EP2811041B1 - Aluminum alloy having excellent wear resistance, extrudability, and forging workability - Google Patents
Aluminum alloy having excellent wear resistance, extrudability, and forging workability Download PDFInfo
- Publication number
- EP2811041B1 EP2811041B1 EP12867174.0A EP12867174A EP2811041B1 EP 2811041 B1 EP2811041 B1 EP 2811041B1 EP 12867174 A EP12867174 A EP 12867174A EP 2811041 B1 EP2811041 B1 EP 2811041B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- extrusion
- aluminum alloy
- eutectic
- size
- abrasion resistance
- 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.)
- Active
Links
- 229910000838 Al alloy Inorganic materials 0.000 title claims description 31
- 238000005242 forging Methods 0.000 title claims description 8
- 238000001125 extrusion Methods 0.000 claims description 76
- 238000005299 abrasion Methods 0.000 claims description 34
- 230000005496 eutectics Effects 0.000 claims description 31
- 239000011856 silicon-based particle Substances 0.000 claims description 10
- 235000012438 extruded product Nutrition 0.000 claims description 6
- 239000012535 impurity Substances 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 2
- 229910052748 manganese Inorganic materials 0.000 claims description 2
- 229910052782 aluminium Inorganic materials 0.000 claims 1
- 239000000463 material Substances 0.000 description 75
- 238000012360 testing method Methods 0.000 description 15
- 230000000694 effects Effects 0.000 description 14
- 238000012545 processing Methods 0.000 description 14
- 239000000203 mixture Substances 0.000 description 13
- 238000009721 upset forging Methods 0.000 description 13
- 230000000052 comparative effect Effects 0.000 description 9
- 238000007670 refining Methods 0.000 description 6
- 229910052802 copper Inorganic materials 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 229910052710 silicon Inorganic materials 0.000 description 5
- 230000007423 decrease Effects 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 230000003287 optical effect Effects 0.000 description 4
- 238000011282 treatment Methods 0.000 description 4
- 230000000007 visual effect Effects 0.000 description 4
- 239000000654 additive Substances 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 229910018125 Al-Si Inorganic materials 0.000 description 2
- 229910018520 Al—Si Inorganic materials 0.000 description 2
- 229910019752 Mg2Si Inorganic materials 0.000 description 2
- 230000000996 additive effect Effects 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 230000032683 aging Effects 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 239000000498 cooling water Substances 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 239000012208 gear oil Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/002—Extruding materials of special alloys so far as the composition of the alloy requires or permits special extruding methods of sequences
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J1/00—Preparing metal stock or similar ancillary operations prior, during or post forging, e.g. heating or cooling
- B21J1/003—Selecting material
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
- C22C21/04—Modified aluminium-silicon alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/043—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with silicon as the next major constituent
Definitions
- the present invention relates to aluminum alloy with superior abrasion resistance, extrusion property and forge processing property, such aluminum alloy being used for parts such as compressors in automobiles and home electric appliances.
- Patent Literature 1 discloses an aluminum alloy for sliding use with superior fatigue resistance and seizure resistance. In order to obtain such fatigue resistance and seizure resistance, Si is added to the aluminum alloy as an essential element by 1 to 15%. However, the literature also discloses that the aluminum alloy becomes brittle when the amount of Si added exceeds 15%.
- aluminum alloys used for compressors and the like are added with a quite amount of Si to obtain the required properties of superior abrasion resistance, rate of thermal expansion and the like.
- Such aluminum alloys are improved in abrasion resistance, rate of thermal expansion and the like, they have problems in that processability such as extrusion processability may decrease and surface texture may deteriorate. This is observed since processability decreases by increasing the concentration of additives in the aluminum alloy.
- Si added to the aluminum alloy for improving abrasion resistance decreases the productivity in the processes of extrusion process and forge process.
- abrasion resistance, rate of thermal expansion and the like of the aluminum alloy often exceed the degree required for its actual use. Therefore, when such an extremely superior abrasion resistance and the like are not necessary, it is desirable to optimize the required properties (such as abrasion resistance) of the aluminum alloy within the required degree, from the view of productivity.
- an object of the present invention is to provide an aluminum alloy of Al-Si series which possesses superior extrusion property and forge property, and also enables the production of forged products maintaining their abrasion resistance.
- the present inventors have made a diligent investigation and found that an aluminum alloy with balanced required properties and productivity can be obtained, by adjusting the amount of each compositions and controlling the size of eutectic Si. That is, the present inventors have found that the object of the present invention can be achieved by the following means.
- an aluminum alloy possessing superior abrasion resistance, extrusion property and forging property comprising: 5.5 to 7.0 mass% (hereinafter referred to as %) of Si, 1.0 to 2.0% of Cu, 0.4 to 0.8% of Mg, 0.05 to 0.15% of Cr, 0.05 to 0.25% of Ni, with the rest consisting of A1 and unavoidable impurities, wherein Sc (defined as the size of an eutectic Si in the central portion of the cross section which is vertical with respect to the longitudinal direction of the aluminum alloy extruded) and Ss (defined as the size of the eutectic Si at the surface side of the cross section which is vertical with respect to the longitudinal direction of the aluminum alloy extruded) satisfies an equation of "Sc-Ss ⁇ 15 ⁇ m 2 ", and the number of the eutectic Si particles having the size of 20 ⁇ m 2 or smaller is 1000 to 3000 /mm 2 , is provided.
