• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The invention relates to a thin sheet for reinforcing part or aluminum alloy car body structure of composition, in% by weight: Si: 10 - 14, Mg: 0.05 - 0.8, Cu: 0 - 0.2, Fe: 0 - 0.5, Mn: 0 - 0.5, optionally at least one element chosen from Na, Ca, Sr, Ba, Yt and Li, the quantity of said element, if chosen, being from 0.01 - 0.05 for Na, Ca, Sr, Ba Yt and 0.1 - 0.3 for Li, Sb: 0 - 0.05, Cr: 0 - 0.1, Ti: 0 - 0.2 , other elements <0.05 each and <0.15 in total, remains aluminum. The invention also relates to the method of manufacturing such a sheet and the use of a thin sheet of alloy of the 4XXX series having a silicon content of at least 10% by weight, the modulus of elasticity of which is minus 77 GPa to make a reinforcement part or bodywork structure.
    公开号:FR3044328A1
    申请号:FR1655564
    申请日:2016-06-15
    公开日:2017-06-02
    发明作者:Petar Ratchev；Jean-Philippe Masse；Christophe Chabriol；Ravi Shahani；Lukasz Dolega
    申请人:Constellium Neuf Brisach SAS；
    IPC主号:
    专利说明:

    FIELD OF THE INVENTION The invention relates to the field of aluminum alloy sheets intended for the stamping production of lining, structural or reinforcement parts of the white body of motor vehicles. .
    State of the art
    Aluminum alloys are increasingly used in the construction of motor vehicles because their use reduces the weight of vehicles and thus reduce fuel consumption and greenhouse gas emissions.
    Aluminum alloy sheets are used in particular for the production of many parts of the "white box", among which are: body skin parts (or exterior body panels) such as the front fenders, the roof or roof , bonnet, boot or door skin; lining parts such as door, wing, tailgate or hood liners; and finally the structural parts, such as the longitudinal members, the aprons, the load floors and the front, middle and rear feet.
    If many pieces of skin are already made of sheets of aluminum alloys, the transposition of the steel to aluminum for reinforcing pieces, particularly of the lining or structural type, having higher characteristics, proves to be more delicate because initially the poorer formability of aluminum alloys with respect to steels and in fact secondly mechanical characteristics in general lower than those of steels used for this type of parts.
    Indeed, for reinforcing or structural type applications, a set of properties, sometimes antagonistic, is required such as: high formability in the delivery state, state T4, in particular for stamping operations, a limit controlled elasticity in the state of delivery of the sheet to control the elastic return during the shaping, - a high mechanical strength after recovery and / or after cataphoresis and baking paints to obtain good mechanical strength in service while by minimizing the weight of the part, - a good ability to absorb energy in the event of impact for application to bodywork parts, - good behavior in the various assembly methods used in automobile bodywork such as spot welding, laser welding, gluing, clinching or riveting, - good resistance to corrosion, including intergranular corrosion, stress corrosion and filiform corrosion of the finished part, - compatibility with the recycling requirements of manufacturing waste or recycled vehicles, - an acceptable cost for mass production.
    An important property, however, has often been neglected, it is the rigidity of the alloy which is related to its modulus of elasticity. Thus, a material whose modulus of elasticity (sometimes also called Young's modulus) is very high is said to be rigid. Thus when the material is rigid it may be possible for some parts for which it is a limiting factor to reduce the thickness of the part compared to the currently used parts and thus to obtain a weight gain. Parts of this type are essentially encountered for reinforcing or structural parts.
    The patent application WO 95/34691 relates to an aluminum alloy sheet intended for mechanical, aeronautical or space construction characterized by the composition (% by weight) If 6.5 - 11%, Mg 0.5 - 1.0%, Cu <0.8%, Fe <0.3%, Mn <0.5%, and / or Cr <0.5%, Sr 0.008 - 0.025%, Ti <0.02%, total other elements <0, 2%, remains aluminum. The plates according to this patent application have a high modulus of elasticity and a low density and can be used in particular for the wing bottom and the aircraft fuselage lining, as well as for cryogenic rocket tanks.
