US2954023A - Combustion chamber for internal combustion engines - Google Patents

Combustion chamber for internal combustion engines Download PDF

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US2954023A
US2954023A US847604A US84760459A US2954023A US 2954023 A US2954023 A US 2954023A US 847604 A US847604 A US 847604A US 84760459 A US84760459 A US 84760459A US 2954023 A US2954023 A US 2954023A
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chamber
combustion chamber
center
cylinder
combustion
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US847604A
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Lampredi Aurelio
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Fiat SpA
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Fiat SpA
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    • 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
    • F02B23/08Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
    • 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

  • ,Qne of he main characteristics determining thestend- I ard ofacombustion chamber is a low value of the surface area/volume ratio; under this aspect the best chamber is the conventional hemispherical chamber, in which the valve axes extend through the center of the hemisphere.
  • valve axes should diverge through an angle such that valve control is possible only by means of two cam-shafts arranged in the head and crankcase.
  • control is effected by means of one cam-shaft only, it is not possible to arrange the spark plug at a middle zone in the chamber, unless elaborate passages through the top cover are provided.
  • This invention provides a combustion chamber which afiords the high efiiciency of hemispherical chambers, and is on the other hand less binding upon the valve location, whereby devices can be employed for controlling the valves which compare in simplicity with control devices employed in dome-shaped chambers.
  • the improved combustion chamber permits of substantially reducing divergence of the valve axes and of biasing them to each other, whereby the spark plug may be brought nearer to the center of gravity of the chamber.
  • a further object of this invention is to provide'a combustion chamber the surface of which can be machined throughout by a number of operations not exceeding the number required by a conventional hemispherical chamher.
  • the combustion chamber for internal combustion engines is characterized in that its top surface is made up of a plurality of non-concentric spherical zones, two of which have their center situated on the axis of their respective valve, whereby the zones can each be machined at the same time as its respective valve seat.
  • Figure 1 is a plan View from below of the combustion chamber.
  • Figures 2, 3 and 4 are sectional views on lines II-II, III-III and IV-IV, respectively, of Figure 1.
  • the surface of the combustion chamber in the engine head comprises two spherical zones 1 and 2 which are not concentric with each other.
  • the centre 11 of the spherical zone 1 is situated on the axis 21 of the valve seat 31.
  • the center 12 of the spherical zone 2 is situated on the axis 22 of the valve seat 32.
  • the two spherical zones can therefore be each four-strobe, internal cqnrbnstion engines, preferably with 2 manufactured simultaneously with their. reepeotive valve seat by means of a tool of acorres pondi ng rofile,
  • the substantially sharp edgeformed by lntersection of the spherical n s 1 an is m ve by; nash s aa a third spherical zone 3, the diameter. and location of the center of which, denoted by 13 are selected so; that,
  • the sparlg plug seat, 5 isfornred'in one of the curvilinear triangles.
  • thecenters Hi1 ⁇ and 13 are located on acommon plane parallel to and ef -se w t re ec Qt th en r l or l itudi l s the cylinder, as can be readily seen in Figfl oncpmpa the relative posit'ons .of the points 11, 12, 1 and 14. M reove s e to a t in t e h h'Q .1 P .Q $i IT I.
  • the spherical zone 3 therefore conveniently merges into a fourth spherical zone 4 having its center 14 situated on the longitudinal axis 20 of the cylinder.
  • the spherical zone 3 intersects the lower plane of the head along a circle fully or nearly coinciding with the cylinder bore, its surface, when the diameter is conveniently selected, ex.- tending parallel or nearly so with the usually convex pis-- ton top.
  • a further feature of the invention residesin the fact that the spherical zones 3, 4 and the radius 6 joining them (compare Figure 3) are machined by a single operation effected by means of a milling cutter of a corresponding profile rotating on an inclined axis 23 extending through the centers 13, 14 of the spherical zones 3, 4.
  • the spherical zone 4 acts as a laminating zone for the mixture between the piston and head when the piston is at its top dead center. By varying its thickness and width the combustion process can be affected and best performances can be obtained from the chamber from the standpoint both of thermal efiiciency and aging characteristics.
  • valve axes need not be co-planar.
  • the volume required in order to obtain the desired compression ratio being the same, the surface exposed to the flame is substantially the same as with a hemispherical chamber and smaller than with a triangular chamber.
  • the edges formed by intersection of the spherical zones 1, 3 and 2, 3 are rather obtuse, whereby no hot points or
  • the angle between the valve axes can be considerably smaller than which is the average value required by a hemispherical chamber with one center. Therefore the valves can be controlled by one cam-shaft mounted in the crankcase through standard push-rod and beam units, the overall size in a transverse direction of the head cover being kept within reasonable limits.
  • the spark plug may be arranged near the center of gravity of the chamber at the hottest region of the chamber, so that the flame paths are relatively short and V smooth. Moreover, the limited overall size of the head cover in a transverse direction makes it accessible through lateral recesses without requiring elaborate passages through the said cover.
  • a cylinder head for an internal combustion engine including a combustion chamber, and a pair of annular seats in the chamber for the respective valves, and wherein the axes of the said seats are inclined towards each other and with respect to the longitudinal axis of the respective cylinder, the said combustion chamber defined substantially by a basic spherically curved surface, and by a pair of cavities in said surface defined each by a further spherically curved surface surrounding a respective valve seat, each of said further spherically curved surfaces having its center located on the axis of the respective seat.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Description

