EP1221535B1 - Axial combustion engine - Google Patents

Axial combustion engine Download PDF

Info

Publication number
EP1221535B1
EP1221535B1 EP01600029A EP01600029A EP1221535B1 EP 1221535 B1 EP1221535 B1 EP 1221535B1 EP 01600029 A EP01600029 A EP 01600029A EP 01600029 A EP01600029 A EP 01600029A EP 1221535 B1 EP1221535 B1 EP 1221535B1
Authority
EP
European Patent Office
Prior art keywords
flywheel
cylinders
motor
track
spherical
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
EP01600029A
Other languages
German (de)
French (fr)
Other versions
EP1221535A3 (en
EP1221535A2 (en
Inventor
Vasileios Dimos
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of EP1221535A2 publication Critical patent/EP1221535A2/en
Publication of EP1221535A3 publication Critical patent/EP1221535A3/en
Application granted granted Critical
Publication of EP1221535B1 publication Critical patent/EP1221535B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L1/00Valve-gear or valve arrangements, e.g. lift-valve gear
    • F01L1/12Transmitting gear between valve drive and valve
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L1/00Valve-gear or valve arrangements, e.g. lift-valve gear
    • F01L1/02Valve drive
    • F01L1/04Valve drive by means of cams, camshafts, cam discs, eccentrics or the like
    • F01L1/047Camshafts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L1/00Valve-gear or valve arrangements, e.g. lift-valve gear
    • F01L1/12Transmitting gear between valve drive and valve
    • F01L1/18Rocking arms or levers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/26Engines with cylinder axes coaxial with, or parallel or inclined to, main-shaft axis; Engines with cylinder axes arranged substantially tangentially to a circle centred on main-shaft axis

Definitions

  • the invention belongs to the category of internal combustion piston engine which for driving all types of vehicles, ships, aircraft, construction machinery, Agricultural machinery, machinery factories, generators, pumps, Compressors and generally where a drive is needed Use finds.
  • N M • ⁇
  • N M the torque
  • 2 ⁇ -n the angular velocity
  • n the operating speed of the engine.
  • V 1 ⁇ r (sin ⁇ + r sin2 ⁇ / 2s)
  • V 2 wr (sin ⁇ -r sin2 ⁇ / 2s)
  • is the angular velocity
  • r is the radius of the crankshaft
  • is the instantaneous angle of the crankshaft
  • s is the length of the connecting rod.
  • the raceways 33 of the web flywheel 3 are continuous and symmetrical in Reference to an orthogonal coordinate system, wherein the axis Z with the axis the shaft is identical and the coordinate zero point in the middle of the piston stroke lies. This results in symmetry with regard to both the direction of movement the piston as well as the direction of rotation of the shaft.
  • the geometry of the web flywheel forces the arrangement of the cylinders, without limitation of their number, on a uniform polygon whose Center is located on the axis of rotation of the engine.
  • the cylinder axes are running parallel to the axis of the shaft. This peculiarity also allows an aerodynamic Design of the engine, as it has a small front surface, a cylindrical and elongated Shape and a uniform projection of the heat of components of the engine allowed in the air flow.
  • the eccentric flywheel circularly actuates the valves one behind the other. Out For this reason, only one or two eccentrics are required, which are circular one by one actuate the intake and exhaust valves of all cylinders.
  • the new engine allows the use of several fuels (petrol, diesel, Gas u.s.w.) without intervention or modification of the main parts, but only by Add mechanisms or parts to the external auxiliary systems of the Engine. It is also possible, if necessary, a combination of to use different fuels.
  • the raceways 33 of the web flywheel 3 are during a single operation of the engine (intake - compression - expansion - outlet) unevenly claimed.
  • the function of the tracks is reversed. This is a big advantage because of the Life of the tracks is thereby extended.
  • the advantages mentioned can not be realized with a classic engine with crankshaft.
  • Axial internal combustion piston engines are disclosed, for example, in US Pat. No. 4,023,542 and US 4,553,508 A.
  • US 4 023 542 A teaches the formation of the track as a flat surface or as in cross-section rectangular hollow rail, wherein the rolling means as cylindrical rollers or rollers are provided. Accordingly, this provides conventional arrangement no centering property.
  • an axial combustion piston machine with axially arranged Proposed cylinders with intake and exhaust valves and pistons, which each attached to one end of an axially displaceable push rod are having means for receiving rolling means, which on an endless Wavy space curve forming webs run along, the annular circulating are formed on a train flywheel which is coaxial on one rotatably mounted shaft sitting on the shaft next to the train flywheel an outer main flywheel, a regulating flywheel that changes the compression ratio by shifting the web flywheel, and an eccentric flywheel which seats the intake and exhaust valves all cylinders are actuated, with the rolling means as balls or spherical rollers and the tracks are formed as cross-sectionally circular grooves, on which the balls or spherical rollers in the direction of movement of the Rest push rod.
  • Fig. 1 is a longitudinal section of the motor housing, the position, shape and arrangement a cylinder block 6, a cylinder head 7, of fixed bearings 8 as well represented by external auxiliary mechanisms 9.
  • FIG. 2 is a perspective view of the shaft with the components mounted thereon.
  • Fig. 3 is a typical view of the grooves 34, which in section in radial Direction of the web flywheel 3 have the shape of a circular arc.
  • Fig. 4 shows a representation of the shaft with special features, based on the railway flywheel 3 and the eccentric flywheel 4.
  • Fig. 5 shows a detail of the assembly of the web flywheel 3 and a push rod 5 with an indication of the operation of the regulating Flywheel 2 for the control of the parameters ⁇ dw>, through which the compression ratio being affected.
  • FIG. 6 shows a typical piston cross-section.
  • Fig. 7 shows a view of the eccentric flywheel 4 with eccentrics, which operate the intake and exhaust valves of all cylinders.
  • Fig. 8 shows a longitudinal section of a push rod 5 with an indication of the contiguous Components. Likewise, the location and shape of the spherical rollers 54 or balls visible through which the push rod 5 with the web flywheel 3 is coupled.
  • Fig. 9 shows a typical cross section of a 4-cylinder engine.
  • Fig. 10 shows a plan view of a cylinder head 7 of a typical 4-cylinder engine with an indication of the position and shape of the eccentric flywheel 4 as well the necessary organs for the operation of the corresponding intake and exhaust valves 43, 44.
  • Fig. 11 shows a detail of a characteristic view of the shaft, namely especially at the point where the eccentric flywheel 4 is attached, as well as the cooperation of the eccentric flywheel 4 with mechanical organs for the operation of the intake and exhaust valves 43, 44th
  • Fig. 12 shows a view of a web flywheel with eight vertices and a corresponding eccentric flywheel 4 with a twin eccentric.
  • Fig. 13 illustrates a use of the engine in a twin-engined firefighter aircraft represents.
  • the parameter tan ⁇ is related to the piston stroke l.
  • M p • F • R • f (l), where f (l) is a function between ⁇ and l. This means that for a given piston diameter, the torque is proportional to the existing pressure in the combustion chamber, the mean radius of the protruding ring of the web flywheel, and the piston travel.