    US Patent 4,126,486 describes the manufacture of alloy sheets AISi containing 4 to 15% Si by continuous casting between two cooled rolls. The strips obtained are subjected to a thickness reduction of at least 60% by cold rolling and then subjected to a heat treatment at a temperature of 250 to 400 ° C. These sheets are used for applications for which low mechanical strengths are acceptable.
    EP 0 790 325 discloses spun products for machining of composition (% by weight) Si 11 - 13.5%, Mg 0.5 - 2.0%, Cu <0.35%, Fe <1.0% , Mn <1.2%, Cr <0.1%, Sr 0.02 - 0.1%, Zr <0.1%, Ni <0.1%, Zn <0.1% Bi <1.0 %, Pb <1.0%, Sn <1.0%, Ti <0.02%, remains aluminum and unavoidable impurities.
    The patent application US 2004/0143102 describes in particular an aluminum alloy comprising) Si 0.3 - 12.5%, Mg 0.1 - 6%, Cu 0.01 - 1%, Sr 0.001 - 0.5% , Zn 0.01 -3% remains aluminum and unavoidable impurities.
    Problem
    The object of the present invention is to provide aluminum alloy sheets for reinforcement or automobile bodywork structure having a high rigidity, while having the other acceptable characteristics: a mechanical strength in service, after shaping and baking paints as high as the sheets of the prior art, good resistance to corrosion, in particular intergranular or filiform, a formability by stamping at satisfactory ambient temperature and good behavior in the various assembly methods such as spot welding, laser welding, gluing, clinching or riveting.
    OBJECT OF THE INVENTION The subject of the invention is a thin sheet for a reinforcing part or an aluminum alloy automotive bodywork structure of composition, in% by weight:
    If: 10-14,
    Mg: 0.05 - 0.8,
    Cu: 0 - 0.2,
    Fe: 0 - 0.5,
    Mn: 0 - 0.5, optionally at least one element selected from Na, Ca, Sr, Ba, Yt and Li, the amount of said element, if selected, being 0.01 - 0.05 for Na, Ca, Sr, Ba Yt and 0.1 - 0.3 for Li,
    Sb: 0 - 0.05 Cr: 0-0.1 Ti: 0 - 0.2 other elements <0.05 each and <0.15 in total, remains aluminum.
    It also relates to a method of manufacturing thin sheets according to the invention comprising the following successive steps: - typically vertical semi-continuous casting of a composition plate according to the invention and optionally scalping, - optionally homogenization ,
    - heating at a temperature between 400 and 560 ° C - hot rolling of the plate in a strip of thickness between 2 and 12 mm, - optionally cold rolling to the final thickness, - optionally the dissolution of the sheet between 500 and 560 ° C for 1 s to 5 min, followed by cooling to a temperature below 200 ° C, - optionally a heat treatment at a temperature between 40 and 150 ° C for a duration of 1 to 15 hours, aging at room temperature of at least 3 days.
    Yet another object of the invention is the use of an alloy sheet of the 4XXX series whose silicon content is at least 10% by weight and whose modulus of elasticity is at least 77 GPa to achieve a reinforcement piece or automobile body structure.
    Description of figures
    Figure 1 shows the structure obtained after casting for ingots 1 and 2 of Example 1 (Figures 1a and 1b, respectively).
    Figure 2 specifies the dimensions in mm of the tools used to determine the value of the parameter known to those skilled in the art under the name of LDH (Limit Dome Height) characteristic of the drawability of the material.
