US1824992A - Internal combustion engine - Google Patents

Internal combustion engine Download PDF

Info

Publication number
US1824992A
US1824992A US390167A US39016729A US1824992A US 1824992 A US1824992 A US 1824992A US 390167 A US390167 A US 390167A US 39016729 A US39016729 A US 39016729A US 1824992 A US1824992 A US 1824992A
Authority
US
United States
Prior art keywords
cylinders
valve
internal combustion
combustion engine
valves
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
US390167A
Inventor
Ray W Harroun
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.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US390167A priority Critical patent/US1824992A/en
Application granted granted Critical
Publication of US1824992A publication Critical patent/US1824992A/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
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B29/00Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/22Side valves
    • 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

  • Figure 1 is a horizontal section through the combustion chamber of an internal com- 05 bustion engine of my improved construction
  • Figure 2 is a vertical cross section on line 22 of Figure 1;
  • Figure 3 is a plan view of a multi-cylinder block embodying my improvement.
  • a and A are two adj acent'engine cylinders which have a combined volume equal to that of the single cylinder for which they are substituted.
  • B is a combustion chamber formed in an L-head on one side of the pair of cylinders A.
  • A Within this combustion chamber are arranged a single inlet port C controlled by the poppet valve D and a-pair of exhaust ports E. E, controlled by poppet valves F and F.
  • the port C is arranged centrally between the cylinders A and A so as to overlap the same, thereby shifting its axis nearer to the plane of the axes of said cylinders.
  • the exhaust ports E and E are arranged on opposite sides of the port C and preferably directly opposite their respective cylinders.
  • the port C which is of an area sufficient for the combined areas of the cylinders A A is so arranged that the gases passing from said port half way around its perimeter are free to flow in the general direction of, one
  • the two-cylinders A A act as a unit, both simultaneously receiving the combustible charge upon the lifting of the valve D and simultaneously exhausting the products of combustion upon the lifting of the valves F and F.
  • the area of the com ustion chamber in horizontal cross section need be no greater than would be required with a' single cylinder of equal volume and having one inlet and one exhaust valve and inlet and exhaust valves.
  • the depth of the explosion chamber may be reduced. This results either in higher compression without impedance to thefiow of gases between the cylinders and ports or the same compression with larger port areas.
  • a further advantage is that the cross sectional area of the connection between the cylinder and the combustion chamber is restricted which increases the turbulence in the combustible gases.
  • An internal combustion engine comprisng a pair of adjacent cylinders with. parallel axes, a common combustion chamber-having a restricted area connecting the same with said cylinders and provided with a single valve controlled inlet port arranged between and overlapping said cylinders and a pair of exhaust ports of smaller diameter arranged on opposite sides of said inlet port.
  • An internal combustion engine comprising a pair of cylinders, a common laterally off-set combustion chamber connected with said cylinders and provided with a single in let port arranged centrally between and overlapping said cylinders, and a pair of exhaust ports laterally opposite the respective cylinders, the depth of said combustion chamber being restricted to provide merely mechanical clearance for movement of the valves, and poppet valves for said inlet and exhaust ports.
  • a pair of cylinders having parallel axes, a common combustionchamber for said cylinders provided with a single valve controlled inlet port, arranged between and overlapping said cylinders and a pair of exhaust ports of smaller diameter arranged on opposite sides of said inlet port.

