US3085557A - Combustion chambers for pistons - Google Patents

Combustion chambers for pistons Download PDF

Info

Publication number
US3085557A
US3085557A US74653A US7465360A US3085557A US 3085557 A US3085557 A US 3085557A US 74653 A US74653 A US 74653A US 7465360 A US7465360 A US 7465360A US 3085557 A US3085557 A US 3085557A
Authority
US
United States
Prior art keywords
chamber
fuel
combustion
wall
piston
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
US74653A
Inventor
Meurer Siegfried
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.)
MAN AG
Original Assignee
MAN Maschinenfabrik Augsburg Nuernberg AG
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 MAN Maschinenfabrik Augsburg Nuernberg AG filed Critical MAN Maschinenfabrik Augsburg Nuernberg AG
Application granted granted Critical
Publication of US3085557A publication Critical patent/US3085557A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0672—Omega-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder center axis
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/14—Direct injection into combustion chamber
    • 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
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/0621—Squish flow
    • 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
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/0624—Swirl flow
    • 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
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0645—Details related to the fuel injector or the fuel spray
    • F02B23/066—Details related to the fuel injector or the fuel spray the injector being located substantially off-set from the cylinder centre axis
    • 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
    • F02B3/00—Engines characterised by air compression and subsequent fuel addition
    • F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
    • 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

  • the piston of this invention is designed to operate in self-ignition engines such as disclosed in U.S. Patent No. 2,907,308.
  • the liquid fuel is injected into a hollow combustion chamber in the piston.
  • the injection is made in such a way that the major portion of the fuel travels over a short free path and is applied immediately to the wall of the combustion chamber. After striking the chamber wall, the fuel spreads out as a film over a part of the wall.
  • the remaining minor portion of the fuel is atomized directly in the air in the chamber and is self-ignited for igniting the fuel vaporized from the film of fuel. Combustion air is swirled over the film of fuel to vaporize the same.
  • the fuel cover as much as possible of the chamber wall. If the chamber, as in former pistons, is spherical or ellipsoidal and the fuel strikes the wall at a sharp angle, the fuel is spread as a film in a satisfactory maner. Because of the kinetic energy of the fuel, it has a tendency to spread peripherally about the wall of the combustion chamber. However, in these chambers, the spreading of the fuel is handicapped by the concave curve of the spherical or ellipsoi-dal chamber. Such chamber forms act in the nature of a groove with the fuel tending to fiow along the bottom thereof and not completely spread out.
  • the object of this invention is to produce a combustion chamber formed as a body of rotation and having a shape such that the fuel will spread out evenly in all directions on the wall of the chamber.
  • a chamber is in the form of a truncated cone.
  • the bottom of the chamber is also conical with the apex of the bottom pointing toward the interior of the chamber.
  • the chamber is in the form of a hollow conical section forming the side wall and the bottom is shaped as a torus.
  • Combustion chambers which are in the form of a truncated cone having straight side walls and the bottom of which is downwardly and concavely formed.
  • Such a chamber has an unavoidable disadvantage in that a part of the fuel sprayed onto the wall of the chamber is deflected to the downwardly curved bottom by the effect of the air swirling around the longitudinal axis of the chamber and the fuel collects in the bottom in the form of a relatively thick layer or pool. Consequently, the fuel in the pool cannot mix intensively with the swirling combustion air during the short time available forcombustion with the result that the actual combustion takes place irregularly and incompletely. Furthermore, in such chamber, the fuel jet is directed 3,085,557 Patented Apr.
  • FIGURE 1 is a longitudinal cross-sectional view through a piston in a cylinder with thepiston having a combustion chamber according to this invention
  • FIGURE 2 is a similar view of a modified form of the invention.
  • FIGURE 3 is a plan view of the piston shown in FIG- URE 2 with a combustion chamber of circular crosssection;
  • FIGURE 4 is a similar view of the piston having a combustion chamber of elliptical cross-section.
  • the combustion chamber 1 is positioned in the piston head of piston 2, the chamber being coaxial with the axis of piston 2 and cylinder 3.
  • a nozzle 4 is inclined in the cylinder head 4:: above the combustion chamber.
  • the major portion of the injected fuel is applied to the combustion chamber wall by several fuel jets 4b which are directed at a sharp angle toward the wall and form a film thereon. This film is vaporized from the wall and mixed with the air swirling in the chamber to produce a combustible fuel mixture.
  • the minor portion of the fuel is atomized immediately in the air swirling in the chamber. This atomizing is accomplished by either deflecting a part of the injected fuel into the air or by a special ignition jet, not shown. As the fuel leaves the nozzle, it has a. kinetic energy which moves the fuel circumferentially around and upon the combustion chamber wall.
  • the combustion chamber is in the form of a cone and is coaxial with piston 2 and cylinder 3 and opens through the piston head.
  • the side wall 1 1 of chamber 1 is connected by a curved portion 12 with the conical bottom 13.
  • side wall 11 appears as a straight line in that cross-sectional view.
  • the apex of the cone of bottom 13 points to the interior of chamber 1, thus the chamber has a conical side wall 11 and a bottom in the form of a torus.
  • the side wall 11a of the com- Ibustion chamber is convexly curved to further enhance the spreading of the fuel over a large surface of the chamber wall.
  • This is of especial importance for pistons having large diameters and used in engines as disclosed in U.S. Patent No. 2,907,308.
  • the curved surface area of the combustion chamber can receive a large amount of fuel without the necessity of deepening the chamber.
  • the fuel jet strikes the chamber wall adjacent the bulge formed by the curved walls. At this point, the bulge forms a narrowed chamber opening at which the swirling air has an increased velocity and therefor is more active in spreading the fuel evenly over a large wall area.
  • the convexly curved wall 11a also tends to guide the fuel film toward the bottom of the combustion chamber.
  • the curved portion 12 In the bottom of the chamber, the curved portion 12 not only receives a film of fuel, but directs the air toward the conical projection which pushes the mass of rotating air up and against the fuel film on the chamber wall. Consequently, the fuel vaporized from the fuel film is immediately mixed with the air necessary for the combustion of the fuel-air mixture.
  • the combustion chamber can range in shape from an elliptical to a circular truncated cone.
  • the vaporized fuel-air mixture on the bottom 13 of the chamber is forced to flow toward the top of the chamber and out of the chamber into the cylinder space 17 during the combustion stroke of the piston so that the fuel-air mixture is mixed with the remainder of the combustion air in the cylinder and therefore entirely ignited and burned.
  • a piston for a self-ignition internal combustion engine said piston having a combustion chamber which opens through the piston head with a cross-sectional area less than the cross-sectional area at the bottom of said chamber for receiving substantially all of the combustion air in the cylinder as a unidirectional air swirl in said chamber during the piston compression stroke, and for receiving a film of fuel on the combustion chamber side wall, said fuel being supplied from a nozzle offset from the center of said chamber as a solid unatomized jet directed tangentially of the combustion chamber Wall over the shortest possible path, the fuel then being vaporized from said wall and mixed with the combustion air,

