EP2981650A1 - Wear component for compactor wheel - Google Patents

Wear component for compactor wheel

Info

Publication number
EP2981650A1
EP2981650A1 EP14780203.7A EP14780203A EP2981650A1 EP 2981650 A1 EP2981650 A1 EP 2981650A1 EP 14780203 A EP14780203 A EP 14780203A EP 2981650 A1 EP2981650 A1 EP 2981650A1
Authority
EP
European Patent Office
Prior art keywords
wear component
base
tip
tip portion
recesses
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP14780203.7A
Other languages
German (de)
French (fr)
Other versions
EP2981650A4 (en
EP2981650B1 (en
Inventor
Thomas John Yaniak
Thomas Majewski
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Caterpillar Inc
Original Assignee
Caterpillar Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Caterpillar Inc filed Critical Caterpillar Inc
Publication of EP2981650A1 publication Critical patent/EP2981650A1/en
Publication of EP2981650A4 publication Critical patent/EP2981650A4/en
Application granted granted Critical
Publication of EP2981650B1 publication Critical patent/EP2981650B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E02HYDRAULIC ENGINEERING; FOUNDATIONS; SOIL SHIFTING
    • E02DFOUNDATIONS; EXCAVATIONS; EMBANKMENTS; UNDERGROUND OR UNDERWATER STRUCTURES
    • E02D3/00Improving or preserving soil or rock, e.g. preserving permafrost soil
    • E02D3/02Improving by compacting
    • E02D3/026Improving by compacting by rolling with rollers usable only for or specially adapted for soil compaction, e.g. sheepsfoot rollers
    • EFIXED CONSTRUCTIONS
    • E02HYDRAULIC ENGINEERING; FOUNDATIONS; SOIL SHIFTING
    • E02DFOUNDATIONS; EXCAVATIONS; EMBANKMENTS; UNDERGROUND OR UNDERWATER STRUCTURES
    • E02D3/00Improving or preserving soil or rock, e.g. preserving permafrost soil
    • E02D3/02Improving by compacting
    • E02D3/026Improving by compacting by rolling with rollers usable only for or specially adapted for soil compaction, e.g. sheepsfoot rollers
    • E02D3/0265Wheels specially adapted therefor; Cleats for said wheels