- Sc defined as the size of an eutectic Si in
- an aluminum alloy with superior abrasion resistance, extrusion property and forge processing property further containing 0.01 to 0.05% of Sr is provided.
- aluminum alloy material for manufacturing extrusion material and forged material with superior extrusion property and forge processing property, while also maintaining abrasion resistance can be provided by controlling the content of each composition and the size of the eutectic Si in the aluminum alloy.
- FIG 1 This is a figure showing the forge processing of the extruded product manufactured by extrusion.
- Si contributes to the improvement in abrasion resistance by forming a Si compound.
- the amount of Si added is less than 5.5%, the effect observed for the improvement in strength and abrasion resistance is low.
- the amount of Si added exceeds 7.0%, the surface texture deteriorates, and the extrusion property lowers.
- Cu contributes to the improvement in strength. When the amount of Cu added is less than 1.0%, the effect observed for the improvement in strength is low. When the amount of Cu added exceeds 2.0%, the extrusion processability and corrosion resistance lowers.
- Mg together with Si, forms Mg 2 Si and contributes to the improvement in strength.
- the amount of Mg added is less than 0.4%, its effect is low.
- the amount of Mg added exceeds 0.8%, the extrusion processability lowers.
- Mg is added by 0.55 to 0.65%.
- Cr is effective for refining the crystalline grain, and contributes to the improvement in strength.
- amount of Cr added is less than 0.05%, such effect is low.
- amount of Cr added exceeds 0.15%, further increase in such effect cannot be observed.
- Cr is added by 0.07 to 0.10%.
- Ni is effective for improving heat resistance and abrasion resistance, and also contributes to the improvement in strength.
- the amount of Ni added is less than 0.05%, such effect is low.
- the amount of Ni added exceeds 0.25%, further increase in such effect cannot be observed.
- extrusion property lowers.
- Ni is added by 0.07 to 0.13%.
- Sr by being added, is an element which contributes to the improvement in mechanical properties. Sr is used for the modification treatment of the crystallized Si, and addition of Sr gives fine crystals of Si.
- the amount of Sr added is preferably 0.01 to 0.05%. When the amount of Sr added is less than 0.01%, such effect is low. When the amount of Sr added exceeds 0.05%, further increase in such effect cannot be observed.
- Fe and Mn are contained by 0.5% or less, since these elements form compounds with other additive elements and thus leads to lowering of the effects obtained by the additive elements.
- the aluminum alloy according to the present invention consists of the afore-mentioned elements, unavoidable impurities and Al.
- the aluminum alloy may contain a small amount of Ti, Zr or Zn in the range so long as it does not impair the effect of the present invention. Such range is 0.05% or less.
- the uniformity of surface texture and abrasion resistance in extrusion material and forged material depend on the size and distribution of the eutectic Si in these materials, since eutectic Si have influence on such properties. That is, the aluminum alloy of the present invention attained the superior extrusion property and forge processing property by controlling the content of Si and other compositions. In addition, by controlling the size and distribution of the eutectic Si, variation in the surface texture and the properties among the portions of the material can be avoided. Therefore, the present invention can provide extrusion material and forged material having uniform properties with high productivity.
- Ss and Sc are controlled so as to satisfy the equation of "Sc-Ss ⁇ 15 ⁇ m 2 ", the surface texture of the extrusion material becomes superior, and the variation in abrasion resistance among the surface side and the central portion of the extrusion material can be suppressed.
- Ss is obtained as the size of eutectic Si as follows: A cross section obtained by cutting the extrusion material in the vertical direction with respect to the longitudinal direction thereof is used for the observation. The size of the eutectic Si existing slightly inward of 50 ⁇ m from the surface side of the cross section of the extrusion material is observed under an optical microscope with magnification of 100 times.
- the size of the eutectic Si is observed for four sites, each site being placed with an interval of 90 degrees of central angle, with respect to the center of the visual field.
- Ss refers to the largest size of eutectic Si thus observed.
- Sc is defined as the size of eutectic Si observed at the central portion of the cross section of the extrusion material under an optical microscope with magnification of 100 times.
- the size of eutectic Si in the present invention means the crystal area of the eutectic Si.
- the roughness of the surface of the extrusion material can be suppressed by keeping the size of the eutectic Si contained in the extrusion material 20 ⁇ m 2 or smaller.
- the number of eutectic Si particles should be kept in the range of 1000 to 3000 /mm 2 in order to obtain the abrasion resistance.
- the number of eutectic Si particles with the size of 20 ⁇ m 2 or smaller is less than 1000 /mm 2 , the effect on abrasion resistance after the material being forged is low.
- the number of eutectic Si particles exceeds 3000 /mm 2 the extrusion property and the forge processing property are inhibited.
- thermal refining of the aluminum alloy of the present invention there is no particular limitation with respect to the production conditions and the thermal refining of the aluminum alloy of the present invention.
- the thermal refining should be selected depending on the intended application, within the usual production conditions.
- the type of thermal refining adopted for the extrusion material of the present invention is preferably F, T1 or O, and more preferably O.
- T6 is preferable.
- each of the alloy having the composition described in Table 1 was heated within the temperature range of 700°C to 740°C to give the molten aluminum alloy, and then molding was conducted using a metallic mold.
- the amount of cooling water was adjusted to 70 to 100 L/min.
- the samples thus obtained as the extrusion materials were subjected to observation.
- the cross section which is vertical with respect to the longitudinal direction of the extrusion material was used for such observation.