    Description of the invention
    Unless stated otherwise, all the information concerning the chemical composition of the alloys is expressed as a percentage by weight based on the total weight of the alloy. The expression 1.4 Cu means that the copper content expressed in% by weight is multiplied by 1.4. The designation of alloys is in accordance with the regulations of The Aluminum Association, known to those skilled in the art. The definitions of the metallurgical states are given in the European standard EN 515. The static mechanical characteristics in tension, in other words the tensile strength Rm, the conventional yield strength at 0.2% elongation Rp0,2 , the necking elongation Ag% and the elongation at break A% are determined by a tensile test according to standard NF EN ISO 6892-1, the sample and the direction of the test being defined by the EN standard. 485-1.
    The modulus of elasticity is measured according to ASTM 1876.
    Unless otherwise specified, the definitions of EN 12258 apply. A thin sheet is a laminated product of rectangular cross section whose uniform thickness is between 0.20 mm and 6 mm.
    According to the invention thin aluminum alloy sheets comprising 10 to 14% by weight of silicon and 0.05 to 0.8% by weight of magnesium have a significantly higher rigidity than the alloy sheets 5xxx or 6xxx traditionally used. to achieve reinforcing parts or automotive body structure and thus reduce the thickness of these parts when the stiffness is a limiting factor. Thus, the products according to the invention typically have a modulus of elasticity of at least 77 GPa whereas the products for reinforcement pieces or of automobile body structure according to the prior art typically have a modulus of between 67 and 72 GPa.
    Surprisingly it has been possible to obtain sheets whose module is higher than the sheets according to the prior art while obtaining satisfactory characteristics for antagonistic properties such as formability or corrosion. The silicon content must be at least 10% and preferably 11% by weight, in fact a lower content does not achieve a sufficient modulus of elasticity. Advantageously, the silicon content is at least 11.5% by weight and preferably at least 12% by weight. The silicon content must be at most 14% by weight, indeed a higher content does not achieve the desired elongation and formability properties. Advantageously, the silicon content is at most 13.5% by weight and preferably at most 13% by weight.
    The magnesium content must be at least 0.05% by weight and preferably at least 0.1% by weight, in fact a lower content does not achieve sufficient mechanical properties. The magnesium content should be at most 0.8% by weight and preferably at most 0.7%, indeed a higher content does not achieve the desired elongation and formability properties. In one embodiment of the invention, the magnesium content is between 0.1 and 0.3% by weight, which makes it possible to obtain a high formability of the sheet. The use of the plates according to this embodiment for making reinforcing parts, in particular of the type of lining such as door, wing, tailgate or hood linings is advantageous.
    In another embodiment of the invention, the magnesium content is between 0.3 and 0.6% by weight, which makes it possible to obtain a higher mechanical strength while maintaining sufficient formability. The use of the sheets according to this embodiment to produce structural parts, such as longitudinal members, aprons, load floors and front, middle and rear feet is advantageous.
    The copper content is between 0 and 0.2% by weight. A copper content greater than 0.2% by weight has a detrimental effect on the corrosion resistance. It is advantageous to carry out the addition of a quantity of copper of between 0.03 and 0.15% by weight, in particular to improve the formability of the sheets after aging (state T4 for example) and / or the mechanical strength after the treatment. final thermal parts (state T6 or T7 for example).
