WO2000040849A1 - Reciprocating piston engine - Google Patents
Reciprocating piston engine Download PDFInfo
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- WO2000040849A1 WO2000040849A1 PCT/EP1999/010266 EP9910266W WO0040849A1 WO 2000040849 A1 WO2000040849 A1 WO 2000040849A1 EP 9910266 W EP9910266 W EP 9910266W WO 0040849 A1 WO0040849 A1 WO 0040849A1
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- Prior art keywords
- machine according
- reciprocating piston
- filling
- piston machine
- grooves
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F1/00—Cylinders; Cylinder heads
- F02F1/18—Other cylinders
- F02F1/20—Other cylinders characterised by constructional features providing for lubrication
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
- C22C9/01—Alloys based on copper with aluminium as the next major constituent
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
- F16J9/26—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction characterised by the use of particular materials
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F7/00—Casings, e.g. crankcases
- F02F2007/0097—Casings, e.g. crankcases for large diesel engines
Definitions
- the invention relates to a reciprocating piston engine, in particular a large two-stroke diesel engine, with at least one cylinder, the cylinder liner of which, in the area of its tread facing the piston, has greater wear resistance than the material areas having the base material of the cylinder liner for lateral limitation of at least one groove-shaped oil pocket.
- a reciprocating piston internal combustion engine of this type is known from JP 6-105102 B2.
- the cylinder liner is provided with a corrugated contour on the tread side to form groove-shaped oil pockets, the raised areas of this corrugated contour being hardened by a hardening process.
- the hardened areas can be provided with a MoS 2 coating, but this quickly disappears.
- the production of a shaft contour and the implementation of a hardening process that is limited to the raised areas are comparatively complex.
- experience has shown that the hardening depth that can be achieved by the hardening process is comparatively small.
- the degrees of hardness that can only be achieved by a hardening process are also limited.
- the filling can expediently consist of an at least partially ceramic material, preferably a ceramic-metal mixture (cermet). This results in a particularly high level of stability.
- materials of the type mentioned can be obtained in a very simple manner, for example in plasma
- High-speed spraying or laser coating can be applied.
- Another advantageous measure can be that the depth of the grooves that laterally delimit an oil pocket is greater than the maximum wear thickness of the cylinder liner. This ensures that the slot fillings are well anchored in the base material until the cylinder liner is completely worn. This can also be beneficial if the groove cross section increases inwards.
- FIG. 1 shows a cylinder of a large two-stroke diesel engine, partly in section,
- FIG. 2 shows an enlarged section of the region of the arrangement according to FIG. 1 provided with oil pockets and
- FIG. 3 shows an enlarged section through a groove provided with a filling of the arrangement according to FIG. 1.
- the present invention is used in reciprocating piston engines, in particular reciprocating piston internal combustion engines, preferably in the form of slow-running two-stroke large diesel engines.
- reciprocating piston engines in particular reciprocating piston internal combustion engines, preferably in the form of slow-running two-stroke large diesel engines.
- the structure and mode of operation of such arrangements are known per se and therefore require no further explanation in the present context.
- the cylinder of a large two-stroke diesel engine shown in FIG. 1 contains a cylinder liner 2 provided with inlet slots 1, onto which a cylinder head 3 containing an outlet arrangement, not shown, is placed.
- the inside of the cylinder liner 2 is designed as a running surface 4, with which a piston 6, provided with circumferential piston rings 5, interacts and disengages.
- the tread 4 is supplied with lubricating oil via lubricating oil supply lines 7.
- suitable oil pockets 8, which are only indicated in FIG. 1, are provided in this area.
- the depressions forming the oil pockets 8 are not present from the start. However, measures are provided from the start which cause the depressions on which the oil pockets 8 are based to develop automatically during operation due to wear on the base material on which the cylinder liner 2 is based.
- the oil pockets 8 are laterally delimited by material areas 9 flanking them. An oil pocket 8 can form between each two such material areas 9.
- the material regions 9 which laterally delimit an oil pocket 8 are, as can be seen from FIGS. 2 and 3, designed as a filling 11 of a respectively assigned groove 10.
- the material forming the filling 11 has greater wear resistance than the base material of the cylinder liner 2, which generally consists of cast steel.
- the grooves 10, as indicated in FIG. 3 are filled to the level of the tread 4, so that a smooth surface results which can be easily machined, for example honed. First, the grooves 10 are cut. The filling 11 is then introduced. Then the tread 4 is finished.
- a material can be expediently used which consists entirely or at least partially of ceramic material, for example a ceramic-metal mixture (cermet).
- This material can expediently contain carbides and / or oxides and / or nitrides and / or borides and / or silicates with Cu and / or Al bronze and / or Ni and / or NiCr and / or Mo and / or Al graphite and / or Ni graphite and / or Al-Br graphite and an organic binder, the carbides, oxides, nitrides, borides, silicates advantageously being present with 10-60% in the hard phase and 5-80% in the soft phase.
- CrO is a particularly useful material because it not only has high stability and a high working temperature, but is also non-corrosive and non-oxidizing.
- the filling (11) can contain 20-50%, preferably 20-40% carbides and / or oxides and / or nitrides and / or borides and / or silicates as well as at least 20% Al bronze -40%, preferably 60-80%.
- Preferred configurations can be 20-40% oxides mixed with 60-80% Al bronze or 30-50% oxides, nitrides or carbides mixed with at least Al bronze, or preferably with 10-20% Mo and 20-30% Ni or NiC or contain 20-40% AI bronze. Materials of this type can be applied in an arc, flame, plasma or high-speed spraying process or can be introduced into the associated groove 10.