Description

Sept. 29, 1931. R. w. HARROUN INTERNAL COMBUSTION ENGINE Filed Sept. 3. 1929 INVENTOR 37 71472479 0517? ATTO RN EY/ Patented Sept. 29, 1931 UNITED STATES PATENT OFFICE RAY W. HARROUN, OF DETROIT, MICHIGAN INTERNAL COMBUSTION ENGINE Application filed September 3, 1929. Serial No. 390,167.
In the present state of the art with L-head internal combustion engines it is usual to arrange adjacent inlet and exhaust valves of m substantially equal area in the L and at one side of the cylinder. In order to provide free passage for the gases the valve chamber must be made of suflicient depth not only to permit of proper valve lift but also -to provide clearance over the valves for the flow of gases. Furthermore, as the gases enter and leave their respective ports on all sides of the circumfe'renceof .the valve the portion of the gases on the outer side must BIS-make a quick bend to return over the valve in the direction ofthe bylinden- Thus with such construct-ions the free flow of the gases is impeded while the necessary clearance above the valves increases the volume of the compression chamber so as to reduce the height of the compression. Another difficulty encountered is the increased tendency to a detonation incident to higher compressions, particularly where the piston and ex- -haust valve are of relatively large diameter. With my improved construction I have avoided the difiiculties as above outlined, first by substituting for a single cylinder and its compression chamber a pair ofcylinders -of smaller diameters but of combined equal area and a single compression chamber com-H municating with both cylinders: second, by aconstruction and arrangement of valves such that thegases are free to pass between the cylinders and the valve ports without any sharp change in direction or the necessity o the intake gases passing over the top of the inlet valve: third, by the use of a single inlet -valve for both cylinders, said valve being arranged centrally within the combustion chamber intermediate said cylinders; fourth, by the use of a pair of exhaust valves on opposite sides of'the inlet valve and so located as to be bathed by the flow of inlet gases to the cylinder, thereby facilitating the dissi- 1 pation of heat. This arrangement permits of considerably reducing the volume of the compression chamber while still providing the requisite clearance for valve lift. My invention therefore consists in this improved construction and further in various specific features as hereinafter set forth.
In the drawings: Figure 1 is a horizontal section through the combustion chamber of an internal com- 05 bustion engine of my improved construction;
Figure 2 is a vertical cross section on line 22 of Figure 1;
, Figure 3 is a plan view of a multi-cylinder block embodying my improvement.
As illustrated, A and A are two adj acent'engine cylinders which have a combined volume equal to that of the single cylinder for which they are substituted. B is a combustion chamber formed in an L-head on one side of the pair of cylinders A. A. Within this combustion chamber are arranged a single inlet port C controlled by the poppet valve D and a-pair of exhaust ports E. E, controlled by poppet valves F and F. The port C is arranged centrally between the cylinders A and A so as to overlap the same, thereby shifting its axis nearer to the plane of the axes of said cylinders. The exhaust ports E and E are arranged on opposite sides of the port C and preferably directly opposite their respective cylinders. but as these ports are of smaller diameter than the port C they require no further extension of the L- head. The port C which is of an area sufficient for the combined areas of the cylinders A A is so arranged that the gases passing from said port half way around its perimeter are free to flow in the general direction of, one
f of the cylinders and without any sharp bend.
while the gases passing out on the opposite side of the perimeter flow in the general direction of the other cylinder. This dispenses with the necessity for any clearance above the port C greater than required for the lift of the valve. On the otherhand the exhaust valves lie in the path of the flow of the intake gases and are more rapidly cooled thereby.
In operation the two-cylinders A A act as a unit, both simultaneously receiving the combustible charge upon the lifting of the valve D and simultaneously exhausting the products of combustion upon the lifting of the valves F and F. By reason of the more compact arran ement of the valve ports the area of the com ustion chamber in horizontal cross section need be no greater than would be required with a' single cylinder of equal volume and having one inlet and one exhaust valve and inlet and exhaust valves. Also due to the fact that only mechanical clearance 'is required above the valves and further due to the increased perimeter of the two exhaust valves, the depth of the explosion chamber may be reduced. This results either in higher compression without impedance to thefiow of gases between the cylinders and ports or the same compression with larger port areas. A further advantage is that the cross sectional area of the connection between the cylinder and the combustion chamber is restricted which increases the turbulence in the combustible gases.
What I claim as my invention is:
1. An internal combustion engine comprisng a pair of adjacent cylinders with. parallel axes, a common combustion chamber-having a restricted area connecting the same with said cylinders and provided with a single valve controlled inlet port arranged between and overlapping said cylinders and a pair of exhaust ports of smaller diameter arranged on opposite sides of said inlet port.
2. An internal combustion engine comprising a pair of cylinders, a common laterally off-set combustion chamber connected with said cylinders and provided with a single in let port arranged centrally between and overlapping said cylinders, and a pair of exhaust ports laterally opposite the respective cylinders, the depth of said combustion chamber being restricted to provide merely mechanical clearance for movement of the valves, and poppet valves for said inlet and exhaust ports.
3. In an internal combustion engine of the L-head type, a pair of cylinders having parallel axes, a common combustionchamber for said cylinders provided with a single valve controlled inlet port, arranged between and overlapping said cylinders and a pair of exhaust ports of smaller diameter arranged on opposite sides of said inlet port.
4. In an internal combustion engine of the L-head type, a pair of closely arranged cylinders having parallel axes, a common laterally ofi'set combustion chamber connected with said cylinders, provided with a single relatively large inlet port arranged centrally RAY W. HARROUN.
US390167A 1929-09-03 1929-09-03 Internal combustion engine Expired - Lifetime US1824992A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US390167A US1824992A (en) 1929-09-03 1929-09-03 Internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US390167A US1824992A (en) 1929-09-03 1929-09-03 Internal combustion engine