    The iron content is between 0 and 0.5% by weight. An iron content greater than 0.5% by weight has a detrimental effect on the formability. Advantageously, the addition of an amount of iron of between 0.1 and 0.3% by weight is carried out to improve mechanical strength and formability. It may be advantageous to carry out the addition of an amount of iron of between 0.05 and 0.2% by weight in order to improve more particularly the formability, in particular to produce lining parts. The manganese content is between 0 and 0.5% by weight. A manganese content greater than 0.5% by weight has a detrimental effect on the formability. In one embodiment, it is advantageous to add an amount of manganese of between 0.05 and 0.2% by weight, in particular to improve the formability. However, in another embodiment, no manganese is added and the manganese content is less than 0.05% by weight. The addition of at least one element chosen from Na, Ca, Sr, Ba, Yt and Li, the quantity of said element, if it is chosen, being 0.01 - 0.05 for Na, Ca, Sr, Ba, Yt and 0.1 - 0.3 for Li is advantageous. If the element is not chosen as an addition, its content is maintained at less than 0.01% by weight for Na, Ca, Sr, Ba, Yt and less than 0.05% by weight for Li. modifying agents make it possible in particular to control the size of the silicon-containing eutectic compounds during solidification and / or to modify their structure, which has a favorable effect on the mechanical properties, especially the formability, in particular during the casting of large plates. dimensions. Strontium is the preferred modifier and the addition of 0.01 to 0.05 wt% strontium is advantageous. The addition of antimony is particularly advantageous for limiting the presence of phosphorus in the alloy, this element adversely modifying the structure of the eutectic. In one embodiment of the invention the antimony content is between 0.01 and 0.04% by weight, however in this embodiment the addition of a modifying agent such as sodium or strontium is preferably avoided.
    The chromium content is between 0 and 0.5% by weight. Advantageously, the addition of a quantity of chromium of between 0.1 and 0.3% by weight is carried out.
    The titanium content is between 0 and 0.2% by weight. Advantageously, the addition of an amount of titanium of between 0.01 and 0.15% by weight is carried out.
    The method of manufacturing the sheets according to the invention comprises the casting of a plate, typically by vertical semi-continuous casting, composition according to the invention and optionally scalping.
    Optionally it is possible to homogenize the plate thus obtained, however homogenization may not be advantageous and it is generally preferred to proceed directly to reheating at a temperature between 400 and 560 ° C with advantageously a maintenance between 30 min and 6 h. The hot rolling of the plate is then carried out in a strip of thickness of between 2 and 12 mm and then optionally cold rolling to obtain a thin sheet. Preferably, the hot rolling start temperature is between 400 and 550 ° C. In an advantageous embodiment of the invention, the hot rolling start temperature is between 500 and 540 ° C. The end temperature of hot rolling is preferably between 200 and 250 ° C. In an advantageous embodiment of the invention, the temperature of hot rolling end is between 210 and 240 ° C. The present inventors have found that rolling outside of preferred temperatures can lead to a significant decrease in mechanical properties. Preferably, the method comprises a cold rolling step. The dissolution of the thin sheet thus obtained at a temperature between 500 and 560 ° C for 1 s to 5 min is advantageous. The temperature is advantageously a temperature above the solvus temperature of the alloy and lower than the initial melting. The thin sheet is then cooled to a temperature below 200 ° C and preferably below 100 ° C. Preferably cooling is rapid, the cooling rate being more than 10 ° C / s and better still at least 20 ° C / s.
    Optionally the thin sheet then undergoes a heat treatment at a temperature of between 40 and 150 ° C. and preferably between 50 and 100 ° C. for a duration of 1 to 15 hours, this treatment being able in particular to be carried out during the cooling of the coil obtained. .
    The thin sheet is then aged for at least three days, typically to obtain a T4 state.
    The sheets obtained by the process according to the invention advantageously have a modulus of elasticity measured according to the ASTM 1876 standard of at least 77 GPa and preferably at least 79 GPa and at least one of the following characteristics, and preferably all of the following characteristics: a yield strength of between 90, preferably 130 and 200 MPa and preferably between 140 and 190 MPa; an elongation at break of at least 15% and preferably at least 15%; minus 18% - an elongation of at least 13% and preferably at least 15%
    In the embodiment of the invention in which the magnesium content is between 0.1 and 0.3% by weight and which makes it possible to obtain a high formability of the sheet, the sheets obtained by the process according to advantageously have a modulus of elasticity measured according to ASTM 1876 of at least 77 GPa and preferably at least 78 GPa and at least one of the following characteristics, and preferably all of the following characteristics: yield strength between 80 and 150 MPa and preferably between 90 and 130 MPa - an elongation at break A% of at least 18% and preferably at least 20% - an elongation at a stress Ag% of at minus 15% and preferably at least 17%
    In the embodiment of the invention in which the magnesium content is between 0.3 and 0.6% by weight and which makes it possible to obtain a higher mechanical strength while maintaining a sufficient formability, the sheets obtained by the method according to the invention advantageously has a modulus of elasticity measured according to the ASTM 1876 standard of at least 77 GPa and preferably at least 79 GPa and at least one of the following characteristics, and preferably all the following characteristics: - a yield strength of between 130 and 200 MPa and preferably between 140 and 190 MPa - an elongation at rupture A% of at least 15% and preferably at least 18% - a necking elongation Ag% of at least 13% and preferably at least 15%
    Advantageously the value of LDH as defined in Example 2 and measured on a sheet of thickness 3.5 mm according to the invention is at least 20 mm and preferably at least 24 mm and preferably d at least 27 mm.
