Abstract: A piston crown is formed with a cavity including a first flame deflecting member which is located amid three flame dispersion zones and which splits burning gases ejected from a transfer port into a first dispersion zone, while the piston is proximate its TDC position, into two flows. The arrangement additionally induces the two flows to assume two essentially symmetrical swirling patterns in second and third dispersion zones. After the piston has descended by a predetermined amount, the burning gases are supplied directly into the second and third zones.

Abstract: Internal combustion stratified-charge engine having within a cylinder thereof a variable volume space wherein a piston pursuant to an air intake stroke draws a stream of intake air through an entrance end of the combustion chamber and through such chamber into said variable volume space. The inner periphery of a sidewall of such chamber having a series of grooves which may score the head of a poppet type exhaust valve in such periphery and which contribute to stratification of a leading fuel-free mass of such stream and a fuel-containing trailing mass thereof into the variable volume space. A portion of such trailing fuel-containing mass remaining in the chamber and an adjacent portion thereof in the variable volume space adjacent to said chamber, and, pursuant to the ensuing compression stroke of the piston, the masses are caused to flow into the chamber in the reverse order of their formation with the fuel-containing mass compressed adjacent the entrance end of the chamber where combustion is initiated.

Abstract: Combustion chamber assembly of direct injection diesel engine comprising a cylinder head, a cylinder liner, an injection nozzle and a piston with a combustion chamber on its top. An air flow guide ring is provided in the combustion chamber assembly. The guide ring is arranged under and adjacent to the bottom surface of the cylinder and around the nozzle. The front end of the nozzle protrudes from the bottom of the guide ring. The peripheral surface of the guide ring acts as an air flow guide surface to lead the air squish. The air flow guide surface inclines in relation to the bottom surface of the cylinder head and its inclination angle is in the range of 30-70 degrees.

Abstract: A swirl chamber is defined by an approximately spherical cavity formed in a cylinder head of an internal combustion engine with the radius of the swirl chamber being reduced in the direction the swirl flows in the swirl chamber. Therefore, the swirl is accelerated as it flows in the swirl chamber. The swirl chamber communicates with a main combustion chamber formed in a piston top via a passage formed in the cylinder head when the piston is at top dead center, and air in the main combustion chamber is forced into the swirl chamber due to the compression stroke of the piston. The passage is formed in a manner such that it has constant transverse section lengthwise and such that a part of the passage defines a tangential line of the swirl chamber. Therefore, the air forced into the swirl chamber passes through the passage with little friction loss, smoothly enters the swirl chamber and gains velocity in the swirl chamber.

Abstract: A combustion chamber for a spark assisted diesel engine embodying a main combustion chamber and an energy cell. Fuel is injected into the main chamber and into the energy cell and combustion is initiated in the main chamber. The energy cell communicates with the main chamber through a restricted orifice and the increased pressure of the combustion causes auto ignition in the energy cell to generate a high velocity charge out of the energy cell into the main chamber through the orifice for generating turbulence to insure complete combustion.

Abstract: Improved combustion chamber configurations for two-cycle engines with high pressure fuel injected systems having reciprocal pistons, cylinders with multiple injectors for each cylinder and a cylinder head liner with a chamber having a discoidal configuration that cooperates with a piston head structure to generate a toroidal, swirling, compressed air flow during compression strokes of the reciprocating piston.

Abstract: According to the present ivention, a combustion chamber of internal combustion engines comprises: a main combustion chamber which is created by recessing the piston top; a swirl chamber which is contiguous to said main combustion chamber via a passage; and a fuel injection nozzle to supply atomized fuel into said main combustion chamber and swirl chamber. Because of the above arrangement, a relatively quick combustion takes place in the swirl chamber and a relatively sluggish combustion takes place in the main combustion chamber. As a result, the generation of HC, NOx, or smokes are suppressed while improving an output, a fuel consumption rate, and a thermal efficiency.

Abstract: A piston crown is formed with cavity a which includes a first flame deflecting member which divides the flame ejected from a transfer port interconnecting a swirl chamber with a main combustion chamber while the piston is relatively close to its TDC position and a second flame deflecting arrangement which divides the flame flow after the piston has descended by a given amount. The stage deflections of the flame promotes extensive dispersion thereof and the formation of a flame plume which engulfs a relatively large amount of the air in the combustion chamber and improves mixing of the burning gases and unburnt fuel with the air in the combustion chamber.

