US3176668A - Manifold structure for internalcombustion engines - Google Patents
Manifold structure for internalcombustion engines Download PDFInfo
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- US3176668A US3176668A US118563A US11856361A US3176668A US 3176668 A US3176668 A US 3176668A US 118563 A US118563 A US 118563A US 11856361 A US11856361 A US 11856361A US 3176668 A US3176668 A US 3176668A
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- passageways
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- cylinders
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- 238000002485 combustion reaction Methods 0.000 description 8
- 238000005266 casting Methods 0.000 description 7
- 239000000446 fuel Substances 0.000 description 7
- 238000010276 construction Methods 0.000 description 6
- 239000002184 metal Substances 0.000 description 4
- 239000000203 mixture Substances 0.000 description 3
- 238000004891 communication Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000006677 Appel reaction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000004512 die casting Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000007789 sealing Methods 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
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/104—Intake manifolds
- F02M35/116—Intake manifolds for engines with cylinders in V-arrangement or arranged oppositely relative to the main shaft
- F02M35/1165—Boxer or pancake engines
-
- 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
- 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
-
- 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
- F02B61/00—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing
- F02B61/04—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing for driving propellers
- F02B61/045—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing for driving propellers for marine engines
-
- 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
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/10006—Air intakes; Induction systems characterised by the position of elements of the air intake system in direction of the air intake flow, i.e. between ambient air inlet and supply to the combustion chamber
- F02M35/10072—Intake runners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/10242—Devices or means connected to or integrated into air intakes; Air intakes combined with other engine or vehicle parts
- F02M35/10288—Air intakes combined with another engine part, e.g. cylinder head cover or being cast in one piece with the exhaust manifold, cylinder head or engine block
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/10314—Materials for intake systems
- F02M35/10327—Metals; Alloys
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/1034—Manufacturing and assembling intake systems
- F02M35/10347—Moulding, casting or the like
-
- 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
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
-
- 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
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/027—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
-
- 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
- F02B2075/1808—Number of cylinders two
-
- 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
- F02B2075/1816—Number of cylinders four
-
- 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
- F02B75/24—Multi-cylinder engines with cylinders arranged oppositely relative to main shaft and of "flat" type
- F02B75/243—Multi-cylinder engines with cylinders arranged oppositely relative to main shaft and of "flat" type with only one crankshaft of the "boxer" type, e.g. all connecting rods attached to separate crankshaft bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/1015—Air intakes; Induction systems characterised by the engine type
- F02M35/10183—Engines having intake ducts fed from a separate carburettor or injector, the idling system being considered as a separate carburettor
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- 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 a manifold structure for an internal-combustion engine and particularly to a tuned inlet manifold integrally cast within the cylinder and head of the internal-combustion engine.
- the air intake manifold is manufactured as a separate component and releasably attached to the engine block with appropriate sealing gaskets therebetween to establish a hermetic joint. This is particularly true in internal-combustion engines where the exhaust and manifold system is tuned to a specific resonance to increase the efficiency of the system.
- the pulses which are present in the exhaust system are then also present at a negative pressure in the intake manifold.
- the nega-V tive pressure or vacuum developed within the intake manifold tends to destroy the gasket after long periods of use and disrupts the vacuum and the resultant air-fuel mixture.
- the present invention is directed to an integrally cast manifold system having individual passageways for proper tuning to the desired operating speed and more particularly to an integrally cast manifold system for horizontally opposed cylinder engines.
- the inlet manifold passageways are integrally cast into the side of the cylinder block assembly.
- the carburetor of each cylinder is mounted on the opposite end of the cylinder block assembly or-the opposite cylinder head.
- the manifold passageways extend across the cylinder block assembly completely within the wall thereof.
- the width and length of the block of an opposed cylinder engine allows sufficient room for establishing the necessary and equal lengths of each of the manifold conduits by curving the passageway in the plane of the block wall and without projecting the passageways outwardly from the principle plane of the cylinder block. Consequently, the structure provides a compact and neat appearing structure which can be commercially employed.