- Preferred material compositions in this connection are 10-18% Cr, 2-3% Fe, 2-4% Si, 2-4% B, 0.1-0.5% C and Ni as the balance or 10-18% Cr, 2- 3% Fe, 2-4% Si, 2-4% B, 0.1-0.5% C, 6-12% Mo, 0.1-0.5% C, 30-40% Co and Ni as Balance or 10-18% Cr, 2-3% I, 2-4% Si, 2-4% B, 0.1 -0.5% C, 6-12% Mo, 1-6% Cu, 0, 1-0.5% C and Ni as balance or 10-18% Cr, 2-3% I, 2-4% Si, 2-4% B, 0.1-0.5% C, 6- 12% Mo, 10-20% Ni, 65-88% WC and 12% Co. Flame, induction or laser sintering can also be considered here.
- a material can also be used which contains carbides and / or oxides and / or nitrides and / or borides and / or silicates with 10-60% in the hard phase and 5-80% in the soft phase Phase as well as 2-10% Cu, 20-30% Al-bronze, 10-85% Ni or NiCr, 10-30% Cr, 0.1-5% carbon, 1-8% Fe, 2-15% Mo or Mo sulfide or Mo disulfide or Mo oxide or Mo Contains dioxide or Mo peroxide, 2-7% Cu, 10-40% Co, 30-80% WC or 88% WC and 12% Co.
- Powder materials are also suitable.
- a particularly preferred material in this connection consists of 20-30% Cr, 1-10% Mo, 2-3% C, 2-5% V, 0.2-1% Mn, 0.2-4% Si or B and Ni as the rest.
- the filling 11 can also be designed as a welding job.
- a material can be used that 2-20% Al, 0.5-10% Fe, 0.1-8% Mn, 0.1 -2% Si, 0.1 -10% o Ni, 0.1 Contains -2% C and at least one of the components Sb, Co, Be, Cr, Sn, Cd, Zn, Pb with at most 5-20% and the rest Cu.
- a particularly preferred composition can contain 14-17% Al, 3-5% Fe, 1-3% Mn, 0.1-2% Si, a maximum of 0.3% C and the rest Cu.
- the depth of the groove 10 indicated in FIG. 3 at d corresponds at least to the maximum wear thickness of the cylinder liner 4.
- the depth d is expediently greater than the maximum wear thickness, so that even with a completely worn cylinder liner 2, the filling 11 is still well anchored in the base material is.
- the cross section of the groove 10 is widened inwards, as indicated in FIG. 2 by the cross-sectional shape 12 drawn with broken lines.
- a preferred groove depth can be in the range between 0.1 to 0.4% of the diameter D of the tread 4.
- the clear width of the oil pockets 8 formed corresponds to the distance between the associated grooves 10, each provided with a filling 11. This distance, indicated at w in FIG.
- the clear width Width of the grooves 10 and thus the width b of the fillings 11 assigned to them suitably corresponds to the groove depth d. This ensures good stability against shear stress.
- One or more oil pockets 8 can be provided.
- the grooves 10 assigned to them, each provided with a filling 11, are expediently arranged where, according to previous experience, the risk of insufficient lubrication and, accordingly, the risk of heat corrosion etc. is particularly great. This is especially the case in the upper area of the tread.
- the means provided to form an oil pocket 8 are arranged in the region of the running surface delimited by the first and second piston rings 5 in the top dead center position of the piston 6.
- a further oil pocket 8 or the means necessary for this can be provided in the area below the lowest piston ring 5.
- further oil pockets 8, which are arranged even deeper, are also provided.
- the oil pockets 8 and, accordingly, the material areas delimiting them can be formed all around.
- one or more screw-shaped oil pockets 8 and, accordingly, the screw-shaped material regions 9 that delimit them can also be provided. These can extend over an area or over the entire guide length of the tread 4.
- the slope indicated at p in FIG. 1 can amount to approximately 1.5% to 20% of the diameter D of the tread 4. This slope can be constant over the entire length. However, a variable slope would also be conceivable in order to obtain a greater oil pocket density in particularly endangered areas than in less endangered areas.
- the groove 10 and, accordingly, the filling 11 assigned to it have a rectangular or trapezoidal cross section.
- the inner edges can be rounded to avoid notch stresses.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Coating By Spraying Or Casting (AREA)
Abstract
Description
Hubkolbenmaschine Reciprocating machine
Die Erfindung betrifft eine Hubkolbenmaschine, insbesondere einen Zweitakt- Großdieselmotor, mit wenigstens einem Zylinder, dessen Zylinderbüchse im Bereich ihrer dem Kolben zugewandten Lauffläche eine größere Verschleißfestigkeit als das Grundmaterial der Zylinderbüchse aufweisende Materialbereiche zur seitlichen Begrenzung wenigstens einer nutförmigen Oltasche enthält.The invention relates to a reciprocating piston engine, in particular a large two-stroke diesel engine, with at least one cylinder, the cylinder liner of which, in the area of its tread facing the piston, has greater wear resistance than the material areas having the base material of the cylinder liner for lateral limitation of at least one groove-shaped oil pocket.