Description

April 16, 1963 S. MEURER COMBUSTION CHAMBERS FOR PISTONS Filed D90. 8. 1960 INVENTOR an)? m; .EYS
United States Patent 9 3,085,557 COMBUSTION CHAMBERS FOR PISTONS Siegfried Meurer, Nurnberg, Germany, assignor to Maschinenfabrik Augshurg-Nurnberg, Nurnberg, Germany Filed Dec. 3, 1960, Ser. No. 74,653 Claims priority, application Germany July 7, 1957 Claims. (Cl. 123-32) This invention relates to combustion chambers for pistons. In particular, the invention is directed to combustion chambers for self-ignition engines.
This application is a continuation-in-part of my application Serial No. 740,908, filed June 9, 1958, now Patent 2,975,773, issued Mar. 21, 1961, for Combustion Chambers for Pistons.
The piston of this invention is designed to operate in self-ignition engines such as disclosed in U.S. Patent No. 2,907,308. In such engine, the liquid fuel is injected into a hollow combustion chamber in the piston. The injection is made in such a way that the major portion of the fuel travels over a short free path and is applied immediately to the wall of the combustion chamber. After striking the chamber wall, the fuel spreads out as a film over a part of the wall. The remaining minor portion of the fuel is atomized directly in the air in the chamber and is self-ignited for igniting the fuel vaporized from the film of fuel. Combustion air is swirled over the film of fuel to vaporize the same.
In these engines, it is desirable to have the fuel cover as much as possible of the chamber wall. If the chamber, as in former pistons, is spherical or ellipsoidal and the fuel strikes the wall at a sharp angle, the fuel is spread as a film in a satisfactory maner. Because of the kinetic energy of the fuel, it has a tendency to spread peripherally about the wall of the combustion chamber. However, in these chambers, the spreading of the fuel is handicapped by the concave curve of the spherical or ellipsoi-dal chamber. Such chamber forms act in the nature of a groove with the fuel tending to fiow along the bottom thereof and not completely spread out.
p The object of this invention is to produce a combustion chamber formed as a body of rotation and having a shape such that the fuel will spread out evenly in all directions on the wall of the chamber.
In an engine of this type, it is a requirement that the length of the fuel jet be kept as short as possible, that the fuel jet itself be solid, and that the jet be applied as tangentially as possible to the wall of the combustion chamber. In pistons having a small diameter, these demands can be complied with easily. Difficulties arise as the diameter of the piston increases. This invention is used especially when the combustion chamber is to have a large volume in proportion to its height. A chamber is in the form of a truncated cone. The bottom of the chamber is also conical with the apex of the bottom pointing toward the interior of the chamber. Thus the chamber is in the form of a hollow conical section forming the side wall and the bottom is shaped as a torus.
Combustion chambers are known which are in the form of a truncated cone having straight side walls and the bottom of which is downwardly and concavely formed. Such a chamber has an unavoidable disadvantage in that a part of the fuel sprayed onto the wall of the chamber is deflected to the downwardly curved bottom by the effect of the air swirling around the longitudinal axis of the chamber and the fuel collects in the bottom in the form of a relatively thick layer or pool. Consequently, the fuel in the pool cannot mix intensively with the swirling combustion air during the short time available forcombustion with the result that the actual combustion takes place irregularly and incompletely. Furthermore, in such chamber, the fuel jet is directed 3,085,557 Patented Apr. 16, 1963 ice diagonally or even perpendicular to the air swirl so that apart of the fuel will be mixed directly with the combustion air during its travel from the nozzle to its point of impingement on the chamber wall and more than the usual quantity of fuel thereby atomized. Such is avoided by the shape of the combustion chamber of this invention.
The means by which the objects of the invention are obtained are described more fully with reference to the accompanying drawings, in which:
FIGURE 1 is a longitudinal cross-sectional view through a piston in a cylinder with thepiston having a combustion chamber according to this invention;