Definitions

  • the present disclosure relates generally to wear components and, more particularly, to wear components for compactor wheels.
  • Compactors such as, for example, landfill compactors and soil compactors typically include steel wheels, which are fitted with teeth that extend radially outward from the wheels to engage and compact material over which the compactors are driven. Over time, the teeth wear down, and they eventually need to be replaced.
  • U.S. Patent No. 6,632,045 to McCartney (“the '045 patent”) discloses an exemplary tooth.
  • the tooth of the ⁇ 45 patent is a two-part tooth that is adapted to be welded to a steel wheel. It includes a base constructed from a weldable material, and a cap constructed of a harder metal than the metal used for the base.
  • the tooth is manufactured by casting the base in a first mold, moving the base to a second mold, and casting the cap onto the base in the second mold. When casting the cap, molten metal flows into mating formations of the base, ensuring that the cap is firmly keyed to the base when the molten metal solidifies.
  • the tooth of the ⁇ 45 patent may be appropriate for certain applications, it may not be well-suited for others.
  • the tooth of the ⁇ 45 patent may not be well-suited for applications in which its weight stresses drivetrain components of a compactor without meaningfully improving compaction. In such applications, the tooth might cause premature failure of the drivetrain components, thereby unnecessarily increasing maintenance costs associated with the compactor.
  • the various embodiments of the present disclosure are directed toward overcoming one or more deficiencies of the prior art.
  • a wear component in an exemplary embodiment of the present disclosure, includes a base portion and a tip portion.
  • the tip portion includes a proximate end and a distal end.
  • the proximate end is metallurgically bonded to the base portion at a base-tip interface, which has a generally parabolic cross- sectional profile.
  • the distal end defines an exterior surface of the wear component.
  • a wear component in another exemplary embodiment of the present disclosure, includes a base portion and a tip portion.
  • the tip portion includes a proximate end, a distal end, and an at least partially concave side surface extending from the distal end to the proximate end.
  • the proximate end is metallurgically bonded to the base portion at a base-tip interface.
  • the distal end defines an exterior surface of the wear component.
  • a wear component in yet another exemplary embodiment of the present disclosure, includes a base portion and a tip portion.
  • the base portion includes a plurality of protrusions.
  • the tip portion includes a proximate end and a distal end.
  • the proximate end includes a plurality of recesses, and is metallurgically bonded to the base portion at a base-tip interface, where the plurality of protrusions extends into the plurality of recesses.
  • the distal end defines an exterior surface of the wear component.
  • Fig. 1 is a pictorial illustration of an exemplary wheel for use with a compactor
  • Fig. 2 is a pictorial illustration of an exemplary wear component for use with the wheel of Fig. 1 ;
  • Fig. 3 is a magnified cross-sectional view of an exemplary interface between exemplary tip and base portions of the wear component of Fig. 2;
  • Fig. 4 is a cross-sectional view of an exemplary apparatus for casting the wear component of Figs. 2 and 3;
  • Fig. 5 is a cross-sectional view of the wear component of Figs 2-4 in an exemplary mold of the apparatus of Fig. 4;
  • Fig. 6 is a pictorial illustration of another exemplary tip portion
  • Fig. 7 is a cross-sectional view of the tip portion of Fig. 6 bonded to another exemplary base portion;
  • Figs. 8-13 are pictorial illustrations of yet further exemplary tip portions.
  • Figs. 14 and 15 are flow charts describing exemplary disclosed methods of casting articles of manufacture, such as the wear components of the other figures.
  • Fig. 1 illustrates a steel wheel 10 for use with a mobile machine, such as a landfill or soil compactor.
  • wear components 20 in the form of teeth are fitted to wheel 10, and extend radially outward from wheel 10 to engage and compact material over which wheel 10 is driven.
  • wear components 20 may be teeth that are fitted to another type of part (e.g., a bucket) or may be another type of wear component entirely (e.g., hammers on disk rotors of a scrap metal shredder).
  • each wear component 20 may include a tip portion 30 that extends radially outward from wheel 10 to engage and compact material over which steel wheel 10 is driven.
  • tip portion 30 may be connected to wheel 10 by a base portion 40 of its wear component 20, which may be welded to wheel 10.
  • Tip portion 30 may have a distal end 50 defining an exterior surface of its wear component 20. As shown in Fig. 1, distal end 50 may be generally I-shaped. It should be understood, however, that distal end 50 may be otherwise shaped. For example, distal end 50 may be generally +(plus)-shaped. Alternatively, distal end 50 may have another shape conducive to compacting material. Tip portion 30 may also include side surfaces 60 extending from distal end 50 to a proximate end 70 of tip portion 30. In certain embodiments, side surfaces 60 may be at least partially concave, enabling them to deflect material away from base portion 40 and thereby protect base portion 40 from wear. Alternatively, side surfaces 60 may have other shapes that are conducive to compacting material (e.g., shapes that are not at least partially concave).
  • tip portion 30 may be formed from a material with a hardness of at least 45 Rockwell C, making it highly resistant to abrasion resulting from compaction of material.
  • tip portion 30 may be formed from white iron (e.g., high-chromium white iron or Ni-Hard), carbidic iron, austempered iron, high-carbon steel, high-carbon alloy steel, tool steel, carbidic steel, or stainless steel.
  • base portion 40 may include a mounting end 75 for attaching wear component 20 to wheel 10, a distal end 77 opposite mounting end 75, and side surfaces 78 extending from mounting end 75 to distal end 77.
  • mounting end 75 is generally shaped to follow a contour of wheel 10, thereby facilitating the attachment of wear component 20 to wheel 10.
  • mounting end 75 may include a recess 80, which does not follow the contour of wheel 10.
  • Recess 80 may become a hollow cavity when wear component 20 is attached to wheel 10, thereby reducing the weight of wear component 20 relative to a similarly sized (but solid) wear component.
  • Base portion 40 may be formed from a material with a carbon- equivalent (CE) value of less than 0.7, ensuring that it can be welded to steel (e.g., steel wheel 10) using portable welding equipment in the field (as opposed to specialized welding procedures typically required to be performed in a maintenance facility).
  • base portion 40 may be formed from steel (e.g., carbon steel, alloy steel, or stainless steel).
  • Base portion 40 may be metallurgically bonded to tip portion 30, that is, portion 40 may be attached to portion 30 primarily by metallurgical bonding.
  • distal end 77 of base portion 40 may be metallurgically bonded to proximate end 70 of tip portion 30.
  • the interface between distal end 77 and proximate end 70 (“base-tip interface 100") may thus be composed solely of a mixture of the material of base portion 40 and the material of tip portion 30. That is, base-tip interface 100 may include no adhesive or filler metal, no oxide films, and no voids.
  • base-tip interface 100 (and thus distal end 77 and proximate end 70) may be non-planar, and may be related to the method by which wear component 20 is cast.
  • wear component 20 may be centrifugally cast using a dual-pour method in which molten first and second materials are poured through a funnel 120 into a rotating mold 1 10.
  • the molten first material may be poured first to form tip portion 30 while mold 110 is rotated at a first speed.
  • the second material may then be poured over the first material (now tip portion 30) to form base portion 40 while mold 110 is rotated at a second speed, which may or may not be the same as the first speed.
  • Both pours may take place while mold 1 10 is rotated about an axis 1 15 that is generally parallel to a direction of gravitational acceleration (i.e., a direction in which the materials fall as they are poured). Such rotation may cause the first material to creep up the sides of mold 1 10, thereby giving proximate end 70 of tip portion 30 (and thus also base-tip interface 100) a generally parabolic cross-sectional profile, as shown in Fig. 4. It should be noted that, below base- tip interface 100, tip portion 30 may have a solid (i.e., free of voids) cross-section that is perpendicular to axis 1 15, as shown in Fig. 5.