Abstract: High-compression spark-ignited stratified-charge fuel-injection reciprocating-piston engine in which the combustion chamber initial charge includes a discrete air-fuel stratum that is lean with fuel at low speed idle and progressively increased in fuel richness and volume until that stratum ultimately completely fills the chamber with a homogeneous air-fuel mixture using all of the intaken air to attain maximum power. The combustion process minimizes pollutive exhaust emissions.

Abstract: Disclosed herein is a combustion chamber for internal combustion engines using a volatile fuel of low certain number such as gasoline, alcohol or the like. The fuel is directly injected into communicating main and subsidiary combustion chambers which are formed side by side in the top wall of a piston and in which swirls are formed. The fuel is supplied into the main and subsidiary combustion chambers in atomized form to facilitate its volatilization, and partly deposited in the form a film which is easily volatilized by hot compressed air and wall heat in the respective combustion chambers. A spark plug is provided in the main and subsidiary combustion chambers to accelerate ignition of the atomized fuel supplied thereto.

Abstract: A low compression reciprocating internal combustion piston engine with a prechamber in the head connected to a main combustion chamber in the piston, the prechamber having an igniter, a pilot fuel injector and connecting lineal passage; the main chamber including a fuel injector for mixing the prechamber gases with the gases being compressed in the cylinder. The engine is a hybrid having transitional combustion modes from spark-ignited stratified charge mode at low power, to a spark-assisted compression ignition at higher power loads, and a strictly compression ignition mode at maximum power loads.

Abstract: A combustion chamber with a number of jet hole bores that communicate with the clearance space of the cylinder of an internal combustion engine. When the carburated mixture in the combustion chamber is ignited, the flame front bifurcates into a first portion that enters the clearance space from the combustion chamber through a main opening, and a second flame front that enters the clearance space through the jet holes. The flame fronts violently collide in the clearance space, ensuring complete burning of the carburated mixture.

Abstract: The present invention relates the technology to enhance the mixing performance of air-fuel mixture in a combustion chamber with a domed precombustion chamber for a spark-ignition engine, and aims to attain the enhanced mixing performance owing to the forcible generation of a multiplicity of small swirls by forcing the air-fuel mixture to flow into the main combustion chamber centripetally from the inside of the cylinder and then to turns three times in a step-like state with being accelerated on the way into the precombustion chamber through the connecting channel at the compression stroke. The main combustion chamber is formed by hollowing the center side portion of the piston head. The piston head is further provided with the connecting channel formed on the annular bank around the main combustion chamber so as to be faced onto by the domed precombustion chamber in the cylinder head and to be stepped up higher than the bottom of the main combustion chamber.

Abstract: An internal combustion engine having a main combustion chamber in a top portion of a piston, and an ignition chamber which is provided with a fuel injection valve and an ignition plug, in a cylinder head, the direction in which fuel is ejected from the fuel injection valve being set in accordance with the forward direction of a swirl, the axis of the ejected fuel being spaced from a central portion of the main combustion chamber by a distance of not more than 1/2 of the radius thereof, a recess in communication with the main combustion chamber being provided in the section of the top portion of the piston which is on an extension of the ignition chamber.

Abstract: A combustion chamber for a spark assisted diesel engine embodying a main combustion chamber and an energy cell. Fuel is injected into the main chamber and into the energy cell and combustion is initiated in the main chamber. The energy cell communicates with the main chamber through a restricted orifice and the increased pressure of the combustion causes auto ignition in the energy cell to generate a high velocity charge out of the energy cell into the main chamber through the orifice for generating turbulence to insure complete combustion.

Abstract: In order to avoid the formation of smoke and HC when the compression ratio of a swirl chamber type Diesel engine is lowered either by design or by operation in rarified atmospheres, the fuel injector is located on one side of the center axis of the swirl chamber so as to maximize the distance for which the injected fuel can travel before contacting a wall of the chamber and the auxiliary transfer port through which a fraction of the injected fuel is fed to the main combution chamber is arranged so that the axis thereof intersects the axis of the fuel injector and therefore the trajectory along which fuel is injected, at a point defined within the swirl chamber per se and on the opposite side of the center axis with respect to the fuel injector.

