US3230944A - Manifold structure for internalcombustion engines - Google Patents

Manifold structure for internalcombustion engines Download PDF

Info

Publication number
US3230944A
US3230944A US392980A US39298064A US3230944A US 3230944 A US3230944 A US 3230944A US 392980 A US392980 A US 392980A US 39298064 A US39298064 A US 39298064A US 3230944 A US3230944 A US 3230944A
Authority
US
United States
Prior art keywords
cylinder
manifold
block
passageways
cast
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US392980A
Inventor
Kiekhaefer Elmer Carl
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Kiekhaefer Corp
Original Assignee
Kiekhaefer Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US118563A external-priority patent/US3176668A/en
Application filed by Kiekhaefer Corp filed Critical Kiekhaefer Corp
Priority to US392980A priority Critical patent/US3230944A/en
Application granted granted Critical
Publication of US3230944A publication Critical patent/US3230944A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/104Intake manifolds
    • F02M35/116Intake manifolds for engines with cylinders in V-arrangement or arranged oppositely relative to the main shaft
    • F02M35/1165Boxer or pancake engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B27/00Use 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B27/00Use 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
    • F02B27/005Oscillating pipes with charging achieved by arrangement, dimensions or shapes of intakes pipes or chambers; Ram air pipes
    • F02B27/006Oscillating pipes with charging achieved by arrangement, dimensions or shapes of intakes pipes or chambers; Ram air pipes of intake runners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B61/00Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing
    • F02B61/04Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing for driving propellers
    • F02B61/045Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing for driving propellers for marine engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B75/22Multi-cylinder engines with cylinders in V, fan, or star arrangement
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/10006Air 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
    • F02M35/10072Intake runners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/10091Air intakes; Induction systems characterised by details of intake ducts: shapes; connections; arrangements
    • F02M35/10131Ducts situated in more than one plane; Ducts of one plane crossing ducts of another plane
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/1015Air intakes; Induction systems characterised by the engine type
    • F02M35/10183Engines having intake ducts fed from a separate carburettor or injector, the idling system being considered as a separate carburettor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/027Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B2075/1804Number of cylinders
    • F02B2075/1808Number of cylinders two
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B2075/1804Number of cylinders
    • F02B2075/1816Number of cylinders four
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/007Other engines having vertical crankshafts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B75/24Multi-cylinder engines with cylinders arranged oppositely relative to main shaft and of "flat" type
    • F02B75/243Multi-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
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Definitions