FIGURE 2 is a similar view of a modified form of the invention;
FIGURE 3 is a plan view of the piston shown in FIG- URE 2 with a combustion chamber of circular crosssection; and
FIGURE 4 is a similar view of the piston having a combustion chamber of elliptical cross-section.
As shown in FIGURE 1, the combustion chamber 1 is positioned in the piston head of piston 2, the chamber being coaxial with the axis of piston 2 and cylinder 3. A nozzle 4 is inclined in the cylinder head 4:: above the combustion chamber. The major portion of the injected fuel is applied to the combustion chamber wall by several fuel jets 4b which are directed at a sharp angle toward the wall and form a film thereon. This film is vaporized from the wall and mixed with the air swirling in the chamber to produce a combustible fuel mixture. The minor portion of the fuel is atomized immediately in the air swirling in the chamber. This atomizing is accomplished by either deflecting a part of the injected fuel into the air or by a special ignition jet, not shown. As the fuel leaves the nozzle, it has a. kinetic energy which moves the fuel circumferentially around and upon the combustion chamber wall.
In FIGURE 1, the combustion chamber is in the form of a cone and is coaxial with piston 2 and cylinder 3 and opens through the piston head. The side wall 1 1 of chamber 1 is connected by a curved portion 12 with the conical bottom 13. As shown in FIGURE 1, side wall 11 appears as a straight line in that cross-sectional view. The apex of the cone of bottom 13 points to the interior of chamber 1, thus the chamber has a conical side wall 11 and a bottom in the form of a torus.
As shown in FIGURE 2, the side wall 11a of the com- Ibustion chamber is convexly curved to further enhance the spreading of the fuel over a large surface of the chamber wall. This is of especial importance for pistons having large diameters and used in engines as disclosed in U.S. Patent No. 2,907,308. The curved surface area of the combustion chamber can receive a large amount of fuel without the necessity of deepening the chamber. In addition, the fuel jet strikes the chamber wall adjacent the bulge formed by the curved walls. At this point, the bulge forms a narrowed chamber opening at which the swirling air has an increased velocity and therefor is more active in spreading the fuel evenly over a large wall area. The convexly curved wall 11a also tends to guide the fuel film toward the bottom of the combustion chamber. In the bottom of the chamber, the curved portion 12 not only receives a film of fuel, but directs the air toward the conical projection which pushes the mass of rotating air up and against the fuel film on the chamber wall. Consequently, the fuel vaporized from the fuel film is immediately mixed with the air necessary for the combustion of the fuel-air mixture.
The combustion chamber can range in shape from an elliptical to a circular truncated cone. The vaporized fuel-air mixture on the bottom 13 of the chamber, as a result of the conical shape, is forced to flow toward the top of the chamber and out of the chamber into the cylinder space 17 during the combustion stroke of the piston so that the fuel-air mixture is mixed with the remainder of the combustion air in the cylinder and therefore entirely ignited and burned.
Having now described the means by which the objects of the invention are obtained, I claim:
1. In a piston for a self-ignition internal combustion engine, said piston having a combustion chamber which opens through the piston head with a cross-sectional area less than the cross-sectional area at the bottom of said chamber for receiving substantially all of the combustion air in the cylinder as a unidirectional air swirl in said chamber during the piston compression stroke, and for receiving a film of fuel on the combustion chamber side wall, said fuel being supplied from a nozzle offset from the center of said chamber as a solid unatomized jet directed tangentially of the combustion chamber Wall over the shortest possible path, the fuel then being vaporized from said wall and mixed with the combustion air,
References Cited in the file of this patent UNITED STATES PATENTS 2,828,724 Schneider Apr. 1, 1958 2,881,743 Holt Apr. 14, 1959 2,907,308 Meurer et al. Oct. 6, 1959 2,959,161 Bottger Nov. 8, 1960

