portions 177, 178 which support them.
- the portions of the bores 174 are threaded at their outer end to receive plugs 178 after the tubes are assembled in position.
- a pair of tubes is preferred in order to obtain the lowest possible silhouette for the manifold structure. It will be understood, however, that a single tube may be employed if desired. In the present showing for a 331 cu. in. engine I have found that two tubes of in. inside diameter give optimum results.
- the total cross-sectional area of the passages 173 of these tubes is 0.3 square inch.
- the carburetors X and Y are preferably of the type utilizing side-type air cleaners which, as seen, are preferably positioned with their air intake faces at an angle to the horizontal axis 22 of the manifold and parallel to each other so as to make possible use 'of the largest air cleaner surface. It will be understood that concentric-type vertical air cleaners of standard construction may also be used if desired.
- Run No. D was made using a conventional manifold of the general type shown in the application of Carpent'ier et at, Serial No. 283,198, filed April 19,- 1952, and now Patent No. 2,686,506, granted August 17, 1954, and employing a conventional Carter W. C. D. 9315 dual barrel carburetor having 1%! venturis, while run No. S employed the manifold of the subject invention employing two Ball and Ball E7T1 adjustable jet carburetors with conventional concentric air cleaners No. 919801, the carburetors having 1 venturis.
- An intake manifold for an engine having opposite cylinder banks each including a plurality of cylinders said manifold comprising opposite longitudinally extending portions for mounting said manifold on said engine banks, an intermediate portion on which to support a pair of fuel supply means, and conduit means connecting said mounting portions and said intermediate portion, a pair of longitudinally wide spaced intake riser passages on said intermediate portion, one transversely adjacent an end cylinder of one bank, and the other transversely adjacent the end cylinder at the opposite end of the same bank, one of said pair of riser passages each fed by one of said pair of fuel supply means and the other of said pair of riser passages to be fed by the other of said pair of fuel supply means, a plurality of spaced apertures in said mounting portions arranged longitudinally thereof, there being one such aperture for each cylinder, and a plurality of air-fuel passages provided by said conduit means between said apertures and said risers, there being an independent passage directly connecting each aperture with a riser passage; half the number of passages connecting with one riser and
- An intake manifold for an engine having opposite cylinder banks each including a cylinder :head and a plurality of cylinders said manifold comprising opposite longitudinally extending flange portions for mounting said manifold to said cylinder heads, an intermediate portion on which to support a pair of single barrel fuel supply means, and conduit means connecting said mounting portions and said intermediate portion, a pair of longitudinally wide spaced intake riser passages on said intermediate portion, one transversely adjacent an end cylinder of one bank and the other transverselyadjacent the end cylinder at the opposite end of the same bank, one of said pair of riser passages each fed by one of said pair of fuel supply means and the other of said pair of riser passages to be fed by the other of said pair of fuel supply means, a plurality of spaced apertures in each of said mounting portions arranged longitudinally thereof 0116 opposite each cylinder, and a plurality of airfuel passages provided by said conduit means, each independently connecting an intake riser with a different aperture, there being one such passage for each aperture and half the
- An intake manifold for an engine having opposite cylinder banks each including a cylinder head and four cylinders, the cylinders of one bank being successively numbered for refieren'ceyherein 1, 3, 5, 7 and being respectively located substantially. opposite to those cylinders successively numbered 2, 4, 6, 8 in the other bank, said manifold comprising opposite mounting portions for mounting said manifold to said banks, a pair of longi tudinally spaced intermediate portions each containing an intake riser passage, one of said riser passages being located intermediate cylinders 5 and 8, and the other being located intermediate cylinders 1 and 4, conduit portions connecting said intermediate portions and said mounting portions, said conduit portions providing independent passages each haVing an independent inlet opening in one of said riser passages and an independent terminal opening in one of said mounting portions adjacent -a cylinder of the ban-k mounting such mounting portion, said terminal'opening substantially coinciding with the inlet of the intake passage to this cylinder, some of said independent passages being between one of said riser passages and the said mounting portion terminal openings thereof
- each intake riser passage includes a distribution chamber and each conduit passage connects with its riser passage at said chamber.
- An intake manifold for an engine having opposite cylinder banks each including a plurality of cylinders said manifold comprising opposite portions for mounting said manifold on said engine banks, an intermediate portion on which to supporta pair of fuel supply means, conduit means connecting said mounting portions and said intermediate portion, a pair of longitudinally spaced intake riser passages on said intermediate portion for connecting with said fuel supply means, one of said riser passages being transversely adjacent an end cylinder of one bank and the other transversely adjacent the end cylinder at the opposite end of the same bank, said conduit means defining a plurality of air-fuel passages extending between said mounting portions and the risers of said inter-mediate portion, half the number of said passages connecting with one riser, and half connecting with the other riser, and metering control means interconnecting said riser passages.
- An intake manifold for an engine having opposite cylinder banks each including a plurality of cylinders said manifold comprising opposite portions for mounting said manifold on said engine banks, an intermediate portion on which to support a pair of fuel supply means, conduit means connecting said mounting portions and said intermediate portion, a pair of longitudinally spaced intake riser passages on said intermediate portion for connecting with said fuel supply means, one of said-riserpassages being transversely adjacent an end cylinder of one bank and the other transversely adjacent the end cylinder at the opposite end'of the same bank, said conduit means defining a plurality of air fuel passages extending between said mounting portions and the risers of said intermediate portion, half the number of said passages connecting with one riser, and half connecting with the other riser, and longitudinal passage means having a cross-sectional area of lessthan one-half square inch interconnecting said risenpassages.