Abstract: In order to promote a good flame dispersion within the combustion chamber of a swirl chamber type Diesel engine, a shaped recess formed in the piston crown is arranged to have a trench portion into which the flame from the swirl chamber is injected and mirror image flame dispersion portions on either side of the trench which terminates at the periphery of the piston crown. This arrangement inhibits the formation of secondary flame flows which tend impede desirable patterns within the flame disportion portions and simultaneously enlarges the dispersion area. In addition, careful selection of the dimensions of the transfer port which interconnects the swirl chamber and the main combustion chamber, and the various sections of the shaped recess, promotes further reductions in HC and smoke emissions.

Abstract: A direct injection type internal combustion engine has a piston reciprocatably fitted in the bore of a cylinder block defining a combustion chamber together with the cylinder block and a cylinder head. A main recess is formed in the combustion chamber for accelerating the swirl of intake air which is prepared and introduced by an intake device. At least one auxiliary recess is formed in the main recess and is arranged in the direction of the intake air swirl and in the direction of the fuel injection of a fuel injector for generating a secondary swirl different from the intake air swirl and for generating turbulence between the two swirls. Thus, the introduction of air into the fuel droplets fed from the fuel injector is promoted by the intake air swirl and the secondary swirl so that the combustion efficiency of the internal combustion engine is improved.

Abstract: In a pre-chamber type diesel engine, in order to prevent droplets of liquid fuel finding their way into zones of the main combustion chamber wherein they undergo slow combustion and thus tend to form smoke, a recess is formed at the main combustion chamber end of an auxiliary transfer passage in a manner to provide a wall section which deflects droplets of fuel, which have passed through the auxiliary passage during the induction phase and/or initial stage of the compression phase, in a manner that they do not escape toward the perimeter of the piston crown and remain in a zone through which the flame produced by spontaneous combustion of the highly compressed air-fuel mixture in the pre-chamber passes thus ensuring rapid vaporization and subsequent oxidation.

Abstract: A direct injection internal combustion engine of a compression ignition type in which portions of an injected fuel spray which have not been evaporated are prevented from striking the walls of the combustion chamber, and the fuel spray is prevented from catching up the air around it when moving in the combustion chamber, thereby providing an engine having reduced combustion noise, reduced amount of smoke and noxious emissions, and improved fuel economy. A combustion chamber is formed in the piston substantially in the form of a spherical cavity gradually narrowing towards the opening of the cavity at the top surface of the piston. An air intake mechanism swirls intake air supplied to the combustion chamber. A swirl injector injects a fuel spray substantially in the form of a hollow cone having a velocity component in a direction tangential of the central axis of the nozzle.

Abstract: A method for operating a two cycle, spark ignition, internal combustion engine of the class having a combustion chamber divided into a relatively small ignition region and a larger combustion region in which the piston reciprocates. Substantially the same stoichiometric fuel-air mixtures are independently supplied to the ignition region in substantially fixed quantities and to the combustion region in variable quantities. These mixtures are compressed simultaneously so that they remain completely separated prior to ignition. The mixtures are stratified with respect to excess air supplied to both regions and to exhaust gases in the engine cylinder, and combustion initiated in the ignition region ignites the variable-sized mixture in the larger region. Burning proceeds from stoichiometric mixtures to lean mixtures as the stratified excess air is mixed into the burning gases. When no fuel is supplied to the combustion region, the ignition region functions independently and burns its fuel efficiently.

Abstract: A squish jet arrangement for an internal combustion engine is positioned on a piston member or cylinder head member thereof. A substantially cylindrical bowl opens onto the face of the member. At least one pair, and preferably a plurality of pairs, of squish jet passages are arranged to direct flows of gasses tangentially into the bowl. As first ones of the pairs of squish jet passages lie in a lower transverse plane than second ones of the pairs, a counter-rotating, bi-level swirl can be produced by the squish jet outlets. A squish jet arrangement is also provided with outlets of squish jet passages spaced above a lower surface of a bowl, and directed to eject coplanar flows of gasses therefrom, which intercept one another.