Eine Hubkolbenbrennkraftmaschine dieser Art ist aus der JP 6-105102 B2 bekannt. Bei dieser bekannten Anordnung ist die Zylinderbüchse zur Bildung von nutförmigen Öltaschen laufflächenseitig mit einer Wellenkontur versehen, wobei die erhabenen Stellen dieser Wellenkontur durch einen Härtungsprozess gehärtet sind. Zur Verbesserung der Einlaufeigenschaften können die gehärteten Stellen mit einer MoS2-Beschichtung versehen sein, die aber schnell verschwindet. Die Herstellung einer Wellenkontur und die Durchführung eines örtlich auf die erhabenen Stellen beschränkten Härtungsprozesses sind vergleichsweise aufwendig. Hinzu kommt, dass die durch den Härtungsprozess erzielbare Härtungstiefe erfahrungsgemäß vergleichsweise gering ist. Außerdem sind auch die lediglich durch einen Härtungsprozess erzielbaren Härtegrade begrenzt. Bei der bekannten Anordnung wird daher nur eine vergleichsweise geringe Standzeit der Wellenkontur erreicht. Ein weiterer Nachteil ist darin zu sehen, dass die örtlich auf die erhabenen Stellen beschränkte Härtung auch zu einem unerwünschten Verzug und zu unerwünschten Gefügeänderungen in den benachbarten Materialbereichen führen kann. Die bekannte Anordnung erweist sich demnach als nicht einfach und langlebig genug. Hiervon ausgehend ist es daher die Aufgabe der vorliegenden Erfindung, eine Hubkolbenmaschine eingangs erwähnter Art mit einfachen und kostengünstigen Mitteln so zu verbessern, dass eine lange Lebensdauer der Zylinderbüchse erreicht werden kann.A reciprocating piston internal combustion engine of this type is known from JP 6-105102 B2. In this known arrangement, the cylinder liner is provided with a corrugated contour on the tread side to form groove-shaped oil pockets, the raised areas of this corrugated contour being hardened by a hardening process. To improve the running-in properties, the hardened areas can be provided with a MoS 2 coating, but this quickly disappears. The production of a shaft contour and the implementation of a hardening process that is limited to the raised areas are comparatively complex. In addition, experience has shown that the hardening depth that can be achieved by the hardening process is comparatively small. In addition, the degrees of hardness that can only be achieved by a hardening process are also limited. In the known arrangement, therefore, only a comparatively short service life of the shaft contour is achieved. Another disadvantage is that the hardening, which is limited locally to the raised areas, can also lead to undesired warping and to undesirable structural changes in the adjacent material areas. The known arrangement therefore proves to be not simple and durable enough. Proceeding from this, it is therefore the object of the present invention to improve a reciprocating piston machine of the type mentioned at the outset using simple and inexpensive means in such a way that a long service life of the cylinder liner can be achieved.
Diese Aufgabe wird erfindungsgemäß dadurch gelöst, dass die zur seitlichen Begrenzung jeweils einer Oltasche vorgesehenen Materialbereiche als Füllung einer Nut ausgebildet sind, deren Tiefe zumindest der maximalen Verschleißdicke der Zylinderbüchse entspricht.This object is achieved according to the invention in that the material regions provided for the lateral delimitation of an oil pocket are designed as a groove, the depth of which corresponds at least to the maximum wear thickness of the cylinder liner.
Diese Maßnahmen ermöglichen in vorteilhafter Weise eine freie Materialwahl hinsichtlich der Nutfüllungen und damit der Oltaschenbegrenzungen. Es kann daher ein vom Grundmaterial verschiedenes, für die auftretenden Bedürfnisse besser als das gehärtete Grundmaterial geeignetes Material Verwendung finden. Die Tiefe der Nuten kann über die bei einem Härtungsprozess erzielbare Härtungstiefe weit hinausgehen. Bei der Herstellung ergibt sich zunächst eine glatte Oberfläche, die vergleichsweise einfach bearbeitet, beispielsweise gehont, werden kann. Aufgrund der geringeren Verschleißfestigkeit des Grundmaterials verschleißt dieses im Bereich zwischen den aus Fremdmaterial bestehenden Nutfüilungen schneller, womit sich automatisch die gewünschten Öltaschen ergeben. Diese bleiben erhalten, bis die Zylinderbüchse vollständig verschlissen ist. Mit den erfindungsgemäßen Maßnahmen werden daher die eingangs geschilderten Nachteile der bekannten Anordnung vollständig vermieden.These measures advantageously allow a free choice of material with regard to the groove fillings and thus the oil pocket limits. It is therefore possible to use a material that is different from the base material and that is better suited to the needs that arise than the hardened base material. The depth of the grooves can go far beyond the hardening depth that can be achieved in a hardening process. During production, a smooth surface initially results, which can be processed comparatively easily, for example honed. Due to the lower wear resistance of the base material, it wears faster in the area between the groove fillings made of foreign material, which automatically results in the desired oil pockets. These remain until the cylinder liner is completely worn out. The measures according to the invention therefore completely avoid the disadvantages of the known arrangement described at the outset.
Vorteilhafte Ausgestaltungen und zweckmäßige Fortbildungen der übergeordneten Maßnahmen sind in den Unteransprüchen angegeben. So kann die Füllung zweckmäßig aus einem zumindest teilweise keramischen Material, vorzugsweise aus einer Keramik-Metall-Mischung (Cermet) bestehen. Hierbei ergibt sich eine besonders hohe Standsicherheit. Außerdem können Materialien der genannten Art auf höchst einfache Weise beispielsweise im Plasma-Advantageous refinements and appropriate further training of the higher-level measures are specified in the subclaims. The filling can expediently consist of an at least partially ceramic material, preferably a ceramic-metal mixture (cermet). This results in a particularly high level of stability. In addition, materials of the type mentioned can be obtained in a very simple manner, for example in plasma
Hochgeschwindigkeitsspritzverfahren oder im Laser-Beschichtungsverfahren aufgebracht werden. Eine weitere vorteilhafte Maßnahme kann darin bestehen, dass die Tiefe der jeweils eine Oltasche seitlich begrenzenden Nuten größer als die maximale Verschleißdicke der Zylinderbüchse ist. Hierdurch wird sichergestellt, dass die Nutfüllungen bis zum vollständigen Verschleiß der Zylinderbüchse gut im Grundmaterial verankert sind. Dem kann zudem förderlich sein, wenn der Nutquerschnitt nach innen zunimmt.High-speed spraying or laser coating can be applied. Another advantageous measure can be that the depth of the grooves that laterally delimit an oil pocket is greater than the maximum wear thickness of the cylinder liner. This ensures that the slot fillings are well anchored in the base material until the cylinder liner is completely worn. This can also be beneficial if the groove cross section increases inwards.
