EP0754268B1 - Two-stroke diesel engine with a spiral air intake duct - Google Patents

Two-stroke diesel engine with a spiral air intake duct Download PDF

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Publication number
EP0754268B1
EP0754268B1 EP96900828A EP96900828A EP0754268B1 EP 0754268 B1 EP0754268 B1 EP 0754268B1 EP 96900828 A EP96900828 A EP 96900828A EP 96900828 A EP96900828 A EP 96900828A EP 0754268 B1 EP0754268 B1 EP 0754268B1
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cylinder
port
disposed
diesel engine
admission port
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German (de)
French (fr)
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EP0754268A1 (en
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Pierre-Antoine Jeandupeux
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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
    • F02B25/00Engines characterised by using fresh charge for scavenging cylinders
    • F02B25/14Engines characterised by using fresh charge for scavenging cylinders using reverse-flow scavenging, e.g. with both outlet and inlet ports arranged near bottom of piston stroke
    • 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
    • F02B2275/14Direct injection into combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition

Definitions

  • the principle of the invention relates to a diesel engine with two-stroke with volute air intake channel, and more particularly to a diesel engine which has a channel air intake which has a spiral shape and is arranged on part of the circumference of the wall of the cylinder, the intake channel which is arranged at the location of the bottom dead center of the piston being connected to the cylinder by channels of transfer which are separated by walls in the shape of blades.
  • two-stroke diesel engines operate on the principle that the air intake, which is the oxidizer, is constant, and the fuel injection is variable.
  • the action on the accelerator pedal adjusts the amount of fuel which is distributed.
  • the power of two-stroke diesel engines is dependent on the quality of the oxidizer-fuel mixture, the optimal power being obtained when each molecule of fuel can ally to an oxidizer molecule.
  • the mixing of the oxidizer in the cylinder is essential to ensure that an optimal proportion of fuel molecules can ally with molecules of oxidizer. Insufficient mixing of the oxidizer results in a lack of homogeneity of the oxidizer-fuel mixture which reflected in the fact that a certain proportion of the fuel is not burnt and by the fact that the engine whose combustion is incomplete, works with a large excess of oxidizer.
  • valve-light combinations for example, the lights being intended for the intake of oxidizer and the valves to the exhaust of the burnt gases or vice versa.
  • An embodiment known as the Schnurle principle has several lights which are arranged in a way symmetrical on each side of the cylinder. This form of execution has allowed to bring some increase in brewing and by therefore power and efficiency. However, the arrival symmetrical oxidant in the cylinder does not create sufficient mixing which again results in a strong loss of power and efficiency relative to power and optimal performance.
  • the aims of the present invention therefore consist in remedying to the aforementioned drawbacks of known diesel engines.
  • the two-stroke diesel engine with volute air intake channel comprises an air intake channel which is arranged over a large part of the circumference of the cylinder wall and which is connected to the cylinder by transfer channels which are separated from each other by vanes.
  • the air is propelled into the volute intake channel by a turbo-compressor for example.
  • the vanes separating the transfer channels are arranged at angles to the axis of the cylinder. In this way the air admitted when the piston is in bottom dead center, is propelled into the cylinder with a very strong vortex movement. This circular vortex movement is supplemented by an upward movement caused by the fact that the transfer channels gradually present an upward angle of the cylinder.
  • the first transfer channel is arranged so that the air is propelled horizontally into the cylinder and the last channel is arranged so that the air is propelled at an angle of 45 ° upwards by example.
  • the strong vortex and circular movement and the progressive upward mixing of the air thus created in the cylinder are further accentuated by the fact that the volume of air admitted into the cylinder becomes progressively concentrated, by the displacement of the piston towards the high, in the combustion chamber whose volume is much smaller than the cylinder.
  • the very strong mixing of the air thus created makes it possible to guarantee a very significant improvement in the homogeneity of the oxidizer-fuel mixture which makes it possible to approach optimum power and efficiency.
  • the very significant improvement in power and efficiency obtained by the principle of the invention allows, at power -equal supply compared to known two-stroke diesel engines, significantly reduce consumption and pollution.
  • the principle of the invention allows significantly increase engine power while avoiding, by complete combustion, that this increase in power does result in increased pollution.
  • Figures 1 and 2 are sectional views, respectively vertical and horizontal, cylinder and piston of an engine two-stroke diesel with an air intake channel in volute.
  • Figures 3, 4 and 5 are vertical section views of transfer channels, respectively at the start, in a portion intermediate and at the end of the air intake channel.