Abstract: Projecting parts of the piston and the cylinder head are formed in such a manner that two portions of the piston surface are spaced from the inner surface of the cylinder head and a third portion of the piston surface is next to the inner surface of the cylinder head when the piston is at the upper dead center point, said third portion of the surface comprising a zone which is at a distance from the inner surface of the cylinder head and forming a connecting surface between said two first portion, these latter forming, with the cylinder head, respectively, an initial combustion zone and an expansion zone for the gases originating from the combustion, while the connecting zone together with the cylinder head forms an opening for the passage of said gases from the first zone, guiding these latter along the cylinder head toward a wall of the expansion zone, the outline of which, in a plane containing the axis of the above-mentioned opening, is a line which is curved in the direction of the opening forming the me

Abstract: A two cycle, spark ignition, internal combustion engine of the class having a combustion chamber divided into a relatively small ignition region and a larger combustion engine in which the piston reciprocates. Substantially the same stoichiometric fuel-air mixtures are independently supplied to the ignition region in substantially fixed quantities and to the combustion region in variable quantities. These mixtures are compressed simultaneously so that they remain completely separated prior to ignition. The mixtures are stratified with respect to excess air supplied to both regions and to exhaust gases in the engine cylinder, and combustion initiated in the ignition region ignites the variable-sized mixture in the larger region. Burning proceeds from stoichiometric mixtures to lean mixtures as the stratified excess air is mixed into the burning gases. When no fuel is supplied to the combustion region, the ignition region functions independently and burns its fuel efficiently.

Abstract: A direct injection internal combustion engine of compression ignition type is provided with a piston cavity offset from the piston center and with an injection nozzle which injects a hollow conical fuel spray having a tangential velocity component and relatively weak penetration into a swirl set up in the combustion chamber. The injection geometry and the offset are such that squish and swirl flows interact to form an excellent air-fuel mixture over the whole volume of the cavity without forming local fuel concentrations or wetting the cavity wall.

Abstract: A direct injection internal combustion engine of a compression ignition type uses swirl injection nozzle having relatively small penetration and relies on the combination of an intake swirl and compression squish flow as well as a substantial fuel spray angle to uniformly distribute fuel throughout the interior of a throttled combustion cavity recessed in the piston.

Abstract: An internal combustion engine comprising a piston (1) having a recessed combustion bowl (3) with a raised projection (4) in the floor of the bowl so as to define an annulus with the sides of the bowl, swirl means to cause the inlet air to rotate about said raised projection, and a fuel injector (2) having orifices that spray a plurality of jets into the annulus at spaced points around the projection (4), the cross-sectional area of the annulus being such as to vary around the projection (4) and to have a minimum value in a median plane (D--D) through the axis (C) of the projection (4), and the injector nozzle (2) being located in a central region of the bowl (3) and having orifices orientated so as to direct jets of fuel both sides of said median plane. The cross-section area of the annulus is varied by varying the radial width of the annulus, this being achieved conveniently in a circular bowl by offsetting the axis (C) of the projection (4) radially from the axis of the bowl (A).

Abstract: A method of operating air-compressing direct-injecting internal combustion engines including at least one piston with a combustion chamber of a shape of a body of rotation, and a fuel injector with a controllable outlet and a throttle member for controlling the fuel injection-pressure is disclosed. The velocity of combustion air rotating about the longitudinal central axis of the combustion chamber and the velocity of the fuel stream when leaving the injector are coordinated to one another. The surface area of the fuel which is contactable by combustion air is controllable so that on increase of the speed of the internal combustion engine the surface area is decreased.

Abstract: An air-compressing, direct-injection internal combustion engine formed with a combustion chamber in the shape of a solid of revolution in the piston crown into which fuel is injected via only one jet through an injection nozzle arranged obliquely in the cylinder head, in the direction of the rotating air for combustion. The working of the internal combustion engine is proposed to be improved in such a way that fuel deflection liable to occur in all operating ranges, mainly at the start and at the end of injection due to the rotating air flow and, respectively, when the gas is flowing out of the combustion chamber after the top dead center position, is prevented from affecting the working of the engine and from producing erosion on the piston crown and/or cylinder head.