    Thus, the sheets according to the invention have a high modulus of elasticity and have a satisfactory ability to draw at room temperature. Just as advantageously, they have, in use, after forming, assembly, income and / or baking paints, high mechanical properties, good resistance to corrosion, in particular to intergranular corrosion.
    The thin sheets according to the invention advantageously have, in the naturally aged state returned and / or after firing paints, a maximum depth of intergranular corrosion measured according to the ISO 11846 standard of less than 300 μm, preferably less than 250 μm, and preferred way less than 200 μm.
    According to the invention, it is possible to use an alloy sheet of the 4XXX series having a silicon content of at least 10% by weight, whose modulus of elasticity measured according to the ASTM 1876 standard is at least 77 GPa to achieve a reinforcement piece or automobile body structure. The use of the sheets according to the invention to produce a reinforcing part or automotive body structure is preferred. Advantageously, in the use according to the invention, the thin sheet is obtained by the process according to the invention and then shaped typically by stamping, folding and / or rolling and then undergoes a heat treatment of income, this heat treatment can be carried out simultaneously. to the cooking of the paintings.
    The reinforcement parts or automobile body structure of the use according to the invention have advantageously in use, that is to say during their use in the automobile body a yield strength of at least 220 MPa, preferably at least 250 MPa and an elongation at break of at least 6% and preferably at least 10%.
    The reinforcement parts or automobile body structure of the use according to the invention advantageously have a maximum depth of intergranular corrosion measured according to ISO 11846 less than 300 pm and preferably less than 200 pm.
    Examples Example 1
    50 mm thick ingots were cast. The composition of the ingots is given in Table 1.
    Table 1, composition of ingots in% by weight
    The ingots were heated at 540 ° C. for two hours and then hot-rolled to a thickness of 9 mm and then cold-rolled to a thickness of 3.5 mm. The thin sheets thus obtained were dissolved at 540.degree. ° C for one minute then quenched. The sheets were then subjected to an 8 hour heat treatment at a temperature of 85 ° C. The sheets were then aged at room temperature to obtain a T4 state. Some sheets also underwent a two hour heat treatment at 210 ° C.
    The cast structures were observed by light microscopy. Figure la shows the structure obtained for the alloy 1 and the structure lb shows the structure obtained for the alloy 2. The addition of strontium makes it possible to reduce the size of the eutectic compounds which appear in black, which is advantageous.
    The mechanical characteristics were measured according to the standards NF EN ISO 6892-1, EN 485-1 and ASTM 1876 in the direction perpendicular to the rolling direction. The sample size for the E module measurement was 60 x 10 x 3 mm.
    The results of the characterizations are given in Table 2.
    Table 2 - Mechanical Properties of Thin Sheet
    The alloy 4, outside the invention, does not have sufficient elongation.
    Example 2
    Ingots 50 mm thick were cast. The composition of the ingots is given in Table 3.