- An intake manifold for an engine having opposite cylinder banks each including a plurality of cylinders said manifold comprising opposite portions for mounting said manifold on said engine banks, a pair of longitudinally spaced intermediate portions on which to support a pair of single barrel fuel supply means, conduit means connecting said mounting portions and said intermediate portions, each of said intermediate portions having an intake riserpassage connecting with the fuel supply means thereon and said conduit means providing air-fuel passages between said riser passages and said mounting portions, there being an independent air-fuel passage for connecting with each cylinder of the engine and half the number of said passages connecting with one riser and the remainder connecting with the other riser and tubular metering means extending between said intermediate portions and opening into said riser passages for interconnecting the same.
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Description
Oct. 2, 1956 P. M. ROTHWELL 2,764,961
INTAKE MANIFOLD STRUCTURE Filed July 25, 1954 4 Sheets-Sheet 1 ,qrrarkz/s Oct. 2, 1956 P. M. ROTHWELL INTAKE MANIFOLD STRUCTURE Filed July 23, 1954 4 Sheets-Sheet 2 34 71172;? M FaZlwe/Z szdzw) I L 0a. 2, 1956 P. M. RQTHWELL 2,764,961
INTAKE MANIFOLD STRUCTURE Filed July 23, l954 4 Sheets-Sheet 4 II/l III I INVENTOR. 1%; M/Baiizz/e/Z United States Patent INTAKE MANIFOLD STRUCTURE Philip M. Rothwell, Detroit, Mich., assignor to Chrysler Corporation, Highland Park, Mich., a corporation of Delaware Application July 23, 1954, Serial No. 445,225
15 Claims. (Cl. 123-52) This invention relates to intake manifold structures for engines of the type having a pair of cylinder banks arranged at an angle to each other and especially for V engines.
My invention has particular application to improved intake manifolding for V8 engines wherein two inner cylinders of one bank of the engine and two outer or end cylinders of the other bank of the engine are fed from a common supply of air fuel mixture.
It has heretofore been proposed in V-8 engines of the foregoing type to feed the engine from one dual barrel carburetor, each barrel of which feeds four cylinders. Although good performance is thereby possible, it is desirable in certain installations such as for truck or industrial use to obtain optimum mid-speed torque and I have discovered that improvement in this feature of the engine performance is feasible while also providing greater air fuel capacity for the engine by a manifold having a novel arrangement of passages and which employs two simple, inexpensive, single barrel carburetors and in the Widest possible spacing, such that the use of large air cleaners becomes possible.
The use of two individual carburetors is advantageous since the barrels of a dual carburetor even if of the same size are interconnected part way, i. e. in the sense that they employ one air cleaner and one air horn and I find that the effective air-fuel capacity is not as great as that obtained by the use of two single carburetors. In fact even if the air capacity of the total system at high speed (volumetric efliciency) were as a practical matter the same in the case of the dual or two single carburetors or greater in the case of the dual I find that mid-speed torque will be greater in the case of the two single carburetors.
I have further discovered that although the wide spacing of the individual carburetors produces a wide variation in conduit lengths from the carburetor riser to the cylinders, such does not adversely affect power output or air-fuel distribution in the mid-speed range in which the engine must do its principal work in the case of trucks or industrial use and good performance with a good F/ A ratio of about .080 in all cylinders is obtainable. This is believed due in part to a satisfactory pulsating flow set up in the conduits and the frequency of which at the engine speeds 600-4000 R. P. M. and especially in the midspeed range of 2000-3200 R. P. M., in which peak torque output is desired, is not adversely affected by the different pipe lengths of the branches and in part to the fact that my air-fuel conduits directly connect with the manifold intake risers to provide better distribution control than Where the cylinders must be fed off side branches.
The principal object of my invention is therefore to provide engines of the foregoing type with an intake manifold system providing good mid-speed torque output.
Still another object is to provide engines of the foregoing type with an intake manifold system providing optimum torque in the speed range of 2000-3200 R. P. M.
A further object is to provide an engine of the fore- 2,764,961 Patented Oct. 2, 1956 2 going type with an intake manifold system utilizing a pair of spaced single barrel carburetors and whose firing order provides the widest possible separation between suction impulses on the two carburetors.
A further object is to provide such engines with an intake manifold system using a pair of single barrel carburetors arranged with the widest possible spacing and utilizing large air cleaners.
In working with the manifold of my invention, I have found that due to use of a simple form of carburetor that there is tendency for some cylinders to over enrich at certain low speeds, for instance, 1600 R. P. M. possibly due to high pulsations, and such tends to foul up plugs. I have found that this condition may be controlled at the expense of some torque output reduction by the use of special carburetion. However, this is expensive. I have found that the condition may preferably be controlled by the use of conduit-type metering means between the manifold intake risers to damp out high pulsations and thereby prevent over enrichment. The metering control means may be constituted of a single or plurality of conduits whose total area is somewhat critical in that if too large, the value of a firing order producing a wide separation in suction impulses may be somewhat lost with consequent loss of torque. No fixed formula for this area appears possible and hence it is recommended that several sizes be tried to find that which provides the best mixture control and best torque. In general an area of less than /2 sq. in. is preferred. An area of 0.3 sq. in. appears satisfactory for a 331 cu. in. V-8 engine using standard single barrel carburetors, for instance Ball & Ball BBS975S carburetors.
Hence a further object is to provide a manifold system as aforesaid wherein pulsation damping or mixture metering control means are provided between the intake riser passages of the manifold.
I have further discovered that with-a manifold such as I employ, heating of the intake riser passages for normal operation may advantageously be provided by water heating. In the present manifold it is simpler to provide than exhaust gas heating and is practical in the case of truck engines or industrial use because in these operations the operator can take more time for warm up. Moreover, water taps are readily available in the cylinderheads. Furthermore, by using Water heating the refrigeration effect of the air fuel mixture on the water is obtained and this thereby reduces the heat rejection of the coolant water necessary at the radiator.