  • outer edge 125 may be non-circular, as shown in Fig. 5.
  • outer edge 125 may be generally I-shaped (as illustrated), generally +(plus)-shaped, or otherwise shaped.
  • tip portion 30 may be cast, forged, or machined from a first material before being positioned within mold 1 10.
  • a molten second material may then be poured into mold 1 10 over tip portion 30 to form base portion 40, while mold 1 10 is rotated about axis 1 15.
  • proximate end 70 of tip portion 30 may begin with almost any shape.
  • Proximate end 70 's shape may change slightly during molding as a result of the metallurgical bonding process, but it should be understood that the shape of base-tip interface 100 may at least generally track the beginning shape of proximate end 70. For example, as shown in Fig.
  • proximate end 70 may begin with a plurality of recesses 130 extending from a first side 140 of tip portion 30 to a second side 150 of tip portion 30.
  • Each recess 130 may be generally valley-shaped.
  • each recess 130 may be generally U-shaped, and may be wider than it is deep (as illustrated in Fig. 6).
  • proximate end 70 may begin with two recesses 130. Referring to Fig. 7, when the molten second material is poured into mold 1 10 over such recesses 130, the second material may slightly deform recesses 130 into recesses 130'. The second material may then solidify to form base portion 40 with a plurality of protrusions 160, each extending into a
  • protrusions 160 and recesses 130' may mechanically enhance the bond of base portion 40 to tip portion 30.
  • proximate end 70 may begin with recesses 130 that are deeper than they are wide.
  • proximate end 70 may begin with recesses 130 that are generally U-shaped (as illustrated in Fig. 6)
  • proximate end 70 may begin with recesses 130 that are generally V-shaped.
  • proximate end 70 may begin with recesses 230 that are generally box- shaped.
  • proximate end 70 may begin with a single recess 330, as shown in Fig. 9.
  • proximate end 70 may begin with a plurality of recesses 430 in the form of rabbets (i.e., step-shaped recesses) in outer edges 435 of tip portion 30. While Fig. 10 illustrates recesses 430 as extending only from first side 140 to second side 150, recesses 430 may also extend from a third side 440 of tip portion 30 to a fourth side 450 of tip portion 30, as shown in Fig. 1 1.
  • proximate end 70 may begin with one or more recesses 530 in the form of bathtub-shaped depressions. While such recesses 530 could be the only recesses in proximate end 70, proximate end 70 could also include one or more of the recesses discussed above. For example, as shown in Fig. 13, proximate end 70 may include two recesses 530 and four recesses 430. In fact, it should be understood that proximate end 70 may include any combination of any number of recesses 130, 230, 330, 430, 530, and/or any other similarly shaped recesses.
  • Figs. 14 and 15 are flow diagrams describing exemplary methods of casting articles of manufacture such as wear components 20, and they will be discussed in the following section.
  • the disclosed wear components may be fitted to steel components and may be particularly beneficial when fitted to steel wheels of landfill or soil compactors.
  • the wear components may be cast such that they facilitate in-field (as opposed to in-maintenance facility) maintenance of the compactors and also minimize the amount of maintenance the compactors require. Exemplary methods of casting articles of manufacture, such as the disclosed wear components, will now be described.
  • wear component 20 may be centrifugally cast using a dual-pour method in which molten first and second materials are poured into mold 1 10 while mold 1 10 is rotated about axis 1 15 (referring to Fig. 4) (step 1400).
  • a molten first material may be poured through funnel 120 into mold 1 10 to form tip portion 30 while mold 110 is rotated at a first speed (step 1410).
  • the first material may have a hardness of at least 45 Rockwell C, making tip portion 30 highly resistant to abrasion resulting from compaction of material and thereby reducing the number of times wear component must be replaced.
  • the first material may be white iron (e.g., high-chromium white iron or Ni-Hard), carbidic iron, austempered iron, high-carbon steel, high-carbon alloy steel, tool steel, carbidic steel, or stainless steel.
  • funnel 120 may be positioned such that the first material is poured at a fixed location relative to axis 1 15 (e.g., along axis 115), funnel 120 may alternatively be moved during the pouring such that the first material is poured at a plurality of different locations relative to axis 1 15.
  • the rotation of mold 1 10 may cause the first material to creep up the sides of mold 1 10, thereby giving proximate end 70 of tip portion 30 (and thus also base-tip interface 100) a generally parabolic cross-sectional profile, as shown in Fig. 4.
  • Such a profile may enable the first material to protect a large portion of the exterior surface of wear component 20 without occupying a correspondingly large portion of the volume of wear component 20, thereby minimizing the amount of the first material (which may be more costly than the second material) required to form wear component 20.
  • the first material may be allowed to cool (step 1420).
  • a molten second material may then be poured through funnel 120, into mold 1 10, over the first material (now tip portion 30) to form base portion 40 while mold 1 10 is rotated at a second speed, which may or may not be the same as the first speed (step 1430).
  • the second material may have a carbon-equivalent (CE) value of less than 0.7, ensuring that base portion 40 can be welded to steel (e.g., steel wheel 10) using portable welding equipment in the field (as opposed to specialized welding procedures typically required to be performed in a maintenance facility).
  • the second material may be carbon steel, alloy steel, or stainless steel.
  • funnel 120 may be positioned such that the second material is poured at a fixed location relative to axis 1 15 (e.g., along axis 115), funnel 120 may alternatively be moved such that the second material is poured at a plurality of different locations relative to axis 1 15.
  • the rotation of mold 1 10 may cause the second material to move radially outward along a surface of the first material when the second material impacts the first material, displacing any foreign materials (e.g., oxide films) on the surface of the first material.
  • the second material may then metallurgically bond base portion 40 to tip portion 30.
  • the rotation of mold 1 10 may also cause the second material to creep up the sides of mold 1 10, facilitating the formation of recess 80 in mounting end 75 of base portion 40.
  • This recess 80 may, in turn, become a hollow cavity when wear component 20 is attached to wheel 10, thereby reducing the weight of wear component 20 relative to a similarly sized (but solid) wear component.
  • Such weight reduction may minimize stresses on drivetrain components of compactors using wear components 20, thereby extending the life of the drivetrain components and reducing maintenance costs associated with the drivetrain components. Additionally, the weight reduction may minimize the amount of fuel required to operate the compactors, thereby reducing operating costs associated with the compactors.
  • wear component 20 may be centrifugally cast using a tip portion 30 that is cast, forged, or machined from the first material before being positioned within mold 1 10 (step 1500).
  • tip portion 30 may be positioned with its proximate end 70 facing upward such that any material poured over tip portion 30 is poured over proximate end 70.
  • the molten second material may be poured into mold 1 10 over tip portion 30 to form base portion 40 (step 1520).
  • funnel 120 may be positioned such that the second material is poured at a fixed location relative to axis 1 15 (e.g., along axis 115), funnel 120 may alternatively be moved such that the second material is poured at a plurality of different locations relative to axis 1 15.
  • the rotation of mold 1 10 may cause the second material to move radially outward along proximate end 70 when the second material impacts the first material, displacing any foreign materials (e.g., oxide films) on proximate end 70.
  • the movement may be at least partially guided by recesses 130, 230, 330, 430, and/or 530 of proximate end 70, potentially speeding up and/or slowing down the movement, and thereby maximizing the displacement of foreign materials.
  • the second material may then metallurgically bond base portion 40 to tip portion 30.
  • the rotation of mold 1 10 may also cause the second material to creep up the sides of mold 1 10, facilitating the formation of recess 80 in the same way as discussed above with respect to the dual-pour method.