    Table 3, composition of ingots in% by weight
    The ingots A to F were heated at 540 ° C for two hours and then hot rolled to a thickness of 9 mm with a hot rolling start temperature of 518 to 524 ° C and an end of rolling temperature. at a temperature of between 218 and 233 ° C and then cold rolled to a thickness of 3.5 mm. The ingot H was heated at 460 ° C for two hours and then hot rolled to a thickness of 9 mm with a hot rolling start temperature of 451 ° C and a hot rolling end temperature of 201 ° C. C, then cold rolled to a thickness of 3.5 mm. The ingot I was heated at 500 ° C for two hours and then hot rolled to thickness 9 mm with a hot rolling start temperature of 488 ° C and a hot rolling end temperature of 296 ° C. C, then cold rolled to a thickness of 3.5 mm. The thin sheets thus obtained were dissolved at 540 ° C. for one minute and then quenched. The sheets were then subjected to an 8 hour heat treatment at a temperature of 85 ° C. The sheets were then aged at room temperature to obtain a T4 state. Some sheets also underwent a two hour heat treatment at 210 ° C. Other sheets also underwent a heat treatment of 20 minutes at 185 ° C preceded by a pre-deformation of 2% simulating the cooking of automotive paints.
    The mechanical characteristics were measured according to the standards NF EN ISO 6892-1, EN 485-1 and ASTM 1876 in the direction perpendicular to the rolling direction. The sample size for the E module measurement was 60 x 10 x 3 mm.
    In addition, the stamping performance of T4 plates was evaluated using the LDH (Limit Dome Height) test.
    The LDH parameter is widely used for assessing the drawability of sheet metal. He has been the subject of numerous publications, including that of R. Thompson, "The LDH test to evaluate sheet metal formability - Final Report of the LDH Committee of the North American Deep Drawing Research Group," SAE conference, Detroit, 1993, SAE Paper No. 930815. This is a drawing test of a blank blocked at the periphery by a ring. The blanking pressure is controlled to prevent slippage in the rod. The blank, dimensions 120 x 160 mm, is biased in a mode close to the plane strain. The punch used is hemispherical.
    Figure 2 shows the dimensions of the tools used to perform this test.
    The lubrication between the punch and the plate is ensured by graphited grease (Shell HDM2 grease). The speed of descent of the punch is 50 mm / min. The value called LDH is the value of the displacement of the punch at break, the limit depth of the stamping. It actually corresponds to the average of three tests, giving a 95% confidence interval on the 0.2 mm measurement.
    Specimens of 120 x 160 mm for which the 160 mm dimension was positioned perpendicular to the rolling direction were used.
    The results of the characterizations are given in Table 4.
    Table 4 - Mechanical Properties of Thin Sheet
    Alloy D exhibits particularly good formability. The intergranular corrosion resistance properties were measured according to ISO 11846. In particular, the average depth and the maximum depth of intergranular corrosion were evaluated. The results are shown in Table 5. The intergranular corrosion test according to ISO 11846 consists in immersing the test pieces for 24 h in a solution of sodium chloride (30 g / l) and hydrochloric acid (10 ml / l). ) at a temperature of 30 ° C (obtained by means of a holding in a drying oven), after stripping with hot soda (5% by mass) and with nitric acid (70% by mass) at ambient temperature. The type and depth of corrosion is determined by a micrographic cross-sectional examination of
    metal. The average depth of corrosion and the maximum depth of corrosion are measured.
    Table 5. Results of intergranular corrosion tests
    Example 3
    An ingot 420 mm thick was cast. The composition of the ingots is given in Table 6.
    Table 6, composition of ingots in% by weight
    The ingot J was heated at 540 ° C for more than one hour and then hot rolled to the thickness of 6.1 mm and then cold rolled to a thickness of 1.5 mm. The thin sheets thus obtained were dissolved at 540 ° C. and then quenched. The sheets were then aged at room temperature to obtain a T4 state. Some sheets also underwent a heat treatment of 20 minutes at 185 ° C preceded by a predeformation of 2% simulating the cooking of automotive paints.