Abstract

Axial internal combustion engine comprises a linear shaft consisting of an outer main flywheel (1), a regulating flywheel for the compression ratio, a path flywheel (3), and an eccentric flywheel (4). These components form a STROFEA. Preferred Features: The path flywheel has a central cylindrical core (31) surrounded by a shaft-like protruding ring (32) with a cylindrical outer surface. The other two surfaces of the ring form grooves so that each center line represents a continuous, undulating three-dimensional curve (33) with 4 or 8 apexes arranged symmetrically along the periphery.

Description

Die Erfindung gehört zur Kategorie der Verbrennungskolbenmaschine, welche für den Antrieb aller Typen von Fahrzeugen, Schiffen, Flugzeugen, Baumaschinen, Landwirtschaftsmaschinen, Maschinefabriken, Generatoren, Pumpen, Kompressoren und im allgemeinen dort, wo ein Antrieb benötigt wird, Verwendung findet.The invention belongs to the category of internal combustion piston engine which for driving all types of vehicles, ships, aircraft, construction machinery, Agricultural machinery, machinery factories, generators, pumps, Compressors and generally where a drive is needed Use finds.

Bei allen Verbrennungs-Kolbenmaschinen wird die geradlinige Bewegung der Kolben durch die Kurbelwelle in eine gleichmäßige Rotationsbewegung umgewandelt.In all combustion piston engines, the rectilinear motion of Pistons converted by the crankshaft into a uniform rotational motion.

Bei allen 4-Takt-Motoren wird Expansionsarbeit während jeder zweiten Umdrehung der Kurbelwelle geleistet. Für diesen Zweck dreht sich parallel zur Kurbelwelle die Nockenwelle, welche die Einlaß- und Außlaßventile betätigt. Die benötigten Leistungen werden durch Erhöhung der Zylinderzahl erzielt. In all 4-stroke engines, expansion work is performed every other revolution made the crankshaft. For this purpose, parallel to the Crankshaft the camshaft which actuates the intake and exhaust valves. The required services are achieved by increasing the number of cylinders.

Die charakteristische Größe bei allen diesen Motoren ist das abgegebene Drehmoment bei bestimmter Leistung und Betriebsdrehzahl. Der Zusammenhang der oben genannten Größen wird durch die folgende Gleichung wiedergegeben : N=M•ω wobei N die Leistung, M das Drehmoment, ω =2π-n die Winkelgeschwindigkeit und n die Betriebsdrehzahl des Motors darstellt.The characteristic variable in all these engines is the torque delivered at certain power and operating speed. The relationship of the above quantities is represented by the following equation: N = M • ω where N represents the power, M the torque, ω = 2π-n the angular velocity and n the operating speed of the engine.

Die Kolbengeschwindigkeit nach oben ist unterschiedlich zu der nach unten bei allen Motoren mit Kurbelwellen. Der mathematische Zusammenhang dieser Geschwindigkeiten lautet: V1= ω r (sin ϕ +r sin2ϕ/2s) V2= w r (sin ϕ-r sin2ϕ/2s) wobei ω die Winkelgeschwindigkeit, r der Radius der Kurbelwelle, ϕ der augenblickliche Winkel der Kurbelwelle und s die Länge der Pleulstange ist.The piston speed upwards is different to that down in all engines with crankshafts. The mathematical relationship between these speeds is: V 1 = ω r (sin φ + r sin2φ / 2s) V 2 = wr (sin φ-r sin2φ / 2s) where ω is the angular velocity, r is the radius of the crankshaft, φ is the instantaneous angle of the crankshaft, and s is the length of the connecting rod.

Es ist offensichtlich, daß unter der Annahme einer gleichmäßigen Drehbewegung der Welle (ω=konstant), die auftretende Kräfte infolge der hin und her bewegten Massen niemals dynamisch ausgeglichen sind. Dies hat die Begrenzung der Kolbengeschwindigkeit innerhalb bestimmter Sicherheitsgrenzen je nach Motoren-Hersteller zur Folge. Die Einhaltung dieser Grenzen begrenzt selbstverständlich die Leistung und Drehmoment des Motors.It is obvious that assuming a uniform rotational movement the wave (ω = constant), the forces due to the back and forth moved Masses are never dynamically balanced. This has the limitation of Piston speed within certain safety limits depending on engine manufacturer result. Of course, compliance with these limits is limited the power and torque of the engine.