Abstract: In an internal combustion engine including a combustion chamber in a cylinder, an intake port communicated with the combustion chamber at an upper portion of the cylinder, and an intake valve for controlling intake air which flows from the intake port into the combustion chamber at the upper portion of the cylinder, the intake port turns around a valve shaft of an intake valve in a spiral shape so as to produce swirls in the cylinder. The axis of the intake valve is positioned at the plane passing the central axis of the cylinder. The axis of the major intake air flow at an entrance of the intake port is positioned at one side of or out of the plane. The axis of the major intake air flow extends to intersect an inner turning wall of a turning portion of the intake port. The inner turning wall further passes the plane from the one side of the plane to the other side of the plane.

Abstract: Internal combustion reciprocating-piston engine precombustion chamber in which a mass of air or of air mixed with selective amounts of fuel and a spark-ignitable air-fuel mass are relatively segregatively compressed with the latter mass enveloping spark electrodes preparatory to ignition. The chamber is provided by recessing the air intake valve of an engine cylinder into the air intake passage for that cylinder so the chamber forms a section of that passage between the valve and the variable volume space above the piston in the cylinder. Contaminant products of combustion residual in the precombustion chamber upon completion of each combustion stroke are, during the next air intake stroke, vented into the cylinder variable volume space where they become mixed with the fresh intake air and any fuel entrained therein and then forced with this air back into the chamber pursuant to the ensuing compression stroke to be recycled during the next combustion stroke.

Abstract: A method of operating an internal combustion engine of the spark ignition type with a fuel having a high latent heat of vaporization such as methanol by injecting the fuel in two stages, the first major portion of the fuel being injected at the start of the intake stroke into a bowl-in-piston cavity combustion chamber to be vaporized and atomized, the second smaller portion being injected late in the compression stroke just prior to ignition to remain close to the injector tip to richen the mixture adjacent the spark plug, and igniting the mixture.

Abstract: A method and apparatus for combusting diesel, gasoline, kerosene, alcohol and other compression ignition fuels in either direct or indirect injection compression auto ignition internal combustion engines which enables such engines to operate at low compressions. The apparatus includes an ignition chamber which functions to receive a portion of the incoming fuel charge thereby concentrating such portion in an area separate from the auxiliary or primary combustion chambers.

Abstract: An internal combustion engine has a cylinder with a movable piston and a cylinder head, a main combustion chamber and an additional combustion chamber, elements producing a twisted stream rotating about an axis of the additional combustion chamber, an injecting nozzle opening in an aspirating passage, and an external igniting device, wherein the injecting nozzle is formed as a single-hole injecting nozzle and has an injection hole which is directed substantially against the igniting device.

Abstract: A prechamber type diesel engine is provided with a cutoff valve in the throat connecting the prechamber and main chamber of each cylinder and operable in cyclically timed fashion to close and open communication between these chambers. Methods of engine operation are disclosed which utilize the cutoff valve to (1) trap combustion products in the prechamber from the previous expansion stroke for use in mixing with the fresh charge in the following compression stroke to provide internal EGR preferably stratified in the prechamber and (2) permit low compression ratio starting by trapping compression pressure in the prechamber from a previous compression stroke for addition to combustion chamber pressure developed on the following compression stroke to provide a higher cylinder pressure for starting than that provided by the overall compression ratio. Advantages of improved engine efficiency and reduced emission levels are anticipated.

Abstract: The invention sets forth a method and apparatus for improving the injection and mixture of fuel and air in air-compressing combustion engines. The fuel is admitted into a rotationally symmetrical combustion chamber in such a manner that all droplets of the fuel stream are finely atomized at all speed and/or load ranges of the engine, and that the complete spray on entering the combustion chamber is so broken up that, from the combustion chamber wall to a point approximately one third of the combustion chamber radius, the broken-up spray matches the combustion chamber geometry, the injection of the fuel being effected in such a manner as to match the velocity and/or density distribution of the combustion air which rotates in the combustion chamber.

Abstract: The invention relates to a swirl-chamber Diesel engine. A swirl-chamber Diesel engine is disclosed which has a main combustion chamber, a swirl chamber, and a communicating passage for connecting them. The problem encountered is that, when the engine runs at low speeds, fuel droplets within the swirl chamber will gather and flow along the communicating passage into the main combustion chamber. To prevent this unfavorable fuel flow, a depression is formed within the swirl chamber to collect the fuel droplets. The depression is disposed adjacent to and communicating with the communicating passage via a rounded lip to provide an arrangement which will make it easy for the combustion gases flow to draw the collected fuel from the depression. Since the fuel is drawn from the depression by the combustion gases flow, carbonization of fuel on the depression wall will not take place.