Hence still another object of my invention is to provide an intake manifold system as aforesaid in which the intake riser passages are water heated for normal operation and for reducing the heat rejection of the coolant system at the radiator.
Other objects and advantages of my invention will be more apparent from the following description of a preferred embodiment of my invention as applied to a 331 cu. in. V-8 engine, reference being had to the accompanying drawings in which:
Figure l is an end elevational view partly in section of an 8-cylinder V-type overhead valve engine embodying the intake manifold system of my invention, the section through the manifold being taken approximately at ZZ of Figure 2;
Figures 1A and 1B are schematic views of the two preferred two plane crank pin arrangements for an 8-cylinder V engine utilizing my invention, the Roman numerals in the figures indicating the positioning of the crank throws counting from the front or fan end of the engine and the numerals in the brackets indicating cylin der numbers whose pistons are connected with the engine throw;
Figure 2 is a plan view of the manifold of my invention and schematically showing the banks of cylinders in relation thereto;
, Figure 2A is a schematic showing of the air-fuel passages of the manifold of Figure 2;
Figure 3 is a side elevational view of the manifold of Figure 2 showing the carburetors and air cleaners in position thereon;
Figure 4 is a sectional development taken in elevation at A'A of Figure 2 through a pair of conduits connecting with one manifold riser passage and showing a portion of the throttle passage of a carburetor feeding the same; I
Figure 5 is a sectional development taken in elevation at BB of Figure 2 through a second pair of conduits connecting with the same riser;
Figure 6. is, a sectional development taken in elevation at C'C of Figure 2 through a pair of conduits connecting with the other manifold riser;
Figure 7 is a sectional development taken in elevation at D'-'D of Figure 2 through a second pair of conduits connecting with the same riser passage as the conduits of Figure 6 and showing the throttle passage portion of the carburetor feeding the same;
Figure 8 is a sectional elevation taken at E-E of Figure 2 through the riser passages and longitudinal water heating conduit;
.Figure 9 is a sectional elevation taken at FF of Figure 2 through one transverse water heating passage; I Figure 10 is a sectional elevation taken at GG of Figure 2 through a second transverse water heating passage;
Figure 11 is a plan view of a portion of the manifold of Figure 2 showing a modification providing metering means between the carburetor riser passages; and
Figure 12 is a sectional elevationof portions of the riser passages of the manifold of Figure 11 taken at thereof showing the manner of providing metering means therebetween.
Referring now to the drawings wherein similar numerals are used to designate similar parts of the manifold structure and system of my invention, I have illustrated my invention asapplied to a 331 cu; in. 90 V-8 engine of current manufacture having a so-called two-plane 90 crankshaft, hemispherical combustion chambers and proyided with downdraft carburetion of the single barrel type, each carburetor being arranged reread a pair of inner cylinder of one bank and a pair of outer or end cylinders of the opposite bank. -It be understood that my invention is applicable to other engines of the type having opposite banks of cylinders and having a greater or lesser nurnber of cylinders Also the carburetion may be of the downdraft, updraft, horizontal or injection character.
As seen in the drawings, especially Figures 1 and 2, the engine has two banks 9 and 9a of cylinders 10, four in each bank, arranged at 90 in a cylinder block 11, to which cylinder heads 12 and 1221 are secured and provided with hemispherical typecombustion chambers 13 immediately above each cylinder 10. The cylinders of each bank are aligned longitudinally of the axis of the engine and the cylinders of the opposite banks are offset longitudinally relative to each other.
For convenient reference, the cylinders of the lefthand cylinder bank, which is to the left looking forward from the flywheel end of the engine are numbered 1, 3, 5, and 7 respectively, starting such numbering at the fan end of the engine, and those of the right-hand cylinder bank are numbered 2, 4, 6, and 8 respectively, these numbers appearing internally of the cylinder representations in Figure 2.
Each cylinder is provided with a piston 14 recipuocable therein and operably connected to a crankshaft 15 through a connecting rod 16 and wrist pin 17. Crankshaft 15 may be of any of the conventional types but preferably as seen in Figures 1A and 1B is an inherently balanced shaft, for example, a two-plane crankshaft wherein the double crank throws identified by the Roman numerals I, II, III, and IV are arranged 90 apart, with throws I and II being respectively opposite throws IV and III. Throw No. I of Figures 1A and 13 connects with the pistons of cylinders l and 2, throw II with the pistons of cylinders 3 and 4, throw No. III with the pistons of cylinders 5 and 6, and throw No. IV with the pistons of cylinders 7 and 8. In Figure 1A itwill be seen that throw No. III will follow throw, No. I by 90 of crank rotation counting clockwise in that figure and by interchanging throws II and III as in Figure 1B, throw No. II may be arranged 90 of clockwise rotation from throw No. I.
Various firing orders are possible for the two described crank arrangements while affording preferred feeding intervals in the intake manifold of Figure 2. For example, the following firing orders:
may be used with the crank arrangement of Figure 1B.
In Figure 2 my invention has been shown as applied to an engine having a crank arrangement of Figure 1A and preferred firing order of l-8-4-3-65-7-2. The firing sequence is designated by the numerals just outside the ellipses in this figure designating cylinders. In this structure it will be apparent that the suction strokes of cylinders 1 and 6 are 360 out of phase, i. e. the cylinder 6 is beginning its suction stroke as the cylinder 1 starts its power stroke. This is also true of the pairs of cylinders'S, 5; 4, 7 and 3, 2.