Landscapes

  • Engineering & Computer Science (AREA)
  • Structural Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Civil Engineering (AREA)
  • Environmental & Geological Engineering (AREA)
  • Soil Sciences (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Mining & Mineral Resources (AREA)
  • Paleontology (AREA)
  • Agronomy & Crop Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Heat Treatment Of Articles (AREA)
  • Architecture (AREA)

Abstract

A wear component includes a base portion and a tip portion. The tip portion includes a proximate end and a distal end. The proximate end is metallurgically bonded to the base portion at a base-tip interface, which may have a generally parabolic cross-sectional profile. The distal end defines an exterior surface of the wear component.

Description

Description
WEAR COMPONENT FOR COMPACTOR WHEEL
Cross-Reference to Related Application
This application claims the benefit of U.S. Provisional Patent Application No. 61/809,018, filed April 5, 2013, which is hereby incorporated by reference in its entirety.
Technical Field
The present disclosure relates generally to wear components and, more particularly, to wear components for compactor wheels. Background
Compactors such as, for example, landfill compactors and soil compactors typically include steel wheels, which are fitted with teeth that extend radially outward from the wheels to engage and compact material over which the compactors are driven. Over time, the teeth wear down, and they eventually need to be replaced.
U.S. Patent No. 6,632,045 to McCartney ("the '045 patent") discloses an exemplary tooth. The tooth of the Ό45 patent is a two-part tooth that is adapted to be welded to a steel wheel. It includes a base constructed from a weldable material, and a cap constructed of a harder metal than the metal used for the base. According to the Ό45 patent, the tooth is manufactured by casting the base in a first mold, moving the base to a second mold, and casting the cap onto the base in the second mold. When casting the cap, molten metal flows into mating formations of the base, ensuring that the cap is firmly keyed to the base when the molten metal solidifies.
While the tooth of the Ό45 patent may be appropriate for certain applications, it may not be well-suited for others. For example, the tooth of the Ό45 patent may not be well-suited for applications in which its weight stresses drivetrain components of a compactor without meaningfully improving compaction. In such applications, the tooth might cause premature failure of the drivetrain components, thereby unnecessarily increasing maintenance costs associated with the compactor. The various embodiments of the present disclosure are directed toward overcoming one or more deficiencies of the prior art.
Summary
In an exemplary embodiment of the present disclosure, a wear component includes a base portion and a tip portion. The tip portion includes a proximate end and a distal end. The proximate end is metallurgically bonded to the base portion at a base-tip interface, which has a generally parabolic cross- sectional profile. The distal end defines an exterior surface of the wear component.
In another exemplary embodiment of the present disclosure, a wear component includes a base portion and a tip portion. The tip portion includes a proximate end, a distal end, and an at least partially concave side surface extending from the distal end to the proximate end. The proximate end is metallurgically bonded to the base portion at a base-tip interface. The distal end defines an exterior surface of the wear component.
In yet another exemplary embodiment of the present disclosure, a wear component includes a base portion and a tip portion. The base portion includes a plurality of protrusions. The tip portion includes a proximate end and a distal end. The proximate end includes a plurality of recesses, and is metallurgically bonded to the base portion at a base-tip interface, where the plurality of protrusions extends into the plurality of recesses. The distal end defines an exterior surface of the wear component.
Brief Description of the Drawings
Fig. 1 is a pictorial illustration of an exemplary wheel for use with a compactor;
Fig. 2 is a pictorial illustration of an exemplary wear component for use with the wheel of Fig. 1 ;
Fig. 3 is a magnified cross-sectional view of an exemplary interface between exemplary tip and base portions of the wear component of Fig. 2;
Fig. 4 is a cross-sectional view of an exemplary apparatus for casting the wear component of Figs. 2 and 3; Fig. 5 is a cross-sectional view of the wear component of Figs 2-4 in an exemplary mold of the apparatus of Fig. 4;
Fig. 6 is a pictorial illustration of another exemplary tip portion;
Fig. 7 is a cross-sectional view of the tip portion of Fig. 6 bonded to another exemplary base portion;
Figs. 8-13 are pictorial illustrations of yet further exemplary tip portions; and
Figs. 14 and 15 are flow charts describing exemplary disclosed methods of casting articles of manufacture, such as the wear components of the other figures.
Detailed Description
Fig. 1 illustrates a steel wheel 10 for use with a mobile machine, such as a landfill or soil compactor. As shown, wear components 20 in the form of teeth are fitted to wheel 10, and extend radially outward from wheel 10 to engage and compact material over which wheel 10 is driven. It should be understood, however, that wear components 20 may be teeth that are fitted to another type of part (e.g., a bucket) or may be another type of wear component entirely (e.g., hammers on disk rotors of a scrap metal shredder). In any case, in certain embodiments (e.g., the embodiment of Fig. 1), each wear component 20 may include a tip portion 30 that extends radially outward from wheel 10 to engage and compact material over which steel wheel 10 is driven. In these embodiments, tip portion 30 may be connected to wheel 10 by a base portion 40 of its wear component 20, which may be welded to wheel 10.
Tip portion 30 may have a distal end 50 defining an exterior surface of its wear component 20. As shown in Fig. 1, distal end 50 may be generally I-shaped. It should be understood, however, that distal end 50 may be otherwise shaped. For example, distal end 50 may be generally +(plus)-shaped. Alternatively, distal end 50 may have another shape conducive to compacting material. Tip portion 30 may also include side surfaces 60 extending from distal end 50 to a proximate end 70 of tip portion 30. In certain embodiments, side surfaces 60 may be at least partially concave, enabling them to deflect material away from base portion 40 and thereby protect base portion 40 from wear. Alternatively, side surfaces 60 may have other shapes that are conducive to compacting material (e.g., shapes that are not at least partially concave).