Abstract: Disclosed is a two-cycle, internal combustion engine including an engine block, and a cylinder in the engine block having a head and generally opposed inlet and outlet walls respectively including at least one intake port through which a fresh charge is admitted into the cylinder and at least one outlet port through which exhaust gases are exhausted from the cylinder. A piston is mounted for reciprocative movement inside the cylinder between a first position spaced from the cylinder head wherein the intake port is uncovered, a top dead center position, and a third position wherein the piston approaches the top dead center position. The piston has a top, an inlet face portion which periodically covers and uncovers the intake port and an outlet face portion which periodically covers and uncovers the outlet port. The piston and cylinder have a configuration causing increased swirling of the fresh charge in the cylinder as the piston moves from the third position to the top dead center position.

Abstract: In an internal combustion engine, the combination of a cylinder head with a plane lower surface and a cavity, a piston with a plane upper surface and a cavity, the plane surfaces of the piston and the cylinder head cooperating to form a squish area on one side of the cylinder bore, and a spark plug protruding into the combustion chamber defined by the cavities so that its igniting tip lies substantially in the squish plane on the other side of the cylinder bore.

Abstract: A torch ignition apparatus and method, the apparatus including a secondary, torch ignition piston interconnected to the primary piston and operable to produce through compression ignition of a carbureted fuel/air mixture a jet of hot gases capable of igniting a fuel and air mixture compressed in a primary combustion chamber by the primary piston. The apparatus also includes a secondary fuel system for supplementing a low ratio fuel/air mixture in the combustion chamber and a novel hoop valve and exhaust port system for providing a unique, highly efficient flow-through system for exchanging gases in the combustion chamber.

Abstract: An internal combustion engine having an auxiliary combustion chamber connected to only the main combustion chamber via a connecting passage. The engine comprises a first raised portion formed on the inner wall of the cylinder head, a second raised portion formed on the top face of the piston at a position opposite to the first raised portion with respect to the axis of the piston, and a third raised portion formed on the inner wall of the cylinder head above the second raised portion. A first flat squish area is formed between the flat peripheral top face of the piston and the flat bottom face of the first raised portion. A second spherical shell shape squish area is formed between the spherical bottom wall of the third raised portion and the spherical rear face of the second raised portion. A recessed portion is formed on the top wall of the main combustion chamber at a position near the first raised portion. The open end of the connecting passage is arranged in the recessed portion.

Abstract: An injection nozzle for an air-compressing direct injection internal combustion engine which has a combustion chamber in the shape of a body of revolution in the piston head or in the cylinder head, and in which a rotary air movement occurs in the combustion chamber about its longitudinal axis while a portion of the injected liquid fuel is being deposited as a thin film on the wall of the combustion chamber. The injection nozzle has a slot-shaped discharge opening which is so located with regard to the combustion chamber that the fuel spray emitted through this discharge opening, when viewed over its entire width, at nearly the same time impinges upon the combustion chamber wall and spreads thereon in the form of a wide surface film, the cross section of the discharge opening corresponding to the cross section of a one-bore injection nozzle customarily employed for the mixture formation and combustion method under the same conditions.

Abstract: An internal combustion engine comprises a main combustion chamber and an auxiliary combustion chamber which are interconnected to each other via a connecting passage. The spark plug is arranged in the connecting passage. The engine further comprises a first raised portion formed on the inner wall of the cylinder head, a second raised portion formed on the top face of the piston at a position opposite to the first raised portion with respect to the axis of the piston, and a third raised portion formed on the inner wall of the cylinder head above the second raised portion. A first flat squish area is formed between the flat peripheral top face of the piston and the flat bottom face of the first raised portion. A second spherical shell shaped squish area is formed between the spherical bottom wall of the third raised portion and the spherical rear face of the second raised portion. The axis of the connecting passage is located in the extension of the second squish area.