  • the air intake manifold is manufactured as a separate component and releasably attached to the engine block with appropriate sealing gaskets therehetween 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 negative 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.
  • straight passageways having their axes parallel to the axis of the cylinder bores can be em ployed. 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.
  • the present invention thus provides an integrally formed tuned manifold system for an internal-combustion engine which is relatively low in cost and readily produced 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 22 of FIG. 3 is a side elevational view similar to FIG. 1 showing an alternative construction in accordance with the present invention.
  • FIG. 4 is a vertical section taken on lines 44 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.
  • 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 are integrally cast with the cylinder blocks 1 and 2 in vertically arranged side-by-side relation and extend from the associated carburetors 21 and 22 horizontally parallel to and aligned With the axis of the cylinders 7 and cylinder cool' ing jackets 23.
  • the lower passageways 17 and 18 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 18 when casting the cylinder blocks 1 and 2.
  • the cylinder head manifold passageways 19 and 2d 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 2%? 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 select'ed engine speed.
  • valves 13 are opened and closedto sequentially introduce air-fuel charges to the cylinders 6 and 7 from the corresponding carburetors 21 and 22.
  • a backpressure 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 efficiency of the introduction of the air-fuel charge into the cylinders 6 and 7 at the desired speed.
  • the illustrated cylinder 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 23 and 29 close the opposite ends of blocks 24 and 25.
  • a pair of carburetors 30 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 34 to the upper cylinder 2% and 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 33 through the side walls of cylinder blocks 24 and 25 and terminates in communication with a manifold passageway 35 in the head 2? for the lower cylinder 33.
  • Passageways 32 and 33 are formed in 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 3'6 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 PEG. 4.
  • a minimum amount of cast metal 39 is needed to enclose and properly support the pro-formed conduits 38 and results in a light, strong cylinder block construction.
  • the individual conduits 38 can be readily pro-formed to give the necessary configuration for establishing equal length of each manifold passageways while maintaining the passageways within the side walls of the cylinder blocks.
  • the several pro-formed conduits 33 also eliminate expensive and complicated coring of the mold for casting of the cylinder blocks 2d 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 FlGS. l 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 appearing assembly.
  • 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.
  • a cast cylinder block a head assembled with one end of said block and having a fuel inlet passage therein opening into a cylinder in said block, a cast housing member assembled with the other end of said block and providing a crank case therewith, a carburetor mounted on said cast housing member remote from said head and block in a direction generally axial of said head, pie-formed manifold liners integrally cast into the cylinder block and saidcast housing member and defining an integrally cast manifold passageway in the wall of the housing member and the cylinder block for carrying the fuel charge from the carburetor tothe inlet passage for the cylinder and being selected of a length and cross-section to tune the manifold system for a selected operating engine speed.
  • an opposed cylinder engine having back-to-back opposed cylinders in a cast cylinder block unit, individual carburetors for the opposed cylinders and mounted adjacent the opposite cylinder, and a pair of preformed manifold tubular members integrally cast into the wall of the cylinder block unit and defining manifold passageways oppositely extending from the respective can buretor and being selected of a corresponding length and cross-section to tune the manifold system for a selected operating engine speed.
  • carburetors mounted as a part of the engine for supplying a fuel mixture to at least a pair of immediately adjacent non-opposed cylinders, said carburetors being mounted on the opposite end of the engine, and a pair of integrally cast manifold passageways communicating with each carburetor and being integrally cast into the side wall of the cylinder block unit, the pair of passageways extending longitudinally and laterally within the side wall of the block unit from the carburetor to the associated cylinders and being selected of a length and cross section to tune the manifold system for a selected operating engine speed.
  • carburetors mounted as a part of the engine for supplying a fuel mixture to at least a pair of immediately adjacent non-opposed cylinders, said carburetors being mounted in alignment with one of the associated cylinders and on the opposite end of the engine, a pair of integrally cast manifold passageways communicating with each carburetor and being cast in the side wall of the cylinder block unit, one of said passageways in each pair extending longitudinally and laterally in the general form of a U-shape to connect the carburetor to the aligned cylinder, and the second of said passageways in each pair extending longitudinally and laterally to connect the carburetor to the other of the cylinders, said passageways being selected of a length and cross section to tune the manifold system for a selected operating engine speed.
  • carburetors mounted as a part of the engine for supplying a fuel mixture to a pair of immediately adjacent non-opposed cylinders, said carburetors being mounted in alignment with one of the associated cylinders and on the opposite end of the engine, and a plurality of tubular members integrally cast into the cylinder block unit and defining manifold passageways connecting each carburetor with the proper cylinders, the pair of passageways extending longitudinally and laterally within the side wall of the block unit from the carburetor to the associated cylinders and being selected of a length and cross section to tune the manifold system for a selected operating engine speed.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ocean & Marine Engineering (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