Regardless of tip portion 30's shape, tip portion 30 may be formed from a material with a hardness of at least 45 Rockwell C, making it highly resistant to abrasion resulting from compaction of material. For example, tip portion 30 may be formed from white iron (e.g., high-chromium white iron or Ni-Hard), carbidic iron, austempered iron, high-carbon steel, high-carbon alloy steel, tool steel, carbidic steel, or stainless steel.
Referring to Fig. 2, base portion 40 may include a mounting end 75 for attaching wear component 20 to wheel 10, a distal end 77 opposite mounting end 75, and side surfaces 78 extending from mounting end 75 to distal end 77. As shown, mounting end 75 is generally shaped to follow a contour of wheel 10, thereby facilitating the attachment of wear component 20 to wheel 10. Notably, however, mounting end 75 may include a recess 80, which does not follow the contour of wheel 10. Recess 80 may become a hollow cavity when wear component 20 is attached to wheel 10, thereby reducing the weight of wear component 20 relative to a similarly sized (but solid) wear component. Base portion 40 may be formed from a material with a carbon- equivalent (CE) value of less than 0.7, ensuring that it can be welded to steel (e.g., steel wheel 10) using portable welding equipment in the field (as opposed to specialized welding procedures typically required to be performed in a maintenance facility). For example, base portion 40 may be formed from steel (e.g., carbon steel, alloy steel, or stainless steel).
Base portion 40 may be metallurgically bonded to tip portion 30, that is, portion 40 may be attached to portion 30 primarily by metallurgical bonding. In particular, distal end 77 of base portion 40 may be metallurgically bonded to proximate end 70 of tip portion 30. As shown in Fig. 3, the interface between distal end 77 and proximate end 70 ("base-tip interface 100") may thus be composed solely of a mixture of the material of base portion 40 and the material of tip portion 30. That is, base-tip interface 100 may include no adhesive or filler metal, no oxide films, and no voids.
The shape of base-tip interface 100 (and thus distal end 77 and proximate end 70) may be non-planar, and may be related to the method by which wear component 20 is cast. For example, referring to Fig. 4, wear component 20 may be centrifugally cast using a dual-pour method in which molten first and second materials are poured through a funnel 120 into a rotating mold 1 10. The molten first material may be poured first to form tip portion 30 while mold 110 is rotated at a first speed. After allowing the first material to cool, the second material may then be poured over the first material (now tip portion 30) to form base portion 40 while mold 110 is rotated at a second speed, which may or may not be the same as the first speed. Both pours may take place while mold 1 10 is rotated about an axis 1 15 that is generally parallel to a direction of gravitational acceleration (i.e., a direction in which the materials fall as they are poured). Such rotation may cause the first material to creep up the sides of mold 1 10, thereby giving proximate end 70 of tip portion 30 (and thus also base-tip interface 100) a generally parabolic cross-sectional profile, as shown in Fig. 4. It should be noted that, below base- tip interface 100, tip portion 30 may have a solid (i.e., free of voids) cross-section that is perpendicular to axis 1 15, as shown in Fig. 5. Further, it should be understood that the shape of the outer edge 125 of any cross-section of tip portion 30 that is perpendicular to axis 1 15 will be defined by the shape of mold 1 10. Thus, outer edge 125 may be non-circular, as shown in Fig. 5. For example, outer edge 125 may be generally I-shaped (as illustrated), generally +(plus)-shaped, or otherwise shaped.
In another method of centrifugally casting wear component 20, tip portion 30 may be cast, forged, or machined from a first material before being positioned within mold 1 10. A molten second material may then be poured into mold 1 10 over tip portion 30 to form base portion 40, while mold 1 10 is rotated about axis 1 15. With this second method, proximate end 70 of tip portion 30 may begin with almost any shape. Proximate end 70 's shape may change slightly during molding as a result of the metallurgical bonding process, but it should be understood that the shape of base-tip interface 100 may at least generally track the beginning shape of proximate end 70. For example, as shown in Fig. 6, proximate end 70 may begin with a plurality of recesses 130 extending from a first side 140 of tip portion 30 to a second side 150 of tip portion 30. Each recess 130 may be generally valley-shaped. For example, each recess 130 may be generally U-shaped, and may be wider than it is deep (as illustrated in Fig. 6). In certain embodiments, proximate end 70 may begin with two recesses 130. Referring to Fig. 7, when the molten second material is poured into mold 1 10 over such recesses 130, the second material may slightly deform recesses 130 into recesses 130'. The second material may then solidify to form base portion 40 with a plurality of protrusions 160, each extending into a
corresponding one of recesses 130' at base-tip interface 100. It should be noted that, in some embodiments, protrusions 160 and recesses 130' may mechanically enhance the bond of base portion 40 to tip portion 30.
The number, shape, and placement of any protrusions 160 extending into proximate end 70 of tip portion 30 at base-tip interface 100 may be affected by the beginning shape of proximate end 70. For example, rather than beginning with recesses 130 that are wider than they are deep (as illustrated in Fig. 6), proximate end 70 may begin with recesses 130 that are deeper than they are wide. As another example, rather than beginning with recesses 130 that are generally U-shaped (as illustrated in Fig. 6), proximate end 70 may begin with recesses 130 that are generally V-shaped. Alternatively, as illustrated in Fig. 8, proximate end 70 may begin with recesses 230 that are generally box- shaped. In yet another alternative embodiment, rather than beginning with a plurality of recesses 130 or 230 (as illustrated in Figs. 6 and 8), proximate end 70 may begin with a single recess 330, as shown in Fig. 9.
Alternatively, as illustrated in Fig. 10, proximate end 70 may begin with a plurality of recesses 430 in the form of rabbets (i.e., step-shaped recesses) in outer edges 435 of tip portion 30. While Fig. 10 illustrates recesses 430 as extending only from first side 140 to second side 150, recesses 430 may also extend from a third side 440 of tip portion 30 to a fourth side 450 of tip portion 30, as shown in Fig. 1 1.
In yet another alternative embodiment, as shown in Figs. 12 and 13, proximate end 70 may begin with one or more recesses 530 in the form of bathtub-shaped depressions. While such recesses 530 could be the only recesses in proximate end 70, proximate end 70 could also include one or more of the recesses discussed above. For example, as shown in Fig. 13, proximate end 70 may include two recesses 530 and four recesses 430. In fact, it should be understood that proximate end 70 may include any combination of any number of recesses 130, 230, 330, 430, 530, and/or any other similarly shaped recesses.