- the size of the eutectic Si existing slightly inward of 50 ⁇ m from the surface side of the cross section of the extrusion material was observed under an optical microscope with magnification of 100 times.
- the largest size of the eutectic Si (Ss) was obtained by observing four sites within this visual field under the microscope, each site being placed with an interval of 90 degrees of central angle, with respect to the center of the visual field. Further, the size of eutectic Si at the central portion (Sc) was observed at the cross section of the extrusion material under an optical microscope with magnification of 100 times.
- the size and the number of the eutectic Si particles were analyzed using the software "image analysis software A-ZO-KUN" available from Asahi Kasei Engineering Corporation. Surface texture was evaluated by stroking the surface with a pencil with hardness of HB, and the results were judged as passed "Good” when no scratch was observed, and the results were judged as failed "Not Good” when scratch was observed. The results are shown in Table 2. Samples which satisfied the predetermined criteria were judged as passed, and samples which did not meet the predetermined criteria were judged as failed.
- the round bars were subjected to annealing treatment for five hours at 400°C to give an O-material.
- the samples were confirmed that the size and number of eutectic Si particles were in the range of the present invention.
- the round bars were then cut by 100mm length in the longitudinal direction, and were subsequently subjected to upset forging with the processing rate of 80%.
- the forged products were then subjected to solution treatment for two hours at 520°C, followed by immediate heat treatment with 50°C water.
- the forged products further went through artificial aging treatments for ten hours at 180°C to give forged products with thermal refining of T6.
- the processing rate for the upset forging is a value obtained by calculation using the formula: (r1-r2) / r1 X 100 with respect to Fig. 1 .
- Test pieces for the tensile strength test were prepared so that the longitudinal direction of the extrusion bar is used for the longitudinal side of the test piece.
- the test pieces were prepared in accordance with the Japanese Industrial Standards (JIS) as test piece No. 4.
- JIS Japanese Industrial Standards
- the results of the test were evaluated as "passed” when the tensile strength (TS) was 300 MPa or higher, and were evaluated as “failed” when TS was lower than such value.
- Comparative abrasion quantity was evaluated using the Ogoshi-type abrasion tester.
- the conditions for the test were arranged as follows: gear oil (75W-90) was used as the lubricant, SCM415 was used as the opposite material, abrasion distance was set to 1200m, and the load was set to 19kgf.
- the results of the test were evaluated as "passed” when the comparative abrasion quantity was 5.0 x 10 -9 or lower, and were evaluated as "failed” when the comparative abrasion quantity was higher than such value.
- the extrusion materials 1 to 10 according to the present invention showed superior surface texture, while the extrusion materials of comparative Examples 11 to 17 showed inferior surface texture.
- Examples 1 to 10 of the present invention are superior since the composition is within the preferred range. That is, their smooth surface provides superior extrusion property and thus productivity is high.
- composition of the extrusion materials of Comparison Examples 11 to 14, 16 and 17 were out of the preferred range, and thus their surface texture caused the extrusion material to get caught during extrusion, leading to poor extrusion processability.
- the extrusion material of Comparison Example 11 contains a large amount of Si, and the value of Sc-Ss is large. Therefore, the surface texture of the extrusion material caused the extrusion material to get caught during the extrusion, leading to poor extrusion processability.
- the extrusion material of Comparison Example 12 contains a small amount of Si, and the value of Sc-Ss is large. Therefore, the surface texture of the extrusion material caused the extrusion material to get caught during the extrusion, leading to poor extrusion processability.
- the extrusion material of Comparison Example 13 contains a small amount of Si and Cu. Therefore, the surface texture of the extrusion material caused the extrusion material to get caught during the extrusion, leading to poor extrusion processability.
- the extrusion material of Comparison Example 14 contains a large amount of Si, Cu, Mg and Cr. Therefore, the surface texture of the extrusion material caused the extrusion material to get caught during the extrusion, leading to poor extrusion processability.
- the extrusion material of Comparison Example 17 contains a large amount of Si, contains a small amount of Mg, and the value of Sc-Ss is large. Therefore, the surface texture of the extrusion material caused the extrusion material to get caught during the extrusion, leading to poor extrusion processability.
- composition of the extrusion material of Comparison Example 15 is within the preferred range, however, the value of Sc-Ss is large. Therefore, the surface texture of the extrusion material caused the extrusion material to get caught during the extrusion, leading to poor extrusion processability.
- Examples 1 to 10 according to the present invention showed superior appearance after forging, tensile strength and comparative abrasion quantity, while the Comparison Examples 11 to 17 showed inferior results.
- the forged materials of Examples 1 to 10 according to the present invention showed good results in tensile strength test and possessed good comparative abrasion quantity. In addition, since the forged materials have good forge processing property, the appearance after upset forging was superior.
- the forged material of Comparison Example 11 contains a large amount of Si in its composition. Therefore, crack is observed in the appearance of the material after upset forging. That is, the forge processing property of Comparison Example 11 is low, and thus such material is not suitable as a forge material.
- the forged material of Comparison Example 12 contains a small amount of Si in its composition. Therefore, the tensile strength is low, and the abrasion resistance is inferior. Further, as shown in Table 2, abrasion resistance is inferior since the number of eutectic Si particles having the size of 20 ⁇ m 2 or smaller is large.
- the forged material of Comparison Example 13 contains a small amount of Si and Cu in its composition. Therefore, the tensile strength is low, and the abrasion resistance is inferior.