Weitere vorteilhafte Ausgestaltungen und zweckmäßige Fortbildungen der übergeordneten Maßnahmen sind in den restlichen Unteransprüchen angegeben und aus der nachstehenden Beispielsbeschreibung anhand der Zeichnung näher entnehmbar.Further advantageous refinements and expedient further developments of the superordinate measures are specified in the remaining subclaims and can be found in more detail in the following description of the examples with reference to the drawing.
In der nachstehend beschriebenen Zeichnung zeigen:In the drawing described below:
Figur 1 einen Zylinder eines Zweitakt-Großdieselmotors teilweise im Schnitt,FIG. 1 shows a cylinder of a large two-stroke diesel engine, partly in section,
Figur 2 einen vergrößerten Ausschnitt des mit Öltaschen versehenen Bereichs der Anordnung gemäß Figur 1 und Figur 3 einen vergrößerten Schnitt durch eine mit einer Füllung versehene Nut der Anordnung gemäß Figur 1.2 shows an enlarged section of the region of the arrangement according to FIG. 1 provided with oil pockets and FIG. 3 shows an enlarged section through a groove provided with a filling of the arrangement according to FIG. 1.
Die vorliegende Erfindung findet Anwendung bei Hubkolbenmaschinen, insbesondere Hubkolbenbrennkraftmaschinen, vorzugsweise in Form langsam laufender Zweitakt-Großdieselmotoren. Der Aufbau und die Wirkungsweise derartiger Anordnungen sind an sich bekannt und bedürfen daher im vorliegenden Zusammenhang keiner näheren Erläuterung mehr.The present invention is used in reciprocating piston engines, in particular reciprocating piston internal combustion engines, preferably in the form of slow-running two-stroke large diesel engines. The structure and mode of operation of such arrangements are known per se and therefore require no further explanation in the present context.
Der in Figur 1 dargestellte Zylinder eines Zweitakt-Großdieselmotors enthält eine mit Einlassschlitzen 1 versehene Zylinderbuchse 2, auf die ein hier eine nicht näher dargestellte Ausiassanordnung enthaltender Zylinderkopf 3 aufgesetzt ist. Die Innenseite der Zylinderbüchse 2 ist als Lauffläche 4 ausgebildet, mit der ein mit umfangsseitigen Kolbenringen 5 versehender, auf- und abgehender Kolben 6 zusammenwirkt. Die Lauffläche 4 wird über Schmierölzuleitungen 7 mit Schmieröl versorgt. Zur Erzielung einer guten Verteilung des Schmieröls und insbesondere einer guten Schmierölversorgung von Bereichen, in denen erfahrungsgemäß die Schmierölversorgung mangelhaft ist, beispielsweise des oberen Bereichs der Lauffläche 4, sind in diesem Bereich hierzu geeignete, in Figur 1 lediglich angedeutete Öltaschen 8 vorgesehen. Die die Öltaschen 8 bildenden Vertiefungen sind nicht von Anfang an vorhanden. Es sind jedoch von Anfang an Maßnahmen vorgesehen, die bewirken, dass die den Öltaschen 8 zugrundeliegenden Vertiefungen im Laufe des Betriebs durch Verschleiß des der Zylinderbüchse 2 zugrundeliegenden Grundmaterials von selbst entstehen.The cylinder of a large two-stroke diesel engine shown in FIG. 1 contains a cylinder liner 2 provided with inlet slots 1, onto which a cylinder head 3 containing an outlet arrangement, not shown, is placed. The inside of the cylinder liner 2 is designed as a running surface 4, with which a piston 6, provided with circumferential piston rings 5, interacts and disengages. The tread 4 is supplied with lubricating oil via lubricating oil supply lines 7. To achieve a good distribution of the lubricating oil and in particular a good supply of lubricating oil to areas in which experience has shown that the supply of lubricating oil is inadequate, for example the upper area of the running surface 4, suitable oil pockets 8, which are only indicated in FIG. 1, are provided in this area. The depressions forming the oil pockets 8 are not present from the start. However, measures are provided from the start which cause the depressions on which the oil pockets 8 are based to develop automatically during operation due to wear on the base material on which the cylinder liner 2 is based.
Die Öltaschen 8 werden jeweils durch sie flankierende Materialbereiche 9 seitlich begrenzt. Zwischen jeweils zwei derartigen Materialbereichen 9 kann sich eine Oltasche 8 ausbilden. Die jeweils eine Oltasche 8 seitlich begrenzenden Materialbereiche 9 sind, wie den Figuren 2 und 3 entnehmbar ist, als Füllung 11 einer jeweils zugeordneten Nut 10 ausgebildet. Das die Füllung 11 bildende Material besitzt eine größere Verschleißfestigkeit als das Grundmaterial der Zylinderbüchse 2, die in der Regel aus Stahlguss besteht. Im Neuzustand sind die Nuten 10, wie in Figur 3 angedeutet ist, bis auf das Niveau der Lauffläche 4 gefüllt, so dass sich eine glatte Oberfläche ergibt, die leicht bearbeitet, beispielsweise gehont, werden kann. Zunächst werden die Nuten 10 eingeschnitten. Danach wird die Füllung 11 eingebracht. Anschließend wird die Lauffläche 4 fertig bearbeitet.The oil pockets 8 are laterally delimited by material areas 9 flanking them. An oil pocket 8 can form between each two such material areas 9. The material regions 9 which laterally delimit an oil pocket 8 are, as can be seen from FIGS. 2 and 3, designed as a filling 11 of a respectively assigned groove 10. The material forming the filling 11 has greater wear resistance than the base material of the cylinder liner 2, which generally consists of cast steel. In the new state, the grooves 10, as indicated in FIG. 3, are filled to the level of the tread 4, so that a smooth surface results which can be easily machined, for example honed. First, the grooves 10 are cut. The filling 11 is then introduced. Then the tread 4 is finished.