Figs. 14 and 15 are flow diagrams describing exemplary methods of casting articles of manufacture such as wear components 20, and they will be discussed in the following section. Industrial Applicability
The disclosed wear components may be fitted to steel components and may be particularly beneficial when fitted to steel wheels of landfill or soil compactors. The wear components may be cast such that they facilitate in-field (as opposed to in-maintenance facility) maintenance of the compactors and also minimize the amount of maintenance the compactors require. Exemplary methods of casting articles of manufacture, such as the disclosed wear components, will now be described.
Referring to Fig. 14, wear component 20 may be centrifugally cast using a dual-pour method in which molten first and second materials are poured into mold 1 10 while mold 1 10 is rotated about axis 1 15 (referring to Fig. 4) (step 1400). First, a molten first material may be poured through funnel 120 into mold 1 10 to form tip portion 30 while mold 110 is rotated at a first speed (step 1410). The first material may have a hardness of at least 45 Rockwell C, making tip portion 30 highly resistant to abrasion resulting from compaction of material and thereby reducing the number of times wear component must be replaced. For example, as discussed above, the first material may be white iron (e.g., high-chromium white iron or Ni-Hard), carbidic iron, austempered iron, high-carbon steel, high-carbon alloy steel, tool steel, carbidic steel, or stainless steel. While funnel 120 may be positioned such that the first material is poured at a fixed location relative to axis 1 15 (e.g., along axis 115), funnel 120 may alternatively be moved during the pouring such that the first material is poured at a plurality of different locations relative to axis 1 15. In any case, the rotation of mold 1 10 may cause the first material to creep up the sides of mold 1 10, thereby giving proximate end 70 of tip portion 30 (and thus also base-tip interface 100) a generally parabolic cross-sectional profile, as shown in Fig. 4. Such a profile may enable the first material to protect a large portion of the exterior surface of wear component 20 without occupying a correspondingly large portion of the volume of wear component 20, thereby minimizing the amount of the first material (which may be more costly than the second material) required to form wear component 20.
Next, the first material may be allowed to cool (step 1420). A molten second material may then be poured through funnel 120, into mold 1 10, over the first material (now tip portion 30) to form base portion 40 while mold 1 10 is rotated at a second speed, which may or may not be the same as the first speed (step 1430). The second material may have a carbon-equivalent (CE) value of less than 0.7, ensuring that base portion 40 can be welded to steel (e.g., steel wheel 10) using portable welding equipment in the field (as opposed to specialized welding procedures typically required to be performed in a maintenance facility). For example, as discussed above, the second material may be carbon steel, alloy steel, or stainless steel. While funnel 120 may be positioned such that the second material is poured at a fixed location relative to axis 1 15 (e.g., along axis 115), funnel 120 may alternatively be moved such that the second material is poured at a plurality of different locations relative to axis 1 15. Notably, the rotation of mold 1 10 may cause the second material to move radially outward along a surface of the first material when the second material impacts the first material, displacing any foreign materials (e.g., oxide films) on the surface of the first material. The second material may then metallurgically bond base portion 40 to tip portion 30. The rotation of mold 1 10 may also cause the second material to creep up the sides of mold 1 10, facilitating the formation of recess 80 in mounting end 75 of base portion 40. This recess 80 may, in turn, become a hollow cavity when wear component 20 is attached to wheel 10, thereby reducing the weight of wear component 20 relative to a similarly sized (but solid) wear component. Such weight reduction may minimize stresses on drivetrain components of compactors using wear components 20, thereby extending the life of the drivetrain components and reducing maintenance costs associated with the drivetrain components. Additionally, the weight reduction may minimize the amount of fuel required to operate the compactors, thereby reducing operating costs associated with the compactors.
In alternative embodiments and referring to Fig. 15, wear component 20 may be centrifugally cast using a tip portion 30 that is cast, forged, or machined from the first material before being positioned within mold 1 10 (step 1500). In particular, tip portion 30 may be positioned with its proximate end 70 facing upward such that any material poured over tip portion 30 is poured over proximate end 70. Then, while rotating mold 110 about axis 1 15 (step 1510), the molten second material may be poured into mold 1 10 over tip portion 30 to form base portion 40 (step 1520). Although funnel 120 may be positioned such that the second material is poured at a fixed location relative to axis 1 15 (e.g., along axis 115), funnel 120 may alternatively be moved such that the second material is poured at a plurality of different locations relative to axis 1 15. Notably, the rotation of mold 1 10 may cause the second material to move radially outward along proximate end 70 when the second material impacts the first material, displacing any foreign materials (e.g., oxide films) on proximate end 70. In some embodiments, the movement may be at least partially guided by recesses 130, 230, 330, 430, and/or 530 of proximate end 70, potentially speeding up and/or slowing down the movement, and thereby maximizing the displacement of foreign materials. The second material may then metallurgically bond base portion 40 to tip portion 30. The rotation of mold 1 10 may also cause the second material to creep up the sides of mold 1 10, facilitating the formation of recess 80 in the same way as discussed above with respect to the dual-pour method.
It will be apparent to those skilled in the art that various modifications and variations can be made in the disclosed wear components without departing from the scope of the disclosure. Other embodiments of the disclosed components will be apparent to those skilled in the art from consideration of the specification and practice of the components disclosed herein. It is intended that the specification and examples be considered as exemplary only, with a true scope of the disclosure being indicated by the following claims and their equivalents.