- the forged material of comparative Example 14 contains a large amount of Si, Cu, Mg and Cr. Therefore, crack is observed in the appearance of the material after upset forging. That is, the forge processing property of Comparison Example 14 is low, and thus such material is not suitable as a forge material.
- the forged material of Comparison Example 15 has its composition within the preferred range, and thus all of the appearance after upset forging, results of the tensile strength test and the comparative abrasion quantity were satisfactory. However, as shown in Table 2, the productivity of the extrusion material of comparative Example 15 is poor due to its poor extrusion processability. Therefore, productivity of the forged material of comparison 15 is poor.
- the forged material of Comparison Example 16 contains a large amount of Si, Cu and Sr in its composition.
- crack is observed in the appearance of the material after upset forging since the number of eutectic Si particles having the size of 20 ⁇ m 2 or smaller is large. That is, the forge processing property of this material is poor, and is not suitable as a forged material.
- the forged material of Comparison Example 17 contains a large amount of Si and a small amount of Mg in its composition. Accordingly, crack is observed in the appearance of the material after upset forging. That is, the forge processing property of this material is poor, and is not suitable as a forged material.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Forging (AREA)
- Extrusion Of Metal (AREA)
Description
- The present invention relates to aluminum alloy with superior abrasion resistance, extrusion property and forge processing property, such aluminum alloy being used for parts such as compressors in automobiles and home electric appliances.
- Properties such as abrasion resistance and the like are required with aluminum alloy used for compressors and the like in automobiles and home electric appliances. For example, regarding an aluminum alloy used for compressors, Si is added to the Al-Si by 10 mass% (herein after referred to as %) or more, in order to improve abrasion resistance and to decrease the rate of thermal expansion.
Patent Literature 1 discloses an aluminum alloy for sliding use with superior fatigue resistance and seizure resistance. In order to obtain such fatigue resistance and seizure resistance, Si is added to the aluminum alloy as an essential element by 1 to 15%. However, the literature also discloses that the aluminum alloy becomes brittle when the amount of Si added exceeds 15%. - [Patent Literature 1]
JP H03-006345 - As mentioned above, aluminum alloys used for compressors and the like are added with a quite amount of Si to obtain the required properties of superior abrasion resistance, rate of thermal expansion and the like. Although such aluminum alloys are improved in abrasion resistance, rate of thermal expansion and the like, they have problems in that processability such as extrusion processability may decrease and surface texture may deteriorate. This is observed since processability decreases by increasing the concentration of additives in the aluminum alloy. In particular, Si added to the aluminum alloy for improving abrasion resistance decreases the productivity in the processes of extrusion process and forge process. In practical use, abrasion resistance, rate of thermal expansion and the like of the aluminum alloy often exceed the degree required for its actual use. Therefore, when such an extremely superior abrasion resistance and the like are not necessary, it is desirable to optimize the required properties (such as abrasion resistance) of the aluminum alloy within the required degree, from the view of productivity.
- Accordingly, by balancing the required property and the productivity as necessary, aluminum alloy with highly advantageous effect in cost can be obtained without losing productivity.
- Thus, development of a balanced aluminum alloy with required property while suppressing the loss of productivity to its minimum is desired.
- Taking the afore-mentioned circumstances into consideration, an object of the present invention is to provide an aluminum alloy of Al-Si series which possesses superior extrusion property and forge property, and also enables the production of forged products maintaining their abrasion resistance.
- The present inventors have made a diligent investigation and found that an aluminum alloy with balanced required properties and productivity can be obtained, by adjusting the amount of each compositions and controlling the size of eutectic Si. That is, the present inventors have found that the object of the present invention can be achieved by the following means.
- That is, according to the present invention, an aluminum alloy possessing superior abrasion resistance, extrusion property and forging property, comprising: 5.5 to 7.0 mass% (hereinafter referred to as %) of Si, 1.0 to 2.0% of Cu, 0.4 to 0.8% of Mg, 0.05 to 0.15% of Cr, 0.05 to 0.25% of Ni, with the rest consisting of A1 and unavoidable impurities, wherein Sc (defined as the size of an eutectic Si in the central portion of the cross section which is vertical with respect to the longitudinal direction of the aluminum alloy extruded) and Ss (defined as the size of the eutectic Si at the surface side of the cross section which is vertical with respect to the longitudinal direction of the aluminum alloy extruded) satisfies an equation of "Sc-Ss ≤ 15 µm2", and the number of the eutectic Si particles having the size of 20µm2 or smaller is 1000 to 3000 /mm2, is provided.
- Preferably, an aluminum alloy with superior abrasion resistance, extrusion property and forge processing property further containing 0.01 to 0.05% of Sr is provided.
- According to the present invention, aluminum alloy material for manufacturing extrusion material and forged material with superior extrusion property and forge processing property, while also maintaining abrasion resistance, can be provided by controlling the content of each composition and the size of the eutectic Si in the aluminum alloy.
- [
FIG 1 ]
This is a figure showing the forge processing of the extruded product manufactured by extrusion. - Hereinafter, the embodiments of the present invention will be described.
- First, each of the elements added to the aluminum alloy will be explained.
- Si contributes to the improvement in abrasion resistance by forming a Si compound. In addition, Si, together with Mg, forms Mg2Si, and thereby contributes to the improvement in strength. When the amount of Si added is less than 5.5%, the effect observed for the improvement in strength and abrasion resistance is low. When the amount of Si added exceeds 7.0%, the surface texture deteriorates, and the extrusion property lowers.