Aufgrund der höheren Verschleißfestigkeit des die Füllung 11 bildenden Materials gegenüber dem der Zylinderbüchse 2 zugrundeliegenden Grundmaterial ist der Verschleiß des Grundmaterials bereits während der Einlaufphase größer als der Verschleiß der Füllungen 11 , wie in Figur 3 durch unterbrochene Linien angedeutet ist. Hierdurch ergibt sich daher zwischen zwei einander benachbarten Füllungen 11 die jeweils gewünschte, nutförmige Oltasche 8.Due to the higher wear resistance of the material forming the filling 11 compared to the base material on which the cylinder liner 2 is based, the wear of the base material is greater during the running-in phase than the wear of the fillings 11, as indicated by broken lines in FIG. This therefore results in the respectively desired, groove-shaped oil pocket 8 between two mutually adjacent fillings 11.
Zur Bildung der Füllung 11 kann zweckmäßig ein Material Verwendung finden, das ganz oder zumindest teilweise aus keramischem Material besteht, z.B. eine Keramik- Metall-Mischung (Cermet). Dieses Material kann zweckmäßig Carbide und/oder Oxide und/oder Nitride und/oder Boride und/oder Silikate mit Cu und/oder AI-Bronze und/oder Ni und/oder NiCr und/oder Mo und/oder AI-Graphite und/oder Ni-Graphit und/oder Al-Br-Graphite sowie einen organischen Binder enthalten, wobei vorteilhaft die Carbide, Oxide, Nitride, Boride, Silikate mit 10-60% in der harten Phase und 5- 80% in der weichen Phase vorliegen. Als besonders vorteilhaft hat es sich erwiesen, wenn dabei die Carbide, Oxide, Nitride, Boride, Silikate als Cr-Verbindungen vorliegen. Dabei ist CrO ein besonders zweckdienliches Material, da es nicht nur eine hohe Stabilität aufweist und eine hohe Arbeitstemperatur zulässt, sondern auch nicht korrosiv und nicht oxidierend ist.To form the filling 11, a material can be expediently used which consists entirely or at least partially of ceramic material, for example a ceramic-metal mixture (cermet). This material can expediently contain carbides and / or oxides and / or nitrides and / or borides and / or silicates with Cu and / or Al bronze and / or Ni and / or NiCr and / or Mo and / or Al graphite and / or Ni graphite and / or Al-Br graphite and an organic binder, the carbides, oxides, nitrides, borides, silicates advantageously being present with 10-60% in the hard phase and 5-80% in the soft phase. It has proven to be particularly advantageous if the carbides, oxides, nitrides, borides and silicates are present as Cr compounds. CrO is a particularly useful material because it not only has high stability and a high working temperature, but is also non-corrosive and non-oxidizing.
In einer vorteilhaften Ausgestaltung der oben genannten Vorgaben kann die Füllung (11 ) 20-50%, vorzugsweise 20-40% Carbide und/oder Oxide und/oder Nitride und/oder Boride und/oder Silikate sowie zumindest noch AI-Bronze mit mindestens 20-40%, vorzugsweise 60-80%, enthalten. Bevorzugte Ausgestaltungen können 20- 40% Oxide gemischt mit 60-80% AI-Bronze oder 30-50% Oxide, Nitride oder Carbide gemischt mit wenigstens AI-Bronze, oder vorzugsweise mit 10-20% Mo und 20-30% Ni oder NiC oder 20-40% AI-Bronze enthalten. Materialien dieser Art können im Lichtbogen, Flamm-, Plasma- oder Hochgeschwindigkeitssprühverfahren aufgetragen bzw. in die zugeordnete Nut 10 eingebracht werden.In an advantageous embodiment of the above-mentioned specifications, the filling (11) can contain 20-50%, preferably 20-40% carbides and / or oxides and / or nitrides and / or borides and / or silicates as well as at least 20% Al bronze -40%, preferably 60-80%. Preferred configurations can be 20-40% oxides mixed with 60-80% Al bronze or 30-50% oxides, nitrides or carbides mixed with at least Al bronze, or preferably with 10-20% Mo and 20-30% Ni or NiC or contain 20-40% AI bronze. Materials of this type can be applied in an arc, flame, plasma or high-speed spraying process or can be introduced into the associated groove 10.
Eine andere Materialgruppe, die Silikon und Bor mit einem Anteil von jeweils 0,1 - 10% enthält, kann ebenfalls auf die oben genannte Art und Weise aufgebracht werden. Bevorzugte Materialzusammensetzungen in diesem Zusammenhang sind 10-18% Cr, 2-3% Fe, 2-4% Si, 2-4% B, 0.1-0,5% C und Ni als Rest oder 10-18% Cr, 2-3% Fe, 2-4% Si, 2-4% B, 0,1-0,5% C, 6-12% Mo, 0,1-0,5% C, 30-40% Co und Ni als Rest oder 10-18% Cr, 2-3% I, 2-4% Si, 2-4% B, 0,1 -0,5% C, 6-12% Mo, 1-6% Cu, 0,1-0,5% C und Ni als Rest oder 10-18% Cr, 2-3% I, 2-4% Si, 2-4% B, 0,1-0,5% C, 6- 12% Mo, 10-20% Ni, 65-88% WC und 12% Co. Auch eine Flamm-, Induktions- oder Lasersinterung kann hier in Frage kommen.Another group of materials containing silicone and boron, each with a share of 0.1-10%, can also be applied in the above-mentioned manner. Preferred material compositions in this connection are 10-18% Cr, 2-3% Fe, 2-4% Si, 2-4% B, 0.1-0.5% C and Ni as the balance or 10-18% Cr, 2- 3% Fe, 2-4% Si, 2-4% B, 0.1-0.5% C, 6-12% Mo, 0.1-0.5% C, 30-40% Co and Ni as Balance or 10-18% Cr, 2-3% I, 2-4% Si, 2-4% B, 0.1 -0.5% C, 6-12% Mo, 1-6% Cu, 0, 1-0.5% C and Ni as balance or 10-18% Cr, 2-3% I, 2-4% Si, 2-4% B, 0.1-0.5% C, 6- 12% Mo, 10-20% Ni, 65-88% WC and 12% Co. Flame, induction or laser sintering can also be considered here.