The hemispherical combustion chambers 13 of the cylinders 10 are by preference each provided with a single inlet opening or port 18 closed by an inlet valve 19 and with a single smaller exhaust outlet or port 20 closed by an exhaust valve 21, these valves being arranged transversely of the longitudinal axis 22 of the engine and at a substantial angle, for instance, 60 to each other, and preferably on a great arc of the spherical segment forming the combustion chamber 13. As seen in Figure 2, all of the inlet openings 18 are in longitudinal alignment and all of the exhaust openings 20 are similarly arranged.
The inlet and exhaust valves of both banks of the engine are operable from a single camshaft 24 located above the crankshaft 15, the camshaft actuating suitable tappet mechanism associated with the push rods 25 and 26 of the inlet and exhaust valve mechanisms respectively which in turn actuate respectively the inlet valve rocker arms 27 and exhaust valve rocker arms 28, these rocker arms actuating in turn the normally spring-held closed valves 19 and '21.
By preference, the camshaft 24 ,is usually arranged to open the respective inlet valves 19 before top dead center position of the piston and to close the exhaust valves after top dead center position of the piston so as to maintain the intake valve open during a substantial portion of crank rotation and to maintain the exhaust valve open long enough to obtain an overlap between opening of the inlet valve and closing of the exhaust valve of each cylinder.
The intake or induction manifold of my invention generally referred to by the numeral 29, comprises an integral structure having two systems of conduits or passages indicated diagrammatically and generally in Figure 2A by the reference numerals 30, 32. The system 30 comprises four air-fuel passages or conduits generally referred to by the numerals 34, 36, 38, and 40 communicating at one end with a manifold intake or riser passage 42 fed by the single barrel riser or the carburetor X (see Figure 3) and preferably located on the longitudinal axis 22 of the manifold and approximately on a transverse line midway the cylinders 1 and 4 and communicating at the opposite ends with the intake passages 43 leading to the intake ports 18 for the cylinders 1, 4, 6, and 7 respectively. The system 32 comprises four airfuel passages or conduits generally referred to by the numerals 44, 46, 48, and 50 communicating at one end with a manifold intake or riser passage 52 fed by the single barrel of the carburetor Y, preferably located on the longitudinal axis 22 and approximately on a transverse line midway the cylinders 5 and 8 and communicating at the opposite ends with the intake passages 43 leading to the intake ports 18 for the cylinders 2, 3, 5, and 8.
As seen in Figures 2 to 10, the carburetors X and Y are mounted on raised pads or bases 54, 56 respectively of the manifold, defining the riser passages 42, 52, the latter being in vertical alignment with the barrels 58, 60 respectively, of the carburetors X and Y from which gas or air-fuel mixture may be delivered to the risers 42, 52 under control of bladed throttle members 62, 64 located in the barrels 58, 60 respectively, and adapted to assume any condition from fully open to fully closed throttle. These throttle members may be controlled in any suitable manner preferably conjointly.
The pads 54, 56 are carried by the air-fuel conduits aforesaid, these in turn connecting with longitudinally extending manifold mounting portions or flanges 66, 68 provided with inclined finished under faces 70, 72 which are downwardly converging and which coincide with mounting faces 74, 74a of the cylinder heads 12, 12a when seating the manifold. It will be noted that these flanges are somewhat longitudinally offset with respect to each other and symmetrically arranged relative to the risers 42, 52.
The manifold 29 is secured in position on the cylinder heads 12, 12a with intervening gaskets 75 by bolts (not shown) which pass through the mounting holes 76 of the flanges into threaded holes (not shown) of the cylinder heads.
As seen in Figure 8, the riser passage 42 for the carburetor X is shorter than the riser passage 52 for the carburetor Y. The riser 42 comprises a cylindrical portion 42a and an enlarged base portion forming a distri bution chamber 77 into which the conduits 34, 36, 38, and 40 open. The riser passage 52 comprises a similar but somewhat longer cylindrical portion 52a and a base portion forming a chamber 78 into which the conduits 44, 46, 48 and 50 open in a lower plane or level than the conduits of the riser 42 open into the chamber 77. Moreover, it will be observed from Figures 2-10 that the air-fuel conduits of my invention on one side of the axis 22 are when viewed in plan symmetrical with those on the opposite side, that each is preferably of generally the latter on a line normal to the axis 22 and terminating in an opening 82 in the flange 66 coinciding with the entrance of the intake passage 43 for cylinder No. 1. In a similar but opposite manner and starting at a somewhat lower level the conduit 50 extends from its entrance opening 84 in the chamber 78 of the riser 52 and terminates in an opening 86 in the flange 68 coinciding with the entrance opening of the intake passage 43 of cylinder No. 8. It will be observed, however, by reference to Figures 5 and 6, for example, that the passage 50 where it extends from its riser 52 and for some distance prior to meeting the intake passage 43 at its outlet 86 is at a lower level than the conduit 34 where the latter extends from the riser 42, chamber 77. This facilitates pyramiding or stacking of certain conduits or passages, and in this connection, the passages 34, 36, 38, and 40 emanating from the chamber 77 of the riser 42 may be termed the upper level air-fuel passages, these being in the uppermost conduit plane of the manifold, whereas the passages 44, 46, 48, and 50 emanating from the chamber 78 of the riser 52 may be termed the lower level air-fuel passages, these being in the intermediate conduit plane of the manifold,
The upper level passages 36, 38 are in juxtaposition to each other where they emanate from the chamber 77 of the riser 42 and have adjacent rectangular entrance openings 88, 89 respectively. The conduit 36 as seen in Figure 2 is of a generally reverse curve shape. It extends obliquely from the riser 42 until past the conduit 44 and then dips down as seen in Figure 7 and terminates in an opening 90 coinciding with the entrance of the intake passage 43 of cylinder No. 4. The conduit 38 extends alongside the conduit 36 and over the conduit 44. It has a common vertical wall 91 with the conduit 36 until these conduits separate and diverge from each other at the point where the conduit 36 turns outwardly on a line normal to the axis 22 to meet the intake passage of cylinder No. 4. The conduit 38 continues on a line substantially parallel to the axis 22 and then turns outwardly generally normal to the axis 22 when abreast cylinder No. 6 and turns downwardly as seen in Figure 6 to terminate in an opening 92 coinciding with the entrance of the intake passage 43 for cylinder No. 6.