    The mechanical characteristics were measured according to the standards NF EN ISO 6892-1, EN 485-1 and ASTM 1876 in the direction perpendicular to the rolling direction. The sample size for the E module measurement was 60 x 20x1.5 mm. Furthermore, the stamping performance of the plates in the T4 state was evaluated using the LDH (Limit Dome Height) test as described in the previous example.
    The results of the characterizations are given in Table 7.
    Table 7 - Mechanical Properties of Thin Sheet
    The alloy J has a particularly advantageous formability.
    权利要求:
    Claims (10)
    [1" id="c-fr-0001]
    claims
    1. Thin sheet for reinforcing part or bodywork structure of aluminum alloy composition, in% by weight,: Si: 10-14, Mg: 0.05-0.8, Cu: 0-0, 2, Fe: 0-0.5, Mn: 0-0.5, optionally at least one element selected from Na, Ca, Sr, Ba, Yt and Li, the amount of said element, if selected being 0.01 - 0.05 for Na, Ca, Sr, Ba Yt and 0.1 - 0.3 for Li, Sb: 0 - 0.05 Cr: 0-0.1 Ti: 0 - 0.2 other elements <0, 05 each and <0.15 in total, remains aluminum.
    [2" id="c-fr-0002]
    2. Sheet according to claim 1 characterized in that Si: 11 - 13% by weight.
    [3" id="c-fr-0003]
    3. Sheet according to any one of claims 1 to 2 characterized in that Cu: 0.03 - 0.15% by weight.
    [4" id="c-fr-0004]
    4. Sheet according to any one of claims 1 to 3 characterized in that Fe: 0.1 - 0.3% by weight.
    [5" id="c-fr-0005]
    5. Sheet according to any one of claims 1 to 4 characterized in that Mn: 0.05 - 0.2% by weight.
    [6" id="c-fr-0006]
    6. Sheet according to any one of claims 1 to 4 characterized in that Mn: <0.05% by weight.
    [7" id="c-fr-0007]
    7. Sheet according to any one of claims 1 to 6 characterized in that Sr: 0.01 - 0.05% by weight.
    [8" id="c-fr-0008]
    8. Sheet according to any one of claims 1 to 7, whose magnesium content is between 0.3 and 0.6% by weight, having a modulus of elasticity measured according to ASTM 1876 of at least 77 GPa and preferably at least 79 GPa and at least one of the following characteristics, and preferably all of the following characteristics: a yield strength of between 130 and 200 MPa and preferably between 140 and 190 MPa; A% at least 15% and preferably at least 18% elongation at break, A% necking elongation of at least 13% and preferably at least 15%.
    [9" id="c-fr-0009]
    9. Sheet according to any one of claims 1 to 7, whose magnesium content is between 0.1 and 0.3% by weight, having a modulus of elasticity measured according to ASTM 1876 of at least 77 GPa and preferably at least 78 GPa and at least one of the following characteristics, and preferably all of the following characteristics: a yield strength of between 80 and 150 MPa and preferably between 90 and 130 MPa, an elongation at least 1% by weight, preferably at least 20%, and at least 15% by weight and preferably at least 17%.
    [10" id="c-fr-0010]
    10. A method of manufacturing a thin sheet according to any one of claims 1 to 9 comprising the following successive steps: - typically vertical semi-continuous casting a composition plate according to any one of claims 1 to 8 and optionally scalping - optionally homogenization, - heating at a temperature between 400 and 560 ° C - hot rolling of the plate in a strip of thickness between 2 and 12 mm, - optionally cold rolling up to the final thickness, - optionally the solution of the sheet between 500 and 560 ° C for 1 s to 5 min, followed by cooling to a temperature below 200 ° C, - optionally a heat treatment at a temperature of between 40 and 150 ° C for a period of 1 to 15 hours, - aging at room temperature of at least 3 days.