  • Figures 6 and 7 are sectional views, respectively vertical and horizontal, of an embodiment of a cylinder comprising an exhaust channel with closure device.
  • Figures 8 and 9 are sectional views, respectively vertical and horizontal, of a cylinder with a channel volute air intake and an exhaust channel which also has a scroll shape.
  • the wall of a cylinder 2 has an air intake channel 1 which has a scroll shape.
  • the air intake channel 1 is arranged on the much of the circumference of the cylinder wall 2.
  • the air intake channel 1 is connected to the inside of cylinder 2 by transfer channels, for example 3, 4 and 5.
  • the transfer channels are separated from each other by vanes, by example vanes 6, 7 and 8.
  • the vanes are arranged in a angle with respect to the central axis of the cylinder.
  • the canals of transfer are arranged at the bottom dead center of a piston 9, so that they are open when the piston found in bottom dead center.
  • the head of the piston 9 has a combustion chamber 10 in which the fuel-oxidant mixture takes place when the piston is in neutral high and when the fuel injector 11 injects the fuel.
  • combustion of the fuel-oxidant mixture occurs through self-ignition which is caused by the combined effects of the very strong pressure and temperature in the combustion chamber.
  • air, or oxidizer is powered in the intake channel 1 by a turbo-compressor, for example.
  • the air thus propelled into the intake channel 1 is propelled into cylinder 2 by the transfer channels.
  • the vanes that separate the transfer channels are arranged in a angle relative to the central axis of the cylinder so that the air is propelled inside the cylinder with a very strong vortex movement around the cylinder axis.
  • Air or oxidizer is allowed when the piston discovers the transfer.
  • the vortex movement of air or oxidizer is still greatly increased during the rise of the piston, due the difference in volume between the cylinder and the combustion.
  • the intake channel 1 has a volute shape and the intake channel becomes progressively smaller by so that the air pressure propelled by the channels which are sufficient at the end of the air intake channel.
  • Figure 3 shows a channel transfer 3 which is arranged at the start of the intake channel 1.
  • the upper and lower faces of the transfer channel 3 are arranged in the horizontal plane and in this case the air is propelled horizontally in the cylinder.
  • Figure 4 shows a transfer channel 4 which is arranged in a portion intermediate of the intake channel 1.
  • the upper faces and bottom of transfer channel 4 are arranged at an angle upwards from the horizontal plane.
  • Figure 5 shows a transfer channel 5 which is arranged at the end of the channel 1.
  • the upper and lower sides of the transfer 5 are arranged with a strong upward angle by compared to the horizontal plane.
  • the angle of the faces upper and lower transfer channels increase gradually from 0 ° for the first channel to 45 °, by example, for the last channel. In this way, in addition to the vortex movement around the cylinder axis, the air is gradually propelled up the cylinder which further strengthens the vortex movement.
  • the very strong vortex movement is amplified in the combustion chamber when the piston is in neutral high, and this strong vortex movement guarantees a optimal fuel-oxidizer mixture when fuel is distributed. This optimal mixture guarantees combustion complete which allows to obtain a very important improved performance which also results in significant pollution reduction.
  • the air intake channel 1 has a volute shape, or a spiral shape, the intake channel being progressively arranged downward in depending on the angle of the transfer channels.
  • Figures 1 and 2 do not show exhaust.
  • the exhaust is conventional and can consist of a valve arranged in the upper part of the cylinder by example.
  • Figures 6 and 7 show an embodiment of a cylinder 14 which also includes an injector 11, with a piston 9 which has a combustion chamber 10, the piston being in this case shown in top dead center.
  • the air intake channel 12, which is connected inside the cylinder by transfer channels, for example the first channel 13, is shorter than the intake channel shown in FIGS. 1 and 2.
  • An exhaust channel 15 is arranged, in the same horizontal plane, between the beginning and the end of the canal air intake. According to this form of execution, it is the fort eddy air movement which guarantees the evacuation of burnt gases.
  • This embodiment includes a obturation device 16 which temporarily closes the channel exhaust in the first intake phase so as to prevent some of the admitted air from escaping through the channel exhaust.
  • Figures 8 and 9 show an embodiment of a cylinder 16 which comprises an intake channel 17, which comprises transfer channels, for example transfer channel 18, which is shorter than on the forms of executions shown on Figures 1, 2, 6 and 7.
  • This embodiment comprises, on a part of the circumference of the cylinder, an exhaust channel 19 which is connected to the cylinder by transfer channels, the channel transfer 20 for example.
  • Channel transfer channels exhaust are separated by vanes which form an angle by relative to the central axis of the cylinder. This form of execution with exhaust channel can allow better evacuation of burnt gases, depending on the vortex movement of the air admitted.
  • the number of different transfer channels can be varied according to the different engine designs, as well as the angles of the blades or of the upper or lower faces of the transfer channels.
  • the principle of the invention is independent of the number of engine cylinder, the principle can be applied as well single cylinder engines than multiple engines cylinders.