P 1960 I A. LAMPREDI 2,954,023
COMBUSTION CHAMBER FOR INTERNAL COMBUSTION ENGINES I Filed Oct. 20, 1959 2 Sheets-Sheet 1 ENG/NE Sept. 27, 1960 A. LAMPIIQEDIV I 2,954,023
- COMBUSTION CHAMBER FOR INTENAL COMBUSTION mamas Filed Oct. 20, 1959 2 Sheets-Sheet 2 COMBUSTION CHAMBER FOR INTERNAL c M usuQN ENG ES Aurelio Lampredi, Turin, Italy, assignor to Fiat Societa P r Ma i Turin, Italy fi s t-Z9 25.2 er- N 84 5 4 Claims priority, application Italy Nov. 11, 195 8 5. Clai s- (Cl- 23-1 1) This invention relates to a combustion chamber for spark plug ignition.
It is well known that the. shapeof the chamber, size location of the valves and location of the spark plugs considerably. affect the volumetric and thermal .e fiicie'ncies the engine.
,Qne of he main characteristics determining thestend- I ard ofacombustion chamber is a low value of the surface area/volume ratio; under this aspect the best chamber is the conventional hemispherical chamber, in which the valve axes extend through the center of the hemisphere.
However, this chamber is objectionable in that with valves of standard size the valve axes should diverge through an angle such that valve control is possible only by means of two cam-shafts arranged in the head and crankcase. When control is effected by means of one cam-shaft only, it is not possible to arrange the spark plug at a middle zone in the chamber, unless elaborate passages through the top cover are provided.
This invention provides a combustion chamber which afiords the high efiiciency of hemispherical chambers, and is on the other hand less binding upon the valve location, whereby devices can be employed for controlling the valves which compare in simplicity with control devices employed in dome-shaped chambers.
The improved combustion chamber permits of substantially reducing divergence of the valve axes and of biasing them to each other, whereby the spark plug may be brought nearer to the center of gravity of the chamber.
A further object of this invention is to provide'a combustion chamber the surface of which can be machined throughout by a number of operations not exceeding the number required by a conventional hemispherical chamher.
The combustion chamber for internal combustion engines according to this invention is characterized in that its top surface is made up of a plurality of non-concentric spherical zones, two of which have their center situated on the axis of their respective valve, whereby the zones can each be machined at the same time as its respective valve seat.
Further characteristic features and advantages of this invention will be understood from the appended detailed description, referring to the accompanying drawings given by way of a non limiting example only, wherein:
Figure 1 is a plan View from below of the combustion chamber.
Figures 2, 3 and 4 are sectional views on lines II-II, III-III and IV-IV, respectively, of Figure 1.
According to this invention the surface of the combustion chamber in the engine head comprises two spherical zones 1 and 2 which are not concentric with each other. The centre 11 of the spherical zone 1 is situated on the axis 21 of the valve seat 31. The center 12 of the spherical zone 2 is situated on the axis 22 of the valve seat 32. The two spherical zones can therefore be each four-strobe, internal cqnrbnstion engines, preferably with 2 manufactured simultaneously with their. reepeotive valve seat by means of a tool of acorres pondi ng rofile,
The substantially sharp edgeformed by lntersection of the spherical n s 1 an is m ve by; nash s aa a third spherical zone 3, the diameter. and location of the center of which, denoted by 13 are selected so; that,
though the above edge be removed, the. Zone ,3, ,djoes not nt rf r w t t e ve ifl sea s 3-1. 32 situ es. t e ase 1, 2. Looking from below. (Fi re 1), the spherical zone 3 is su sta ia y lh a m o t o ,cunnmea t cs joined at an apex. The sparlg plug seat, 5 isfornred'in one of the curvilinear triangles.
he e r i e p 'eri a eu i 1 1; usuall be situated on the, axislof' its respeetive 'cyl inder'in a preferred embodiment of this invention, thecenters Hi1} and 13 are located on acommon plane parallel to and ef -se w t re ec Qt th en r l or l itudi l s the cylinder, as can be readily seen in Figfl oncpmpa the relative posit'ons .of the points 11, 12, 1 and 14. M reove s e to a t in t e h h'Q .1 P .Q $i IT I. ,9 p e t re red- 1 -sits? s h r ssl a 3 should be kept-within v I in nse? T1swe -'P als ai i sl Q diameter substantially smaller than the cylinder bore. The spherical zone 3 therefore conveniently merges into a fourth spherical zone 4 having its center 14 situated on the longitudinal axis 20 of the cylinder. The spherical zone 3 intersects the lower plane of the head along a circle fully or nearly coinciding with the cylinder bore, its surface, when the diameter is conveniently selected, ex.- tending parallel or nearly so with the usually convex pis-- ton top. A further feature of the invention residesin the fact that the spherical zones 3, 4 and the radius 6 joining them (compare Figure 3) are machined by a single operation effected by means of a milling cutter of a corresponding profile rotating on an inclined axis 23 extending through the centers 13, 14 of the spherical zones 3, 4.