- straight passageways having their axes parallel to the axis of the cylinder bores can be employed. This permits simple casting production because the manifold passageways can be formed by the same cores as the cylinder bores and the water jackets. Therefore, the casting is not unduly expensive.
- Preformed conduits of a material capable of withstanding the heat and pressure developed can also be cast within the cylinder block when die casting'the block.
- the preformed conduits are secured within the mold and enclosed within a minimum amount of casting metal sulficient to maintain the conduits in captive relation with- 3,12%,653 Patented Apr. 6, 1965 'ice in the block wall and thereby forming the tuned manifold system.
- the use of the preformed conduits eliminates the necessity to core the passageways and practically in-, creases the latitude in the configuration in which the individual conduits can be formed in order to provide equal length for the purposes of tuning the entire manifold system to the selected resonant frequency. Because the encircling casting metal need only hold the preformed conduit in place, a relatively light and strong construction can be employed.
- the present invention thus provides an integrally formed tuned manifold system for an internal-combustion engine which is relatively low in cost and readilyproduced as a compact, pleasant appearing unit.
- FIG. 1 is a side elevational view of an opposed cylinder type engine
- FIG. 2 is a horizontal section taken on lines 2-2 of FIG. 1;
- FIG. 3 is a side elevational view similar to FIG. 1-
- FIG. 4 is a vertical section taken on lines 4-4. of FIG. 3.
- an internal-combustion opposed cylinder engine including a left cylinder block 1 and a right cylinder block 2 bolted or otherwise secured in back-toback relation.
- a common crankcase 3 is defined by the adjoining portions of the cylinder blocks 1 and 2 rotatably housing a crankshaft 4 which extends downwardly as a drive shaft 5.
- Each of the cylinder blocks 1 and 2 includes a pair of horizontally opposed cylinders 6 and 7 vertically spaced within the forward or outer portion thereof to form a four cylinder engine.
- the opposed cylinders 6 and the opposed cylinders 7 in the blocks 1 and 2 are vertically. offset with pistons 8 slidably disposed one within each of the cylinders.
- Piston rods 9 connect the opposed pistons 8 to the common crankshaft 3.
- V 7 7 Cylinder heads 10 and 11 are secured respectively to the ends of the cylinder blocks 1 and 2 as by bolts 12 in accordance with known construction.
- Each of the heads 10 and 11 includes a pair of valves 13 one for each of the cylinders 6 and 7.
- Valves 13 are operated through an engine-driven valve positioner or tappet unit 14 each of which is coupled to an engine-driven cam 15 by a rigid link 16.
- Cams 15 are driven in synchronism with the crankshaft 4 to properly open and close valves 13 for sequentially admitting a mixture of air and fuel to the corresponding cylinders 6 or 7 in' timed relation with the movement of the corresponding pistons 8..
- the lower opposed cylinders 6 and the upper opposed cylinders 7 are provided with similar inlet manifold systems and only upper opposed cylinders 7 are particularly described hereinafter. Corresponding elements for' the cylinders 6 are similarly numbered for purposes of simplicity and clarity of description.
- a pair of individual cylinder block manifold passageways 17 and 18 and a pair of related cylinder head manifold passageways 19 and 20 form individual continuous air-fuel charge passageways for introducing the air-fuel charge to the upper cylinders 7 from suitable carburetors 21 and 22.
- the cylinder block manifold passageways 17 and 18 i are integrally cast with the cylinder blocks 1 and 2 in vertically arranged side-by-siderelation and extend from the associated carburetors 21 and 22 horizontally parallel to and aligned with the axis of the cylinders 7 and cylinder cooling jackets 23.'
- the lower passageways17 and18 are similarly located with respect to the lower opposed cylinder 6 as shown in FIG. 1.
