EP1347157B1 - Gas-dynamic pressure wave supercharger - Google Patents

Gas-dynamic pressure wave supercharger Download PDF

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Publication number
EP1347157B1
EP1347157B1 EP02006066A EP02006066A EP1347157B1 EP 1347157 B1 EP1347157 B1 EP 1347157B1 EP 02006066 A EP02006066 A EP 02006066A EP 02006066 A EP02006066 A EP 02006066A EP 1347157 B1 EP1347157 B1 EP 1347157B1
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EP
European Patent Office
Prior art keywords
pressure
pressure exhaust
channel
exhaust channel
duct
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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
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EP02006066A
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German (de)
French (fr)
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EP1347157A1 (en
Inventor
Urs Wenger
Roger Martin
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Swissauto Engineering SA
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Swissauto Engineering SA
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Publication date
Priority to ES02006066T priority Critical patent/ES2252338T3/en
Application filed by Swissauto Engineering SA filed Critical Swissauto Engineering SA
Priority to AT02006066T priority patent/ATE309455T1/en
Priority to EP02006066A priority patent/EP1347157B1/en
Priority to DE50204848T priority patent/DE50204848D1/en
Priority to AU2003200866A priority patent/AU2003200866A1/en
Priority to US10/384,898 priority patent/US7080633B2/en
Priority to JP2003074333A priority patent/JP4335558B2/en
Publication of EP1347157A1 publication Critical patent/EP1347157A1/en
Application granted granted Critical
Publication of EP1347157B1 publication Critical patent/EP1347157B1/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F13/00Pressure exchangers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B33/00Engines characterised by provision of pumps for charging or scavenging
    • F02B33/32Engines with pumps other than of reciprocating-piston type
    • F02B33/42Engines with pumps other than of reciprocating-piston type with driven apparatus for immediate conversion of combustion gas pressure into pressure of fresh charge, e.g. with cell-type pressure exchangers

Definitions

  • the invention relates to a gas-dynamic Pressure wave machine according to the preamble of claim 1.
  • EP-B-885 352 discloses a method which it in a standard pressure wave machine with a so-called Waste gate allows excess high pressure exhaust gas, e.g. in the partial load range of the internal combustion engine, from Redirect high-pressure exhaust gas channel in the low-pressure exhaust duct and thus to lower the pressure in front of the pressure wave machine. Then the pressure drops after the pressure wave machine and thus the pressure in the intake passage of the internal combustion engine.
  • opening the waste gate does not existing inflow to the gas pocket, in addition to blowing off Excess high pressure exhaust gas a collapse of the Flushing the rotor of the pressure wave machine. This causes in the worst case even a recirculation of the exhaust gas in the intake duct of the internal combustion engine and in any case a significant deterioration of the Compression efficiency of the pressure wave machine.
  • FIG. 1 shows a development of the rotor of FIG gas dynamic pressure wave machine 2 with the Combustion engine 1, the high pressure exhaust duct 3 and the Low-pressure exhaust duct 4 including the purge air S, the rotor 6 with the individual cells 18, the fresh air inlet 8, or low pressure fresh air supply channel 14, the high pressure charge air duct 10, which merges into the charge air duct 11 and leads to the internal combustion engine 1.
  • the pressure wave machine with known Methods, such as characteristics method and Design calculations, by the combustion engine manufacturer desired point, usually at nominal speed of the Motors, optimally designed, this being either without pockets or with one or two or all three pockets can happen.
  • the gas pocket 21 located as For example, in the aforementioned CH-A-681 738 is available.
  • This gas pocket and especially the there necessarily existing web 21 A between the high-pressure exhaust passage and gas pocket generates additional losses, especially if at low to medium speeds, Temperatures and flow rates usually blow off is unnecessary.
  • Figures 3 to 6a of the present invention relate also on the influence of the high pressure exhaust stream.
  • Figures 3 and 3A of the present Invention is the unwound rotor 40 with the cells 41st and, in contrast to the gas pocket 21 in FIG. 2, a serving as a gas pocket recess 48 in the gas housing 34th provided, which are changed by a slider 49 can, as indicated by the arrow 50.
  • the slider 49 is fully engaged in the arrow direction, so that the high-pressure exhaust duct is widened without a Footbridge has emerged.
  • the slider so be moved, that the high-pressure exhaust duct masses widened until the pressure in it has dropped so far is that generated by the pressure wave process Boost pressure drops to the desired level.
  • FIG. 4 and 4A is a variant of the slider shown, which is a pivotable part 51st act, which is hinged to a hinge 52 and through a similar control electronics can be moved as above, which causes a widening 53 of the exhaust high-pressure channel.
  • 3A is a valve 58 schematically in Figure 5, 5A represented as e.g. in CH-A-681 738 for control the gas pocket inflow is used.
  • 5A represented as e.g. in CH-A-681 738 for control the gas pocket inflow is used.
  • the valve 58 is then opened further and a line 56 is released.
  • This line 56 is over a suitable connection channel with the low pressure exhaust duct 35 connected.
  • This line 56 can now be a additional exhaust gas directly into the practically under Ambient pressure low pressure exhaust passage 35th be blown off. This reduces the pressure in the high pressure exhaust duct 31 to the desired lower level.
  • FIGS. 6 and 6A schematically show a roller 59 as shown in similar form in EP-A-0 210 328 is used to control the gas pocket inflow. Also Here, the roller 59 is only moved so far that a sufficient large proportion of high-pressure exhaust 31 to maintain the Rotor purge is diverted in the broadening 53.
  • the roller 59 is then rotated further and gives the Connecting channel 57 free.
  • the connecting channel 57 is with connected to the low pressure exhaust passage 35.
  • an additional amount of exhaust gas can be used directly in the practical under ambient pressure low pressure exhaust duct 35th be blown off. This reduces the pressure in the high pressure exhaust duct 31 to the desired lower level.
  • the same measures can be applied to previously known other methods for controlling the high pressure exhaust stream be made in the gas pockets.
  • control technology ensures that the first Exhaust gas flow from the high pressure exhaust duct either through a Broadening of the high-pressure exhaust passage 31 as in the Figures 4A and 5A shown, or by a partial Redirecting the exhaust gas flow is conducted into the gas pocket, before the additional control organ the further opening directly from the high pressure exhaust passage 31 into the low pressure exhaust passage 35 releases.
  • This control technique becomes the Maintaining the rotor flush needed.
  • the pressure wave machine according to the invention makes it possible over the entire area of the map of a Internal combustion engine both the negative pressure difference and thus the increased expulsion work of the internal combustion engine so to keep low as possible, as well as the Abblasemenge so far as to increase the pressure in the high-pressure exhaust duct as far as can be lowered, that the pressure in the Charge air duct can be reduced so far that a partial closure of the throttle valve Internal combustion engine can be omitted in the partial load range.
  • the Effectiveness of the invention is given in particular when can be guaranteed that a sufficiently large Exhaust gas quantity first by increasing the high-pressure exhaust gas duct 31, or through the gas pockets, directly into the Rotor is blown off, otherwise the pressure wave process is disturbed and thus the flushing of the rotor collapses and unwanted exhaust gas is passed to the engine. This is by suitable control technical design of the invention sure.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)
  • Control Of Fluid Pressure (AREA)
  • Mechanical Treatment Of Semiconductor (AREA)