V The spherical zone 4 acts as a laminating zone for the mixture between the piston and head when the piston is at its top dead center. By varying its thickness and width the combustion process can be affected and best performances can be obtained from the chamber from the standpoint both of thermal efiiciency and aging characteristics.
It will be understood from the above that with a combustion chamber of this shape a wider choice is left as to location of the valves and, as will be clearly seen from Figure 1, the valve axes need not be co-planar.
The volume required in order to obtain the desired compression ratio being the same, the surface exposed to the flame is substantially the same as with a hemispherical chamber and smaller than with a triangular chamber. The edges formed by intersection of the spherical zones 1, 3 and 2, 3 are rather obtuse, whereby no hot points or The angle between the valve axes can be considerably smaller than which is the average value required by a hemispherical chamber with one center. Therefore the valves can be controlled by one cam-shaft mounted in the crankcase through standard push-rod and beam units, the overall size in a transverse direction of the head cover being kept within reasonable limits.
The spark plug may be arranged near the center of gravity of the chamber at the hottest region of the chamber, so that the flame paths are relatively short and V smooth. Moreover, the limited overall size of the head cover in a transverse direction makes it accessible through lateral recesses without requiring elaborate passages through the said cover.
It will be understood that, the principle of the invention being left unaltered, the arrangement, number and radius of the spherical zones may be widely varied with respect to the disclosure in the drawings and specification without departing from the scope of this invention.
What I claim is:
1. In a cylinder head for an internal combustion engine including a combustion chamber, and a pair of annular seats in the chamber for the respective valves, and wherein the axes of the said seats are inclined towards each other and with respect to the longitudinal axis of the respective cylinder, the said combustion chamber defined substantially by a basic spherically curved surface, and by a pair of cavities in said surface defined each by a further spherically curved surface surrounding a respective valve seat, each of said further spherically curved surfaces having its center located on the axis of the respective seat.
2. In a cylinder head as claimed in claim 1, in which the center of the three spherically curved surfaces are located on a common plane parallel to and off-set with respect to the longitudinal axis of the cylinder.
3. In a cylinder head as claimed in claim 1, which the center of the basic spherically curved surface is located offset from the longitudinal axis of the cylinder, and an annular spherically curved concave surface disposed radially outwardly of the three first-mentioned surfaces and substantially enclosing said three first-mentioned surfaces, the said annular spherically curved concave surface having its center located on the longitudinal axis of the cylinder.
4. In a cylinder head as claimed 1, the centers of said further spherically curved surfaces are spaced therebetween lengthwise of the engine axis.
5. In a cylinder head as claimed in claim 1, in which the centers of the three spherically curved surfaces are located on a common plane parallel to and olf-set with respect to the longitudinal axis of'the cylinder, and a spark plug seat in the basic spherically curved surface located oppositely to said plane with respect to the axis of the cylinder.
References Cited in the file of this patent UNITED STATES PATENTS 2,109,298 Mock Feb. 22, 1938 2,669,227 Drinkard 1.. Feb. 16, 1954 2,769,434 Witzky Nov. 6, 1956 2,833,254 Carpentier et al May 6, 1958
US847604A 1958-11-11 1959-10-20 Combustion chamber for internal combustion engines Expired - Lifetime US2954023A (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3094977A (en) * 1960-11-07 1963-06-25 Achilles C Sampietro Cylinder head assemblies for spark ignition internal combustion engines
US3174467A (en) * 1962-04-23 1965-03-23 Kaiser Jeep Corp Diesel cylinder head
US3306271A (en) * 1966-01-19 1967-02-28 Gen Motors Corp Internal combustion engine with single overhead camshaft and hemispherical combustion chambers
US3468295A (en) * 1966-11-08 1969-09-23 Renault Cylinder heads of internal combustion engines
US3557766A (en) * 1967-06-22 1971-01-26 Leander Engineering Co Ltd Combustion engines
US4259933A (en) * 1978-07-20 1981-04-07 Toyota Jidosha Kogyo Kabushiki Kaisha Combustion chamber of an internal combustion engine
US4284044A (en) * 1978-07-20 1981-08-18 Toyota Jidosha Kogyo Kabushiki Kaisha Combustion chamber of an internal combustion engine
US4289099A (en) * 1978-07-20 1981-09-15 Toyota Jidosha Kogyo Kabushiki Kaisha Combustion chamber of an internal combustion engine
US4300499A (en) * 1978-07-20 1981-11-17 Toyota Jidosha Kogyo Kabushiki Kaisha Combustion chamber of an internal combustion engine
DE3322544A1 (en) * 1983-06-23 1985-01-10 Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart PISTON PISTON ENGINE
US5941221A (en) * 1998-08-18 1999-08-24 Marocco; Gregory M. Reciprocating engine combustion chamber