- the parallel construction permits relatively simple casting of the manifold passageways 17 and 13 when casting the cylinder blocks 1 and 2.
- individual carburetors 21 and 22 are provided for each of the opposed cylinders 7 and are properly connected by the individual passageways defined by passageways 17-2t).
- the carburetors 21 and 22 are secured to the opposite cylinder blocks 1 and 2 in alginment with and immediately adjacent the end of the corresponding cylinder block manifold passageways 17 and. 18.
- the cylinder head manifold passageways 19 and 20 are integrally cast in the heads 10 and 11 as substantially U-shaped passages terminating in alignment with the corresponding opposed cylinders 7 at one end and with the cylinder block passageways 17 and 18 at the opposite end.
- the manifold passageways at the inlet end slant slightly upwardly in the left hand head 10 and downwardly in the right hand head 11 to align the inlet end of each passageway 19 and 20 with the adjacent end of passageways 17 and 18.
- the complete inlet manifold passageways thus defined are similarly of a given length and diameter to tune the inlet manifold system to a predetermined resonance in accordance with the pulse frequency developed at a selected engine speed.
- valves 13 are opened and closed to sequentially introduce air-fuel charges to the cylinders 6 and 7 from the corresponding carburetors 21 and 22.
- a backpressurized pulse wave is developed.
- the tuned manifold passageways, defined by the integrally cast passageways 17-20, correlate the introduction of the air-fuel charge into the cylinders 6 and 7 at the negative portion of the pulse wave when the engine is operating at the selected resonant speed. This produces maximum eificiency of the introduction of the air-fuel charge into the cylinders 6 and 7 at the desired speed.
- the illustratedcylinder block passageways 17 and 18 are integrally cast completely within the side Walls of the opposed cylinder blocks 1 and 2 .to provide a compact and practical construction.
- the tuned passageways are generally straight and parallel to the axes of the cylinders '6 and 7 and may therefore be readily cast by the same cores. which form the cylinders 6 and 7 and water jackets 23.
- FIGS. 3 and 4 illustrate a similar opposed four-cylinder engine wherein the desired tuning demands inlet passageways longer than the width of the cylinder block structure.
- a pair of back-to-back cylinder blocks 24 and 25 also includes opposed upper cylinders 26 and opposed lower cylinders 27. Cylinder heads 28 and 29 close the opposite ends of blocks 24 and 25.
- a pair of carburetors 3t) and 31 are mounted one each on the heads 28 and 29. Each carburetor 30 and 31 supplies a desired mixture to the pair of vertically arranged cylinders 26 and 27 in the opposite cylinder blocks 24 and 25.
- An upper cylinder manifold passageway 32 and a separate lower manifold passageway 33 are integrally cast in the side walls of cylinder blocks 24 and 25.
- Passageway 32 connects carburetor 30 to the upper cylinder 26 and 4 passageway 33 connects carburetor 30 to the lower cylinder 27 in the block 25.
- the upper cylinder manifold passageway 32 extends through the side walls of cylinder blocks 24 and 25 and initially curves downwardly through cylinder block 24 and the initial portion of the opposite cylinder block 25. Thereafter, passageway 32 curves upwardly defining a generally U-shaped passageway terminating in communication with a manifold passageway 34 in the head 29.
- the curved configuration increases the length of the manifold passageway 32 to allow any desired tuning.
- the lower cylinder manifold passageway 33 extends longitudinally and continuously downwardly from the carburetor 36 through the side walls of cylinder blocks 24 and, 25 and terminates in communication with a manifold passageway 35 in the head 29 for the lower cylinder 33.
- Passageways 32 and 33 are formed of the same length and diameter to establish similar tuning of the cylinders 26 and 27 in the cylinder block 25.
- the opposite carburetor 31 is secured to head 29.
- Each of the manifold passageways 32, 33, 36 and 37 includes an inner metallic conduit 38 integrally connected and captured within the side walls of the cylinder blocks 24 and 25 by a relatively thin thickness-of cast metal 39, as most clearly shown in FIG. 4.