Die oben genannten Nachteile der klassischen Motoren mit Kurbel- und Nockenwelle werden durch eine Axialverbrennungskolbenmaschine aufgehoben, bei dem die Kurbel- und Nockenwellen entfallen, welche durch eine einzige gerade Welle ersetzt werden. Die Umwandlung der reziproken Kolbenbewegung in eine gleichförmige Drehbewegung geschieht durch Laufbahnen 33 eines Bahn-Schwungrades 3, deren Funktion auf den Eigenschaften der schiefen Ebene basiert. Die Arbeit der Ventile wird von einem Exzenter-Schwungrad 4 gesteuert. The above-mentioned disadvantages of the classic engines with crankshaft and camshaft are picked up by an axial combustion piston machine which accounts for the crankshafts and camshafts, which are straight through a single Wave to be replaced. The conversion of the reciprocal piston movement into one uniform rotational movement is done by tracks 33 of a web flywheel 3, whose function is based on the properties of the inclined plane. The work of the valves is controlled by an eccentric flywheel 4.

Diese zwei Schwungräder und ein äußeres Hauptschwungrad 1 sind auf einer gerade Welle montiert.These two flywheels and an outer main flywheel 1 are on one straight shaft mounted.

Die Laufbahnen 33 des Bahn-Schwungrades 3 sind stetig und symmetrisch in Bezug auf ein orthogonales Koordinatensystem, wobei die Achse Z mit der Achse der Welle identisch ist und der Koordinaten-Nullpunkt in der Mitte des Kolbenweges liegt. Es entsteht dadurch Symmetrie im Hinblick sowohl auf die Bewegungsrichtung der Kolben als auch die Richtung der Drehbewegung der Welle.The raceways 33 of the web flywheel 3 are continuous and symmetrical in Reference to an orthogonal coordinate system, wherein the axis Z with the axis the shaft is identical and the coordinate zero point in the middle of the piston stroke lies. This results in symmetry with regard to both the direction of movement the piston as well as the direction of rotation of the shaft.

Die Bewegung (Geschwindigkeit, Beschleunigung) der nach oben und nach unten bewegten Schubstangen ist zu jeder Zeit gleich und entgegengesetzt. Dies bedeutet, daß zu jeder Zeit ein dynamischer Ausgleich der entstehenden Massenkräfte stattfindet. Ebenso findet auch gleichzeitig ein statischer Ausgleich statt. Dies liegt daran, daß die Bewegung der Kolben im Gegensatz zum klassischen Motor von der Länge der Schubstangen nicht beeinflusst wird, weil sie sich geradlinig und immer parallel zur Achse der Welle bewegen. Die Expansionsarbeit hängt nun ausschließlich von der Geometrie des Bahn-Schwungrades ab.The movement (speed, acceleration) of the up and down moving push rods is the same and opposite at all times. This means that at any time a dynamic balance of the resulting mass forces takes place. At the same time there is also a static balance instead of. This is because the movement of the pistons in contrast to the classic Motor is not affected by the length of the push rods, because they themselves straight and always parallel to the axis of the shaft. The expansion work now depends solely on the geometry of the train flywheel.

Wenn das Bahn-Schwungrad vier Scheitel entlang des Umfangs hat, dann werden die vier Takte während einer Umdrehung der Welle abgeschlossen - im Gegensatz zum klassischen Motor, bei dem die vier Takte in zwei Umdrehungen der Kurbelwelle erzielt werden. Folglich erzielt bei gleicher Betriebsdrehzahl der neue Motor genau die doppelte Arbeit gegenüber dem entsprechenden klassischen Motor. Aus Gleichung (1) kann man herleiten, daß das Drehmoment doppelt so groß ist wie beim klassischen Motor. Dies bedeutet, daß bei vorgegebener Leistung der neue Motor das entsprechende Drehmoment bei halber Betriebsdrehzahl gegenüber dem klassischen Motor erzeugt.If the train flywheel has four vertices along the circumference, then the four bars completed during one revolution of the wave - in contrast to the classic engine, in which the four bars in two turns of Crankshaft can be achieved. Consequently, achieved at the same operating speed of the new Motor exactly twice the work compared to the corresponding classic Engine. From equation (1) one can deduce that the torque is twice that big is like the classic engine. This means that for a given power the new engine the corresponding torque at half operating speed generated compared to the classic engine.

Wenn das Bahn-Schwungrad acht Scheitel entlang des Umfangs hat, dann sind die vier Takte nach halber Umdrehung der Welle abgeschlossen. Folglich erzeugt bei gleicher Betriebsdrehzahl der neue Motor genau die vierfache Arbeit gegenüber dem entsprechenden klassischen Motor. Dies bedeutet, daß bei vorgegebener Leistung der neue Motor das entsprechende Drehmoment bei einem Viertel der Betriebsdrehzahl gegenüber dem klassischen Motor erzeugt. If the train flywheel has eight vertices along the circumference, then there are completed the four bars after half turn of the shaft. Consequently generated at the same operating speed of the new engine exactly four times the work opposite the corresponding classic engine. This means that for a given Performance of the new engine the corresponding torque at one Quarter of the operating speed compared to the classic engine generated.

Bei der mathematischen Herleitung des Drehmomentes des neuen Motors geht außer dem Kolbenweg auch der Radius des Bahn-Schwungrades in die Rechnung ein. Dieser Parameter hat eine positive Wirkung auf die Auslegung des Motors.At mathematical derivation of a torque of the new engine passes except the piston stroke and the radius of the train flywheel in the bill one. This parameter has a positive effect on the design of the engine.

Weiterhin zwingt die Geometrie des Bahn-Schwungrades die Anordnung der Zylinder, ohne Begrenzung von deren Anzahl, auf ein gleichmäßiges Polygon, dessen Mittelpunkt auf der Drehachse des Motors liegt. Die Zylinderachsen laufen parallel zur Achse der Welle. Diese Eigenart erlaubt auch eine aerodynamische Gestaltung des Motors, da er eine kleine Frontfläche, eine zylindrische und längliche Form und eine gleichmäßige Projektion der Wärme von Bauteilen des Motors in der Luftströmung ermöglicht.Furthermore, the geometry of the web flywheel forces the arrangement of the cylinders, without limitation of their number, on a uniform polygon whose Center is located on the axis of rotation of the engine. The cylinder axes are running parallel to the axis of the shaft. This peculiarity also allows an aerodynamic Design of the engine, as it has a small front surface, a cylindrical and elongated Shape and a uniform projection of the heat of components of the engine allowed in the air flow.