Abstract

Gas dynamic pressure wave machine has a line (54, 57) leading from a high pressure exhaust gas channel (31) to a low pressure exhaust gas channel (35). The line is regulated via a suitable device to maintain the pressure wave process. A part of the exhaust gas stream from the high pressure exhaust gas stream is led from the high pressure channel into an enlarged section (53) before further exhaust gas is led from the high pressure exhaust gas channel to the low pressure exhaust gas channel. Preferred Features: The enlarged section consists of a recess or extension having a device for changing the enlargement without forming bar. The width of the opening of the line can be changed using an adjusting part. The adjusting part is regulated using a microprocessor.

Description

Die Erfindung bezieht sich auf eine gasdynamische Druckwellenmaschine gemäss Oberbegriff von Patentanspruch 1.The invention relates to a gas-dynamic Pressure wave machine according to the preamble of claim 1.

Eine solche gasdynamische Druckwellenmaschine ist in der WO 99/11914 des gleichen Anmelders ausführlich beschrieben und es wird darauf Bezug genommen.Such a gas-dynamic pressure wave machine is in WO 99/11914 of the same applicant described in detail and it is referred to.

Bei einer gasdynamischen Druckwellenmaschine zur Aufladung von Verbrennungsmotoren, welche mit vier Kanälen ohne zusätzliche Regeleinrichtungen in Form von Taschen verwendet wird, ist die Prozessabstimmung nur auf einen Betriebspunkt des Verbrennungsmotors abgestimmt. Man spricht in diesem Zusammenhang vom Auslegepunkt der Druckwellenmaschine. Durch Anwendung sogenannter Taschen in den Gehäusewänden kann die Druckwellenmaschine abstimmungsunempfindlicher und der Last-Drehzahl- und Volumenbereich stark ausgedehnt werden. Der Nachteil dieser Methode ist eine Erhöhung der Verluste durch die in den Taschen stattfindenden Nebenprozesse, wie Einströmen und Ausströmen der Gase und die Erzeugung von Druck- und Expansionswellen durch die Taschen.In a gas-dynamic pressure wave machine for charging of internal combustion engines, which with four channels without used additional control devices in the form of pockets is, the process vote is only on one operating point tuned to the internal combustion engine. One speaks in this Connection from the design point of the pressure wave machine. By Application of so-called pockets in the housing walls, the Pressure wave machine tuned insensitive and the load-speed and volume range are greatly expanded. Of the Disadvantage of this method is an increase in losses due to the secondary processes taking place in the pockets, such as Inflow and outflow of the gases and the generation of Pressure and expansion waves through the pockets.

Der Übergang vom sogenannten Primärprozess auf den Hauptprozess, abgestimmter Prozess, verursacht Störungen im Druckwellenprozess, welche Spülungseinbrüche und somit Bereiche hoher Rezirkulation von Abgas in die Ladeluft verursachen. Um in diesen Bereichen, wie auch im Startfall, erhöhte Rezirkulation zu vermeiden, muss ein Zufluss zur Gastasche, entweder als gefräste Schwelle oder als gesteuerter Zufluss z.B. gemäss CH-A-681 738, verwendet werden.The transition from the so-called primary process to the Main process, coordinated process, causes disturbances in the Pressure wave process, which rinse dips and thus Areas of high recirculation of exhaust gas in the charge air cause. To be able to work in these areas, as well as in To avoid increased recirculation, must be an inflow to the Gas pocket, either as milled threshold or as controlled inflow e.g. according to CH-A-681 738 become.

Aus z.B. der EP-B-885 352 ist ein Verfahren bekannt, das es bei einer Standard-Druckwellenmaschine mit einem sogenannten Waste-Gate ermöglicht, überschüssiges Hochdruckabgas, z.B. im Teillastbereich des Verbrennungsmotors, vom Hochdruckabgaskanal in den Niederdruckabgaskanal umzuleiten und somit den Druck vor der Druckwellenmaschine abzusenken. Daraufhin sinkt auch der Druck nach der Druckwellenmaschine und somit der Druck im Ansaugkanal des Verbrennungsmotors. Durch das Öffnen des Waste-Gate erfolgt jedoch, bei nicht vorhandenem Zufluss zur Gastasche, zusätzlich zum Abblasen des überschüssigen Hochdruckabgases ein Zusammenbruch der Spülung des Rotors der Druckwellenmaschine. Dies bewirkt im schlimmsten Falle sogar eine Rezirkulation des Abgases in den Ansaugkanal des Verbrennungsmotors und auf jeden Fall eine deutliche Verschlechterung des Kompressionswirkungsgrades der Druckwellenmaschine.Made of e.g. EP-B-885 352 discloses a method which it in a standard pressure wave machine with a so-called Waste gate allows excess high pressure exhaust gas, e.g. in the partial load range of the internal combustion engine, from Redirect high-pressure exhaust gas channel in the low-pressure exhaust duct and thus to lower the pressure in front of the pressure wave machine. Then the pressure drops after the pressure wave machine and thus the pressure in the intake passage of the internal combustion engine. However, opening the waste gate does not existing inflow to the gas pocket, in addition to blowing off Excess high pressure exhaust gas a collapse of the Flushing the rotor of the pressure wave machine. This causes in the worst case even a recirculation of the exhaust gas in the intake duct of the internal combustion engine and in any case a significant deterioration of the Compression efficiency of the pressure wave machine.