Description

Le principe de l'invention se rapporte à un moteur diesel à deux temps avec canal d'admission d'air en volute, et plus particulièrement à un moteur diesel qui comporte un canal d'admission d'air qui présente une forme de spirale et qui est disposé sur une partie de la circonférence de la paroi du cylindre, le canal d'admission qui est disposé à l'endroit du point mort bas du piston étant relié au cylindre par des canaux de tranfert qui sont séparés par des parois en forme d'aubes.The principle of the invention relates to a diesel engine with two-stroke with volute air intake channel, and more particularly to a diesel engine which has a channel air intake which has a spiral shape and is arranged on part of the circumference of the wall of the cylinder, the intake channel which is arranged at the location of the bottom dead center of the piston being connected to the cylinder by channels of transfer which are separated by walls in the shape of blades.

D'une manière générale, les moteurs diesel à deux temps fonctionnent selon le principe que l'admission d'air, qui est le comburant, est constante, et que l'injection du carburant est variable. Dans le cas d'un véhicule par exemple, l'action sur la pédale d'accélérateur permet de régler la quantité de carburant qui est distribuée.Generally speaking, two-stroke diesel engines operate on the principle that the air intake, which is the oxidizer, is constant, and the fuel injection is variable. In the case of a vehicle for example, the action on the accelerator pedal adjusts the amount of fuel which is distributed.

La puissance des moteurs diesel à deux temps est dépendant de la qualité du mélange comburant-carburant, la puissance optimale étant obtenue lorsque chaque molécule de carburant peut s'allier à une molécule de comburant. Le brassage du comburant dans le cylindre est essentiel pour garantir qu'une proportion optimale de molécules de carburant puisse s'allier aux molécules de comburant. Un brassage insuffisant du comburant se traduit par un manque d'homogénéité du mélange comburant-carburant qui se traduit par le fait qu'une certaine proportion du carburant n'est pas brûlée et par le fait que le moteur dont la combustion est incomplète, fonctionne avec un important excédent de comburant.The power of two-stroke diesel engines is dependent on the quality of the oxidizer-fuel mixture, the optimal power being obtained when each molecule of fuel can ally to an oxidizer molecule. The mixing of the oxidizer in the cylinder is essential to ensure that an optimal proportion of fuel molecules can ally with molecules of oxidizer. Insufficient mixing of the oxidizer results in a lack of homogeneity of the oxidizer-fuel mixture which reflected in the fact that a certain proportion of the fuel is not burnt and by the fact that the engine whose combustion is incomplete, works with a large excess of oxidizer.

Tous les moteurs diesel à deux temps connus fonctionnent avec un brassage insuffisant du comburant et cet inconvénient essentiel provoque des diminutions de puissance et de rendement importantes.All known two-stroke diesel engines operate with insufficient mixing of the oxidizer and this drawback essential causes reductions in power and efficiency important.

La plupart des moteurs diesel à deux temps connus comportent des combinaisons soupapes-lumières, par exemple, les lumières étant destinées à l'admission du comburant et les soupapes à l'échappement des gaz brûlés ou inversément.Most known two-stroke diesel engines have valve-light combinations, for example, the lights being intended for the intake of oxidizer and the valves to the exhaust of the burnt gases or vice versa.