- a minimum amount of cast metal 39 is needed to enclose and properly support the pre-formed conduits 38 and results in a light, strong cylinder block construction.
- the individual conduits 38 can be readily pre-formed to give the necessary configuration for establishing equal length of each manifold passageway while maintaining the passageways within the side walls of the cylinder blocks.
- the several preformed conduits 38 also eliminate expensive and complicated coring of the mold for casting of the cylinder blocks 24 and 25.
- FIGS. 3 and 4 In operation, the illustrated embodiment of FIGS. 3 and 4 is the same as that of the embodiment of FIGS. 1 and 2 and no further description thereof is given.
- the present invention provides an improved opposed cylinder engine having a tuned intake manifold system integrally formed with the block structure in a compact and neat appearingassemblyj
- the manifold passageway may be provided with a curved configuration to properly and similarly tune all cylinders without unsightly projections formed as a part of the engine structure and in an inexpensive manufacturing process.
- carburetors for each of the opposed cylinder blocks and mounted adjacent the opposite cylinder block, and a pair of manifold passageways integrally formed in the wall of the cylinder block assembly oppositely extending from the respective carburetor and being selected of a corresponding length and cross-section to tune the manifold system for a selected operating engine speed.
- an opposed cylinder engine having a pair of cylinders in a cast cylinder block unit, an individual carburetor for each cylinder being mounted on the block unit adjacent the other opposed cylinder of the cylinder pair, and manifold passageways integrally cast in the wall of the block unit connecting each carburetor to a proper cylinder and such passageways being selected. with a length and cross-section tuning the manifold system for a selected operating engine speed.
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- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Ocean & Marine Engineering (AREA)
- Characterised By The Charging Evacuation (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Description
April 6, 1965 E. c. KIEKHAEFER MANIFOLD STRUCTURE FOR INTERNAL-COMBUSTION ENGINES Filed June 21, 1961 ig} 3 INVENTOR. ELMER c. KIEKHAEFER BY fi drus 9' Stun-lie Attorneys United States Patent 3,17 6,668 MANWQLD STRUCTURE FQR INTERNAL- COMBUSTION ENGINES Elmer Carl Kiekhaefer, Cedarhurg, Wis, assignor, by
mesne assignments, to Kiekhaefer Corporation, Chicago, 111., a corporation of Delaware Filed June 21, 1961, Ser. No. 118,563 3 Claims. (Cl. 123--56) This invention relates to a manifold structure for an internal-combustion engine and particularly to a tuned inlet manifold integrally cast within the cylinder and head of the internal-combustion engine.
Generally, the air intake manifold is manufactured as a separate component and releasably attached to the engine block with appropriate sealing gaskets therebetween to establish a hermetic joint. This is particularly true in internal-combustion engines where the exhaust and manifold system is tuned to a specific resonance to increase the efficiency of the system. The pulses which are present in the exhaust system are then also present at a negative pressure in the intake manifold. The nega-V tive pressure or vacuum developed within the intake manifold tends to destroy the gasket after long periods of use and disrupts the vacuum and the resultant air-fuel mixture.
A practical problem encountered in providing individual tuned intake systems has been the provision of equal lengths of conduit to each of the cylinders Without the resulting manifold system including a great number of projections in order to provide the proper length of the individual conduits.
The present invention is directed to an integrally cast manifold system having individual passageways for proper tuning to the desired operating speed and more particularly to an integrally cast manifold system for horizontally opposed cylinder engines.
In accordance with the present invention, the inlet manifold passageways are integrally cast into the side of the cylinder block assembly. The carburetor of each cylinder is mounted on the opposite end of the cylinder block assembly or-the opposite cylinder head. The manifold passageways extend across the cylinder block assembly completely within the wall thereof. The width and length of the block of an opposed cylinder engine allows sufficient room for establishing the necessary and equal lengths of each of the manifold conduits by curving the passageway in the plane of the block wall and without projecting the passageways outwardly from the principle plane of the cylinder block. Consequently, the structure provides a compact and neat appearing structure which can be commercially employed.