Das Exzenter-Schwungrad betätigt kreisförmig die Ventile hintereinander. Aus diesem Grund sind nur ein oder zwei Exzenter erforderlich, welche kreisförmig hintereinander die Einlaß-und Auslaßventile aller Zylinder betätigen.The eccentric flywheel circularly actuates the valves one behind the other. Out For this reason, only one or two eccentrics are required, which are circular one by one actuate the intake and exhaust valves of all cylinders.

Außer den vorgenannten Vorteilen besteht auch die Möglichkeit der Verschiebung des Bahn-Schwungrades mit gekoppelten Schubstangen nach Bedarf in Längsrichtung der Achse der Welle. Die Verschiebung wird durch einen besonderen Mechanismus des regulierenden Schwungrades gewährleistet. Dadurch wird das Verdichtungsverhältnis beeinflusst gemäß der Gleichung:

Figure 00040001
wobei dV die Volumenänderung des Zylinders 11, R der Radius des Kolbens 10 und dw die gewählte Verschiebung des regulierenden Schwungrades 2 ist.In addition to the aforementioned advantages, there is also the possibility of displacement of the web flywheel with coupled push rods as needed in the longitudinal direction of the axis of the shaft. The displacement is ensured by a special mechanism of the regulating flywheel. This affects the compression ratio according to the equation:
Figure 00040001
where dV is the volume change of the cylinder 11, R is the radius of the piston 10 and dw is the selected displacement of the regulating flywheel 2.

Der neue Motor erlaubt die Verwendung von mehreren Kraftstoffen (Benzin, Diesel, Gas u.s.w.) ohne Eingriff oder Umbau an den Hauptteilen, sondern nur durch Hinzufügen von Mechanismen oder Teilen an den äußeren Hilfssystemen des Motors. Außerdem besteht die Möglichkeit, nach Bedarf eine Kombination von verschiedenen Kraftstoffen zur verwenden. The new engine allows the use of several fuels (petrol, diesel, Gas u.s.w.) without intervention or modification of the main parts, but only by Add mechanisms or parts to the external auxiliary systems of the Engine. It is also possible, if necessary, a combination of to use different fuels.

Die Laufbahnen 33 des Bahn-Schwungrades 3 werden während eines Arbeitsganges des Motors (Einlaß - Verdichtung - Expansion - Auslaß) ungleichmäßig beansprucht. Durch Drehung des Bahn-Schwungrades um die Achse der Welle wird die Funktion der Laufbahnen vertauscht. Dies ist ein großer Vorteil, weil die Lebensdauer der Laufbahnen dadurch verlängert wird. Die genannten Vorteile können mit einem klassischen Motor mit Kurbelwelle nicht verwirklicht werden.The raceways 33 of the web flywheel 3 are during a single operation of the engine (intake - compression - expansion - outlet) unevenly claimed. By rotation of the web flywheel about the axis of the shaft the function of the tracks is reversed. This is a big advantage because of the Life of the tracks is thereby extended. The advantages mentioned can not be realized with a classic engine with crankshaft.

Axial Verbrennungskolbenmaschinen sind beispielsweise in der US 4 023 542 A und der US 4 553 508 A offenbart.Axial internal combustion piston engines are disclosed, for example, in US Pat. No. 4,023,542 and US 4,553,508 A.

Die US 4 023 542 A lehrt die Ausbildung der Laufbahn als ebene Fläche bzw. als im Querschnitt rechteckige Hohlschiene, wobei die Rollmittel als zylindrische Rollen oder Walzen vorgesehen sind. Demnach bietet diese herkömmliche Anordnung keine Zentriereigenschaft.US 4 023 542 A teaches the formation of the track as a flat surface or as in cross-section rectangular hollow rail, wherein the rolling means as cylindrical rollers or rollers are provided. Accordingly, this provides conventional arrangement no centering property.

Zwar zeigt die US 4 553 508 A als Bahnen vorgesehene teilkreisförmige Nuten, in denen Kugeln laufen. Allerdings liegen die Kugeln quer zur Bewegungsrichtung der Schubstange in den Nuten. Demnach findet bei dieser herkömmlichen Anordnung eine Übertragung der Kolbenkraft quer zur Bewegungsrichtung der Schubstangen statt. Hieraus ist ersichtlich, dass die Kolbenkraft nicht voll ausgenutzt, sondern nur eine Vektorkomponente und somit ein Anteil der Kolbenkraft übertragen wird und die Arbeit verrichtet. Dies führt aber zu einem schlechten Wirkungsgrad der Maschine. Ferner hat diese bekannte Anordnung nachteilig zur Folge, dass die Nut nicht symmetrisch belastet wird, so dass nach kurzer Zeit die teilkreisförmige Nut eine unerwünscht elliptische Gestalt annimmt. Da sowohl die als Rollmittel ausgebildeten Kugeln und als Kugellagerung zusätzliche vorgesehene kleine Kugeln unendlich viele Freiheitsgrade haben, können diese nicht rollen, sondern vielmehr nur gleiten. Dadurch entstehen in den Berührungspunkten der Kugeln mit den jeweiligen Laufflächen große Flächenpressungen, was zu weiteren Schäden führt. Schließlich besteht ein weiterer Nachteil dieser herkömmlichen Anordnung darin, dass zwischen den rotierenden und den sich translatorisch bewegenden Teilen ein Spalt gebildet wird, der sich im wesentlichen in Bewegungsrichtung der Schubstangen und somit in Richtung der Kolbenkraft erstreckt, so dass spätestens nach einer bestimmten Zeit die Kugeln nach Art eines Keils in jenen Spalt gepresst werden und diesen auseinander drücken, was weitere Schäden zur Folge hat.Although US Pat. No. 4,553,508 discloses part-circular grooves provided as webs, in which balls run. However, the balls are transverse to the direction of movement the push rod in the grooves. Accordingly, takes place in this conventional Arrangement a transmission of the piston force transverse to the direction of movement of Push rods instead. From this it can be seen that the piston force is not fully utilized, but only a vector component and thus a proportion of the piston force is transferred and does the work. But this leads to a bad one Efficiency of the machine. Furthermore, this known arrangement disadvantageous to Result that the groove is not loaded symmetrically, so that after a short time part-circular groove assumes an undesirable elliptical shape. Because both the designed as rolling means balls and ball bearings as additional provided small balls have infinite degrees of freedom, they can not but rather just glide. This results in the points of contact the balls with the respective running surfaces large surface pressures, what to further damage. Finally, there is another disadvantage of these conventional ones Arrangement in that between the rotating and the translationally moving parts, a gap is formed, which is substantially in the direction of movement of the push rods and thus in the direction of the piston force extends so that at the latest after a certain time the balls pressed in the manner of a wedge in that gap and push it apart, which causes further damage.