Claims (1)

1. IN A PISTON FOR A SELF-IGNITION INTERNAL COMBUSTION ENGINE, SAID PISTON HAVING A COMBUSTION CHAMBER WHICH OPENS THROUGH THE PISTON HEAD WITH A CROSS-SECTIONAL AREA LESS THAN THE CROSS-SECTIONAL AREA AT THE BOTTOM OF SAID CHAMBER FOR RECEIVING SUBSTANTIALLY ALL OF THE COMBUSTION AIR IN THE CYLINDER AS A UNIDIRECTIONAL AIR SWIRL IN SAID CHAMBER DURING THE PISTON COMPRESSION STROKE, AND FOR RECEIVING A FILM OF FUEL ON THE COMBUSTION CHAMBER SIDE WALL, SAID FUEL BEING SUPPLIED FROM A NOZZLE OFFSET FROM THE CENTER OF SAID CHAMBER AS A SOLID UNATOMIZED JET DIRECTED TANGENTIALLY OF THE COMBUSTION CHAMBER WALL OVER THE SHORTEST POSSIBLE PATH, THE FUEL THEN BEING VAPORIZED FROM SAID WALL AND MIXED WITH THE COMBUSTION AIR, THE IMPROVEMENT COMPRISING A CHAMBER OF LARGE VOLUME RELATIVE TO ITS HEIGHT AND FORMED AS A BODY OF ROTATION WITH SAID SIDE WALL CONVEXLY CURVED TOWARD THE CENTER OF SAID CHAMBER, A CONICAL BOTTOM SURFACE WITH AN APEX POINTED TOWARD THE CENTER OF SAID CHAMBER, AND A CURVED WALL PORTION EXTENDING BETWEEN SAID SIDE WALL AND SAID BOTTOM.
US74653A 1957-07-07 1960-12-08 Combustion chambers for pistons Expired - Lifetime US3085557A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3085557X 1957-07-07

Publications (1)

Publication Number Publication Date
US3085557A true US3085557A (en) 1963-04-16

Family

ID=8086266

Family Applications (1)

Application Number Title Priority Date Filing Date
US74653A Expired - Lifetime US3085557A (en) 1957-07-07 1960-12-08 Combustion chambers for pistons

Country Status (1)