Une forme d'exécution connue sous le nom de principe Schnurle comporte plusieurs lumières qui sont disposées d'une manière symétrique de chaque côté du cylindre. Cette forme d'exécution a permis d'apporter une certaine augmentation du brassage et par conséquent de la puissance et du rendement. Toutefois, l'arrivée symétrique du comburant dans le cylindre ne permet pas de créer un brassage suffisant ce qui se traduit encore par une forte perte de puissance et de rendement par rapport à la puissance et rendement optimaux.An embodiment known as the Schnurle principle has several lights which are arranged in a way symmetrical on each side of the cylinder. This form of execution has allowed to bring some increase in brewing and by therefore power and efficiency. However, the arrival symmetrical oxidant in the cylinder does not create sufficient mixing which again results in a strong loss of power and efficiency relative to power and optimal performance.

En fonction des inconvénients précités des moteurs diesels à deux temps connus et en fonction des problèmes d'environnement et de ressources d'énergie, il est envisageable que ces moteurs, qui sont actuellement utilisés principalement en fonction de leur fiabilité et du faible coût du carburant, soient progressivement proscrits si des améliorations importantes ne sont pas apportées.Depending on the aforementioned drawbacks of diesel engines two known times and depending on environmental issues and of energy resources, it is conceivable that these motors, which are currently used mainly based on their reliability and low fuel cost, are gradually prohibited if significant improvements are not made.

Les buts de la présente invention consistent donc à remédier aux inconvénients précités des moteurs diesel connus.The aims of the present invention therefore consist in remedying to the aforementioned drawbacks of known diesel engines.

Les buts sont atteints selon le principe de l'invention décrit dans la revendication 1.The objects are achieved according to the principle of the invention described in claim 1.

Le moteur diesel à deux temps avec canal d'admission d'air en volute, selon le principe de l'invention, comporte un canal d'admission d'air qui est disposé sur une grande partie de la circonférence de la paroi du cylindre et qui est reliée au cylindre par des canaux de transfert qui sont séparés entre eux par des aubes. L'air est propulsé dans le canal d'admission en volute par un turbo-compresseur par exemple. Les aubes séparant les canaux de transfert sont disposées selon des angles par rapport à l'axe du cylindre. De cette manière l'air admis lorsque le piston se trouve au point mort bas, est propulsé dans le cylindre avec un très fort mouvement tourbillonaire. Ce mouvement tourbillonaire circulaire est complété par un mouvement vers le haut provoqué par le fait que les canaux de tranferts présentent progressivement un angle vers le haut du cylindre. En effet, le premier canal de transfert est disposé de manière à ce que l'air soit propulsé horizontalement dans le cylindre et le dernier canal est disposé de manière à ce que l'air soit propulsé selon un angle de 45° vers le haut par exemple. Le fort mouvement tourbillonaire et circulaire et le brassage progressif vers le haut de l'air ainsi créés dans le cylindre sont encore fortement accentués par le fait que le volume d'air admis dans le cylindre devient progressivement concentré, par le déplacement du piston vers le haut, dans la chambre de combustion dont le volume est beaucoup plus petit que le cylindre.
Le très fort brassage de l'air ainsi créé permet de garantir une très importante amélioration de l'homogénéité du mélange comburant-carburant qui permet de s'approcher de la puissance et du rendement optimaux.
The two-stroke diesel engine with volute air intake channel, according to the principle of the invention, comprises an air intake channel which is arranged over a large part of the circumference of the cylinder wall and which is connected to the cylinder by transfer channels which are separated from each other by vanes. The air is propelled into the volute intake channel by a turbo-compressor for example. The vanes separating the transfer channels are arranged at angles to the axis of the cylinder. In this way the air admitted when the piston is in bottom dead center, is propelled into the cylinder with a very strong vortex movement. This circular vortex movement is supplemented by an upward movement caused by the fact that the transfer channels gradually present an upward angle of the cylinder. In fact, the first transfer channel is arranged so that the air is propelled horizontally into the cylinder and the last channel is arranged so that the air is propelled at an angle of 45 ° upwards by example. The strong vortex and circular movement and the progressive upward mixing of the air thus created in the cylinder are further accentuated by the fact that the volume of air admitted into the cylinder becomes progressively concentrated, by the displacement of the piston towards the high, in the combustion chamber whose volume is much smaller than the cylinder.
The very strong mixing of the air thus created makes it possible to guarantee a very significant improvement in the homogeneity of the oxidizer-fuel mixture which makes it possible to approach optimum power and efficiency.