- Cu contributes to the improvement in strength. When the amount of Cu added is less than 1.0%, the effect observed for the improvement in strength is low. When the amount of Cu added exceeds 2.0%, the extrusion processability and corrosion resistance lowers.
- Mg, together with Si, forms Mg2Si and contributes to the improvement in strength. When the amount of Mg added is less than 0.4%, its effect is low. When the amount of Mg added exceeds 0.8%, the extrusion processability lowers. Preferably, Mg is added by 0.55 to 0.65%.
- Cr is effective for refining the crystalline grain, and contributes to the improvement in strength. When the amount of Cr added is less than 0.05%, such effect is low. When the amount of Cr added exceeds 0.15%, further increase in such effect cannot be observed. Preferably, Cr is added by 0.07 to 0.10%.
- Ni is effective for improving heat resistance and abrasion resistance, and also contributes to the improvement in strength. When the amount of Ni added is less than 0.05%, such effect is low. When the amount of Ni added exceeds 0.25%, further increase in such effect cannot be observed. In addition, extrusion property lowers. Preferably, Ni is added by 0.07 to 0.13%.
- Sr, by being added, is an element which contributes to the improvement in mechanical properties. Sr is used for the modification treatment of the crystallized Si, and addition of Sr gives fine crystals of Si. The amount of Sr added is preferably 0.01 to 0.05%. When the amount of Sr added is less than 0.01%, such effect is low. When the amount of Sr added exceeds 0.05%, further increase in such effect cannot be observed.
- Fe and Mn are contained by 0.5% or less, since these elements form compounds with other additive elements and thus leads to lowering of the effects obtained by the additive elements.
- Here, the aluminum alloy according to the present invention consists of the afore-mentioned elements, unavoidable impurities and Al. For example, the aluminum alloy may contain a small amount of Ti, Zr or Zn in the range so long as it does not impair the effect of the present invention. Such range is 0.05% or less.
- The uniformity of surface texture and abrasion resistance in extrusion material and forged material depend on the size and distribution of the eutectic Si in these materials, since eutectic Si have influence on such properties. That is, the aluminum alloy of the present invention attained the superior extrusion property and forge processing property by controlling the content of Si and other compositions. In addition, by controlling the size and distribution of the eutectic Si, variation in the surface texture and the properties among the portions of the material can be avoided. Therefore, the present invention can provide extrusion material and forged material having uniform properties with high productivity.
- When Ss and Sc are controlled so as to satisfy the equation of "Sc-Ss ≤ 15 µm2", the surface texture of the extrusion material becomes superior, and the variation in abrasion resistance among the surface side and the central portion of the extrusion material can be suppressed. Here, regarding the size of eutectic Si, Ss is obtained as the size of eutectic Si as follows: A cross section obtained by cutting the extrusion material in the vertical direction with respect to the longitudinal direction thereof is used for the observation. The size of the eutectic Si existing slightly inward of 50µm from the surface side of the cross section of the extrusion material is observed under an optical microscope with magnification of 100 times. Within this visual field under the microscope, the size of the eutectic Si is observed for four sites, each site being placed with an interval of 90 degrees of central angle, with respect to the center of the visual field. Ss refers to the largest size of eutectic Si thus observed. Sc is defined as the size of eutectic Si observed at the central portion of the cross section of the extrusion material under an optical microscope with magnification of 100 times. The size of eutectic Si in the present invention means the crystal area of the eutectic Si.
- Further, the roughness of the surface of the extrusion material can be suppressed by keeping the size of the eutectic Si contained in the extrusion material 20µm2 or smaller. In addition, the number of eutectic Si particles should be kept in the range of 1000 to 3000 /mm2 in order to obtain the abrasion resistance. When the number of eutectic Si particles with the size of 20µm2 or smaller is less than 1000 /mm2, the effect on abrasion resistance after the material being forged is low. When the number of eutectic Si particles exceeds 3000 /mm2, the extrusion property and the forge processing property are inhibited.
- Here, it should be noticed that there is no particular limitation with respect to the production conditions and the thermal refining of the aluminum alloy of the present invention. The thermal refining should be selected depending on the intended application, within the usual production conditions.
- When the extrusion material is used as the forged product, the processability during the forging process is influenced by the hardness of the material. Therefore, the type of thermal refining adopted for the extrusion material of the present invention is preferably F, T1 or O, and more preferably O.
- In addition, the type of thermal refining after the forging process should be selected depending on the required properties. Here, in the present invention, T6 is preferable.
- The present invention will be described in detail by referring to the Examples. However, the present invention shall not be limited to these Examples.
- First, each of the alloy having the composition described in Table 1 was heated within the temperature range of 700°C to 740°C to give the molten aluminum alloy, and then molding was conducted using a metallic mold. The amount of cooling water was adjusted to 70 to 100 L/min.
- After obtaining ingots with 220mm diameter, these ingots were subjected to surface finishing for four hours at 490°C. The ingots were then extruded through a single hole at 500°C to give a round bar with 30mm diameter.