Aus z.B. den bereits genannten CH-A-681 738 und EP-A-0 210 328 ist ein Verfahren bekannt, aus welchem das vom Verbrennungsmotor ausgestossene Abgas über einen abzweigenden Zufluss zur Gastasche der Druckwellenmaschine ein Abblasen des überschüssigen Hochdruckgases in die Gastaschen ermöglicht und somit eine Verbesserung des Kompressionswirkungsgrades durch die verbesserte Spülung des Rotors erreicht wird.Made of e.g. the aforementioned CH-A-681 738 and EP-A-0 210 328, a method is known from which the of Internal combustion engine exhausted exhaust via a branching inflow to the gas pocket of the pressure wave machine a blow-off of the excess high-pressure gas in the Gastaschen allows and thus improve the Compression efficiency through the improved flushing of the Rotor is achieved.

Die eingangs erwähnte WO 99/11914 widerum verhindert den dauernden Einsatz einer Gastasche mit ihren Verlusten, und eliminiert den den Druckwellenprozess störenden Steg zwischen dem Abgaskanal und der Gastasche bei geöffnetem Zufluss, sowie die durch die Leitungsführung zur Gastasche auftretenden Energieverluste in Form von Strömungs- und Temperaturverlusten und die Einschränkungen in der Gestaltung der anderen Kanäle.The aforementioned WO 99/11914 again prevents the continuous use of a gas pocket with their losses, and eliminates the web disturbing the pressure wave process between the exhaust duct and the gas pocket when open Inflow, as well as through the wiring to the gas pocket occurring energy losses in the form of flow and Temperature losses and limitations in the Design of the other channels.

Bei allen diesen Verfahren ist aber nachteilig, dass im Teillastbereich des Verbrennungsmotors durch das Abblasen des überschüssigen Hochdruckgases in die Gastaschen oder der Vergrösserung des Hochdruck-Abgaskanals, der Druck im Hochdruck-Abgaskanal immer noch zu hoch bleibt, das heisst, die sich somit einstellende negative Druckdifferenz Ladeluftaustritt aus der Druckwellenmaschine gegenüber Hochdruck-Abgaseintritt in die Druckwellenmaschine, bewirkt erhöhte Ausstossverluste des Verbrennungsmotors und somit schlechtere Verbrauchswerte im Teillastbereich des Verbrennungsmotors. Gleichzeitig bleibt aber durch die ungenügende Absenkung des Abgasdruckes über den Druckwellenprozess ein ungewollter Ladedruck nach der Druckwellenmaschine bestehen. Beim Ottomotor mit seiner Laststeuerung über die Drosselklappe muss nun dieser höhere Druck in der Ansaugleitung noch zusätzlich durch das teilweise Schliessen der Drosselklappe reduziert werden, was weitere Verluste in Form von Drosselverlusten bewirkt.In all these methods, however, is disadvantageous that in Part load range of the internal combustion engine by blowing off the excess high-pressure gas in the gas pockets or the Enlargement of the high-pressure exhaust gas duct, the pressure in the High-pressure exhaust duct still remains too high, that is, the thus adjusting negative pressure difference Charge air outlet from the pressure wave machine opposite High-pressure exhaust gas inlet into the pressure wave machine causes increased output losses of the internal combustion engine and thus worse consumption values in the partial load range of Combustion engine. At the same time, however, remains through the insufficient lowering of the exhaust gas pressure over the Pressure wave process an unwanted boost pressure after the Pressure wave machine exist. When gasoline engine with his Load control via the throttle now has this higher Pressure in the intake still by the partially closing the throttle to be reduced, which causes further losses in the form of throttle losses.

Die Verfahren aus CH-A-681 738, EP-A-0 210 328 und WO 99/11194 zum Abblasen des überschüssigen Hochdruckgases haben den Nachteil, dass über einen weiten Bereich des Verbrennungsmotoren-Kennfeldes, hauptsächlich aber im Teillastberich des Verbrennungsmotors, nicht genügend abgeblasen werden kann, das heisst, dass der Druck vor der Druckwellenmaschine auf einem höheren Niveau ist als der Druck nach der Druckwellenmaschine. Dies ergibt eine negative Druckdifferenz auch über den Verbrennungsmotor und somit eine erhöhte Ausstossarbeit der Kolben des Verbrennungsmotors. Beim Ottomotor muss durch die Qualitätsregelung sogar noch die Drosselklappe teilweise geschlossen werden, um den über den Druckwellenprozess entstehenden Überdruck im Ansaugkanal des Motors zu reduzieren. Dies hat weitere Verluste in Form von Drosselverlusten zur Folge. Beide Verlustgrössen wirken sich negativ auf den Teillastverbrauch des Verbrennungsmotors aus. The methods of CH-A-681 738, EP-A-0 210 328 and WO 99/11194 for blowing off the excess high-pressure gas have the disadvantage that over a wide range of Internal combustion engine characteristic field, but mainly in the Part load report of the internal combustion engine, not enough can be blown off, that is, the pressure before the Pressure wave machine is at a higher level than the Pressure after the pressure wave machine. This gives a negative pressure difference also over the internal combustion engine and thus increased output of the piston of the Combustion engine. When gasoline engine must by the Quality control even the throttle partially closed to the over the pressure wave process resulting pressure in the intake port of the engine too to reduce. This has further losses in the form of Throttle losses result. Both loss factors affect each other negative on the partial load consumption of the internal combustion engine out.