La très importante amélioration de puissance et de rendement obtenue par le principe de l'invention permet, à puissance -fournie égale par rapport aux moteurs diesel deux temps connus, de réduire considérablement la consommation et la pollution. A consommation égale, le principe de l'invention permet d'augmenter considérablement la puissance du moteur tout en évitant, par une combustion complète, que cette augmentation de puissance ne se traduise par une augmentation de la pollution.The very significant improvement in power and efficiency obtained by the principle of the invention allows, at power -equal supply compared to known two-stroke diesel engines, significantly reduce consumption and pollution. AT equal consumption, the principle of the invention allows significantly increase engine power while avoiding, by complete combustion, that this increase in power does result in increased pollution.

Les dessins annexés illustrent schématiquement et à titre d'exemple les principes de l'invention.The accompanying drawings illustrate schematically and by way of of example the principles of the invention.

Les figures 1 et 2 sont des vues en coupe, respectivement verticale et horizontale, du cylindre et du piston d'un moteur diesel à deux temps comportant un canal d'admission d'air en volute.Figures 1 and 2 are sectional views, respectively vertical and horizontal, cylinder and piston of an engine two-stroke diesel with an air intake channel in volute.

Les figures 3, 4 et 5, sont des vues en coupe verticale de canaux de tranfert, respectivement au début, dans une portion intermédiaire et au bout du canal d'admission d'air.Figures 3, 4 and 5 are vertical section views of transfer channels, respectively at the start, in a portion intermediate and at the end of the air intake channel.

Les figures 6 et 7 sont des vues en coupe, respectivement verticale et horizontale, d'une forme d'exécution d'un cylindre comportant un canal d'échappement avec dispositif d'obturation.Figures 6 and 7 are sectional views, respectively vertical and horizontal, of an embodiment of a cylinder comprising an exhaust channel with closure device.

Les figures 8 et 9 sont des vues en coupe, respectivement verticale et horizontale, d'un cylindre comportant un canal d'admission d'air en volute et un canal d'échappement qui présente également une forme de volute.Figures 8 and 9 are sectional views, respectively vertical and horizontal, of a cylinder with a channel volute air intake and an exhaust channel which also has a scroll shape.

En référence tout d'abord aux figures 1 et 2, la paroi d'un cylindre 2 comporte un canal d'admission d'air 1 qui présente une forme de volute. Le canal d'admission d'air 1 est disposé sur la grande partie de la circonférence de la paroi du cylindre 2. Le canal d'admission d'air 1 est relié à l'intérieur du cylindre 2 par des canaux de transfert, par exemple les 3, 4 et 5. Les canaux de transfert sont séparés entre eux par des aubes, par exemple les aubes 6, 7 et 8. Les aubes sont disposées selon un angle par rapport à l'axe central du cylindre. Les canaux de transfert sont disposés à l'endroit du point mort bas d'un piston 9, de manière à ce qu'ils soient ouverts lorsque le piston se trouve au point mort bas. La tête du piston 9 comporte une chambre de combustion 10 dans laquelle le mélange carburant-comburant s'effectue lorsque le piston se trouve au point mort haut et lorsque l'injecteur de carburant 11 injecte le carburant. Selon le principe des moteurs diesel à deux temps, la combustion du mélange carburant-comburant se produit par un auto-allumage qui est provoqué par les effets conjugués de la très forte pression et de la température dans la chambre de combustion. Selon le principe de l'invention, de l'air, ou comburant, est propulsé dans le canal d'admission 1 par un turbo-compresseur, par exemple. L'air ainsi propulsé dans le canal d'admission 1, est propulsé dans le cylindre 2 par les canaux de tranfert. Les aubes qui séparent les canaux de tranfert sont disposées selon un angle par rapport à l'axe central du cylindre de manière à ce que l'air soit propulsé à l'intérieur du cylindre avec un très fort mouvement tourbillonaire autour de l'axe du cylindre. L'air ou comburant est admis lorsque le piston découvre les canaux de transfert. Le mouvement tourbillonaire de l'air ou comburant est encore fortement augmenté lors de la montée du piston, en raison de la différence de volume entre le cylindre et la chambre de combustion. Le canal d'admission 1 présente une forme de volute et le canal d'admission devient progressivement plus petit de manière à ce la pression d'air propulsée par les canaux qui se trouvent en bout du canal d'admission d'air soit suffisante.Referring first to Figures 1 and 2, the wall of a cylinder 2 has an air intake channel 1 which has a scroll shape. The air intake channel 1 is arranged on the much of the circumference of the cylinder wall 2. The air intake channel 1 is connected to the inside of cylinder 2 by transfer channels, for example 3, 4 and 5. The transfer channels are separated from each other by vanes, by example vanes 6, 7 and 8. The vanes are arranged in a angle with respect to the central axis of the cylinder. The canals of transfer are arranged at the bottom dead center of a piston 9, so that they are open when the piston found in bottom dead center. The head of the piston 9 has a combustion chamber 10 in which the fuel-oxidant mixture takes place when the piston is in neutral high and when the fuel injector 11 injects the fuel. According to the principle of two-stroke diesel engines, combustion of the fuel-oxidant mixture occurs through self-ignition which is caused by the combined effects of the very strong pressure and temperature in the combustion chamber. According to the principle of the invention, air, or oxidizer, is powered in the intake channel 1 by a turbo-compressor, for example. The air thus propelled into the intake channel 1, is propelled into cylinder 2 by the transfer channels. The vanes that separate the transfer channels are arranged in a angle relative to the central axis of the cylinder so that the air is propelled inside the cylinder with a very strong vortex movement around the cylinder axis. Air or oxidizer is allowed when the piston discovers the transfer. The vortex movement of air or oxidizer is still greatly increased during the rise of the piston, due the difference in volume between the cylinder and the combustion. The intake channel 1 has a volute shape and the intake channel becomes progressively smaller by so that the air pressure propelled by the channels which are sufficient at the end of the air intake channel.