Bei der Ausbildung der Füllung 11 als Sinterfüllung kann auch ein Material Verwendung finden, das Carbide und/oder Oxide und/oder Nitride und/oder Boride und/oder Silikate mit 10-60% in der harten Phase und 5-80% in der weichen Phase sowie 2-10% Cu, 20-30% AI-Bronze, 10-85% Ni oder NiCr, 10-30% Cr, 0,1-5% Carbon, 1-8% Fe, 2-15% Mo oder Mo-Sulfid oder Mo-Disulfid oder Mo-Oxid oder Mo- Dioxid oder Mo-Peroxid, 2-7% Cu, 10-40% Co, 30-80% WC oder 88% WC und 12% Co enthält.When the filling 11 is formed as a sintered filling, a material can also be used which contains carbides and / or oxides and / or nitrides and / or borides and / or silicates with 10-60% in the hard phase and 5-80% in the soft phase Phase as well as 2-10% Cu, 20-30% Al-bronze, 10-85% Ni or NiCr, 10-30% Cr, 0.1-5% carbon, 1-8% Fe, 2-15% Mo or Mo sulfide or Mo disulfide or Mo oxide or Mo Contains dioxide or Mo peroxide, 2-7% Cu, 10-40% Co, 30-80% WC or 88% WC and 12% Co.
Auch Pudermaterialien sind geeignet. So kann z.B. ein Puder mit 0,2-5% C, 20-50% Cr, 1-20% Mo, 1 -20% V, 0,1-4% Si oder B, 0,1-5% Mn, 0,1 -5% Fe, 0,5-50% Carbiden, Oxiden, Nitriden, Boriden oder Silikaten, Mo-Sulfiden/-Dioxiden/-Oxiden/- Disulfiden oder Mo-Peroxiden Verwendung finden, wobei Silikon und/oder Bor mit jeweils 0,1 -5% und als Rest Ni vorgesehen sein können. Ein besonders bevorzugtes Material in diesem Zusammenhang besteht aus 20-30% Cr, 1-10% Mo, 2-3% C, 2- 5% V, 0,2-1 % Mn, 0,2-4% Si oder B und Ni als Rest.Powder materials are also suitable. For example, a powder with 0.2-5% C, 20-50% Cr, 1-20% Mo, 1 -20% V, 0.1-4% Si or B, 0.1-5% Mn, 0.1 -5% Fe, 0.5-50% carbides, oxides, nitrides, borides or silicates, Mo sulfides / dioxides / oxides / disulfides or Mo peroxides are used, silicone and / or boron each having 0, 1 -5% and the rest Ni can be provided. A particularly preferred material in this connection consists of 20-30% Cr, 1-10% Mo, 2-3% C, 2-5% V, 0.2-1% Mn, 0.2-4% Si or B and Ni as the rest.
Alternativ kann die Füllung 11 aber auch als Schweißauftrag ausgebildet werden. Dabei kann ein Material Verwendung finden, das 2-20% AI, 0,5-10% Fe, 0,1-8% Mn, 0,1 -2% Si, 0,1 -10%o Ni, 0,1 -2% C und zumindest eine der Komponenten Sb, Co, Be, Cr, Sn, Cd, Zn, Pb mit höchstens 5-20% und Rest Cu enthält. Eine besonders bevorzugte Zusammensetzung kann dabei 14-17% AI, 3-5% Fe, 1-3% Mn, 0,1 -2% Si, maximal 0,3% C und Rest Cu enthalten.Alternatively, the filling 11 can also be designed as a welding job. A material can be used that 2-20% Al, 0.5-10% Fe, 0.1-8% Mn, 0.1 -2% Si, 0.1 -10% o Ni, 0.1 Contains -2% C and at least one of the components Sb, Co, Be, Cr, Sn, Cd, Zn, Pb with at most 5-20% and the rest Cu. A particularly preferred composition can contain 14-17% Al, 3-5% Fe, 1-3% Mn, 0.1-2% Si, a maximum of 0.3% C and the rest Cu.