The conduits 46, 48 extend between their risers 52 and mounting in a flange manner similar to that which the conduits 36, 38 extend between the chamber 78 of the riser 52 and mounting flange 66 but in an opposite direction and at the lower air-fuel passage level aforesaid, they being -below the air-fuel passage 40. These conduits 46, 48 have juxtaposed entrance openings 93, 94 in the chamber 77 of the riser 52 and terminal openings 95, 96 respectively in the flange 66 where they coincide with the entrances of the intake passages 43 for cylinders Nos. 3 and 5 respectively. As in the case of the conduits 36, 38 the conduits 46, 48 have a common vertical wall 97 extending a portion of their length from the riser 52.
The conduit 40 extends at the upper air-fuel level from its entrance opening 98 in the chamber 77 of the riser 42 along a path generally paralleling the axis 22 and over the conduit 46 crossing the conduit 48 and curving outwardly when past intermediate cylinders 5 and 7 and downwardly when past the conduit 48 to terminate in an opening 99 coinciding with the intake passage 43 for cylinder No. 7.
It will be observed that the entrance opening 98 of the conduit 40 is juxtaposed the entrances 80 and 89 of the conduits 34 and 38 respectively; and that the entrance openings 80, 98, 89, and 88 are arranged one in juxtaposition to the next at the level of the chamber 77. Moreover, as seen in Figure 7, for example, the upper level conduit 40 has a common horizontal wall 100 with the lower level air- fuel conduits 46 and 48 where it is immediately above the same. It will also be seen that the vertical wall 101 of the conduit 40 intersects at 102 with the vertical wall 103 of the conduit 38 to form a common vertical edge for the juxtaposed openings 98 and 89 of these conduits, that the vertical wall 1640f the conduit 40 intersects at 105 with the vertical wall 106 of the conduit 34 to define a common edge of the juxtaposedentrance openings 93 and 80 of these conduits and that the terminal end 99a of the common vertical wall 91 of the conduits 36, 38 provides a common edge for the juxtaposed entrance openings 88, 89 of these conduits in the chamber 77.
The lower level air-fuel conduit 44 extends between its chamber 73 of the riser 52 and its mounting flange 68 in the same manner to that in which the conduit 40 extends from its riser 42 but below the conduits 36, 38. It has an entrance opening 107 in the chamber 78 of the riser 52 and a terminal opening 108 in the flange 68 where it coincides with the intake passage 43 of cylinder No. 2.
The entrance openings 84, 107, 93, and 94 to the chamber 78 of riser passage 52 are at the same level and one juxtaposed the other. Thus the entrance 197 is juxtaposed the entrance 84 and has a common vertical edge 110 formed by the intersection of the vertical wall 112 of the conduit 44 with a vertical wall 114 of the conduit 50; the entrance 107 is also juxtaposed the entrance 93 and these have a common vertical edge 116 formed by intersection of the vertical wall 118 of the conduit 44 and the vertical wall 129 of conduit 46 and the entrance 93 of conduit 46 is juxtaposed the entrance 94 of conduit 48 and these have a common terminal edge 122 determined by their common vertical wall 97.
As seen in Figures 4 and 7, the lower level air-fuel conduit 44 crosses the upper conduit 36 and substantially coincides part way with the upper level conduit 38 so as to have in part a common horizontal wall 124 with the conduits 36, 38.
As previously noted, the manifold of this invention lends itself particularly to water heating of the carburetor riser hot spot and although exhaust gas heating may be used therefor, water heating is preferred since it avoids the need of a pair of exhaust gas crossover passages in the cylinder head of each bank. For the purpose of water heating the carburetor intake riser passages, I provide intermediate each of the end pairs of cylinders of each bank in the cylinder heads thereof, suitable water outlet passages 129 which conduct water to suitable passages to be described of the manifold 29 and provided adjacent the risers 42, 52 thereof and from which the water is returned to the radiator of the vehicle.