Claims

Claims
1. A wear component (20), comprising:
a base portion (40); and
a tip portion (30) including:
a proximate end (70) metallurgically bonded to the base portion (40) at a base-tip interface (100); and
a distal end (50) defining an exterior surface of the wear component (20),
wherein the base-tip interface (100) has a generally parabolic cross-sectional profile.
2. The wear component (20) of claim 1, wherein:
the base portion (40) includes a side surface extending from the base-tip interface (100) to a mounting end (75) of the base portion (40); and the mounting end (75) includes a recess (130).
3. The wear component (20) of claim 1, wherein the tip portion (30) includes an at least partially concave side surface extending from the distal end (50) to the proximate end (70).
4. The wear component (20) of claim 1, wherein:
the base portion (40) is formed from a first material with a carbon-equivalent (CE) value of less than 0.7; and
the tip portion (30) is formed from a second material with a hardness of at least 45 Rockwell C.
5. The wear component (20) of claim 4, wherein:
the first material is steel; and
the second material is steel or iron.
6. The wear component (20) of claim 5, wherein:
the first material is carbon steel, alloy steel, or stainless steel; and the second material is high-chromium white iron or Ni-Hard.
7. The wear component (20) of any of claims 1-6, wherein: the base portion (40) includes a plurality of protrusions (160); and the tip portion (30) includes a plurality of recesses (130);
wherein, at the base-tip interface (100), the plurality of protrusions (160) extend into the plurality of recesses (130).
8. The wear component (20) of claim 7, wherein the plurality of recesses (130) extend from a first side of the tip portion (30) to a second side of the tip portion (30) opposite the first side.
9. The wear component (20) of claim 8, wherein each of the plurality of recesses (130) is a rabbet in an outer edge (125) of the tip portion (30).
10. The wear component (20) of claim 7, wherein the proximate end (70) includes two recesses (130).
1 1. The wear component (20) of claim 7, wherein:
the base portion (40) includes a side surface extending from the base-tip interface (100) to a mounting end (75) of the base portion (40); and the mounting end (75) includes a recess (130).
EP14780203.7A 2013-04-05 2014-04-03 Wear component for compactor wheel Active EP2981650B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201361809018P 2013-04-05 2013-04-05
US14/243,379 US20140301786A1 (en) 2013-04-05 2014-04-02 Wear component for compactor wheel
PCT/US2014/032854 WO2014165689A1 (en) 2013-04-05 2014-04-03 Wear component for compactor wheel

Publications (3)

Publication Number Publication Date
EP2981650A1 true EP2981650A1 (en) 2016-02-10
EP2981650A4 EP2981650A4 (en) 2016-11-16
EP2981650B1 EP2981650B1 (en) 2017-11-22

Family

ID=51654563

Family Applications (1)

Application Number Title Priority Date Filing Date
EP14780203.7A Active EP2981650B1 (en) 2013-04-05 2014-04-03 Wear component for compactor wheel

Country Status (5)

Country Link
US (1) US20140301786A1 (en)
EP (1) EP2981650B1 (en)
CN (1) CN105229234A (en)
CA (1) CA2908359C (en)
WO (1) WO2014165689A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2565073B (en) * 2017-07-31 2021-10-13 Bernard Mccartney Ltd Compactor tooth, base therefor and related method

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4784922A (en) * 1985-10-11 1988-11-15 Mitsubishi Steel Mfg. Co., Ltd. Corrosion-resistant clad steel and method for producing the same
AU706813B2 (en) * 1995-03-15 1999-06-24 Caron Compactor Company Improved transfer station wheels
US6712551B2 (en) * 2001-11-27 2004-03-30 Caterpillar Inc Compactor tooth
CN2769323Y (en) * 2004-09-15 2006-04-05 徐州工程机械科技股份有限公司徐工研究院 Surface tread type compacting roller
CN101134232B (en) * 2006-08-28 2011-01-19 赤峰市恒泰特种钢铸造有限责任公司 Technique for producing anticentripetal composite abrasion-proof hammer tools
US20090045669A1 (en) * 2007-08-17 2009-02-19 Caterpillar Inc. Two-Piece Compactor Wheel Tip
EP2344681B1 (en) * 2008-09-19 2017-08-30 Acme United Corporation Coatings for cutting implements
CN201366806Y (en) * 2008-12-05 2009-12-23 山推工程机械股份有限公司 Wear resistant lug of compactor
US7959375B2 (en) * 2009-11-04 2011-06-14 Terra Compactor Wheel Corp. Horizontal scissor-tip compaction wheel cleat
US20120213586A1 (en) * 2011-02-23 2012-08-23 Caterpillar, Inc. Wrapper Tip Assembly For Compactor Wheel Assembly
US8696239B2 (en) * 2011-08-24 2014-04-15 Terra Compactor Wheel Corp. Full metal jacket compaction wheel cleat and method of manufacturing thereof
US20130075456A1 (en) * 2011-09-23 2013-03-28 Michael Hans Hinrichsen Compactor wheel assembly