In certain designs, straight passageways having their axes parallel to the axis of the cylinder bores can be employed. This permits simple casting production because the manifold passageways can be formed by the same cores as the cylinder bores and the water jackets. Therefore, the casting is not unduly expensive.
Preformed conduits of a material capable of withstanding the heat and pressure developed can also be cast within the cylinder block when die casting'the block. The preformed conduits are secured within the mold and enclosed within a minimum amount of casting metal sulficient to maintain the conduits in captive relation with- 3,12%,653 Patented Apr. 6, 1965 'ice in the block wall and thereby forming the tuned manifold system. The use of the preformed conduits eliminates the necessity to core the passageways and practically in-, creases the latitude in the configuration in which the individual conduits can be formed in order to provide equal length for the purposes of tuning the entire manifold system to the selected resonant frequency. Because the encircling casting metal need only hold the preformed conduit in place, a relatively light and strong construction can be employed.
The present invention thus provides an integrally formed tuned manifold system for an internal-combustion engine which is relatively low in cost and readilyproduced as a compact, pleasant appearing unit.
The drawings furnished herewith illustrate the best mode presently contemplated for carrying out the invention.
In the drawings:
FIG. 1 is a side elevational view of an opposed cylinder type engine;
FIG. 2 is a horizontal section taken on lines 2-2 of FIG. 1;
FIG. 3 is a side elevational view similar to FIG. 1-
showing an alternative construction in accordance with the present invention; and
FIG. 4 is a vertical section taken on lines 4-4. of FIG. 3.
Referring to the drawings'and particularly to FIGS. 1 and 2, an internal-combustion opposed cylinder engine is illustrated including a left cylinder block 1 and a right cylinder block 2 bolted or otherwise secured in back-toback relation. A common crankcase 3 is defined by the adjoining portions of the cylinder blocks 1 and 2 rotatably housing a crankshaft 4 which extends downwardly as a drive shaft 5. i
Each of the cylinder blocks 1 and 2 includes a pair of horizontally opposed cylinders 6 and 7 vertically spaced within the forward or outer portion thereof to form a four cylinder engine. The opposed cylinders 6 and the opposed cylinders 7 in the blocks 1 and 2 are vertically. offset with pistons 8 slidably disposed one within each of the cylinders. Piston rods 9 connect the opposed pistons 8 to the common crankshaft 3. V 7 7 Cylinder heads 10 and 11 are secured respectively to the ends of the cylinder blocks 1 and 2 as by bolts 12 in accordance with known construction. Each of the heads 10 and 11 includes a pair of valves 13 one for each of the cylinders 6 and 7. .Valves 13 are operated through an engine-driven valve positioner or tappet unit 14 each of which is coupled to an engine-driven cam 15 by a rigid link 16.. Cams 15 are driven in synchronism with the crankshaft 4 to properly open and close valves 13 for sequentially admitting a mixture of air and fuel to the corresponding cylinders 6 or 7 in' timed relation with the movement of the corresponding pistons 8..
The lower opposed cylinders 6 and the upper opposed cylinders 7 are provided with similar inlet manifold systems and only upper opposed cylinders 7 are particularly described hereinafter. Corresponding elements for' the cylinders 6 are similarly numbered for purposes of simplicity and clarity of description.
A pair of individual cylinder block manifold passageways 17 and 18 and a pair of related cylinder head manifold passageways 19 and 20 form individual continuous air-fuel charge passageways for introducing the air-fuel charge to the upper cylinders 7 from suitable carburetors 21 and 22.
The cylinder block manifold passageways 17 and 18 i are integrally cast with the cylinder blocks 1 and 2 in vertically arranged side-by-siderelation and extend from the associated carburetors 21 and 22 horizontally parallel to and aligned with the axis of the cylinders 7 and cylinder cooling jackets 23.'