Erfindungsgemäß wird eine Axialverbrennungskolbenmaschine mit axial angeordneten Zylindern mit Einlass- und Auslassventilen und Kolben vorgeschlagen, welche jeweils auf einem Ende einer axial verschiebbare Schubstange befestigt sind, die Mittel zur Aufnahme von Rollmitteln aufweist, welche auf eine endlose wellenförmige Raumkurve bildenden Bahnen entlang laufen, die ringförmig umlaufend auf einem Bahn-Schwungrad ausgebildet sind, das koaxial auf einer drehbar gelagerten Welle sitzt, wobei auf der Welle neben dem Bahn-Schwungrad ein äußeres Hauptschwungrad, ein regulierendes Schwungrad, das durch Verschiebung des Bahn-Schwungrades das Verdichtungsverhältnis ändert, und ein Exenter-Schwungrad sitzen, welches die Einlass- und Auslassventile aller Zylinder betätigt, wobei die Rollmittel als Kugeln oder sphärische Walzen und die Bahnen als im Querschnitt kreisbogenförmige Laufrillen ausgebildet sind, auf denen die Kugeln oder sphärischen Walzen in Bewegungsrichtung der Schubstange aufliegen.According to the invention, an axial combustion piston machine with axially arranged Proposed cylinders with intake and exhaust valves and pistons, which each attached to one end of an axially displaceable push rod are having means for receiving rolling means, which on an endless Wavy space curve forming webs run along, the annular circulating are formed on a train flywheel which is coaxial on one rotatably mounted shaft sitting on the shaft next to the train flywheel an outer main flywheel, a regulating flywheel that changes the compression ratio by shifting the web flywheel, and an eccentric flywheel which seats the intake and exhaust valves all cylinders are actuated, with the rolling means as balls or spherical rollers and the tracks are formed as cross-sectionally circular grooves, on which the balls or spherical rollers in the direction of movement of the Rest push rod.

Bevorzugte Ausführungen der Erfindung sind in den abhängigen Ansprüchen angegeben.Preferred embodiments of the invention are defined in the dependent claims specified.

Nachfolgend werden bevorzugte Ausführungsbeispiele der Erfindung anhand der beiliegenden Zeichnungen näher erläutert. Es zeigen:

Fig. 1
einen Längsschnitt durch das Gehäuse einer Axialverbrennungskolbenmaschine;
Fig. 2
eine Ansicht der Welle mit den darauf befestigten Komponenten;
Fig. 3
eine Draufsicht auf das Bahn-Schwungrad;
Fig. 4
eine teilweise geschnittene Seitenansicht der Welle mit den daran befestigten Komponenten;
Fig. 5
in teilweise geschnittener Seitenansicht ausschnittsweise eine Anordnung des Bahn-Schwungrades mit Schubstange;
Fig. 6
einen Querschnitt durch einen Kolben;
Fig. 7
eine Draufsicht auf ein Exzenter-Schwungrad;
Fig. 8
einen Längsschnitt durch die Schubstange;
Fig. 9
einen Querschnitt durch einen typischen 4-Zylinder-Motor;
Fig. 10
eine Draufsicht auf den Zylinderkopf eines typischen 4-Zylinder-Motors;
Fig. 11
in teilweise geschnittener Seitenansicht ausschnittsweise die Anordnung des Exzenter-Schwungrades;
Fig. 12
eine perspektivische Ansicht eines Bahn-Schwungrades mit acht Scheiteln; und
Fig. 13
die Verwendung der Axialverbrennungskolbenmaschine in einem Flugzeug.
Hereinafter, preferred embodiments of the invention will be explained in more detail with reference to the accompanying drawings. Show it:
Fig. 1
a longitudinal section through the housing of a Axialverbrennenkolbenmaschine;
Fig. 2
a view of the shaft with the components mounted thereon;
Fig. 3
a plan view of the web flywheel;
Fig. 4
a partially sectioned side view of the shaft with the components attached thereto;
Fig. 5
partially sectional side view of a detail of an arrangement of the web flywheel with push rod;
Fig. 6
a cross section through a piston;
Fig. 7
a plan view of an eccentric flywheel;
Fig. 8
a longitudinal section through the push rod;
Fig. 9
a cross section through a typical 4-cylinder engine;
Fig. 10
a plan view of the cylinder head of a typical 4-cylinder engine;
Fig. 11
in a partially sectioned side view detail the arrangement of the eccentric flywheel;
Fig. 12
a perspective view of a train flywheel with eight vertices; and
Fig. 13
the use of the axial combustion piston engine in an aircraft.

In Fig. 1 ist im Längsschnitt des Motorgehäuses die Lage, Form und Anordnung eines Zylinderblocks 6, eines Zylinderkopfs 7, von festen Lagerungen 8 sowie von äußeren Hilfsmechanismen 9 dargestellt.In Fig. 1 is a longitudinal section of the motor housing, the position, shape and arrangement a cylinder block 6, a cylinder head 7, of fixed bearings 8 as well represented by external auxiliary mechanisms 9.