Die in Figur 3 bei d angedeutete Tiefe der Nut 10 entspricht zumindest der maximalen Verschleißdicke der Zylinderbüchse 4. Zweckmäßig ist die Tiefe d größer als die maximale Verschleißdicke, so dass auch noch bei einer vollständig verschlissenen Zylinderbüchse 2 eine gute Verankerung der Füllung 11 im Grundmaterial gewährleistet ist. In diesem Zusammenhang kann es auch vorteilhaft sein, wenn der Querschnitt der Nut 10 nach innen erweitert ist, wie in Figur 2 durch die mit unterbrochenen Linien gezeichnete Querschnittsform 12 angedeutet ist. Eine bevorzugte Nuttiefe kann im Bereich zwischen 0,1 bis 0,4 % des Durchmessers D der Lauffläche 4 liegen. Die lichte Weite der sich bildenden Öltaschen 8 entspricht dem Abstand der zugeordneten, mit jeweils einer Füllung 11 versehenen, Nuten 10. Dieser in Figur 2 bei w angedeutete Abstand liegt vorzugsweise im Bereich zwischen 1 bis 2 % des Durchmessers D der Lauffläche 4. Die lichte Weite der Nuten 10 und damit die Breite b der diesen zugeordneten Füllungen 11 entspricht zweckmäßig der Nuttiefe d. Hierdurch wird eine gute Standsicherheit gegen Scherbeanspruchung erreicht. Es können eine oder mehrere Öltaschen 8 vorgesehen sein. Die diesen zugeordneten, mit jeweils einer Füllung 11 versehenen Nuten 10 sind zweckmäßig dort angeordnet, wo nach der bisherigen Erfahrung die Gefahr einer ungenügenden Schmierung und dementsprechend die Gefahr von Wärmekorrosion etc. besonders groß ist. Dies ist vor allem im oberen Bereich der Lauffläche der Fall. In Figur 1 sind in dem vom ersten und zweiten Kolbenring 5 in der oberen Totpunktstellung des Kolbens 6 begrenzten Bereich der Lauffläche die zur Bildung einer Oltasche 8 vorgesehenen Mittel angeordnet. Eine weitere Oltasche 8 bzw. die hierzu notwendigen Mittel können im Bereich unterhalb des untersten Kolbenrings 5 vorgesehen sein. Im dargestellten Beispiel sind auch noch weitere, noch tiefer angeordnete Öltaschen 8 vorgesehen.The depth of the groove 10 indicated in FIG. 3 at d corresponds at least to the maximum wear thickness of the cylinder liner 4. The depth d is expediently greater than the maximum wear thickness, so that even with a completely worn cylinder liner 2, the filling 11 is still well anchored in the base material is. In this context it can also be advantageous if the cross section of the groove 10 is widened inwards, as indicated in FIG. 2 by the cross-sectional shape 12 drawn with broken lines. A preferred groove depth can be in the range between 0.1 to 0.4% of the diameter D of the tread 4. The clear width of the oil pockets 8 formed corresponds to the distance between the associated grooves 10, each provided with a filling 11. This distance, indicated at w in FIG. 2, is preferably in the range between 1 to 2% of the diameter D of the tread 4. The clear width Width of the grooves 10 and thus the width b of the fillings 11 assigned to them suitably corresponds to the groove depth d. This ensures good stability against shear stress. One or more oil pockets 8 can be provided. The grooves 10 assigned to them, each provided with a filling 11, are expediently arranged where, according to previous experience, the risk of insufficient lubrication and, accordingly, the risk of heat corrosion etc. is particularly great. This is especially the case in the upper area of the tread. In FIG. 1, the means provided to form an oil pocket 8 are arranged in the region of the running surface delimited by the first and second piston rings 5 in the top dead center position of the piston 6. A further oil pocket 8 or the means necessary for this can be provided in the area below the lowest piston ring 5. In the example shown, further oil pockets 8, which are arranged even deeper, are also provided.
Die Öltaschen 8 und dementsprechend die diese begrenzenden Materialbereiche können umlaufend ausgebildet sein. Zusätzlich oder alternativ hierzu können aber auch eine oder mehrere, schraubenförmig verlaufende Öltaschen 8 und dementsprechend diese begrenzende, schraubenförmige Materialbereiche 9 vorgesehen sein. Diese können sich über einen Bereich oder über die ganze Führungslänge der Lauffläche 4 erstrecken.The oil pockets 8 and, accordingly, the material areas delimiting them can be formed all around. In addition or as an alternative to this, one or more screw-shaped oil pockets 8 and, accordingly, the screw-shaped material regions 9 that delimit them can also be provided. These can extend over an area or over the entire guide length of the tread 4.
Im Falle einer schraubenförmig verlaufenden Oltasche 8 kann die in Figur 1 bei p angedeutete Steigung etwa 1 ,5 % bis 20 % des Durchmessers D der Lauffläche 4 betragen. Diese Steigung kann über der ganzen Länge konstant sein. Es wäre aber auch eine variable Steigung denkbar, um in besonders gefährdeten Bereichen eine größere Öltaschendichte zu bekommen als in weniger gefährdeten Bereichen.In the case of a screw-shaped oil pocket 8, the slope indicated at p in FIG. 1 can amount to approximately 1.5% to 20% of the diameter D of the tread 4. This slope can be constant over the entire length. However, a variable slope would also be conceivable in order to obtain a greater oil pocket density in particularly endangered areas than in less endangered areas.
Im dargestellten Beispiel besitzen die Nut 10 und dementsprechend auch die dieser zugeordnete Füllung 11 einen rechteckförmigen bzw. trapezförmigen Querschnitt. Die inneren Kanten können zur Vermeidung von Kerbspannungen abgerundet sein. In the example shown, the groove 10 and, accordingly, the filling 11 assigned to it have a rectangular or trapezoidal cross section. The inner edges can be rounded to avoid notch stresses.