The lower passageways17 and18 are similarly located with respect to the lower opposed cylinder 6 as shown in FIG. 1. The parallel construction permits relatively simple casting of the manifold passageways 17 and 13 when casting the cylinder blocks 1 and 2. a
In the embodiment of FIG. 1, individual carburetors 21 and 22 are provided for each of the opposed cylinders 7 and are properly connected by the individual passageways defined by passageways 17-2t). The carburetors 21 and 22 are secured to the opposite cylinder blocks 1 and 2 in alginment with and immediately adjacent the end of the corresponding cylinder block manifold passageways 17 and. 18.
Referring particularly to FIG. 2, the cylinder head manifold passageways 19 and 20 are integrally cast in the heads 10 and 11 as substantially U-shaped passages terminating in alignment with the corresponding opposed cylinders 7 at one end and with the cylinder block passageways 17 and 18 at the opposite end. The manifold passageways at the inlet end slant slightly upwardly in the left hand head 10 and downwardly in the right hand head 11 to align the inlet end of each passageway 19 and 20 with the adjacent end of passageways 17 and 18.
The complete inlet manifold passageways thus defined are similarly of a given length and diameter to tune the inlet manifold system to a predetermined resonance in accordance with the pulse frequency developed at a selected engine speed.
In the operation of the engine, the valves 13 are opened and closed to sequentially introduce air-fuel charges to the cylinders 6 and 7 from the corresponding carburetors 21 and 22. At each intake portion of the cycle, a backpressurized pulse wave is developed. The tuned manifold passageways, defined by the integrally cast passageways 17-20, correlate the introduction of the air-fuel charge into the cylinders 6 and 7 at the negative portion of the pulse wave when the engine is operating at the selected resonant speed. This produces maximum eificiency of the introduction of the air-fuel charge into the cylinders 6 and 7 at the desired speed.
The illustratedcylinder block passageways 17 and 18 are integrally cast completely within the side Walls of the opposed cylinder blocks 1 and 2 .to provide a compact and practical construction. The tuned passageways are generally straight and parallel to the axes of the cylinders '6 and 7 and may therefore be readily cast by the same cores. which form the cylinders 6 and 7 and water jackets 23.
FIGS. 3 and 4 illustrate a similar opposed four-cylinder engine wherein the desired tuning demands inlet passageways longer than the width of the cylinder block structure.
In FIGS. 3 and 4, a pair of back-to-back cylinder blocks 24 and 25 also includes opposed upper cylinders 26 and opposed lower cylinders 27. Cylinder heads 28 and 29 close the opposite ends of blocks 24 and 25. A pair of carburetors 3t) and 31 are mounted one each on the heads 28 and 29. Each carburetor 30 and 31 supplies a desired mixture to the pair of vertically arranged cylinders 26 and 27 in the opposite cylinder blocks 24 and 25.
The carburetor 30, which is shown secured to the head 28, is mounted adjacent the upper portion of the head. An upper cylinder manifold passageway 32 and a separate lower manifold passageway 33 are integrally cast in the side walls of cylinder blocks 24 and 25. Passageway 32 connects carburetor 30 to the upper cylinder 26 and 4 passageway 33 connects carburetor 30 to the lower cylinder 27 in the block 25.
The upper cylinder manifold passageway 32 extends through the side walls of cylinder blocks 24 and 25 and initially curves downwardly through cylinder block 24 and the initial portion of the opposite cylinder block 25. Thereafter, passageway 32 curves upwardly defining a generally U-shaped passageway terminating in communication with a manifold passageway 34 in the head 29. The curved configuration increases the length of the manifold passageway 32 to allow any desired tuning.