Also Published As

Publication number Publication date
US20140301786A1 (en) 2014-10-09
EP2981650A4 (en) 2016-11-16
EP2981650B1 (en) 2017-11-22
WO2014165689A1 (en) 2014-10-09
CA2908359C (en) 2021-08-10
CA2908359A1 (en) 2014-10-09
CN105229234A (en) 2016-01-06

Similar Documents

Publication Publication Date Title
US9522425B2 (en) Method of casting
US9027266B2 (en) Wear resistant component
CN103785817B (en) A kind of production method of biliquid metal composite casting teeth
KR101250165B1 (en) Tip for a bucket of an excavator and method for manufacturing the same
EP2981650B1 (en) Wear component for compactor wheel
CN104907134A (en) Wear-resisting crusher hammer head with adjustable installation site and manufacture method thereof
CN113198982B (en) Casting method of flywheel casting
CN102281965A (en) Method of manufacturing sprocket segment, and sprocket segment
CN202343917U (en) A casting device for a double liquid bimetallic vertical parting hammer
CN206392163U (en) Screw-thread steel and rich chromium cast iron composite plate hammer
CN104801366B (en) The breaking wall of spindle breaker and method be made of Mn13 and rich chromium cast iron
CN214780253U (en) Isolated foundation hoisting tool
CN203835794U (en) Steel-making ID converter gas fan rotor set
CN223701192U (en) A flip-type shield tunnel segment mold
CN207187870U (en) Full metallurgical binding composite grinding roll
KR100402015B1 (en) Method for mounting hi-mn casting on the elbow of dust collecting duct
KR100475631B1 (en) Braker chisel with improved were-resistance and crushing-ability, manufacturing apparatus and method, and high-manganese steel thereof
CN222206561U (en) Anti-fracture guide wheel of bulldozer
CN113857431B (en) A method for preparing steel-rubber composite wear-resistant parts with a three-dimensional interpenetrating network structure
CN201579085U (en) Toothed plate of crusher
CN203695162U (en) Dual-use aggregate crusher
CN106552904A (en) A kind of sand shooting mouth for improving precoated sand mo ld void
CN211412199U (en) Hammer head structure of construction waste crusher
JPH0754381A (en) Composite material tooth and manufacturing method thereof
CN202862400U (en) Double-metal drum raceway of concrete mixer truck

Legal Events

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

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20150928

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAX Request for extension of the european patent (deleted)
A4 Supplementary search report drawn up and despatched

Effective date: 20161018

RIC1 Information provided on ipc code assigned before grant

Ipc: E01C 19/26 20060101AFI20161012BHEP

Ipc: E02D 3/026 20060101ALI20161012BHEP

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20170519

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 948515

Country of ref document: AT

Kind code of ref document: T

Effective date: 20171215

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602014017657

Country of ref document: DE

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 5

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20171122

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 948515

Country of ref document: AT

Kind code of ref document: T

Effective date: 20171122

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

Ref country code: LT

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

Effective date: 20171122

Ref country code: NL

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

Effective date: 20171122

Ref country code: NO

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

Effective date: 20180222

Ref country code: ES

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

Effective date: 20171122

Ref country code: SE

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

Effective date: 20171122

Ref country code: FI

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

Effective date: 20171122

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

Ref country code: RS

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

Effective date: 20171122

Ref country code: AT

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

Effective date: 20171122

Ref country code: LV

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

Effective date: 20171122

Ref country code: BG

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

Effective date: 20180222

Ref country code: GR

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

Effective date: 20180223

Ref country code: HR

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

Effective date: 20171122

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

Ref country code: CZ

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

Effective date: 20171122

Ref country code: SK

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

Effective date: 20171122

Ref country code: EE

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

Effective date: 20171122

Ref country code: CY

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

Effective date: 20171122

Ref country code: DK

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

Effective date: 20171122

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602014017657

Country of ref document: DE

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

Ref country code: PL

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

Effective date: 20171122

Ref country code: RO

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

Effective date: 20171122

Ref country code: IT

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

Effective date: 20171122

Ref country code: SM

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

Effective date: 20171122

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

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

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

26N No opposition filed

Effective date: 20180823

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

Ref country code: SI

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

Effective date: 20171122

Ref country code: MC

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

Effective date: 20171122

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20180430

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

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

Ref country code: LU

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

Effective date: 20180403

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

Ref country code: CH

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

Effective date: 20180430

Ref country code: LI

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

Effective date: 20180430

Ref country code: BE

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

Effective date: 20180430

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

Ref country code: IE

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

Effective date: 20180403

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

Ref country code: MT

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

Effective date: 20180403

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

Ref country code: TR

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

Effective date: 20171122

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

Ref country code: PT

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

Effective date: 20171122

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

Ref country code: MK

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

Effective date: 20171122

Ref country code: HU

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

Effective date: 20140403

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

Ref country code: AL

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

Effective date: 20171122

Ref country code: IS

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

Effective date: 20180322

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230517

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

Ref country code: DE

Payment date: 20250319

Year of fee payment: 12

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

Ref country code: GB

Payment date: 20260319

Year of fee payment: 13

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

Ref country code: FR

Payment date: 20260319

Year of fee payment: 13