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2109298A (en) * 1935-12-10 1938-02-22 Eclipse Aviat Corp Internal combustion engine
US2669227A (en) * 1950-04-15 1954-02-16 Chrysler Corp Overhead valve engine
US2769434A (en) * 1953-11-04 1956-11-06 Studebaker Packard Corp Overhead valve arrangement for engines
US2833254A (en) * 1955-01-04 1958-05-06 Chrysler Corp Overhead valve engine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2109298A (en) * 1935-12-10 1938-02-22 Eclipse Aviat Corp Internal combustion engine
US2669227A (en) * 1950-04-15 1954-02-16 Chrysler Corp Overhead valve engine
US2769434A (en) * 1953-11-04 1956-11-06 Studebaker Packard Corp Overhead valve arrangement for engines
US2833254A (en) * 1955-01-04 1958-05-06 Chrysler Corp Overhead valve engine

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3094977A (en) * 1960-11-07 1963-06-25 Achilles C Sampietro Cylinder head assemblies for spark ignition internal combustion engines
US3174467A (en) * 1962-04-23 1965-03-23 Kaiser Jeep Corp Diesel cylinder head
US3306271A (en) * 1966-01-19 1967-02-28 Gen Motors Corp Internal combustion engine with single overhead camshaft and hemispherical combustion chambers
US3468295A (en) * 1966-11-08 1969-09-23 Renault Cylinder heads of internal combustion engines
US3557766A (en) * 1967-06-22 1971-01-26 Leander Engineering Co Ltd Combustion engines
US4259933A (en) * 1978-07-20 1981-04-07 Toyota Jidosha Kogyo Kabushiki Kaisha Combustion chamber of an internal combustion engine
US4284044A (en) * 1978-07-20 1981-08-18 Toyota Jidosha Kogyo Kabushiki Kaisha Combustion chamber of an internal combustion engine
US4289099A (en) * 1978-07-20 1981-09-15 Toyota Jidosha Kogyo Kabushiki Kaisha Combustion chamber of an internal combustion engine
US4300499A (en) * 1978-07-20 1981-11-17 Toyota Jidosha Kogyo Kabushiki Kaisha Combustion chamber of an internal combustion engine
DE3322544A1 (en) * 1983-06-23 1985-01-10 Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart PISTON PISTON ENGINE
US5941221A (en) * 1998-08-18 1999-08-24 Marocco; Gregory M. Reciprocating engine combustion chamber
WO2000011331A1 (en) * 1998-08-18 2000-03-02 Marocco Gregory M Reciprocating engine combustion chamber

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