Abstract: An air-compressing direct injection internal combustion engine having a combustion chamber in the shape of a body of revolution which combustion chamber at the end of the compression stroke contains nearly the entire necessary amount of combustion air which by suitable means is circulated about the cylinder axis of the respective pertaining cylinder of the engine. In this engine, a substantial portion of the liquid fuel is in the form of a thin film applied to the combustion chamber wall where it is processed so as to be picked up by and intermixed with the combustion air, whereupon the fuel air mixture is burnt. For purposes of facilitating the processing of the above mentioned fuel film and/or the realization of a pre-oxidation of the fuel, and for facilitating the pick-up of the fuel in the direction of the rotation of the air, additional means are provided and arranged in or on the combustion chamber wall and, when viewed in the direction of rotation of the air are located ahead of the fuel film.

Abstract: Internal combustion engine wherein a main air fuel charge is ignited by first igniting a pilot air fuel charge and bringing the two charges together, the main charge being compressed before ignition to a higher compression ratio than the pilot charge.

Abstract: The invention relates to a swirl-chamber Diesel engine. A swirl-chamber Diesel engine is disclosed which has a piston formed with a curved groove at its crown and in which a communicating passage, between a main combustion and a swirl chamber, connects tangentially into the swirling air charge within the main combustion chamber. The curved groove has one end which, when the piston is on its top dead center, communicates with the swirl chamber through the communicating passage. It is curved generally along the swirling air charge and has an opposite end widened and arranged so as to direct the subsequent combustion gases toward the center of the main combustion chamber and permit them to diffuse thereabout. With this arrangement, the swirling air charge within the main combustion chamber and the penetrating force of the subsequent combustion gases entering into the main combustion chamber from the communicating passage are fully utilized to encourage the feeding of air to the fuel.

Abstract: A multi-cylinder internal combustion engine having a plurality of cylinders, each comprising a combustion chamber and an accumulation chamber which are interconnected to each other via an accumulation valve. The accumulation chambers are interconnected to each other via a common connecting passage. The opening operation of the accumulation valve is controlled so that the accumulation valve remains opened during the compression stroke. In the first half of the compression stroke, a jet of the combustible mixture is spouted out into the combustion chamber from the accumulation chamber to create a strong swirl motion in the combustion chamber. In the latter half of the compression stroke, the combustible mixture in the combustion chamber flows into the accumulation chamber to accumulate the combustible mixture under high pressure, which is spouted out into the combustion chamber at the next cycle.

Abstract: Several embodiments of internal combustion engines each having an arrangement for increasing turbulence in the combustion chamber under at least certain load and/or speed conditions so as to permit the use of a relatively simple spark advance mechanism. In each embodiment, the flame propogation is controlled by controlling the degree of turbulence to achieve the desired effect. The turbulence is generated by causing induction of at least a portion of the engine charge requirements through a relatively small cross sectional area auxilliary induction passage. Because of the small cross sectional area, high flow velocities are generated which are maintained in the combustion chamber. In accordance with certain embodiments of the invention, the degree of turbulence is controlled by either shunting some of the air flow through the main induction passage or by introducing controlled amounts of exhaust gas products.

Abstract: An internal combustion engine comprising a combustion chamber and an accumulation chamber which are interconnected to each other via an accumulation valve. The accumulation chamber is filled with catalyzer pellets for reforming the combustible mixture accumulated in the accumulation chamber. The accumulation valve is opened during the compression stroke. In the first half of the compression stroke, a jet of the reformed combustible mixture is spouted into the combustion chamber from the accumulation chamber to create a strong swirl motion in the combustion chamber. In the latter half of the compression stroke, the combustible mixture in the combustion chamber flows into the accumulation chamber where the combustible mixture accumulates under high pressure, and the mixture is then spouted into the combustion chamber at the next cycle, from the accumulation chamber.

Abstract: An internal combustion engine comprising a combustion chamber, an injection chamber connected thereto through an injection port, a secondary inlet passage opening to the injection chamber, and a secondary inlet valve for opening and closing the secondary inlet passage. A spark plug is extended into the combustion chamber so as to dispose a spark gap of the plug close to the injection port. At the suction stroke of the engine, air in the injection chamber is injected near to the spark gap through the injection port to blow away the combustion gas around the gap and also to generate a strong swirl and turbulence of the mixture in the combustion chamber, thereby improving firing and combustion of the lean mixture in the combustion chamber to reduce the discharge of noxious components in the exhaust gas and improve the fuel consumption.