Claims
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2000592532A JP3419762B2 (en) | 1999-01-08 | 1999-12-22 | Reciprocating piston engine |
| GB0104423A GB2361759B (en) | 1999-01-08 | 1999-12-22 | Reciprocating piston engine |
| AU30420/00A AU3042000A (en) | 1999-01-08 | 1999-12-22 | Reciprocating piston engine |
| NO20012894A NO20012894L (en) | 1999-01-08 | 2001-06-12 | Reciprocating piston engine |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19900385.8 | 1999-01-08 | ||
| DE19900385A DE19900385C2 (en) | 1999-01-08 | 1999-01-08 | Reciprocating machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2000040849A1 true WO2000040849A1 (en) | 2000-07-13 |
Family
ID=7893736
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/EP1999/010266 Ceased WO2000040849A1 (en) | 1999-01-08 | 1999-12-22 | Reciprocating piston engine |
Country Status (10)
| Country | Link |
|---|---|
| JP (1) | JP3419762B2 (en) |
| KR (1) | KR100417185B1 (en) |
| CN (1) | CN1112510C (en) |
| AU (1) | AU3042000A (en) |
| DE (1) | DE19900385C2 (en) |
| GB (1) | GB2361759B (en) |
| NO (1) | NO20012894L (en) |
| PL (1) | PL348869A1 (en) |
| TW (1) | TW463015B (en) |
| WO (1) | WO2000040849A1 (en) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE10134736C2 (en) * | 2001-07-17 | 2003-10-09 | Man B&W Diesel A/S, Copenhagen Sv | Large machine with at least one sliding surface and method for producing a sliding surface |
| DE10136788C2 (en) * | 2001-07-27 | 2003-06-05 | Diehl Metall Stiftung & Co Kg | aluminum Bronze |
| FI124135B (en) * | 2010-06-08 | 2014-03-31 | Wärtsilä Finland Oy | PISTON ENGINE CYLINDER SOCKET |
| DE102011106564A1 (en) * | 2011-07-05 | 2013-01-10 | Mahle International Gmbh | Method for producing a cylinder surface and cylinder liner |
| KR20150140309A (en) * | 2013-04-05 | 2015-12-15 | 페더럴-모걸 코오포레이숀 | Piston made using additive manufacturing techniques |
| JP2017057825A (en) * | 2015-09-18 | 2017-03-23 | トヨタ自動車株式会社 | Cylinder bore surface treatment method |
| DE102016222299A1 (en) * | 2016-11-14 | 2018-05-17 | Man Diesel & Turbo Se | Cylinder of an internal combustion engine |
| CN109321778A (en) * | 2018-11-21 | 2019-02-12 | 中国兵器科学研究院宁波分院 | A kind of wear-resisting aluminium bronze and preparation method thereof containing rare earth |
| JPWO2021075326A1 (en) * | 2019-10-17 | 2021-11-04 | Tpr株式会社 | Compression ring, and piston with compression ring |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1900699A1 (en) * | 1968-01-09 | 1969-09-04 | Ramsey Corp | Piston cylinder, in particular cylinder lining sleeve for an internal combustion engine |
| CH493738A (en) * | 1968-07-01 | 1970-07-15 | Sulzer Ag | Cylinder of a piston internal combustion engine |
| US3808955A (en) * | 1972-10-12 | 1974-05-07 | Yanmar Diesel Engine Co | Cylinders of internal-combustion engines |
| US4393821A (en) * | 1979-05-22 | 1983-07-19 | Nippon Piston Ring Co., Ltd. | Cylinder or cylinder liner |
| JPS61171963A (en) * | 1985-01-23 | 1986-08-02 | Mitsubishi Heavy Ind Ltd | Cylinder liner of reciprocating engine |
-
1999
- 1999-01-08 DE DE19900385A patent/DE19900385C2/en not_active Expired - Fee Related
- 1999-12-22 TW TW088122640A patent/TW463015B/en not_active IP Right Cessation
- 1999-12-22 WO PCT/EP1999/010266 patent/WO2000040849A1/en not_active Ceased
- 1999-12-22 GB GB0104423A patent/GB2361759B/en not_active Expired - Fee Related
- 1999-12-22 JP JP2000592532A patent/JP3419762B2/en not_active Expired - Lifetime
- 1999-12-22 KR KR10-2001-7005131A patent/KR100417185B1/en not_active Expired - Lifetime
- 1999-12-22 AU AU30420/00A patent/AU3042000A/en not_active Abandoned
- 1999-12-22 CN CN99812246A patent/CN1112510C/en not_active Expired - Lifetime
- 1999-12-22 PL PL99348869A patent/PL348869A1/en unknown
-
2001
- 2001-06-12 NO NO20012894A patent/NO20012894L/en not_active Application Discontinuation
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1900699A1 (en) * | 1968-01-09 | 1969-09-04 | Ramsey Corp | Piston cylinder, in particular cylinder lining sleeve for an internal combustion engine |
| CH493738A (en) * | 1968-07-01 | 1970-07-15 | Sulzer Ag | Cylinder of a piston internal combustion engine |
| US3808955A (en) * | 1972-10-12 | 1974-05-07 | Yanmar Diesel Engine Co | Cylinders of internal-combustion engines |
| US4393821A (en) * | 1979-05-22 | 1983-07-19 | Nippon Piston Ring Co., Ltd. | Cylinder or cylinder liner |
| JPS61171963A (en) * | 1985-01-23 | 1986-08-02 | Mitsubishi Heavy Ind Ltd | Cylinder liner of reciprocating engine |
Non-Patent Citations (1)
| Title |
|---|
| PATENT ABSTRACTS OF JAPAN vol. 010, no. 381 (M - 547) 19 December 1986 (1986-12-19) * |
Also Published As
| Publication number | Publication date |
|---|---|
| AU3042000A (en) | 2000-07-24 |
| DE19900385C2 (en) | 2001-02-01 |
| KR20010085951A (en) | 2001-09-07 |
| GB2361759A (en) | 2001-10-31 |
| CN1112510C (en) | 2003-06-25 |
| JP2002534634A (en) | 2002-10-15 |
| GB0104423D0 (en) | 2001-04-11 |
| NO20012894D0 (en) | 2001-06-12 |
| DE19900385A1 (en) | 2000-07-20 |
| TW463015B (en) | 2001-11-11 |
| CN1323375A (en) | 2001-11-21 |
| JP3419762B2 (en) | 2003-06-23 |
| KR100417185B1 (en) | 2004-02-05 |
| NO20012894L (en) | 2001-06-12 |
| PL348869A1 (en) | 2002-06-17 |
| GB2361759B (en) | 2002-07-10 |
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