Jan. 25, 1956 E. c. KIEKHAEFER MANIFOLD STRUCTURE FOR INTERNAL-COMBUSTION ENGINES Original Filed June 21, 1961 INVENTOR. ELMER C. KIEKHAEFER 7 lndrus 92 StarKg Attorneys United States Patent 3,230,944 MANIFOLD STRUCTURE FGR INTERNAL- COMBUSTIQN ENGINES Elmer Carl Kiekhaefer, Cedar-burg, Wis, assignor, by
mesne assignments, to Kiekhaefer Corporation, Chicago, Ill., a corporation of Delaware Original application June 21, 1961, Ser. No. 118,563, now Patent No. 3,176,668, dated Apr. 6, 1965. Divided and this application July 29, 1964, Ser. No. 392,980
Claims. (Cl. 12356) This is a division of applicants copending application Serial No. 118,563 filed on June 21, 1961, now Patent No. 3,176,668 entitled Manifold Structure for Internal- Combustion Engines.
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 therehetween 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 negative 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 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 manitold 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. 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 principal plane of the cylinder block. Consequently, the structure provides a compact and neat appearing structure which can be commerically employed.
In certain designs, straight passageways having their axes parallel to the axis of the cylinder bores can be em ployed. 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 sufficient to maintain the conduits in captive relation within the block Wall and thereby forming the tuned manifold system. The use of the preformed conduits eliminates the The width and a "ice necessity to core the passageways and practically increases 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 readily produced 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 22 of 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 44 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.
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. 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 are integrally cast with the cylinder blocks 1 and 2 in vertically arranged side-by-side relation and extend from the associated carburetors 21 and 22 horizontally parallel to and aligned With the axis of the cylinders 7 and cylinder cool' ing jackets 23.
The lower passageways 17 and 18 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 18 when casting the cylinder blocks 1 and 2.
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 172@. The carburetors 21 and 22 are secured to the opposite cylinder blocks 1 and 2 in alignment with and immediately adjacent the end of the corresponding cylinder block manifold passageways l7 and 18.
Referring particularly to FIG. 2, the cylinder head manifold passageways 19 and 2d 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 2%? 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 select'ed engine speed.
In the operation of the engine, the valves 13 are opened and closedto 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 backpressure 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 efficiency of the introduction of the air-fuel charge into the cylinders 6 and 7 at the desired speed.
The illustrated cylinder 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 23 and 29 close the opposite ends of blocks 24 and 25. A pair of carburetors 30 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 34 to the upper cylinder 2% and 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.
4. 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 33 through the side walls of cylinder blocks 24 and 25 and terminates in communication with a manifold passageway 35 in the head 2? for the lower cylinder 33. Passageways 32 and 33 are formed in 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 3'6 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 PEG. 4. A minimum amount of cast metal 39 is needed to enclose and properly support the pro-formed conduits 38 and results in a light, strong cylinder block construction. The individual conduits 38 can be readily pro-formed to give the necessary configuration for establishing equal length of each manifold passageways while maintaining the passageways within the side walls of the cylinder blocks. The several pro-formed conduits 33 also eliminate expensive and complicated coring of the mold for casting of the cylinder blocks 2d and 25.
In operation, the illustrated embodiment of FIGS. 3 and 4 is the same as that of the embodiment of FlGS. l 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 appearing assembly. 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:
It. In an internal-combustion engine a cast cylinder block, a head assembled with one end of said block and having a fuel inlet passage therein opening into a cylinder in said block, a cast housing member assembled with the other end of said block and providing a crank case therewith, a carburetor mounted on said cast housing member remote from said head and block in a direction generally axial of said head, pie-formed manifold liners integrally cast into the cylinder block and saidcast housing member and defining an integrally cast manifold passageway in the wall of the housing member and the cylinder block for carrying the fuel charge from the carburetor tothe inlet passage for the cylinder and being selected of a length and cross-section to tune the manifold system for a selected operating engine speed.
2. In an opposed cylinder engine having back-to-back opposed cylinders in a cast cylinder block unit, individual carburetors for the opposed cylinders and mounted adjacent the opposite cylinder, and a pair of preformed manifold tubular members integrally cast into the wall of the cylinder block unit and defining manifold passageways oppositely extending from the respective can buretor and being selected of a corresponding length and cross-section to tune the manifold system for a selected operating engine speed.
3. In an opposed cylinder engine having a multiple of in-line opposed cylinder pairs in a cast cylinder block unit, carburetors mounted as a part of the engine for supplying a fuel mixture to at least a pair of immediately adjacent non-opposed cylinders, said carburetors being mounted on the opposite end of the engine, and a pair of integrally cast manifold passageways communicating with each carburetor and being integrally cast into the side wall of the cylinder block unit, the pair of passageways extending longitudinally and laterally within the side wall of the block unit from the carburetor to the associated cylinders and being selected of a length and cross section to tune the manifold system for a selected operating engine speed.
4. In an opposed cylinder engine having a multiple of in-line opposed cylinder pairs in a cast cylinder block unit, carburetors mounted as a part of the engine for supplying a fuel mixture to at least a pair of immediately adjacent non-opposed cylinders, said carburetors being mounted in alignment with one of the associated cylinders and on the opposite end of the engine, a pair of integrally cast manifold passageways communicating with each carburetor and being cast in the side wall of the cylinder block unit, one of said passageways in each pair extending longitudinally and laterally in the general form of a U-shape to connect the carburetor to the aligned cylinder, and the second of said passageways in each pair extending longitudinally and laterally to connect the carburetor to the other of the cylinders, said passageways being selected of a length and cross section to tune the manifold system for a selected operating engine speed.
5. In an opposed cylinder engine having a multiple of in-line opposed cylinder pairs in a cast cylinder block unit, carburetors mounted as a part of the engine for supplying a fuel mixture to a pair of immediately adjacent non-opposed cylinders, said carburetors being mounted in alignment with one of the associated cylinders and on the opposite end of the engine, and a plurality of tubular members integrally cast into the cylinder block unit and defining manifold passageways connecting each carburetor with the proper cylinders, the pair of passageways extending longitudinally and laterally within the side wall of the block unit from the carburetor to the associated cylinders and being selected of a length and cross section to tune the manifold system for a selected operating engine speed.
References Cited by the Examiner UNITED STATES PATENTS 1,190,252 7/1916 Fornaca 12359 1,442,510 1/1923 Aitkin 12356 1,903,607 4/1933 Moorhouse 123-52 2,506,250 5/1950 Taub 12356 2,963,009 12/1960 Dolza 123-52 X FOREIGN PATENTS 863,570 1/1953 Germany.
MARK NEWMAN, Primary Examiner.
FRED E. ENGELTHALER, Examiner.