En référence aux figures 1 à 5, la figure 3 montre un canal de transfert 3 qui est disposé au début du canal d'admission 1. Les faces supérieure et inférieure du canal de transfert 3 sont disposées dans le plan horizontal et dans ce cas l'air est propulsée horizontalement dans le cylindre. La figure 4 montre un canal de transfert 4 qui est disposé dans une portion intermédiaire du canal d'admission 1. Les faces supérieure et inférieure du canal de transfert 4 sont disposées avec un angle vers le haut par rapport au plan horizontal. La figure 5 montre un canal de transfert 5 qui est disposé au bout du canal d'admission 1. Les faces supérieure et inférieure du canal de transfert 5 sont disposées avec un fort angle vers le haut par rapport au plan horizontal. En résumé, l'angle des faces supérieure et inférieure des canaux de transfert augmentent progressivement de 0° pour le premier canal jusqu'à 45°, par exemple, pour le dernier canal. De cette manière, en plus du mouvement tourbillonaire autour de l'axe de cylindre, l'air est progressivement propulsée vers le haut du cylindre ce qui renforce encore le mouvement tourbillonaire.Referring to Figures 1 to 5, Figure 3 shows a channel transfer 3 which is arranged at the start of the intake channel 1. The upper and lower faces of the transfer channel 3 are arranged in the horizontal plane and in this case the air is propelled horizontally in the cylinder. Figure 4 shows a transfer channel 4 which is arranged in a portion intermediate of the intake channel 1. The upper faces and bottom of transfer channel 4 are arranged at an angle upwards from the horizontal plane. Figure 5 shows a transfer channel 5 which is arranged at the end of the channel 1. The upper and lower sides of the transfer 5 are arranged with a strong upward angle by compared to the horizontal plane. In summary, the angle of the faces upper and lower transfer channels increase gradually from 0 ° for the first channel to 45 °, by example, for the last channel. In this way, in addition to the vortex movement around the cylinder axis, the air is gradually propelled up the cylinder which further strengthens the vortex movement.

Le très fort mouvement tourbillonaire est amplifié dans la chambre de combustion lorsque le piston se trouve au point mort haut, et ce fort mouvement tourbillonaire permet de garantir un mélange optimal carburant-comburant lorsque le carburant est distribué. Ce mélange optimal permet de garantir une combustion complète ce qui permet d'obtenir une très importante amélioration du rendement qui se traduit aussi par une importante diminution de la pollution.The very strong vortex movement is amplified in the combustion chamber when the piston is in neutral high, and this strong vortex movement guarantees a optimal fuel-oxidizer mixture when fuel is distributed. This optimal mixture guarantees combustion complete which allows to obtain a very important improved performance which also results in significant pollution reduction.