Aus der US-A1-4,488,532 (= EP 0 080 741 B1) ist eine Druckwellen-Maschine nach dem Oberbegriff des Anspruchs 1 bekannt geworden. Bei dieser Maschine wird eine Anpassung der Höhenlagen des Fahrzeugs zum Beispiel beim Befahren von Pass-Strassen oder dergleichen mittels einer Regelung des Durchflusses von Abgas vom Hochdruck-Abgaskanal zum Niederdruck-Abgaskanal mittels einer Klappensteuerung bewirkt, wobei ein Teil dieses Abgases bei geöffneter Bypass-Leitung in eine rotorseitig geöffnete Gastasche geleitet wird. Hierdurch wird die erforderliche Niederdruck-Spülung des Rotors aufrecht erhalten. Ziel und Zweck dieser Abgasführung ist der Ausgleich einer Höhenkorrektur mittels einer Bypass-Verstelleinrichtung. From US-A1-4,488,532 (= EP 0 080 741 B1) is a Pressure wave machine according to the preamble of claim 1 known. This machine will be an adaptation of the Altitudes of the vehicle, for example when driving on pass roads or the like by means of a regulation of Flow of exhaust gas from the high pressure exhaust duct to Low pressure exhaust duct by means of a flap control causes, with a portion of this exhaust gas with open bypass line passed into a rotor side open gas pocket becomes. This will provide the required low pressure flush maintained of the rotor. Purpose and purpose of this Exhaust system is the compensation of a height correction means a bypass adjustment.

Es ist gegenüber diesem bekannten und beschriebenen Stand der Technik Aufgabe der vorliegenden Erfindung, eine gasdynamische Druckwellenmaschine anzugeben, die über den gesamten Bereich des Kennfeldes eines Verbrennungsmotors und insbesondere im Teillastbereich, verbesserte Verbrauchswerte und eine höhere Leistung erbringt. Diese Aufgabe wird mit der gasdynamischen Druckwellenmaschine gemäss Patentanspruch 1 gelöst.It is opposite this known and described state the technology object of the present invention, a Specify gas-dynamic pressure wave machine, which over the entire area of the map of an internal combustion engine and especially in the partial load range, improved fuel consumption and higher performance. This task is with the gas-dynamic pressure wave machine according to claim 1 solved.

Weitere Vorteile und Ausführungsbeispiele sind in den abhängigen Ansprüchen definiert.Further advantages and embodiments are in the dependent claims defined.

Die Erfindung wird im folgenden anhand von Zeichnungen von Ausführungsbeispielen näher erläutert.

Figur 1
zeigt schematisch einen abgewickelten zylindrischen Schnitt durch die Zellen eines Rotors einer Druckwellenmachine gemäss Stand der Technik,
Figur 2
zeigt schematisch ein Detail eines abgewickelten zylindrischen Schnittes durch die Zellen des Rotors der Figur 1,
Figuren 3, 3A
zeigen schematisch ein Detail eines abgewickelten zylindrischen Schnittes durch die Zellen eines Rotors gemäss Erfindung bei geschlossenem und offenem Schieber,
Figuren 4, 4A
zeigen eine Variante zur Ausführung nach den Figuren 3, 3A,
Figuren 5, 5A
zeigen eine Variante zur Ausführung nach den Figuren 3, 3A, und
Figuren 6, 6A
zeigen eine Variante zur Ausführung nach den Figuren 4, 4A.
The invention will be explained in more detail below with reference to drawings of exemplary embodiments.
FIG. 1
shows schematically a developed cylindrical section through the cells of a rotor of a pressure wave machine according to the prior art,
FIG. 2
1 schematically shows a detail of a developed cylindrical section through the cells of the rotor of FIG. 1, FIG.
FIGS. 3, 3A
show schematically a detail of a developed cylindrical section through the cells of a rotor according to the invention with the slide closed and open,
FIGS. 4, 4A
show a variant of the embodiment according to FIGS. 3, 3A,
FIGS. 5, 5A
show a variant of the embodiment of Figures 3, 3A, and
FIGS. 6, 6A
show a variant of the embodiment of Figures 4, 4A.

Der Einfachheit halber ist in den Abwicklungen ein Druckwellen-Zyklus dargestellt und beschrieben. Die Erfindung ist jedoch von der Anzahl der Druckwellen-Zyklen unabhängig; sie kann für Druckwellenmaschinen mit nur einem Zyklus oder aber mit zwei oder mehr Zyklen angewandt werden.For the sake of simplicity, there is one in the settlements Pressure wave cycle shown and described. The Invention, however, is on the number of pressure wave cycles independently; It can be used for pressure wave machines with only one Cycle or with two or more cycles.

Figur 1 zeigt eine Abwicklung des Rotors einer gasdynamischen Druckwellenmaschine 2 mit der Verbrennungsmaschine 1, den Hochdruck-Abgaskanal 3 und den Niederdruck-Abgaskanal 4 inklusive der Spülluft S, den Rotor 6 mit den einzelnen Zellen 18, den Frischlufteintritt 8, bzw. Niederdruck-Frischluftzufuhrkanal 14, den Hochdruck-ladeluftkanal 10, der in den Ladeluftkanal 11 übergeht und zur Verbrennungsmaschine 1 führt.FIG. 1 shows a development of the rotor of FIG gas dynamic pressure wave machine 2 with the Combustion engine 1, the high pressure exhaust duct 3 and the Low-pressure exhaust duct 4 including the purge air S, the rotor 6 with the individual cells 18, the fresh air inlet 8, or low pressure fresh air supply channel 14, the high pressure charge air duct 10, which merges into the charge air duct 11 and leads to the internal combustion engine 1.

Wie bereits eingangs erwähnt wurde, ist die Prozessabstimmung auf die Verbrennungsmaschine bei der Verwendung der vier Kanäle ohne zusätzliche Regeleinrichtungen nur auf einen Betriebspunkt der Verbrennungsmaschine möglich. Dabei spricht man in diesem Zusammenhang vom Auslegepunkt der Druckwellenmaschine. Durch die Verwendung von Taschen in der Gehäusewand kann die Druckwellenmaschine abstimmungsunempfindlicher gemacht werden und damit der Last-, Drehzahl- und Volumenbereich stark ausgedehnt werden. Im Verlaufe der langjährigen Entwicklung von solchen Druckwellenmaschinen wurden verschiedene Taschen in der Gehäusewand 24 ausgefräst, z. B. eine Kompressionstasche 19, eine Expansionstasche 20 und eine Gastasche 21 mit Steg 21A, deren Anwendungen dem Fachmann wohlbekannt sind. Bei der Verwendung solcher Taschen ist es ein Nachteil, dass der Druckwellenprozess im nicht abgestimmten Kennfeldbereich über Nebenprozesse geleitet wird, welche nie einen optimalen Wirkungsgrad ergeben.As already mentioned, is the Process tuning to the combustion engine at the Use of the four channels without additional Control devices only on one operating point of Combustion engine possible. This one speaks in this Connection from the design point of the pressure wave machine. By the use of pockets in the housing wall can be the Pressure wave machine made less sensitive to voting and thus the load, speed and volume range be greatly expanded. In the course of many years of development from such pressure wave machines have been milled various pockets in the housing wall 24, z. B. a compression pocket 19, an expansion pocket 20 and a gas pocket 21 with web 21A, whose applications the Skilled in the art. When using such Pockets it is a disadvantage that the pressure wave process in uncoordinated map area via ancillary processes which is never optimal efficiency result.