Claims (1)

1. IN AN INTERNAL-COMBUSTION ENGINE A CAST CYLINDER BLOCK, A HEAD ASSEMBLED WITH ONE END OF SAID BLOCK AND HAVING A FUEL INLET PASSAGE THEREIN OPENING INTO A CYLINDER IN SAID BLOCK, A CAST HOUSING MEMBER ASSEMBLED WITH THE OTHER END OF SAID BLOCK AND PROVIDING A CRANK CASE THEREWITH, A CARBURETOR MOUNTED ON SAID CAST HOUSING MEMBER REMOTE FROM SAID HEAD AND BLOCK IN A DIRECTION GENERALLY AXIAL OF SAID HEAD, PRE-FORMED MANIFOLD LINERS INTEGRALLY CAST INTO THE CYLINDER BLOCK AND SAID CAST HOUSING MEMBER AND DEFINING AN INTEGRALLY CAST MANIFOLD PASSAGEWAY IN THE WALL OF THE HOUSING MEMBER AND THE CYLINDER BLOCK FOR CARRYING THE FUEL CHARGE FROM THE CARBURETOR TO THE INLET PASSAGE FOR THE CYLINDER AND BEING SELECTED OF A LENGTH AND CROSS-SECTION TO TUNE THE MANIFOLD SYSTEM FOR A SELECTED OPERATING ENGINE SPEED.
US392980A 1961-06-21 1964-07-29 Manifold structure for internalcombustion engines Expired - Lifetime US3230944A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US392980A US3230944A (en) 1961-06-21 1964-07-29 Manifold structure for internalcombustion engines

Applications Claiming Priority (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

Publications (1)

Publication Number Publication Date
US3230944A true US3230944A (en) 1966-01-25

Family

ID=26816505

Family Applications (1)

Application Number Title Priority Date Filing Date
US392980A Expired - Lifetime US3230944A (en) 1961-06-21 1964-07-29 Manifold structure for internalcombustion engines