Comme montré par les figures 1 à 5, la canal d'admission d'air 1 présente une forme de volute, soit une forme de spirale, le canal d'admission étant progressivement disposé vers le bas en fonction de l'angle des canaux de transfert.As shown in Figures 1 to 5, the air intake channel 1 has a volute shape, or a spiral shape, the intake channel being progressively arranged downward in depending on the angle of the transfer channels.

Les figures 1 et 2 ne montrent pas d'échappement. Dans ce cas l'échappement est conventionnel et peut être constitué par une soupape disposée dans la partie supérieure du cylindre par exemple.Figures 1 and 2 do not show exhaust. In that case the exhaust is conventional and can consist of a valve arranged in the upper part of the cylinder by example.

Les figures 6 et 7 montrent une forme d'exécution d'un cylindre 14 qui comporte aussi un injecteur 11, avec un piston 9 qui comporte une chambre de combustion 10, le piston étant dans ce cas montré au point mort haut. Selon cette forme d'exécution, le canal d'admission d'air 12, qui est relié à l'intérieur du cylindre par des canaux de tranfert, par exemple le premier canal de transfert 13, est moins long que le canal d'admission montré sur les figures 1 et 2. Un canal d'échappement 15 est disposé, dans le même plan horizontal, entre le début et le bout du canal d'admission d'air. Selon cette forme d'exécution, c'est le fort mouvement tourbillonaire de l'air admis qui permet de garantir l'évacuation des gaz brûlés. Cette forme d'exécution comporte un dispositif d'obturation 16 qui obture momentanément le canal d'échappement dans la première phase d'admission de manière à éviter qu'une partie de l'air admis ne s'échappe par le canal d'échappement.Figures 6 and 7 show an embodiment of a cylinder 14 which also includes an injector 11, with a piston 9 which has a combustion chamber 10, the piston being in this case shown in top dead center. According to this embodiment, the air intake channel 12, which is connected inside the cylinder by transfer channels, for example the first channel 13, is shorter than the intake channel shown in FIGS. 1 and 2. An exhaust channel 15 is arranged, in the same horizontal plane, between the beginning and the end of the canal air intake. According to this form of execution, it is the fort eddy air movement which guarantees the evacuation of burnt gases. This embodiment includes a obturation device 16 which temporarily closes the channel exhaust in the first intake phase so as to prevent some of the admitted air from escaping through the channel exhaust.

Les figures 8 et 9 montrent une forme d'exécution d'un cylindre 16 qui comporte un canal d'admission 17, qui comporte des canaux de transfert, par exemple le canal de transfert 18, qui est plus court que sur les formes d'exécutions montrées sur figures 1, 2, 6 et 7. Cette forme d'exécution comporte, sur une partie de la circonférence du cylindre, un canal d'échappement 19 qui est relié au cylindre par des canaux de transfert, le canal de transfert 20 par exemple. Les canaux de transfert du canal d'échappement sont séparés par des aubes qui forment un angle par rapport à l'axe central du cylindre. Cette forme d'exécution avec canal d'échappement peut permettre une meilleure évacuation des gaz brûlés, en fonction du mouvement tourbillonaire de l'air admis.Figures 8 and 9 show an embodiment of a cylinder 16 which comprises an intake channel 17, which comprises transfer channels, for example transfer channel 18, which is shorter than on the forms of executions shown on Figures 1, 2, 6 and 7. This embodiment comprises, on a part of the circumference of the cylinder, an exhaust channel 19 which is connected to the cylinder by transfer channels, the channel transfer 20 for example. Channel transfer channels exhaust are separated by vanes which form an angle by relative to the central axis of the cylinder. This form of execution with exhaust channel can allow better evacuation of burnt gases, depending on the vortex movement of the air admitted.

Le nombre des différents canaux de transfert peut être varié en fonction des différentes conception des moteurs, de même que les angles des aubes ou des faces supérieure ou inférieure des canaux de transfert.The number of different transfer channels can be varied according to the different engine designs, as well as the angles of the blades or of the upper or lower faces of the transfer channels.