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    同族专利:
    公开号 | 公开日
    CN108368569A|2018-08-03|
    AR106891A1|2018-02-28|
    FR3044326B1|2017-12-01|
    FR3044327A1|2017-06-02|
    FR3044328B1|2021-06-18|
    EP3384060A1|2018-10-10|
    JP2019501287A|2019-01-17|
    US20180347016A1|2018-12-06|
    WO2017093627A1|2017-06-08|
    FR3044327B1|2017-11-24|
    WO2017093627A9|2018-07-05|
    FR3044326A1|2017-06-02|
    KR20180089475A|2018-08-08|
    CA3006346A1|2017-06-08|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    JP2009263720A|2008-04-24|2009-11-12|Nippon Light Metal Co Ltd|Low thermal expansion aluminum alloy sheet material having excellent proof stress, and method for producing the same|
    JPH0239575B2|1983-01-06|1990-09-06|Furukawa Aluminium|
    JPH0239577B2|1983-02-25|1990-09-06|Mitsubishi Aluminium|CHOSOSEIALGOKIN|
    FR2721041B1|1994-06-13|1997-10-10|Pechiney Recherche|Aluminum-silicon alloy sheet intended for mechanical, aeronautical and space construction.|
    JP3548709B2|2000-05-08|2004-07-28|九州三井アルミニウム工業株式会社|Method for producing semi-solid billet of Al alloy for transportation equipment|
    JP5532520B2|2010-09-29|2014-06-25|日本軽金属株式会社|Surface brazing method for aluminum alloy members|
    CN102899539B|2012-11-07|2015-03-18|南京宁铁有色合金科技开发有限公司|High-plasticity aluminum-silicon alloy for die casting and preparation method thereof|
    EP2735621B1|2012-11-21|2015-08-12|Georg Fischer Druckguss GmbH & Co. KG|Aluminium die casting alloy|
    CN103243260B|2013-04-28|2016-06-29|首钢总公司|Deep draw dual phase steel and production method thereof|
    CN104372210B|2014-12-01|2017-11-17|北京科技大学|A kind of automobile using low cost high formability aluminum alloy materials and preparation method thereof|CN109468477B|2018-11-07|2021-03-23|东北轻合金有限责任公司|Production method of aluminum alloy sheet for welding|
    JP2020152956A|2019-03-20|2020-09-24|日本軽金属株式会社|Aluminum alloy and aluminum alloy die-casting material|
    CN112981188A|2020-12-30|2021-06-18|江苏鼎胜新能源材料股份有限公司|High-toughness aluminum material for battery external package|
    法律状态:
    2017-06-27| PLFP| Fee payment|Year of fee payment: 2 |
    2017-09-29| PLSC| Publication of the preliminary search report|Effective date: 20170929 |
    2018-06-26| PLFP| Fee payment|Year of fee payment: 3 |
    2020-06-25| PLFP| Fee payment|Year of fee payment: 5 |
    2021-06-25| PLFP| Fee payment|Year of fee payment: 6 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1561647A|FR3044326B1|2015-12-01|2015-12-01|HIGH-RIGIDITY THIN SHEET FOR AUTOMOTIVE BODYWORK|US15/780,463| US20180347016A1|2015-12-01|2016-11-07|Highly rigid sheet for car body|
    KR1020187018716A| KR20180089475A|2015-12-01|2016-11-07|High rigidity seat for body|
    JP2018528278A| JP2019501287A|2015-12-01|2016-11-07|High rigidity thin plate for automobile body|
    CN201680070602.1A| CN108368569A|2015-12-01|2016-11-07|High rigidity light sheet for vehicle body|
    PCT/FR2016/052878| WO2017093627A1|2015-12-01|2016-11-07|Highly rigid thin sheet metal for car body|
    EP16804833.8A| EP3384060A1|2015-12-01|2016-11-07|Highly rigid thin sheet metal for car body|
    CA3006346A| CA3006346A1|2015-12-01|2016-11-07|Highly rigid thin sheet metal for car body|
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