The lower cylinder manifold passageway 33 extends longitudinally and continuously downwardly from the carburetor 36 through the side walls of cylinder blocks 24 and, 25 and terminates in communication with a manifold passageway 35 in the head 29 for the lower cylinder 33. Passageways 32 and 33 are formed of the same length and diameter to establish similar tuning of the cylinders 26 and 27 in the cylinder block 25.
The opposite carburetor 31 is secured to head 29.
and is similarly connected by manifold passageways 36 and 37 to cylinders 26 and 27 in cylinder block 24.
Each of the manifold passageways 32, 33, 36 and 37 includes an inner metallic conduit 38 integrally connected and captured within the side walls of the cylinder blocks 24 and 25 by a relatively thin thickness-of cast metal 39, as most clearly shown in FIG. 4. A minimum amount of cast metal 39 is needed to enclose and properly support the pre-formed conduits 38 and results in a light, strong cylinder block construction. The individual conduits 38 can be readily pre-formed to give the necessary configuration for establishing equal length of each manifold passageway while maintaining the passageways within the side walls of the cylinder blocks. The several preformed conduits 38 also eliminate expensive and complicated coring of the mold for casting of the cylinder blocks 24 and 25.
In operation, the illustrated embodiment of FIGS. 3 and 4 is the same as that of the embodiment of FIGS. 1 and 2 and no further description thereof is given.
Although the present invention has been described as a component part of an outboard motor, the invention is equally applicable to all other internal-combustion engines wherein the manifold system is to be tuned to a selected operating speed.
The present invention provides an improved opposed cylinder engine having a tuned intake manifold system integrally formed with the block structure in a compact and neat appearingassemblyj The manifold passageway may be provided with a curved configuration to properly and similarly tune all cylinders without unsightly projections formed as a part of the engine structure and in an inexpensive manufacturing process.
Various modes of carrying out the invention are contemplated as being within the scope of the following claims particularly pointing out and distinctly claiming the subject matter which is regarded as the invention.
I claim:
1. In an opposed cylinder engine having back-to-back opposed cylinder blocks in a cylinder block assembly, carburetors for each of the opposed cylinder blocks and mounted adjacent the opposite cylinder block, and a pair of manifold passageways integrally formed in the wall of the cylinder block assembly oppositely extending from the respective carburetor and being selected of a corresponding length and cross-section to tune the manifold system for a selected operating engine speed.
2. In an opposed cylinder engine having a pair of cylinders in a cast cylinder block unit, an individual carburetor for each cylinder being mounted on the block unit adjacent the other opposed cylinder of the cylinder pair, and manifold passageways integrally cast in the wall of the block unit connecting each carburetor to a proper cylinder and such passageways being selected. with a length and cross-section tuning the manifold system for a selected operating engine speed.
3. In an opposed cylinder engine having a multiple of opposed cylinder pairs in a cast cylinder block unit, an individual carburetor for each cylinder being mounted on the block unit adjacent the other opposed cylinder of each cylinder pair, and straight manifold passageways inte 5 grally cast in the side wall of the block unit with an axis parallel to the cylinders and connecting each carburetor to a proper cylinder and such passageways being selected with a length and cross-section tuning the manifold system for a selected operating engine speed. 10
References Cited by the Examiner UNlTED STATES PATENTS 1,190,252 7/16 Fornaca 12359 1,247,318 11/17 Nelson 123-59 15 5 Appel 12359 Fekete 12352 Bastien 123-52 Turlay 12352 Chayne et a1 123-52 X Dolza 123-52 X Rohm 12356 X FOREIGN PATENTS 2/40 Great Britain.
FRED E. ENGELTHALER, Primary Examiner.
KARL J. ALBRECHT, RICHARD B. WILKINSON,
Examiners.