Publications (1)

Publication Number Publication Date
US1824992A true US1824992A (en) 1931-09-29

Family

ID=23541365

Family Applications (1)

Application Number Title Priority Date Filing Date
US390167A Expired - Lifetime US1824992A (en) 1929-09-03 1929-09-03 Internal combustion engine

Country Status (1)

Country Link
US (1) US1824992A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2713852A (en) * 1950-12-29 1955-07-26 Clarence O Trout Opposed piston internal combustion engine frame structure
DE3034053A1 (en) * 1979-09-10 1981-03-12 Honda Giken Kogyo K.K., Tokyo FOUR-STROKE INTERNAL COMBUSTION ENGINE AND OPERATING METHOD FOR THIS INTERNAL COMBUSTION ENGINE.
US6640780B2 (en) * 2000-11-15 2003-11-04 Xrdi, Inc. Side valve arrangement for an internal combustion engine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2713852A (en) * 1950-12-29 1955-07-26 Clarence O Trout Opposed piston internal combustion engine frame structure
DE3034053A1 (en) * 1979-09-10 1981-03-12 Honda Giken Kogyo K.K., Tokyo FOUR-STROKE INTERNAL COMBUSTION ENGINE AND OPERATING METHOD FOR THIS INTERNAL COMBUSTION ENGINE.
US4363300A (en) * 1979-09-10 1982-12-14 Honda Giken Kogyo Kabushiki Kaisha Four-cycle internal combustion engine and associated methods of fuel combustion
US6640780B2 (en) * 2000-11-15 2003-11-04 Xrdi, Inc. Side valve arrangement for an internal combustion engine

Similar Documents

Publication Publication Date Title
US4363300A (en) Four-cycle internal combustion engine and associated methods of fuel combustion
JPH055416A (en) Structure of combustion chamber of engine
US1824992A (en) Internal combustion engine
US1782395A (en) Engine combustion chamber
US4058092A (en) V-Type engines
US3334618A (en) Four stroke high r.p.m. internal combustion engine for racing purposes
US2201292A (en) Internal combustion engine
CA1075988A (en) Internal combustion engine having two spark plugs for each combustion chamber and exhaust gas recirculation circuit
US1205095A (en) Internal-combustion engine.
US3313278A (en) Valve port passages and the arrangement thereof in engines
GB583652A (en) Improvements relating to the cooling arrangements of compression ignition internal combustion engines
US2003677A (en) Internal combustion engine
US1865849A (en) Combustion chamber for internal combustion engines
US4151716A (en) Exhaust manifold system for internal combustion engine
US1893183A (en) Air manifold for internal combustion engines
US1659659A (en) Manifold construction
US2722923A (en) Internal combustion engine
US1887897A (en) Combustion chamber of internal combustion engines
US2012512A (en) Internal combustion engine
US1616942A (en) Internal-combustion engine
US2811149A (en) Internal combustion engines
US1614709A (en) Valve gearing for internal-combustion engines
WO2018158952A1 (en) Intake port structure for internal combustion engine
US1311148A (en) John w
US1660860A (en) Internal-combustion engine