Normalerweise wird die Druckwellenmaschine mit bekannten Verfahren, beispielsweise Charakteristikenverfahren und Auslegungsberechnungen, auf den vom Verbrennungsmaschinen-Hersteller gewünschten Punkt, meist bei Nenndrehzahl des Motors, optimal ausgelegt, wobei dies entweder ohne Taschen oder auch mit einer oder zwei oder allen drei Taschen geschehen kann.Normally, the pressure wave machine with known Methods, such as characteristics method and Design calculations, by the combustion engine manufacturer desired point, usually at nominal speed of the Motors, optimally designed, this being either without pockets or with one or two or all three pockets can happen.

In Figur 2 ist, in Anlehnung an Figur 1, ein Hochdruck-Abgaskanal 3 dargestellt, der keinerlei Mittel zur Beeinflussung des Hochdruck-Abgasstromes aufweist. Der Rotor 6 mit seinen Zellen 18 ist in abgewickelter Form dargestellt und man erkennt ferner das Gasgehäuse 24, den Hochdruck-Abgaskanal 3 sowie den Niederdruck-Abgaskanal 4.In Figure 2, based on Figure 1, a high-pressure exhaust passage 3, which does not provide any means for Influencing the high-pressure exhaust gas stream has. The rotor 6 with its cells 18 is shown in unwound form and one also recognizes the gas housing 24, the high pressure exhaust passage 3 and the low pressure exhaust duct 4.

Ferner ist in Figur 2 die Gastasche 21 eingezeichnet, wie sie beispielsweise in der eingangs erwähnten CH-A-681 738 vorhanden ist. Diese Gastasche sowie vor allem der dort notwendigerweise vorhandene Steg 21 A zwischen Hochdruck-Abgaskanal und Gastasche erzeugt zusätzliche Verluste, besonders dann, wenn bei tiefen bis mittleren Drehzahlen, Temperaturen und Durchsätzen ein Abblasen im Normalfall unnötig ist.Further, in Figure 2, the gas pocket 21 located as For example, in the aforementioned CH-A-681 738 is available. This gas pocket and especially the there necessarily existing web 21 A between the high-pressure exhaust passage and gas pocket generates additional losses, especially if at low to medium speeds, Temperatures and flow rates usually blow off is unnecessary.

In den Figuren 4, 4A und 5, 5A der WO 99/11914, auf die ausdrücklich Bezug genommen wird, ist eine Beeinflussung des Hochdruck-Abgaskanals mittels Schieber schematisch dargestellt.In Figures 4, 4A and 5, 5A of WO 99/11914, to the is expressly referred to, is an influence of the High-pressure exhaust gas ducts by means of a slide schematically shown.

Die Figuren 3 bis 6a der vorliegenden Erfindung beziehen sich ebenfalls auf die Beeinflussung des Hochdruck-Abgasstromes. In den Figuren 3 und 3A der vorliegenden Erfindung ist der abgewickelte Rotor 40 mit den Zellen 41 dargestellt und, im Gegensatz zur Gastasche 21 in Figur 2, eine als Gastasche dienende Aussparung 48 im Gasgehäuse 34 vorgesehen, die durch einen Schieber 49 verändert werden kann, wie dies durch den Pfeil 50 angedeutet ist. In Figur 3A ist der Schieber 49 ganz in Pfeilrichtung eingerückt, so dass der Hochdruck-Abgaskanal verbreitert ist, ohne dass ein Steg entstanden ist. Durch eine geeignete und für einen Fachmann berechenbare Steuerung kann der Schieber derart verschoben werden, dass der Hochdruck-Abgaskanal dermassen verbreitert wird, bis der Druck darin so weit abgesunken ist, dass der durch den Druckwellenprozess erzeugte Ladedruck auf das gewünschte Niveau absinkt.Figures 3 to 6a of the present invention relate also on the influence of the high pressure exhaust stream. In Figures 3 and 3A of the present Invention is the unwound rotor 40 with the cells 41st and, in contrast to the gas pocket 21 in FIG. 2, a serving as a gas pocket recess 48 in the gas housing 34th provided, which are changed by a slider 49 can, as indicated by the arrow 50. In FIG 3A, the slider 49 is fully engaged in the arrow direction, so that the high-pressure exhaust duct is widened without a Footbridge has emerged. By a suitable and for a Professional calculable control, the slider so be moved, that the high-pressure exhaust duct masses widened until the pressure in it has dropped so far is that generated by the pressure wave process Boost pressure drops to the desired level.

In den Figuren 4 und 4A ist eine Variante des Schiebers dargestellt, wobei es sich dabei um ein schwenkbares Teil 51 handelt, das an einem Scharnier 52 angelenkt ist und durch eine ähnliche Steuerelektronik wie oben bewegt werden kann, die eine Verbreiterung 53 des Abgashochdruckkanals bewirkt.In Figures 4 and 4A is a variant of the slider shown, which is a pivotable part 51st act, which is hinged to a hinge 52 and through a similar control electronics can be moved as above, which causes a widening 53 of the exhaust high-pressure channel.