As seen in Figure 2 and Figures 8 to 10, water may enter the manifold structure 29 through openings 130 and 132 in the mounting flange 66 of the left hand cylinder bank and through openings 131 and 133 in the mounting flange 68 of the right hand cylinder bank. The openings 130, 131 communicate with a cross conduit or passage 135 of rectangular shape seen best in Figures 2 and 10 which passes immediately below and in joinder with the chamber 78. This passage 135 has a common horizontal wall 137 with the chamber 78 of the riser 52 by which to communicate heat to the passage riser. Since the air- fuel passages 44, 46, 48, and S emanate from the chamber 78 at the lower air-fuel passage level and the cross passage 135 must transverse these air-fuel passages, the level of the cross passage 135 is below that of these air- fuel passages 44, 46, 48, and 60 and may be designated the lowermost or bottom conduit plane of the manifold 29. Due to the offset between the cylinders of the opposite banks of the engine the cross passage 135 as seen in Figure 2, has its portions or branches on the opposite side of the axis 22 offset somewhat from each other. As also seen in Figure 2, the cross passage 135 extends intermediate the cylinders Nos. and 7 of the left hand bank, and cylinders Nos. 6 and 8 of the right hand s The second pair of water inlet apertures 1 32 and 133 are, as seen in Figure 2, located in the mounting flanges 66 and68 respectively, intermediate the cylinders Nos. 1 and 3 of the left hand bank, and the cylinders Nos. 2 and 4 of the right hand bank. These apertures are connected by a cross passage 138 which, as seen in Figures 2 and 9 and by reference to Figure 10, extends transversely from the aperture 133 to just past the axis 22 of the manifold and at the same level as the water passage extends across the manifold. This portion or branch of the water passage 138, identified by the numeral 140, has its top horizontal wall 142 in the same plane common with the bottom wall 144 of the conduit 44. Just past the conduit 44 the water passage 138 extends upwardly and then horizontally at the intermediate conduit level to connect the water inlet 132 of the left hand bank. The vertical portion 146 of the water passage has a vertical Wall 150 common with a vertical wall of the conduit 44 and has a horizontal wall 152 common with the floor of the chamber 77 of the riser 42 by which to directly communicate heat thereto. Connecting the two cross water passages 135 and 138 is a central longitudinal water passage or chamber 154 in the plane of the passage 135 and which is defined by side Walls 156 and 157 seen in Figure 2 and bottom wall 158, and a top wall 160 seen in Figure '8, the latter wall lying intermediate the longitudinally directed air-fuel passages 38, 4t 44, and 46 of Figure 2. Moreover as seen in Figures 2 and 8 the central chamber 154 and the cross water passage 138 are connected by a passage 162 which extends upwardly therefrom, it terminating in an outlet 164 having a mounting face 165 for receiving a water connection with the radiator. It will be evident that by the described water system, adequate heating will be conducted to the riser passages of the spaced carburetors.
As previously described, I have found it possible to control over-enrichment of certain cylinders during low speed operation 'by the use of metering means between the intake risers of the manifold whose effect is to damp out high pulsations. In Figures 11 and 12 I have shown one form of accomplishing this result and which comprises a pair of tubes 170, 172 extending between the bosses 54 and 56 of the manifold and opening into the riser passages 42, 52 so as to efiect a limited communication or passage 173 between the risers. It will be evident from Figure 12 that I effect this result by providing a pair of tube-receiving stepped bores 174 entirely across the boss 56 and through one side of the boss 54. It will be observed that the portions 175, 176 of the bore 174 are somewhat larger than the remaining portions 177, 178 and larger than the tubes 170, 172. Such facilitates easy assembly of the tubes in the portions 177, 178 which support them. The portions of the bores 174 are threaded at their outer end to receive plugs 178 after the tubes are assembled in position. A pair of tubes is preferred in order to obtain the lowest possible silhouette for the manifold structure. It will be understood, however, that a single tube may be employed if desired. In the present showing for a 331 cu. in. engine I have found that two tubes of in. inside diameter give optimum results. The total cross-sectional area of the passages 173 of these tubes is 0.3 square inch.
As seen in Figures 1 and 3, the carburetors X and Y are preferably of the type utilizing side-type air cleaners which, as seen, are preferably positioned with their air intake faces at an angle to the horizontal axis 22 of the manifold and parallel to each other so as to make possible use 'of the largest air cleaner surface. It will be understood that concentric-type vertical air cleaners of standard construction may also be used if desired.
Some idea of the increase in midspeed torque possible with the novel manifold of my invention will be evident from the following comparison of two test runs at wide open throttle with a 331 cu. in. V-8 engine of the character described. Run No. D was made using a conventional manifold of the general type shown in the application of Carpent'ier et at, Serial No. 283,198, filed April 19,- 1952, and now Patent No. 2,686,506, granted August 17, 1954, and employing a conventional Carter W. C. D. 9315 dual barrel carburetor having 1%! venturis, while run No. S employed the manifold of the subject invention employing two Ball and Ball E7T1 adjustable jet carburetors with conventional concentric air cleaners No. 919801, the carburetors having 1 venturis.
Run No. D Run No. S
Speed Torque B. H. P. Torque B. H. P.
(lb. ft.) (1b. 11:.)
From this test data it will be apparent that the manifold of the subject invention produces a considerable increase in midspeed torque.
From the foregoing description of my invention it will be apparent that I have provided a novel manifold structure and system capable of providing optimum midspeed torque and particularly adapted for use for truck engines. It will be understood that various changes and modifications may be made in the novel features of my invention without departing from the intent and spirit thereof and all such changes and modifications as are embraced by the appended claims and equivalents thereof are to be included.
I claim:
1. An intake manifold for an engine having opposite cylinder banks each including a plurality of cylinders, said manifold comprising opposite longitudinally extending portions for mounting said manifold on said engine banks, an intermediate portion on which to support a pair of fuel supply means, and conduit means connecting said mounting portions and said intermediate portion, a pair of longitudinally wide spaced intake riser passages on said intermediate portion, one transversely adjacent an end cylinder of one bank, and the other transversely adjacent the end cylinder at the opposite end of the same bank, one of said pair of riser passages each fed by one of said pair of fuel supply means and the other of said pair of riser passages to be fed by the other of said pair of fuel supply means, a plurality of spaced apertures in said mounting portions arranged longitudinally thereof, there being one such aperture for each cylinder, and a plurality of air-fuel passages provided by said conduit means between said apertures and said risers, there being an independent passage directly connecting each aperture with a riser passage; half the number of passages connecting with one riser and 'half connecting with the other.