- The samples thus obtained as the extrusion materials were subjected to observation. Here, the cross section which is vertical with respect to the longitudinal direction of the extrusion material was used for such observation. The size of the eutectic Si existing slightly inward of 50µm from the surface side of the cross section of the extrusion material was observed under an optical microscope with magnification of 100 times. The largest size of the eutectic Si (Ss) was obtained by observing four sites within this visual field under the microscope, each site being placed with an interval of 90 degrees of central angle, with respect to the center of the visual field. Further, the size of eutectic Si at the central portion (Sc) was observed at the cross section of the extrusion material under an optical microscope with magnification of 100 times. Here, the size and the number of the eutectic Si particles were analyzed using the software "image analysis software A-ZO-KUN" available from Asahi Kasei Engineering Corporation. Surface texture was evaluated by stroking the surface with a pencil with hardness of HB, and the results were judged as passed "Good" when no scratch was observed, and the results were judged as failed "Not Good" when scratch was observed. The results are shown in Table 2. Samples which satisfied the predetermined criteria were judged as passed, and samples which did not meet the predetermined criteria were judged as failed.
- Next, the round bars were subjected to annealing treatment for five hours at 400°C to give an O-material. Before evaluating the forged product, the samples were confirmed that the size and number of eutectic Si particles were in the range of the present invention.
- The round bars were then cut by 100mm length in the longitudinal direction, and were subsequently subjected to upset forging with the processing rate of 80%. The forged products were then subjected to solution treatment for two hours at 520°C, followed by immediate heat treatment with 50°C water. The forged products further went through artificial aging treatments for ten hours at 180°C to give forged products with thermal refining of T6.
- Here, the processing rate for the upset forging is a value obtained by calculation using the formula: (r1-r2) / r1 X 100 with respect to
Fig. 1 . - Tensile strength test, observation of appearance after upset forging and abrasion test were conducted for the test samples of forged alloy products obtained as above. Results are given in Table 3.
- Appearance after upset forging with the processing rate of 80 % was observed. Samples with no cracks were judged as passed (shown as "Good"), and samples with cracks were judged as failed (shown as "Not Good").
- Test pieces for the tensile strength test were prepared so that the longitudinal direction of the extrusion bar is used for the longitudinal side of the test piece. The test pieces were prepared in accordance with the Japanese Industrial Standards (JIS) as test piece No. 4. The results of the test were evaluated as "passed" when the tensile strength (TS) was 300 MPa or higher, and were evaluated as "failed" when TS was lower than such value.
- Comparative abrasion quantity was evaluated using the Ogoshi-type abrasion tester. Here, the conditions for the test were arranged as follows: gear oil (75W-90) was used as the lubricant, SCM415 was used as the opposite material, abrasion distance was set to 1200m, and the load was set to 19kgf. The results of the test were evaluated as "passed" when the comparative abrasion quantity was 5.0 x 10-9 or lower, and were evaluated as "failed" when the comparative abrasion quantity was higher than such value.
- As shown in Table 1 and Table 2, the
extrusion materials 1 to 10 according to the present invention showed superior surface texture, while the extrusion materials of comparative Examples 11 to 17 showed inferior surface texture. - Surface texture of Examples 1 to 10 of the present invention are superior since the composition is within the preferred range. That is, their smooth surface provides superior extrusion property and thus productivity is high.
- The composition of the extrusion materials of Comparison Examples 11 to 14, 16 and 17 were out of the preferred range, and thus their surface texture caused the extrusion material to get caught during extrusion, leading to poor extrusion processability.
- The extrusion material of Comparison Example 11 contains a large amount of Si, and the value of Sc-Ss is large. Therefore, the surface texture of the extrusion material caused the extrusion material to get caught during the extrusion, leading to poor extrusion processability.
- The extrusion material of Comparison Example 12 contains a small amount of Si, and the value of Sc-Ss is large. Therefore, the surface texture of the extrusion material caused the extrusion material to get caught during the extrusion, leading to poor extrusion processability.
- The extrusion material of Comparison Example 13 contains a small amount of Si and Cu. Therefore, the surface texture of the extrusion material caused the extrusion material to get caught during the extrusion, leading to poor extrusion processability.
- The extrusion material of Comparison Example 14 contains a large amount of Si, Cu, Mg and Cr. Therefore, the surface texture of the extrusion material caused the extrusion material to get caught during the extrusion, leading to poor extrusion processability.
- Sr contained in the extrusion material of Comparison Example 16 is out of the preferred range, and the number of eutectic Si particles having the size of 20µm2 or smaller is large. Therefore, the surface texture of the extrusion material caused the extrusion material to get caught during the extrusion, leading to poor extrusion processability.
- The extrusion material of Comparison Example 17 contains a large amount of Si, contains a small amount of Mg, and the value of Sc-Ss is large. Therefore, the surface texture of the extrusion material caused the extrusion material to get caught during the extrusion, leading to poor extrusion processability.
- The composition of the extrusion material of Comparison Example 15 is within the preferred range, however, the value of Sc-Ss is large. Therefore, the surface texture of the extrusion material caused the extrusion material to get caught during the extrusion, leading to poor extrusion processability.
- As shown in Table 3, Examples 1 to 10 according to the present invention showed superior appearance after forging, tensile strength and comparative abrasion quantity, while the Comparison Examples 11 to 17 showed inferior results.
- The forged materials of Examples 1 to 10 according to the present invention showed good results in tensile strength test and possessed good comparative abrasion quantity. In addition, since the forged materials have good forge processing property, the appearance after upset forging was superior.
- The forged material of Comparison Example 11 contains a large amount of Si in its composition. Therefore, crack is observed in the appearance of the material after upset forging. That is, the forge processing property of Comparison Example 11 is low, and thus such material is not suitable as a forge material.