Da die gemäss WO 99/11914 dargestellte Vergrösserung des Hochdruck-Abgaskanals mittels der Aussparungen 48 oder Verbreiterungen 53 nicht ausreichend ist, um das Druckniveau des Hochdruck-Abgases soweit abzusenken, dass der Druck in diesem Hochdruck-Abgasteil das erwünschte Niveau nahe bei Umgebungsdruck erreicht, werden zusätzliche Mittel zur Druckreduktion benötigt.As shown in WO 99/11914 magnification of High-pressure exhaust passage by means of the recesses 48 or Broadening 53 is insufficient to the pressure level Lower the high-pressure exhaust gas so far that the pressure in This high-pressure exhaust part near the desired level Ambient pressure achieved, will be additional funds to Pressure reduction needed.

Diese Mittel zur Druckreduktion enthalten die in den Figuren 3, 3A - 6, 6A dargestellte zusätzliche Leitung 54 -57. In den Figuren 3, 3A ist dies der Verbindungskanal 54, der die Leitung zwischen der Aussparung 48 und dem Hochdruck-Abgaskanal 35 herstellt. In Figur 3 ist der Schieber 49 geschlossen und damit sowohl die Aussparung als auch der Verbindungskanal 54 geschlossen. In Figur 4A ist sowohl die Aussparung als auch der Verbindungskanal 54 offen.These pressure reduction means include those in the figures 3, 3A-6, 6A show additional line 54-57. In In FIGS. 3, 3A, this is the connecting channel 54, which is the Line between the recess 48 and the high-pressure exhaust passage 35 produces. In FIG. 3, the slide 49 closed and thus both the recess and the Connection channel 54 closed. In FIG. 4A, both the Recess as well as the connecting channel 54 open.

Durch diese freiwerdende Leitung 54 kann nun eine zusätzliche Abgasmenge direkt in den praktisch unter Umgebungsdruck stehenden Niederdruck-Abgaskanal 35 abgeblasen werden. Dadurch sinkt der Druck im Hochdruck-Abgaskanal 31 auf das gewünschte tiefere Niveau ab. Wichtig ist, dass der freigegebene zusätzliche Verbindungskanal 54 erst öffnet, wenn eine genügend grosse Abgasmenge zuerst durch die Vergrösserung des Hochdruck-Abgaskanals 31 direkt in den Rotor abgeblasen wird, da sonst der Druckwellen-Prozess gestört wird und somit die Spülung des Rotors zusammenbricht und unerwünschtes Abgas zum Motor geleitet wird.Through this liberated line 54 can now be a additional exhaust gas directly into the practically under Ambient pressure low pressure exhaust passage 35th be blown off. This reduces the pressure in the high pressure exhaust duct 31 to the desired lower level. Important is that the shared additional connection channel 54 only opens when a sufficiently large amount of exhaust gas first by the enlargement of the high pressure exhaust passage 31 directly is blown off into the rotor, otherwise the pressure wave process is disturbed and thus the flushing of the rotor collapses and unwanted exhaust passed to the engine becomes.

Analog zu den Figuren 3, 3A ist in den Figuren 4, 4A ein Verbindungskanal 55 eingezeichnet, der die Leitung zwischen der als Gastasche dienenden Verbreiterung 53 und dem Niederdruck-Abgaskanal 35 herstellt, wobei die Verbreiterung 53 und der Verbindungskanal 55 durch das schwenkbare Teil 51 verschlossen und geöffnet werden können.Analogous to the figures 3, 3A is in the figures 4, 4A a Connection channel 55 located between the line serving as a gas pocket widening 53 and the Low-pressure exhaust passage 35 produces, with the broadening 53 and the connecting channel 55 through the pivotable part 51st can be closed and opened.

In einer Variante zur Ausführung gemäss den Figuren 3, 3A ist in den Figure 5, 5A schematisch ein Ventil 58 dargestellt, wie es z.B. in der CH-A-681 738 zur Steuerung des Gastaschenzuflusses verwendet wird. Auch hier sorgt die Steuerung dafür, dass das Ventil 58 erst soweit bewegt wird, dass ein genügend grosser Anteil Hochdruckabgas 31 zur Aufrechterhaltung der Rotorspülung in die Aussparung 48 umgeleitet wird. Das Ventil 58 wird dann weiter geöffnet und eine Leitung 56 freigegeben. Diese Leitung 56 ist über einen geeigneten Verbindungskanal mit dem Niederdruck-Abgaskanal 35 verbunden. Über diese Leitung 56 kann nun eine zusätzliche Abgasmenge direkt in den praktisch unter Umgebungsdruck stehenden Niederdruck-Abgaskanal 35 abgeblasen werden. Dadurch sinkt der Druck im Hochdruck-Abgaskanal 31 auf das gewünschte tiefere Niveau ab.In a variant of the embodiment according to FIGS. 3, 3A is a valve 58 schematically in Figure 5, 5A represented as e.g. in CH-A-681 738 for control the gas pocket inflow is used. Again, the Control that the valve 58 is moved so far that a sufficiently large proportion of high pressure exhaust gas 31 to Maintaining the rotor rinse in the recess 48th is redirected. The valve 58 is then opened further and a line 56 is released. This line 56 is over a suitable connection channel with the low pressure exhaust duct 35 connected. About this line 56 can now be a additional exhaust gas directly into the practically under Ambient pressure low pressure exhaust passage 35th be blown off. This reduces the pressure in the high pressure exhaust duct 31 to the desired lower level.

In den Figuren 6 und 6A wird schematisch eine Walze 59 dargestellt, wie sie in ähnlicher Form in der EP-A-0 210 328 zur Steuerung des Gastaschenzuflusses verwendet wird. Auch hier wird die Walze 59 erst soweit bewegt, dass ein genügend grosser Anteil Hochdruckabgas 31 zur Aufrechterhaltung der Rotorspülung in die Verbreiterung 53 umgeleitet wird.FIGS. 6 and 6A schematically show a roller 59 as shown in similar form in EP-A-0 210 328 is used to control the gas pocket inflow. Also Here, the roller 59 is only moved so far that a sufficient large proportion of high-pressure exhaust 31 to maintain the Rotor purge is diverted in the broadening 53.