2. An intake manifold for an engine having opposite cylinder banks each including a cylinder :head and a plurality of cylinders, said manifold comprising opposite longitudinally extending flange portions for mounting said manifold to said cylinder heads, an intermediate portion on which to support a pair of single barrel fuel supply means, and conduit means connecting said mounting portions and said intermediate portion, a pair of longitudinally wide spaced intake riser passages on said intermediate portion, one transversely adjacent an end cylinder of one bank and the other transverselyadjacent the end cylinder at the opposite end of the same bank, one of said pair of riser passages each fed by one of said pair of fuel supply means and the other of said pair of riser passages to be fed by the other of said pair of fuel supply means, a plurality of spaced apertures in each of said mounting portions arranged longitudinally thereof 0116 opposite each cylinder, and a plurality of airfuel passages provided by said conduit means, each independently connecting an intake riser with a different aperture, there being one such passage for each aperture and half the number of said pas-sages directly connecting only with one of said riser passages while the other half thereof directly connect only with the other of said riser passages.
3. An intake manifold for an engine having opposite cylinder banks each including a cylinder head and .a plurality of cylinders, said manifold comprising opposite longitudinally extending flange portions for mounting said manifold to said cylinder heads, an intermediate portion on which to support a pair of single barrel fuel supply means, and conduit means connecting said mounting portions and said intermediate portion, a pair of longitudinally spaced intake riser passages on said intermediate portion, one transversely adjacent an end cylinder of one bank and the other transversely adjacent the end cylinder at the opposite end of the same bank, each riser passage including a distribution chamber at the lower end thereof, that of one riser being in a lower plane than the chamber of the other, a plurality of peripherally adjacent apertures in each of said chambers, a plurality of spaced apertures in each of said mounting portions arranged longitudinally thereof, one opposite each cylinder, and a plurality of air-fuel passages provided by said conduit means, each connecting a chamber aperture with a mounting aperture, no two of said passages connecting with the same apertures and half the number of said passages being associated with one riser chamber and the remainder with the other riser chamber.
4. An intake manifold as claimed in claim 3 wherein some of the air-fuel passages associated with each riser chamber connect with the apertures of the mounting portion of one bank and the remainder with apertures of the mounting portion of the other bank.
5. An intake manifold for an engine having opposite cylinder banks each including a cylinder head and four cylinders, the cylinders of one bank starting from one end of the engine being successively numbered for reference herein 1, 3, 5 and 7 and being respectively located substantially opposite to those cylinders in the other bank which starting from the same end of the engine are numbered 2, 4, 6 and 8, said manifold comprising opposite mounting portions for mounting said manifold to said bank, a pair of longitudinally spaced intermediate portions each containing an intake riser passage, one located intermediate cylinders 5 and 8 and the other intermediate cylinders 1 and 4, air-fuel conduit portions connecting said intermediate portions and said mounting portions, said conduit portions providing independent air-fuel passages between one riser passage iand said mounting portions for feeding cylinders 1, 4, 6, and 7 and corresponding independent air-fuel passages between the other riser passage and said mounting portions for feeding cylinders 8, 5, 3, 2. I
6. An intake manifold for an engine having opposite cylinder banks each including a cylinder head and four cylinders, the cylinders of one bank being successively numbered for refieren'ceyherein 1, 3, 5, 7 and being respectively located substantially. opposite to those cylinders successively numbered 2, 4, 6, 8 in the other bank, said manifold comprising opposite mounting portions for mounting said manifold to said banks, a pair of longi tudinally spaced intermediate portions each containing an intake riser passage, one of said riser passages being located intermediate cylinders 5 and 8, and the other being located intermediate cylinders 1 and 4, conduit portions connecting said intermediate portions and said mounting portions, said conduit portions providing independent passages each haVing an independent inlet opening in one of said riser passages and an independent terminal opening in one of said mounting portions adjacent -a cylinder of the ban-k mounting such mounting portion, said terminal'opening substantially coinciding with the inlet of the intake passage to this cylinder, some of said independent passages being between one of said riser passages and the said mounting portion terminal openings thereof adjacent cylinders 1, 4, 6, 7 and others corresponding thereto when viewed in plan being between the other riser passage and the said mounting portion terminal openings thereof adjacent cylinders 8, 5, 3, the inlet openings for said passages in one riser being in a lower plane than those of the other riser passage, and one of said conduits defining a passage from one riser being in part immediately above a pair of conduits defining passages from theother riser and a portion of a further conduit defining a passage from said other "riser corresponding to said passage defined by said one conduit being immediately below a pair of other conduits defining passages from said one riser corresponding to those defined by said first mentioned pair of conduits.
7. An intake manifold as claimed in claim 6 wherein each intake riser passage includes a distribution chamber and each conduit passage connects with its riser passage at said chamber.
8. An intake manifold as claimed in claim 6 wherein the inlet openings for the conduit passages for cylinders l, 4, 6, and 7 are peripherally spaced around the riser passage with which these passages connect and are adjacent the lower end of said passage and wherein the inlet openings for the conduit passages for cylinders 8, 5, 3, 2 are similarly disposed with respect to the riser passage with which they connect.
'9. An intake manifold as claimed in claim wherein the inlet openings of the conduit passages connecting with each riser passage are adjacent each other and wherein the said conduit passages for the pairs of cylinders 3 and 5, and 4 and 6 respectively, have a common vertical wall terminating at the riser passage with which their inlet openings are associated.