Le principe de l'invention est indépendant du nombre de cylindre du moteur, le principe pouvant être appliqué aussi bien à des moteurs mono-cylindre qu'à des moteurs à plusieurs cylindres.The principle of the invention is independent of the number of engine cylinder, the principle can be applied as well single cylinder engines than multiple engines cylinders.

Claims (5)

  1. A two-stroke diesel engine with a spiral-shaped air admission port comprising a cylinder (2) comprising transfer ports disposed at bottom dead center of a piston (9) comprising a combustion chamber (10), characterized in that a spiral-shaped air admission port (1) is disposed at the place of bottom dead center of the piston (9) on the greatest part of the circumference of the wall of the cylinder (2), the air admission port being connected to the cylinder by transfer ports separated from each other by vanes having an angle relative to the central axis of the cylinder such that air driven into the admission port and into the transfer ports is driven into the cylinder with a strong swirling movement around the central axis of the cylinder, and the upper and lower faces of the transfer ports progressively have an angle upward, the upper and lower faces of the transfer port disposed at the beginning of the admission port having a zero or very small angle relative to the horizontal plan and the upper and lower faces of the port disposed at the end of the admission port having a large angle upward relative to the horizontal plan such that air thus driven progressively toward the top of the cylinder creates an agitated movement.
  2. The diesel engine of claim 1, characterized in that the spiral-shaped air admission port becomes progressively smaller from its beginning to the end.
  3. The diesel engine of claim 1 or 2, characterized in that the air admission port has a spiral shape directed progressively downwards.
  4. The diesel engine of claim 1, characterized in that an exhaust port is disposed in the same horizontal plane as the transfer ports admitting air, and said exhaust port is disposed on part of the circumference of the cylinder wall between the beginning and the end of the admission port.
  5. The diesel engine of claim 1, characterized in that an exhaust port is disposed at the place of bottom dead center of the piston on part of the circumference of the cylinder wall, and said exhaust port is connected to the cylinder by transfer ports separated by vanes forming an angle relative to the central axis of the cylinder so as to facilitate escape of the exhaust gases in accordance with the swirling movement created in the cylinder.
EP96900828A 1995-02-06 1996-02-06 Two-stroke diesel engine with a spiral air intake duct Expired - Lifetime EP0754268B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CH32195A CH690307A5 (en) 1995-02-06 1995-02-06 diesel engine with two-stroke air intake channel volute.
CH321/95 1995-02-06
PCT/CH1996/000045 WO1996024757A1 (en) 1995-02-06 1996-02-06 Two-stroke diesel engine with a spiral air intake duct

Publications (2)

Publication Number Publication Date
EP0754268A1 EP0754268A1 (en) 1997-01-22
EP0754268B1 true EP0754268B1 (en) 1999-05-06

Family

ID=4184361

Family Applications (1)

Application Number Title Priority Date Filing Date
EP96900828A Expired - Lifetime EP0754268B1 (en) 1995-02-06 1996-02-06 Two-stroke diesel engine with a spiral air intake duct

Country Status (5)

Country Link
EP (1) EP0754268B1 (en)
AU (1) AU4480296A (en)
CH (1) CH690307A5 (en)
DE (1) DE69602317T2 (en)
WO (1) WO1996024757A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2496479A (en) 2011-11-11 2013-05-15 Ecomotors Internat Inc Intake System for an Opposed-Piston Engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB321514A (en) * 1928-09-28 1929-11-14 Charles Gordon Curtis Improvements in or relating to two-cycle internal combustion engines
FR724741A (en) * 1930-11-13 1932-05-02 Development of two-stroke internal combustion engines
GB541368A (en) * 1939-08-04 1941-11-25 Sulzer Ag Improvements in or relating to cylinders for internal combustion engines operating on the two-stroke cycle
US3059626A (en) * 1960-03-15 1962-10-23 Nordberg Manufacturing Co Two-cycle scavenging system

Also Published As

Publication number Publication date
WO1996024757A1 (en) 1996-08-15
EP0754268A1 (en) 1997-01-22
AU4480296A (en) 1996-08-27
CH690307A5 (en) 2000-07-14
DE69602317D1 (en) 1999-06-10
DE69602317T2 (en) 2000-01-13

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