Die Walze 59 wird dann weiter gedreht und gibt den Verbindungskanal 57 frei. Der Verbindungskanal 57 ist mit dem Niederdruck-Abgaskanal 35 verbunden. Über diese Leitung kann nun eine zusätzliche Abgasmenge direkt in den praktisch unter Umgebungsdruck stehenden Niederdruck-Abgaskanal 35 abgeblasen werden. Dadurch sinkt der Druck im Hochdruck-Abgaskanal 31 auf das gewünschte tiefere Niveau ab.The roller 59 is then rotated further and gives the Connecting channel 57 free. The connecting channel 57 is with connected to the low pressure exhaust passage 35. About this line Now an additional amount of exhaust gas can be used directly in the practical under ambient pressure low pressure exhaust duct 35th be blown off. This reduces the pressure in the high pressure exhaust duct 31 to the desired lower level.

Die gleichen Massnahmen können selbstverständlich auch bei vorbekannten anderen Verfahren zur Regelung des Hochdruck-Abgasstroms in die Gastaschen vorgenommen werden. In einer weiteren Ausbildung der Erfindung kann bei allen möglichen Anwendungen, entweder wie vorgehend beschrieben oder bei Verwendung von an sich bekannten Gastaschen, der zusätzliche, direkt vom Hochdruck-Abgaskanal 31 in den Niederdruck-Abgaskanal 35 geleitete Abgasstrom über ein zusätzliches Stellglied erfolgen, das beispielsweise durch einen Mikroprozessor gesteuert ist. Dabei ist es unerheblich, ob dieses zusätzliche Stellglied eine Klappe, ein Ventil, eine Walze oder ein ähnliches Regelorgan zur zusätzlichen Abblasung vom Hochdruck-Abgaskanal 31 in den Niederdruck-Abgaskanal 35 aufweist. Wichtig ist jedoch, dass steuerungstechnisch gewährleistet ist, dass zuerst der Abgasstrom vom Hochdruck-Abgaskanal entweder durch eine Verbreiterung des Hochdruck-Abgaskanals 31 wie in den Figuren 4A und 5A dargestellt, oder durch eine teilweise Umleitung des Abgasstromes in die Gastasche geführt wird, bevor das zusätzliche Regelorgan die weitere Öffnung direkt vom Hochdruck-Abgaskanal 31 in den Niederdruck-Abgaskanal 35 freigibt. Diese regelungstechnische Vorgehensweise wird zur Aufrechterhaltung der Rotorspülung benötigt.Of course, the same measures can be applied to previously known other methods for controlling the high pressure exhaust stream be made in the gas pockets. In a Further development of the invention can be used in all possible ways Applications, either as previously described or at Use of known gas pockets, the additional, directly from the high-pressure exhaust passage 31 in the Low-pressure exhaust passage 35 led exhaust gas flow over a additional actuator done, for example, by a microprocessor is controlled. That's it irrelevant whether this additional actuator has a flap, a valve, a roller or a similar control organ to additional blow-off from the high pressure exhaust duct 31 in the Low-pressure exhaust passage 35 has. However, it is important that control technology ensures that the first Exhaust gas flow from the high pressure exhaust duct either through a Broadening of the high-pressure exhaust passage 31 as in the Figures 4A and 5A shown, or by a partial Redirecting the exhaust gas flow is conducted into the gas pocket, before the additional control organ the further opening directly from the high pressure exhaust passage 31 into the low pressure exhaust passage 35 releases. This control technique becomes the Maintaining the rotor flush needed.

Dabei ist von Vorteil, wenn auch nicht Bedingung, dass die Leitung vom Hochdruck-Abgaskanal in den Niederdruck-Abgaskanal von der Gastasche, bzw. Aussparung oder Verbreiterung aus geht.It is advantageous, although not a condition that the Line from the high-pressure exhaust duct into the low-pressure exhaust duct from the gas pocket, or recess or Broadening goes out.

Aus der obigen Beschreibung geht hervor, dass damit ein Verfahren zur Teillastverbrauchsreduktion von Hubkolbenmotoren mittels einer Wirkungsgradverbesserung an einer gasdynamischen Druckwellenmaschine ermöglicht wird. Das Verfahren kann dabei mit anderen Verfahren kombiniert, oder aber auch einzeln mittels thermodynamischer Verbesserung einer Druckwellenmaschine gemäss den Patentansprüchen verwendet werden.From the above description it is apparent that with it Method for partial load reduction of Reciprocating engines by means of an efficiency improvement a gas-dynamic pressure wave machine is made possible. The method can be combined with other methods, or also individually by means of thermodynamic Improvement of a pressure wave machine according to the Claims are used.

Es geht ferner daraus hervor, dass der Druck im Hochdruckabgaskanal und somit auch der Ladedruck sowie die negative Druckdifferenz über den Lader deutlich verringert werden. Da sich dadurch auch die negative Druckdifferenz über den Verbrennungsmotor verringert, kann mit diesem i Verfahren auch der Teillastkraftstoffverbrauch des Verbrennungsmotors reduziert werden. Zusätzlich entfällt bei Ottomotoren im Teillastbereich grösstenteils eine Drosselung mittels Drosselklappe, da der Ladedruck durch die fast vollständige Absenkung des Abgasdruckes dem Umgebungsdruck weitgehend entspricht. Dies bewirkt eine weitere Reduktion des Teillastverbrauchs. It also shows that the pressure in the Hochdruckabgaskanal and thus also the boost pressure and the negative pressure difference across the loader significantly reduced become. As a result, this also the negative pressure difference reduced by the internal combustion engine, can with this i Procedure also the partial load fuel consumption of Internal combustion engine can be reduced. In addition, at Gasoline engines in the partial load range largely throttling by throttle, since the boost pressure by the almost complete reduction of the exhaust gas pressure to the ambient pressure largely corresponds. This causes a further reduction of partial load consumption.