Fig. 2 ist eine räumliche Darstellung der Welle mit den darauf befestigten Komponenten, von denen das Bahn-Schwungrad 3 vier Scheitel besitzt.FIG. 2 is a perspective view of the shaft with the components mounted thereon. FIG. of which the train flywheel 3 has four vertices.

Fig. 3 ist eine typische Ansicht der Laufrillen 34, welche im Schnitt in radialer Richtung des Bahn-Schwungrades 3 die Form eines Kreisbogens haben.Fig. 3 is a typical view of the grooves 34, which in section in radial Direction of the web flywheel 3 have the shape of a circular arc.

Fig. 4 zeigt eine Darstellung der Welle mit Besonderheiten, bezogen auf das Bahn- Schwungrad 3 und das Exzenter-Schwungrad 4. Fig. 4 shows a representation of the shaft with special features, based on the Railway flywheel 3 and the eccentric flywheel 4.

Fig. 5 zeigt eine Einzelheit des Zusammenbaus des Bahn-Schwungrades 3 und einer Schubstange 5 mit Andeutung der Arbeitsweise des regulierenden Schwungrades 2 für die Kontrolle der Parameter <dw>, durch welche das Verdichtungsverhältnis beeinflusst wird.Fig. 5 shows a detail of the assembly of the web flywheel 3 and a push rod 5 with an indication of the operation of the regulating Flywheel 2 for the control of the parameters <dw>, through which the compression ratio being affected.

In Fig. 6 ist ein typischer Kolbenquerschnitt dargestellt.FIG. 6 shows a typical piston cross-section.

Fig. 7 zeigt eine Ansicht des Exzenter-Schwungrades 4 mit Exzentern, welche die Einlaß- und Auslaßventile aller Zylinder betätigen.Fig. 7 shows a view of the eccentric flywheel 4 with eccentrics, which operate the intake and exhaust valves of all cylinders.

Fig. 8 zeigt einen Längsschnitt einer Schubstange 5 mit Andeutung der zusammenhängenden Bauteile. Ebenso ist die Lage und Form der sphärischen Walzen 54 oder Kugeln erkennbar, durch welche die Schubstange 5 mit dem Bahn-Schwungrad 3 gekoppelt wird.Fig. 8 shows a longitudinal section of a push rod 5 with an indication of the contiguous Components. Likewise, the location and shape of the spherical rollers 54 or balls visible through which the push rod 5 with the web flywheel 3 is coupled.

Fig. 9 zeigt einen typischen Querschnitt eines 4-Zylinder-Motors.Fig. 9 shows a typical cross section of a 4-cylinder engine.

Fig. 10 zeigt eine Draufsicht eines Zylinderkopfes 7 eines typischen 4-Zylinder-Motors mit Andeutung der Lage und Form des Exzenter-Schwungrades 4 sowie die notwendigen Organe für die Betätigung der entsprechenden Einlaß- und Auslassventile 43, 44.Fig. 10 shows a plan view of a cylinder head 7 of a typical 4-cylinder engine with an indication of the position and shape of the eccentric flywheel 4 as well the necessary organs for the operation of the corresponding intake and exhaust valves 43, 44.

Fig. 11 zeigt eine Einzelheit einer charakteristischen Ansicht der Welle, und zwar insbesondere an der Stelle, wo das Exzenter-Schwungrad 4 befestigt ist, sowie die Zusammenarbeit des Exzenter-Schwungrades 4 mit mechanischen Organen für die Betätigung der Einlaß- und Auslassventile 43, 44.Fig. 11 shows a detail of a characteristic view of the shaft, namely especially at the point where the eccentric flywheel 4 is attached, as well as the cooperation of the eccentric flywheel 4 with mechanical organs for the operation of the intake and exhaust valves 43, 44th

Fig. 12 zeigt eine Ansicht eines Bahn-Schwungrades mit acht Scheiteln und einem entsprechenden Exzenter-Schwungrad 4 mit einem Zwillings-Exzenter.Fig. 12 shows a view of a web flywheel with eight vertices and a corresponding eccentric flywheel 4 with a twin eccentric.

Fig. 13 stellt eine Verwendung des Motors in einem zweimotorigen Feuerwehrflugzeug dar. Fig. 13 illustrates a use of the engine in a twin-engined firefighter aircraft represents.

Nach alledem ergibt sich, daß für die Auslegung der Axialverbrennungskolbenmaschine die Form des Bahn-Schwungrades 3 und die Form der Schubstangen 5 sowie deren Verbindung mit den sphärischen Walzen 54 eine besondere Rolle spielen. Die Schubstangen sind hohl, um die Massenkräfte in den toten Punkten zu vermindern. Der Radius der Laufrillen 34 in radialer Richtung des Bahn-Schwungrades 3 ist gleich dem Radius der sphärischen Walzen 54 an den Schubstangen, so dass ein Verklemmen der rollenden Bauteile vermieden werden kann. Die Längshauptachse der Schubstangen läuft immer durch die Mitte der Laufrillen 34, so daß bauliche Toleranzen und demzufolge kleinere Reibungswiederstände und örtliche Belastungen der entsprechenden Komponenten ausgeglichen werden können.After all, it follows that for the design of Axialverbrennenkolbenmaschine the shape of the track flywheel 3 and the shape of the push rods 5 and their connection with the spherical rollers 54 a special role play. The push rods are hollow, around the mass forces in the dead spots to diminish. The radius of the grooves 34 in the radial direction of the web flywheel 3 is equal to the radius of the spherical rollers 54 at the Push rods, so that jamming of the rolling components are avoided can. The longitudinal main axis of the push rods always runs through the middle the grooves 34 so that structural tolerances and consequently smaller Reibungswiederstände and local loads of the corresponding components can be compensated.