- The forged material of Comparison Example 12 contains a small amount of Si in its composition. Therefore, the tensile strength is low, and the abrasion resistance is inferior. Further, as shown in Table 2, abrasion resistance is inferior since the number of eutectic Si particles having the size of 20µm2 or smaller is large.
- The forged material of Comparison Example 13 contains a small amount of Si and Cu in its composition. Therefore, the tensile strength is low, and the abrasion resistance is inferior.
- The forged material of comparative Example 14 contains a large amount of Si, Cu, Mg and Cr. Therefore, crack is observed in the appearance of the material after upset forging. That is, the forge processing property of Comparison Example 14 is low, and thus such material is not suitable as a forge material.
- The forged material of Comparison Example 15 has its composition within the preferred range, and thus all of the appearance after upset forging, results of the tensile strength test and the comparative abrasion quantity were satisfactory. However, as shown in Table 2, the productivity of the extrusion material of comparative Example 15 is poor due to its poor extrusion processability. Therefore, productivity of the forged material of comparison 15 is poor.
- The forged material of Comparison Example 16 contains a large amount of Si, Cu and Sr in its composition. In addition, as shown in Table 2, crack is observed in the appearance of the material after upset forging since the number of eutectic Si particles having the size of 20µm2 or smaller is large. That is, the forge processing property of this material is poor, and is not suitable as a forged material.
- The forged material of Comparison Example 17 contains a large amount of Si and a small amount of Mg in its composition. Accordingly, crack is observed in the appearance of the material after upset forging. That is, the forge processing property of this material is poor, and is not suitable as a forged material.
-
- 1
- extruded bar after cutout (before forging)
- 2
- forging machine
- r1
- height of material before upset forging
- r2
- height of material after upset forging
Claims (2)
- An extruded product of an aluminum alloy possessing superior abrasion resistance, extrusion property and forging property, comprising:5.5 to 7.0 mass% (hereinafter referred to as %) of Si, 1.0 to 2.0% of Cu, 0.4 to 0.8% of Mg, 0.05 to 0.15% of Cr, 0.05 to 0.25% of Ni, with the rest consisting of Al, 0.5% or less of Fe and Mn, and unavoidable impurities, whereinSc (defined as the size of an eutectic Si in the central portion of the cross section of the extruded product which is vertical with respect to the longitudinal direction of the extruded product) and Ss (defined as the size of the eutectic Si at the surface side of the cross section which is vertical with respect to the longitudinal direction of the extruded product) satisfies an equation of "Sc-Ss ≤ 15 µm2", andthe number of the eutectic Si particles having the size of 20µm2 or smaller is 1000 to 3000 per mm2.
- The extruded product of Claim 1, further comprising 0.01 to 0.05% of Sr.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/JP2012/052215 WO2013114582A1 (en) | 2012-02-01 | 2012-02-01 | Aluminum alloy having excellent wear resistance, extrudability, and forging workability |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2811041A1 EP2811041A1 (en) | 2014-12-10 |
EP2811041A4 EP2811041A4 (en) | 2015-09-02 |
EP2811041B1 true EP2811041B1 (en) | 2016-07-06 |
Family
ID=48904660
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP12867174.0A Active EP2811041B1 (en) | 2012-02-01 | 2012-02-01 | Aluminum alloy having excellent wear resistance, extrudability, and forging workability |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP2811041B1 (en) |
CN (1) | CN104160049B (en) |
WO (1) | WO2013114582A1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2018033177A1 (en) * | 2016-08-15 | 2018-02-22 | Ksm Castings Group Gmbh | Al casting alloy |
CN108193094A (en) * | 2018-01-22 | 2018-06-22 | 湖北大旗液压有限公司 | Wear-resistant aluminium alloy material for gear pump floating side plate and preparation method thereof |
JP7318283B2 (en) * | 2019-04-05 | 2023-08-01 | 株式会社レゾナック | Aluminum alloys for compressor sliding parts and forgings for compressor sliding parts |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH01104742A (en) * | 1987-10-16 | 1989-04-21 | Furukawa Alum Co Ltd | Wear-resistant aluminum alloy |
JPH036345A (en) | 1989-06-02 | 1991-01-11 | Daido Metal Co Ltd | Aluminum-base alloy for sliding use excellent in fatigue resistance and seizure resistance |
JPH05287427A (en) * | 1992-04-08 | 1993-11-02 | Furukawa Alum Co Ltd | Wear resistant aluminum alloy for cold forging and its manufacture |
JPH07197164A (en) * | 1993-12-28 | 1995-08-01 | Furukawa Electric Co Ltd:The | Aluminum alloy having high strength and high workability and its production |
JPH0828493A (en) * | 1994-07-14 | 1996-01-30 | Furukawa Electric Co Ltd:The | Manufacture of aluminum alloy-made scroll |
JP3261056B2 (en) * | 1997-01-14 | 2002-02-25 | 住友軽金属工業株式会社 | High-strength wear-resistant aluminum alloy extruded material excellent in ease of forming anodized film and uniformity of film thickness and method for producing the same |
JP4633972B2 (en) * | 2001-07-17 | 2011-02-16 | 住友電気工業株式会社 | Wear-resistant aluminum alloy elongated body, manufacturing method thereof, and piston for car air conditioner |
EP1479785B1 (en) * | 2002-02-28 | 2008-12-31 | Aisin Keikinzoku Co., Ltd. | Wear-resistant aluminum alloy excellent in caulking property and extruded product made thereof |
FR2841164B1 (en) * | 2002-06-25 | 2004-07-30 | Pechiney Aluminium | ALLOY MOLDING WITH HIGH FLUID RESISTANCE |
EP1715084B1 (en) * | 2003-11-21 | 2019-01-16 | Showa Denko K.K. | Anodized aluminum alloy and manufacturing method thereof |
JP2010018875A (en) * | 2008-07-14 | 2010-01-28 | Toyota Central R&D Labs Inc | High strength aluminum alloy, method for producing high strength aluminum alloy casting, and method for producing high strength aluminum alloy member |
MY155638A (en) * | 2009-01-27 | 2015-11-13 | Daiki Aluminium Industry Co Ltd | An aluminum alloy for pressure casting and an alumium alloy cast made of the same |
-
2012
- 2012-02-01 WO PCT/JP2012/052215 patent/WO2013114582A1/en active Application Filing
- 2012-02-01 CN CN201280068314.4A patent/CN104160049B/en active Active
- 2012-02-01 EP EP12867174.0A patent/EP2811041B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP2811041A4 (en) | 2015-09-02 |