10. An intake manifold for an engine having opposite cylinder banks each including a cylinder head and four cylinders, the cylinders of one bankstarting from one end of the engine being successively numbered for reference herein 1, 3, 5, and 7 and being respectively located substantially opposite to those cylinders in the other bank which starting from the same end of the engine are numbered 2, 4, 6, and 8, said manifold comprising opposite mounting portions for mounting said manifold to said bank, a pair of longitudinally spaced intermediate portions each containing an intake riser passage, one located intermediate cylinders 5 and 8 and the other intermediate cylinders l and 4, air-fuel conduit portions connecting said intermediate portions and said mounting portions, said conduit portions providing independent air-fuel passages between one riser passage and said mounting portions for feeding cylinders l, 4, 6, and 7 and corresponding independent air-fuel passages between the other riser passage and said mounting portions for feeding cylinders 8, 5, 3, 2, said risers each including a distribution chamber into which the air-fuel passages connecting with these risers open, said chambers being in different planes, and the air-fuel passages emanating therefrom being in different planes, certain of said passages from one chamber having longitudinally extending portions which are stacked with respect to other passages from the other chamber, a pair of water conduits defining water passages extending transversely between said mounting portions in planes below said riser passages each such conduit having an upper wall portion common with the lower wall of the riser passage which it traverses and a longitudinally extending water conduit interconnecting said transverse water conduits defining a water passage -12 interconnecting said-traverse water passages, the opposite endsof said transverse water passages being open and defining water inlets and one end of said longitudinal water passage being open and defining a water outlet.
11. A manifold as claimed in claim 10 wherein said water inlet is in a portion of said longitudinally extending water conduit that extends outwardly past one of said riser passages.
12. An intake manifold for an engine having opposite cylinder banks each including a plurality of cylinders, said manifold comprising opposite portions for mounting said manifold on said engine banks, an intermediate portion on which to supporta pair of fuel supply means, conduit means connecting said mounting portions and said intermediate portion, a pair of longitudinally spaced intake riser passages on said intermediate portion for connecting with said fuel supply means, one of said riser passages being transversely adjacent an end cylinder of one bank and the other transversely adjacent the end cylinder at the opposite end of the same bank, said conduit means defining a plurality of air-fuel passages extending between said mounting portions and the risers of said inter-mediate portion, half the number of said passages connecting with one riser, and half connecting with the other riser, and metering control means interconnecting said riser passages.
13. An intake manifold for an engine having opposite cylinder banks each including a plurality of cylinders, said manifold comprising opposite portions for mounting said manifold on said engine banks, an intermediate portion on which to support a pair of fuel supply means, conduit means connecting said mounting portions and said intermediate portion, a pair of longitudinally spaced intake riser passages on said intermediate portion for connecting with said fuel supply means, one of said-riserpassages being transversely adjacent an end cylinder of one bank and the other transversely adjacent the end cylinder at the opposite end'of the same bank, said conduit means defining a plurality of air fuel passages extending between said mounting portions and the risers of said intermediate portion, half the number of said passages connecting with one riser, and half connecting with the other riser, and longitudinal passage means having a cross-sectional area of lessthan one-half square inch interconnecting said risenpassages.
14. An intake manifold for an engine having opposite cylinder banks each including a plurality of cylinders, said manifold comprising opposite portions for mounting said manifold on said engine banks, a pair of longitudinally spaced intermediate portions on which to support a pair of single barrel fuel supply means, conduit means connecting said mounting portions and said intermediate portions, each of said intermediate portions having an intake riserpassage connecting with the fuel supply means thereon and said conduit means providing air-fuel passages between said riser passages and said mounting portions, there being an independent air-fuel passage for connecting with each cylinder of the engine and half the number of said passages connecting with one riser and the remainder connecting with the other riser and tubular metering means extending between said intermediate portions and opening into said riser passages for interconnecting the same.
15. An intake manifold as-claimed in claim 14 wherein said tubular metering means comprises a plurality of tubes.
References Cited in the file of this patent UNIT ED STATES PATENTS 2,640,471 Ha'ltenberger June 2, 1953
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US445225A US2764961A (en) | 1954-07-23 | 1954-07-23 | Intake manifold structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US445225A US2764961A (en) | 1954-07-23 | 1954-07-23 | Intake manifold structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2764961A true US2764961A (en) | 1956-10-02 |
Family
ID=23768068
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US445225A Expired - Lifetime US2764961A (en) | 1954-07-23 | 1954-07-23 | Intake manifold structure |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2764961A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3303832A (en) * | 1967-02-14 | High output engines | ||
| US20130112158A1 (en) * | 2011-10-12 | 2013-05-09 | Engineered Propulsion Systems, Inc. | Aerodiesel engine |
| US11428157B2 (en) | 2017-07-21 | 2022-08-30 | General Atomics Aeronautical Systems, Inc. | Enhanced aero diesel engine |
| US11473520B2 (en) | 2011-10-05 | 2022-10-18 | General Atomics Aeronautical Systems, Inc. | Aero compression combustion drive assembly control system |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2640471A (en) * | 1950-04-24 | 1953-06-02 | Haltenberger Jules | Automobile v engine symmetrical manifold |
-
1954
- 1954-07-23 US US445225A patent/US2764961A/en not_active Expired - Lifetime
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2640471A (en) * | 1950-04-24 | 1953-06-02 | Haltenberger Jules | Automobile v engine symmetrical manifold |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3303832A (en) * | 1967-02-14 | High output engines | ||
| US11473520B2 (en) | 2011-10-05 | 2022-10-18 | General Atomics Aeronautical Systems, Inc. | Aero compression combustion drive assembly control system |
| US20130112158A1 (en) * | 2011-10-12 | 2013-05-09 | Engineered Propulsion Systems, Inc. | Aerodiesel engine |
| US9181868B2 (en) * | 2011-10-12 | 2015-11-10 | Engineered Propulsion Systems, Inc. | Aerodiesel engine |
| US9447729B2 (en) | 2011-10-12 | 2016-09-20 | Engineered Propulsion Systems, Inc. | Aerodiesel engine |
| US11428157B2 (en) | 2017-07-21 | 2022-08-30 | General Atomics Aeronautical Systems, Inc. | Enhanced aero diesel engine |
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