Das Drehmoment des neues Motors wird durch die Gleichung M=p•F•R tan ϕ wiedergegeben, wobei p der Druck im Verbrennungsraum, F die Kolbenfläche, R der mittlere Radius des herausragenden Ringes 32 des Bahn-Schwungrades 3 und ϕ der Winkel zwischen Z-Achse und Tangente an einer beliebigen Stelle der auf der Ebene OXZ abgewickelten Raumkurve 33 ist. Der Parameter tan ϕ hängt mit dem Kolbenweg ℓ zusammen. Demnach kann das Drehemoment des neuen Motors wie folgt geschrieben werden: M=p•F•R•f(ℓ), wobei f(ℓ) eine Funktion zwischen ϕ und ℓ ist. Dies bedeutet, daß für einen gegebenen Kolbendurchmesser das Drehmoment proportional zu dem vorhandenen Druck im Verbrennungsraum, dem mittleren Radius des herausragenden Ringes des Bahn-Schwungrades und dem Kolbenweg ist.The torque of the new engine is given by the equation M = p • F • R tan φ where p is the pressure in the combustion chamber, F is the piston area, R is the mean radius of the protruding ring 32 of the web flywheel 3, and φ is the angle between the Z axis and tangent at any point in the space curve 33 developed on the plane OXZ. The parameter tan φ is related to the piston stroke ℓ. Thus, the three-phase torque of the new engine can be written as follows: M = p • F • R • f (ℓ), where f (ℓ) is a function between φ and ℓ. This means that for a given piston diameter, the torque is proportional to the existing pressure in the combustion chamber, the mean radius of the protruding ring of the web flywheel, and the piston travel.

Die oben genannten Angaben werden vollständig für die Auslegung des Bahn-Schwungrades verwertet. Das Optimum wird dadurch erreicht, wenn für kleine und mittlere Motorenhubräume Bahn-Schwungräder mit vier Scheiteln und für größere Motorenhubräume Bahn-Schwungräder mit acht Scheiteln verwendet werden. Die restlichen Bauteile des Motors bleiben unverändert, allerdings mit der Ausnahme, daß bei Bahn-Schwungrädem mit acht Scheiteln Zwillings-Exzenter zur Anwendung kommen, wie in Fig. 12 dargestellt ist.The above details are complete for the design of the railway flywheel recycled. The optimum is achieved if for small and mid-engine hoists four-cornered and four-cornered flywheels for larger engine hubs use eight-bladed railway flywheels become. The remaining components of the engine remain unchanged, but with with the exception that in railway flywheels with eight vertices twin eccentric are used, as shown in Fig. 12.

Zum Schluss wird betont, daß im Gegensatz zum klassischen Motor mit Kurbelwelle mit der Axialverbrennungskolbenmaschine die Geschwindigkeitsgrenzen erweitert werden können, weil sie gleichmäßig von 200 bis 8000 U/min ohne Getriebe arbeiten kann. Aus diesem Grund werden hohe Leistungen und Drehmomente gewährleistet. Außerdem ist sie aus wirtschaftlicher Sicht für Anwendungen mit besonderen Bedingungen oder Ansprüchen geeignet.Finally, it is emphasized that in contrast to the classic engine with crankshaft with the axial combustion piston machine, the speed limits can be extended because they are even from 200 to 8000 rpm without transmission can work. For this reason, high powers and torques guaranteed. In addition, it is from an economic point of view for applications suitable for special conditions or requirements.

Claims (10)

  1. An internal combustion axial piston engine with axial positioned cylinders (11), with import and export valves and pistons (10), that are permanently positioned at one end of the sliding connecting rod (5), which is able to support the sliding mechanisms, that moves on the formed tracks alongside a endless wavy curve (33), which is in a circular shape on a track flywheel (3) that is positioned coaxially on the turning axle, where, except the track flywheel (3) an external flywheel (1) is attached, an adjusting flywheel (2), which by sliding on the track flywheel (3) changes the compression ratio, and a cam flywheel (4), which activates the import and exhaust valves of all cylinders (11), where the rolling bodies are formed as spheres (54) or spherical cylinders and the tracks in their transversal cross section are formed like arched grooves (34) on top of them the spheres (54) or the spherical cylinders come in contact (touch) in the directional movement of the connecting rod (5).
  2. Motor according to claim 1, features the radius of the groove (34) that is basically equal to the radius of the spheres (54) or spherical cylinders.
  3. Motor according to claim 1 or 2, where the track flywheel (3) has a center cylindrical nucleus (31) and a wavy, radially projecting ring (32), that is around the externally central cylindrical nucleus (31) positioned alongside the cylindrical surface, where on each of the opposite surfaces of the ring (32) a groove is formed (34),and the connecting rods (5) have the means for a dual acceptance of the spheres (54) or spherical cylinders, where their center of mass has a constant distance, one sphere (54) or spherical cylinder moves in the groove (34) of one surface of the ring (32) and the other sphere (54) or spherical cylinder moves on the groove of the other side of the ring (32).
  4. Motor with at least one of the aforementioned claims, in which the endless wavy curve in space (33) has four identical curves peripherally on the track flywheel (3) positioned peaks.
  5. Motor with at least one of the claims 1 through 4, in which an endless wavy curve in space (33) possesses eight identical curves peripherally on the track flywheel (3) positioned peaks.
  6. Motor with at least one of the aforementioned claims, in which the adjusting flywheel (2) is mechanically connected to the track flywheel (3) and in order to change the compression ratio it moves along the axle.
  7. Motor with at least one of the aforementioned claims, in which the cam flywheel (4) possesses two cams (41,42), the mechanism (43,44) in order to activate the respective valves import and exhaust of a cylinder (11), where the valves import and exhaust of the other cylinders through the consecutive turning of the cam flywheel (4) open and close.
  8. Motor with at least one of the claims I through 6 in which the cam flywheel (4) has one unique cam, which opens concurrently the import valve of one cylinder (11) and the exhaust valve of the following cylinder.
  9. Motor with at least one of the aforementioned claims, in which the cylinders (11) are positioned on the peaks of a uniform polygon and the axles of the cylinders (11) are parallel with the axle (of the motor).
  10. Motor with at least one of the aforementioned claims, in which the axle of the cylinders (11) and the pistons (10) go through the center of the spheres (54) or the spherical cylinders and cut into the symmetrical line of the grooves (34).
EP01600029A 2001-01-09 2001-12-21 Axial combustion engine Expired - Lifetime EP1221535B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GR2001010008 2001-01-09
GR2001010008 2001-01-09