Claims (1)
1. IN AN OPPOSED CYLINDER ENGINE HAVING BACK-TO-BACK OPPOSED CYLINDER BLOCKS IN A CYLINDER BLOCK ASSEMBLY, CARBURETORS FOR EACH OF THE OPPOSED CYLINDER BLOCKS AND MOUNTED ADJACENT THE OPPOSITE CYLINDER BLOCK, AND A PAIR OF MANIFOLD PASSAGEWAYS INTEGRALLY FORMED IN THE WALL OF THE CYLINDER BLOCK ASSEMBLY OPPOSITELY EXTENDING FROM THE RESPECTIVE CARBURETOR AND BEING SELECTED OF A CORRESPONDING LENGTH AND CROSS-SECTION TO TUNE THE MANIFOLD SYSTEM FOR A SELECTED OPERATING ENGINE SPEED.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US118563A US3176668A (en) | 1961-06-21 | 1961-06-21 | Manifold structure for internalcombustion engines |
| US392980A US3230944A (en) | 1961-06-21 | 1964-07-29 | Manifold structure for internalcombustion engines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US118563A US3176668A (en) | 1961-06-21 | 1961-06-21 | Manifold structure for internalcombustion engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3176668A true US3176668A (en) | 1965-04-06 |
Family
ID=22379380
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US118563A Expired - Lifetime US3176668A (en) | 1961-06-21 | 1961-06-21 | Manifold structure for internalcombustion engines |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3176668A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040123938A1 (en) * | 2002-12-26 | 2004-07-01 | Neculescu Cristian M. | Method of making strand-reinforced elastomeric composites |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1190252A (en) * | 1909-12-17 | 1916-07-04 | F I A T | Combustion-engine. |
| US1247318A (en) * | 1914-12-17 | 1917-11-20 | Emil A Nelson | Internal-combustion engine. |
| US1422810A (en) * | 1922-07-18 | Internal-combustion engine | ||
| US1656051A (en) * | 1927-04-19 | 1928-01-10 | Hudson Motor Car Co | Internal-combustion engine |
| US1785108A (en) * | 1925-12-17 | 1930-12-16 | Bastien Paul | Engine |
| GB518518A (en) * | 1937-08-20 | 1940-02-29 | Audi Ag | Improvements in or relating to induction pipes for v-type internal combustion engines |
| US2725859A (en) * | 1954-01-07 | 1955-12-06 | Gen Motors Corp | Intake manifold |
| US2916027A (en) * | 1956-12-28 | 1959-12-08 | Gen Motors Corp | Charge forming means |
| US2963009A (en) * | 1955-01-19 | 1960-12-06 | Gen Motors Corp | Engine |
| US3015322A (en) * | 1960-04-18 | 1962-01-02 | Avco Corp | Air induction system for an internal combustion engine |
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1961
- 1961-06-21 US US118563A patent/US3176668A/en not_active Expired - Lifetime
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1422810A (en) * | 1922-07-18 | Internal-combustion engine | ||
| US1190252A (en) * | 1909-12-17 | 1916-07-04 | F I A T | Combustion-engine. |
| US1247318A (en) * | 1914-12-17 | 1917-11-20 | Emil A Nelson | Internal-combustion engine. |
| US1785108A (en) * | 1925-12-17 | 1930-12-16 | Bastien Paul | Engine |
| US1656051A (en) * | 1927-04-19 | 1928-01-10 | Hudson Motor Car Co | Internal-combustion engine |
| GB518518A (en) * | 1937-08-20 | 1940-02-29 | Audi Ag | Improvements in or relating to induction pipes for v-type internal combustion engines |
| US2725859A (en) * | 1954-01-07 | 1955-12-06 | Gen Motors Corp | Intake manifold |
| US2963009A (en) * | 1955-01-19 | 1960-12-06 | Gen Motors Corp | Engine |
| US2916027A (en) * | 1956-12-28 | 1959-12-08 | Gen Motors Corp | Charge forming means |
| US3015322A (en) * | 1960-04-18 | 1962-01-02 | Avco Corp | Air induction system for an internal combustion engine |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040123938A1 (en) * | 2002-12-26 | 2004-07-01 | Neculescu Cristian M. | Method of making strand-reinforced elastomeric composites |
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