Country Link
US (1) US3085557A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3814066A (en) * 1970-07-31 1974-06-04 Maschf Augsburg Nuernberg Ag Air compressing internal combustion engine with direct injection
US4313407A (en) * 1976-12-24 1982-02-02 Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft Injection nozzle for air-compressing direct injection internal combustion engines
FR2491148A1 (en) * 1980-09-30 1982-04-02 Alcan Aluminiumwerke PISTON FOR INTERNAL COMBUSTION ENGINES
US4441500A (en) * 1980-04-17 1984-04-10 Ferris Manufacturing Corp. EKG Electrode
US4693219A (en) * 1983-04-11 1987-09-15 Fiat Auto S.P.A. Internal combustion engine with direct fuel injection
EP1350014B1 (en) * 2001-01-12 2008-01-02 Nissan Motor Co., Ltd. Piston for internal combustion engines
US8783218B2 (en) 2011-07-15 2014-07-22 EcoMotors International Toroidal combustion chamber with side injection

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2828724A (en) * 1953-10-08 1958-04-01 Schweizerische Lokomotiv Internal combustion engines of the injection type
US2881743A (en) * 1956-12-20 1959-04-14 Ricardo & Co Engineers Internal combustion engines of the liquid fuel injection compression ignition type
US2907308A (en) * 1951-12-17 1959-10-06 Meurer Siegfried Operation of internal combustion engines
US2959161A (en) * 1957-08-20 1960-11-08 Ustav Pro Vyzkum Motorovych Vo Internal-combustion compression-ignition engine with localised self-ignition of the fuel

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2907308A (en) * 1951-12-17 1959-10-06 Meurer Siegfried Operation of internal combustion engines
US2828724A (en) * 1953-10-08 1958-04-01 Schweizerische Lokomotiv Internal combustion engines of the injection type
US2881743A (en) * 1956-12-20 1959-04-14 Ricardo & Co Engineers Internal combustion engines of the liquid fuel injection compression ignition type
US2959161A (en) * 1957-08-20 1960-11-08 Ustav Pro Vyzkum Motorovych Vo Internal-combustion compression-ignition engine with localised self-ignition of the fuel

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3814066A (en) * 1970-07-31 1974-06-04 Maschf Augsburg Nuernberg Ag Air compressing internal combustion engine with direct injection
US4313407A (en) * 1976-12-24 1982-02-02 Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft Injection nozzle for air-compressing direct injection internal combustion engines
US4441500A (en) * 1980-04-17 1984-04-10 Ferris Manufacturing Corp. EKG Electrode
FR2491148A1 (en) * 1980-09-30 1982-04-02 Alcan Aluminiumwerke PISTON FOR INTERNAL COMBUSTION ENGINES
US4693219A (en) * 1983-04-11 1987-09-15 Fiat Auto S.P.A. Internal combustion engine with direct fuel injection
EP1350014B1 (en) * 2001-01-12 2008-01-02 Nissan Motor Co., Ltd. Piston for internal combustion engines
US8783218B2 (en) 2011-07-15 2014-07-22 EcoMotors International Toroidal combustion chamber with side injection

Similar Documents

Publication Publication Date Title
EP0172253B1 (en) Combustion chamber structure for diesel engines
US3318292A (en) Internal combustion engine
US6158409A (en) Two-stroke engine piston bowl configurations
US3083700A (en) Internal combustion engine construction
US5996548A (en) Method of operating an internal combustion engine
US3244159A (en) Fuel injection internal combustion engine
US2709992A (en) Piston and combustion chamber construction for compression ignition engine
US2975773A (en) Combustion chambers for pistons
JP3295975B2 (en) gasoline engine
US4641617A (en) Direct injection type internal combustion engine
US3085557A (en) Combustion chambers for pistons
US4401071A (en) Injection and mixture formation process and apparatus to implement same
US3294072A (en) Internal combustion engine
US2921566A (en) Internal combustion engine and method of operating it
JPS63134813A (en) Combustion chamber of internal combustion engine
US4286557A (en) Target injection stratified charge spark ignition engine
US4633830A (en) Direct injection internal combustion engine of compression ignition type
US2828724A (en) Internal combustion engines of the injection type
US3498275A (en) Fuel injection type engine
US2779320A (en) Internal combustion engine
US4392465A (en) Self-igniting internal combustion engine with a rotationally symmetrical piston trough
US2561628A (en) Internal-combustion engine of the liquid fuel injection type
US3046959A (en) Combustion chambers for pistons
US2855907A (en) Internal combustion engine system
KR950011685B1 (en) Diesel engine