Publications (3)

Publication Number Publication Date
EP1221535A2 EP1221535A2 (en) 2002-07-10
EP1221535A3 EP1221535A3 (en) 2003-03-26
EP1221535B1 true EP1221535B1 (en) 2005-09-14

Family

ID=10944604

Family Applications (1)

Application Number Title Priority Date Filing Date
EP01600029A Expired - Lifetime EP1221535B1 (en) 2001-01-09 2001-12-21 Axial combustion engine

Country Status (4)

Country Link
EP (1) EP1221535B1 (en)
AT (1) ATE304650T1 (en)
DE (1) DE50107417D1 (en)
ES (1) ES2249401T3 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB455585A (en) * 1934-10-29 1936-10-23 Anthony George Maldon Michell Improved means for varying the compression ratio in internal combustion engines of the swash-plate or equivalent type
US4023542A (en) * 1976-02-27 1977-05-17 Ango Alvino J Load responsive variable stroke internal combustion engine
US4553508A (en) * 1981-04-27 1985-11-19 Stinebaugh Donald E Internal combustion engine
US5083532A (en) * 1990-11-23 1992-01-28 Bernard Wiesen Mechanism for variable compression ratio axial engines

Also Published As

Publication number Publication date
ATE304650T1 (en) 2005-09-15
EP1221535A3 (en) 2003-03-26
ES2249401T3 (en) 2006-04-01
DE50107417D1 (en) 2005-10-20
EP1221535A2 (en) 2002-07-10

Similar Documents

Publication Publication Date Title
DE3224482C2 (en) PISTON MACHINE
DE69725864T2 (en) INTERNAL COMBUSTION ENGINE WITH CENTRAL COMBUSTION CHAMBER
DE4019384A1 (en) INTERNAL COMBUSTION ENGINE
DE69906971T2 (en) MACHINE WITH DOUBLE LIFT
EP0658688A1 (en) Machine
EP1221535B1 (en) Axial combustion engine
WO1993001395A1 (en) Oscillating piston engine
DE19500854C2 (en) Reciprocating machine
DE19726501A1 (en) Piston engine
EP0650419B1 (en) Hydraulic device
DE4224074A1 (en) Internal combustion engine
WO2018033276A1 (en) Connection rod for an internal combustion engine with a variable compression
DE3114459A1 (en) Crank gear for a reciprocating piston engine
DE3920620A1 (en) ROTATION MACHINE
DE898373C (en) Crank mechanism for converting back and forth movements into rotating movement and vice versa
DE316923C (en)
DE10019959A1 (en) Control method for IC engine uses variation in engine compression and alteration of crankshaft synchronization to change their relative positions
DE2237119A1 (en) CRANK DRIVE
DE3313611A1 (en) Motor/pump unit
DE3419582A1 (en) Swash plate engine
AT412804B (en) TRANSMISSION FOR A PISTON ENGINE OR PUMP REGULATOR
DE3040445A1 (en) Radial cylinder high pressure pump - has driving eccentric formed by two rings with varying diameter rollers between them
DE19533696A1 (en) Piston=type IC engine
EP1485583A1 (en) Internal combustion engine comprising rotary valves
EP0274400A2 (en) Rotary-piston engine

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

AX Request for extension of the european patent

Free format text: AL;LT;LV;MK;RO;SI

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

AX Request for extension of the european patent

Extension state: AL LT LV MK RO SI

17P Request for examination filed

Effective date: 20021126

AKX Designation fees paid

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

AXX Extension fees paid

Extension state: RO

Payment date: 20030103

17Q First examination report despatched

Effective date: 20040121

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

AX Request for extension of the european patent

Extension state: RO

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050914

Ref country code: IE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050914

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20050914

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: GB

Ref legal event code: ERR

Free format text: NOTIFICATION HAS BEEN RECEIVED FROM THE EUROPEAN PATENT OFFICE THAT IT WAS PUBLISHED IN GERMAN

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REF Corresponds to:

Ref document number: 50107417

Country of ref document: DE

Date of ref document: 20051020

Kind code of ref document: P

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: MC

Payment date: 20051122

Year of fee payment: 5

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20051214

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20051214

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20051221

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20060214

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 20060202

NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2249401

Country of ref document: ES

Kind code of ref document: T3

REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

ET Fr: translation filed
PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20060615

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20061231

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: LU

Payment date: 20071219

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 20080331

Year of fee payment: 7

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20081231

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20081231

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20091230

Year of fee payment: 9

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20081221

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: BE

Payment date: 20101229

Year of fee payment: 10

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20101221

BERE Be: lapsed

Owner name: DIMOS, VASILEIOS

Effective date: 20111231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20111231

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: TR

Payment date: 20121221

Year of fee payment: 12

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: AT

Payment date: 20121221

Year of fee payment: 12

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20131231

Year of fee payment: 13

Ref country code: SE

Payment date: 20131227

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 20131227

Year of fee payment: 13

Ref country code: FR

Payment date: 20131227

Year of fee payment: 13

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 304650

Country of ref document: AT

Kind code of ref document: T

Effective date: 20131221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20131221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20141222

REG Reference to a national code

Ref country code: SE

Ref legal event code: EUG

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20141221

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20150831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20131221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20141221

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20141231

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20160129

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20141222

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20161231

Year of fee payment: 16

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 50107417

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20180703