CN104160049A (en) | 2014-11-19 |
CN104160049B (en) | 2016-09-14 |
WO2013114582A1 (en) | 2013-08-08 |
EP2811041A1 (en) | 2014-12-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR102013886B1 (en) | High-tensile brass alloy and alloy product | |
JP5046178B2 (en) | Magnesium alloy material and manufacturing method thereof | |
RU2695852C2 (en) | α-β TITANIUM ALLOY | |
JP5848259B2 (en) | Manufacturing method of brake piston shape material | |
JP2007084864A (en) | alpha-beta TYPE TITANIUM ALLOY SUPERIOR IN MACHINABILITY AND HOT WORKABILITY | |
US20230151457A1 (en) | Lead-Free Brass Alloy | |
EP2811041B1 (en) | Aluminum alloy having excellent wear resistance, extrudability, and forging workability | |
US20100303667A1 (en) | Novel lead-free brass alloy | |
JP6612029B2 (en) | High strength aluminum alloy extruded material with excellent impact resistance and method for producing the same | |
WO2018088351A1 (en) | Aluminum alloy extruded material | |
WO2010086372A1 (en) | Titanium alloy, a method of producing the alloy and an article made of the alloy | |
CN108929985B (en) | Medium carbon wire rod excellent in strength and cold workability and method for producing same | |
KR20180081603A (en) | Aluminum alloy material and manufacturing method thereof | |
JP4798943B2 (en) | Aluminum alloy plate for forming and method for producing the same | |
JP2016027193A (en) | Copper alloy, cold-rolled metal plate and method for manufacturing the same | |
JP2019019373A (en) | Manufacturing method of aluminum alloy-made piston of compressor, and the aluminum alloy for piston | |
EP3263725B1 (en) | Heat-resistant magnesium alloy | |
JP6485692B2 (en) | Heat resistant alloy with excellent high temperature strength, method for producing the same and heat resistant alloy spring | |
WO2017168645A1 (en) | Heat-resistant magnesium alloy | |
CN103384727B (en) | High strength copper alloy forged material | |
WO2016152663A1 (en) | α-β TITANIUM ALLOY | |
JP6405626B2 (en) | β-type titanium alloy, titanium product using the same, β-type titanium alloy manufacturing method, and titanium product manufacturing method | |
JPWO2013114582A1 (en) | Aluminum alloy with excellent wear resistance, extrudability, and forgeability | |
EP3649266B1 (en) | Titanium-containing zinc wrought alloy | |
JP4987640B2 (en) | Titanium alloy bar wire for machine parts or decorative parts suitable for manufacturing cold-worked parts and method for manufacturing the same |
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: 20140723 |
|
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) | ||
RA4 | Supplementary search report drawn up and despatched (corrected) |
Effective date: 20150805 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: C22C 21/02 20060101AFI20150730BHEP Ipc: C22F 1/043 20060101ALI20150730BHEP |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: C22C 21/02 20060101AFI20160126BHEP Ipc: C22F 1/043 20060101ALI20160126BHEP |
|
INTG | Intention to grant announced |
Effective date: 20160224 |
|
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: AT Ref legal event code: REF Ref document number: 810755 Country of ref document: AT Kind code of ref document: T Effective date: 20160715 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: DE Ref legal event code: R096 Ref document number: 602012020324 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20160706 |
|
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: 810755 Country of ref document: AT Kind code of ref document: T Effective date: 20160706 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20160706 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: 20161006 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: 20160706 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: 20160706 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: 20160706 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: 20160706 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: 20161106 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: 20160706 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 6 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160706 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: 20161007 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: 20160706 Ref country code: BE 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: 20160706 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: 20160706 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: 20160706 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: 20160706 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: 20161107 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602012020324 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20160706 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: 20160706 |
|
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 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160706 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: 20160706 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: 20160706 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: 20160706 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: 20161006 |
|
26N | No opposition filed |
Effective date: 20170407 |
|
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: 20160706 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 602012020324 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160706 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20170201 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170228 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170228 |
|
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: 20170201 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 7 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170901 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170201 Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170201 |
|
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: 20170201 |
|
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: 20160706 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20120201 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160706 |
|
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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160706 |
|
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: 20160706 |
|
P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230816 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20240103 Year of fee payment: 13 |