Country Status (1)

Country Link
US (1) US3230944A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4026377A (en) * 1975-12-02 1977-05-31 Allis-Chalmers Corporation Vertical crankshaft engine having longitudinally opposed cylinders
US4373475A (en) * 1980-12-18 1983-02-15 Outboard Marine Corporation Internal combustion engine
US4893597A (en) * 1989-04-24 1990-01-16 Tecumseh Products Company Engine cylinder assembly having an intake cross-passageway
US4898144A (en) * 1985-03-30 1990-02-06 Yamaha Hatsudoki Kabushiki Kaisha Intake system for internal combustion engine

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1190252A (en) * 1909-12-17 1916-07-04 F I A T Combustion-engine.
US1442510A (en) * 1922-06-28 1923-01-16 Andrew W Aitken Internal-combustion engine
US1903607A (en) * 1928-05-10 1933-04-11 Packard Motor Car Co Internal combustion engine
US2506250A (en) * 1946-04-22 1950-05-02 Taub Engine Corp Internal-combustion engine
DE863570C (en) * 1950-12-16 1953-01-19 Nsu Werke Ag Internal combustion engine
US2963009A (en) * 1955-01-19 1960-12-06 Gen Motors Corp Engine

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1190252A (en) * 1909-12-17 1916-07-04 F I A T Combustion-engine.
US1442510A (en) * 1922-06-28 1923-01-16 Andrew W Aitken Internal-combustion engine
US1903607A (en) * 1928-05-10 1933-04-11 Packard Motor Car Co Internal combustion engine
US2506250A (en) * 1946-04-22 1950-05-02 Taub Engine Corp Internal-combustion engine
DE863570C (en) * 1950-12-16 1953-01-19 Nsu Werke Ag Internal combustion engine
US2963009A (en) * 1955-01-19 1960-12-06 Gen Motors Corp Engine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4026377A (en) * 1975-12-02 1977-05-31 Allis-Chalmers Corporation Vertical crankshaft engine having longitudinally opposed cylinders
US4373475A (en) * 1980-12-18 1983-02-15 Outboard Marine Corporation Internal combustion engine
US4898144A (en) * 1985-03-30 1990-02-06 Yamaha Hatsudoki Kabushiki Kaisha Intake system for internal combustion engine
US4893597A (en) * 1989-04-24 1990-01-16 Tecumseh Products Company Engine cylinder assembly having an intake cross-passageway

Similar Documents

Publication Publication Date Title
US4244332A (en) Induction system for a V-type two-cycle engine
US4284037A (en) Internal combustion engine coolant system
US5829402A (en) Induction system for engine
US6978744B2 (en) Two-cycle combustion engine with air scavenging system
US4951465A (en) Exhaust system for multi-cylinder engine
US4369627A (en) Internal combustion engine
GB1263979A (en) Air-cooled internal combustion engine with soundproofing casing
US5778833A (en) Water vehicle having a "V" shaped multi-cylinder crankcase scavenging engine
JPS6315542Y2 (en)
US5899177A (en) Four-cycle marine engine
US5524579A (en) Air cooled rotary distribution valve for internal combustion engine
US3230944A (en) Manifold structure for internalcombustion engines
US3813880A (en) Exhaust tuning system for two-stroke engines
US3400695A (en) Internal combustion engine and cylinder block
US5690069A (en) Internal combustion engine having rotary distribution valves
US6408809B2 (en) Intake control device for multi-cylinder V-type engine
US4920933A (en) V-shaped two cycle engine for outboard
JP3271502B2 (en) V-type 4-cycle engine for outboard motor
JPS6042333B2 (en) V type engine
JP2003129921A (en) Four-cycle engine for outboard engine
US3176668A (en) Manifold structure for internalcombustion engines
US4408579A (en) Induction system for a two-cycle engine
US2759463A (en) High torque v-8 engines
US3020707A (en) Engine exhaust manifold construction
US2056056A (en) Engine cylinder