Die erfindungsgemässe Druckwellenmaschine ermöglicht es, über den gesamten Bereich des Kennfeldes eines Verbrennungsmotors sowohl die negative Druckdifferenz und somit die erhöhte Ausstossarbeit des Verbrennungsmotors so gering als möglich zu halten, als auch die Abblasemenge soweit zu erhöhen, dass der Druck im Hochdruck-Abgaskanal soweit gesenkt werden kann, dass auch der Druck im Ladeluftkanal soweit verringert werden kann, dass eine teilweise Schliessung der Drosselklappe des Verbrennungsmotors im Teillastbereich entfallen kann. Die Wirksamkeit der Erfindung ist insbesondere gegeben, wenn gewährleistet werden kann, dass eine genügend grosse Abgasmenge zuerst durch die Vergrösserung des Hochdruck-Abgaskanals 31, bzw. durch die Gastaschen, direkt in den Rotor abgeblasen wird, da sonst der Druckwellenprozess gestört wird und somit die Spülung des Rotors zusammenbricht und unerwünschtes Abgas zum Motor geleitet wird. Dies ist durch geeignete regelungtechnische Gestaltung der Erfindung sicherzustellen.The pressure wave machine according to the invention makes it possible over the entire area of the map of a Internal combustion engine both the negative pressure difference and thus the increased expulsion work of the internal combustion engine so to keep low as possible, as well as the Abblasemenge so far as to increase the pressure in the high-pressure exhaust duct as far as can be lowered, that the pressure in the Charge air duct can be reduced so far that a partial closure of the throttle valve Internal combustion engine can be omitted in the partial load range. The Effectiveness of the invention is given in particular when can be guaranteed that a sufficiently large Exhaust gas quantity first by increasing the high-pressure exhaust gas duct 31, or through the gas pockets, directly into the Rotor is blown off, otherwise the pressure wave process is disturbed and thus the flushing of the rotor collapses and unwanted exhaust gas is passed to the engine. This is by suitable control technical design of the invention sure.

Claims (6)

  1. Gas dynamic pressure wave machine, which is designed to supply charge air to a internal combustion engine, with a rotor (6, 40) comprising a cell (18, 41), a low-pressure fresh air inlet channel (14), a high-pressure charge air channel (10) leading to the internal combustion engine (1), a high-pressure exhaust channel (3, 31) coming from the internal combustion engine and a low-pressure exhaust channel (4, 35), wherein the high-pressure exhaust channel (3, 31) and the low-pressure exhaust channel (4, 35) are arranged in a gas enclosure (24, 34) and the low-pressure fresh air inlet channel (14) and the high-pressure charge air channel (10) are arranged in an air enclosure, and the high-pressure exhaust channel (3, 31) on the rotor side has an enlarged section (21, 48, 53) from which a bypass duct (54 -57) leads to the low-pressure exhaust channel (4, 35), characterised in that the bypass duct (54-57) is regulated for maintaining the pressure wave process by suitable means such that firstly a portion of the exhaust flow is always conducted from the high-pressure exhaust channel (3, 31) into the enlarged section (21; 48; 53) before additional exhaust is conducted from the high-pressure exhaust channel (3; 31) to the low-pressure exhaust channel (4, 35) along the duct (54-57), whereby the enlarged section (21; 48; 53) comprises a cut-out (48) or widening (53) on the rotor side, which comprises means (49, 51, 58, 59) for varying the enlarged section (21; 48; 53) without forming a web, and whereby the means for varying the enlarged section (21, 48, 53) are designed in such a way that the aperture of the bypass duct (54-57) can also be changed.
  2. Gas dynamic pressure wave machine according to claim 1, characterised in that the aperture of the duct (54-57) can be varied by an actuating member.
  3. Gas dynamic pressure wave machine according to claim 2, characterised in that the actuating member is controlled by means of a microprocessor.
  4. Gas dynamic pressure wave machine according to one of claims 1 to 3, characterised in that the means for varying the cut out (48) and the aperture of the duct (56) comprise a valve (58), whereby in a displacement of the valve firstly a sufficient amount of the exhaust flow is conducted into the cut out (48), and with a further displacement of the valve the duct (56) is also opened into the low-pressure exhaust channel.
  5. Gas dynamic pressure wave machine according to one of claims 1 to 4, characterised in that the means for varying the widened section (53) of the high-pressure exhaust channel and the aperture of the duct (57) comprise a roller (59), which is controlled so that firstly a sufficiently large amount of the exhaust flow is conducted into the widened section (53) and with a further rotation the duct (57) is also opened in the low-pressure exhaust channel.
  6. Gas dynamic pressure wave machine according to one of claims 1 to 5, characterised in that it comprises a device for controlling a branching from the high-pressure exhaust channel to the enlarged section or to the gas pocket channel.
EP02006066A 2002-03-18 2002-03-18 Gas-dynamic pressure wave supercharger Expired - Lifetime EP1347157B1 (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
AT02006066T ATE309455T1 (en) 2002-03-18 2002-03-18 GAS-DYNAMIC PRESSURE WAVE MACHINE
EP02006066A EP1347157B1 (en) 2002-03-18 2002-03-18 Gas-dynamic pressure wave supercharger
DE50204848T DE50204848D1 (en) 2002-03-18 2002-03-18 Gas dynamic pressure wave machine
ES02006066T ES2252338T3 (en) 2002-03-18 2002-03-18 Supercharger for gas pressure waves.
AU2003200866A AU2003200866A1 (en) 2002-03-18 2003-03-06 Gas-dynamic pressure wave machine
US10/384,898 US7080633B2 (en) 2002-03-18 2003-03-07 Gas-dynamic pressure wave machine
JP2003074333A JP4335558B2 (en) 2002-03-18 2003-03-18 Gas dynamic pressure wave supercharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP02006066A EP1347157B1 (en) 2002-03-18 2002-03-18 Gas-dynamic pressure wave supercharger

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EP1347157A1 EP1347157A1 (en) 2003-09-24
EP1347157B1 true EP1347157B1 (en) 2005-11-09

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US (1) US7080633B2 (en)
EP (1) EP1347157B1 (en)
JP (1) JP4335558B2 (en)
AT (1) ATE309455T1 (en)
AU (1) AU2003200866A1 (en)
DE (1) DE50204848D1 (en)
ES (1) ES2252338T3 (en)

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DE50204848D1 (en) 2005-12-15
AU2003200866A1 (en) 2003-10-02
ES2252338T3 (en) 2006-05-16
ATE309455T1 (en) 2005-11-15
EP1347157A1 (en) 2003-09-24
JP4335558B2 (en) 2009-09-30
JP2004003451A (en) 2004-01-08
US20030226353A1 (en) 2003-12-11
US7080633B2 (en) 2006-07-25

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