JP6223670B2 - Aluminum alloy sheet for automobile parts - Google Patents

Description

  The present invention relates to a high-strength aluminum alloy plate for automobile members.

  In recent years, due to consideration for the global environment, social demands for reducing the weight of automobile bodies are increasing. In order to meet such demands, panels (outer panels such as hoods, doors, and roofs, inner panels), bumper force (bumper R / F), and reinforcing materials such as door beams, etc., are partly made of steel, etc. Instead of the steel material, an aluminum alloy material is applied.

  However, in order to reduce the weight of the automobile body, it is necessary to expand the application of the aluminum alloy material to automobile structural members such as frames and pillars that contribute particularly to weight reduction among the automobile members. However, these automobile structural members need to have higher strength than the automobile panel, for example, the required 0.2% proof stress is 350 MPa or more. In this respect, the composition and tempering (solution treatment and quenching) of the JIS to AA6000 series aluminum alloy plates, which are used in the above-mentioned automobile panels, are excellent in formability, strength, corrosion resistance, low alloy composition and recyclability. Control of the treatment, and further, the artificial age hardening treatment, is far from achieving the high strength.

Therefore, it is necessary to use a JIS or AA 7000 series aluminum alloy plate used as the reinforcing material requiring the same high strength for such a high-strength automobile structural member. However, a 7000 series aluminum alloy, which is an Al—Zn—Mg series aluminum alloy, is an alloy that achieves high strength by distributing precipitates MgZn ₂ composed of Zn and Mg at a high density. Therefore, there is a risk of causing stress corrosion cracking (hereinafter referred to as SCC), and in order to prevent this, it is unavoidable that it is over-aged and used at a proof stress of about 300 MPa. The characteristics of are fading.

  For this reason, various composition control of the 7000 series aluminum alloy excellent in both strength and SCC resistance and structure control of precipitates have been conventionally proposed.

As a typical example of composition control, for example, in Patent Document 1, Mg added in excess of Zn and Mg content (stoichiometry ratio of MgZn ₂ ) of a 7000 series aluminum alloy extruded material that forms MgZn ₂ without excess or deficiency. but by utilizing the fact that contributes to high strength by adding Mg to excess over stoichiometric ratio of MgZn _2, to suppress the MgZn ₂ amount, without reducing the SCC resistance, and high strength Yes.

As a representative example of the structure control of precipitates and the like, for example, in Patent Document 2, a 7000-series aluminum alloy extruded material after artificial age hardening treatment is used for a precipitate having a particle diameter of 1 to 15 nm in crystal grains. As a result of observation by (TEM), it is made to exist at a density of 1000 to 10000 / μm ² to reduce the potential difference between the inside of the grain and the grain boundary, thereby improving the SCC resistance.

  In addition to this, although not all can be exemplified, examples of composition control to improve both the strength and SCC resistance of 7000 series aluminum alloy extruded materials and examples of structure control such as precipitates are many practical applications in extruded materials. There are many in proportion to On the other hand, there are very few examples of conventional structure control such as composition control and precipitates in a 7000 series aluminum alloy plate according to the small practical use of the plate.

For example, in Patent Document 3, in a structural material made of a clad plate in which 7000 series aluminum alloy plates are welded together, the diameter of an aging precipitate after artificial age hardening treatment is 50 mm (angstrom) or less in order to improve strength. It has been proposed that a certain amount exists as a spherical shape. However, there is no disclosure about the SCC resistance performance, and there is no corrosion resistance data in the examples.
Further, Patent Document 4 discloses that the crystal precipitates in the crystal grains of the 7000 series aluminum alloy plate after the artificial age hardening treatment are measured with a 400 times optical microscope to obtain a size (equivalent to an equivalent circle diameter in area). Conversion) is 3.0 μm or less, and the average area fraction is 4.5% or less to improve strength and elongation.

  There have been some proposals regarding the control of the plate structure. For example, in Patent Documents 5 and 6, in order to increase the strength and SCC resistance of a 7000 series plate for a structural material, the ingot is forged and rolled repeatedly in a warm working region after being forged. Is fine. This is because, by making the structure fine, a large tilt grain boundary having an orientation difference of 20 ° or more, which causes a potential difference between the grain boundary and the grain boundary, which causes a decrease in SCC resistance, is suppressed. This is to obtain a structure having a low-angle grain boundary of 25 ° or more. However, such warm rolling is repeated because the conventional hot rolling and cold rolling methods cannot obtain a structure in which such a low-angle grain boundary is 25% or more. Yes. Therefore, since the process is greatly different from the conventional method, it is difficult to say that it is a practical method for producing a plate.

  Regarding the control of this structure, although it is an extruded material instead of a 7000 series aluminum alloy plate, in Patent Document 7, in order to improve the warm workability, it is composed of a fibrous structure composed of sub-crystal grains, and the main orientation is There is also a proposal of a texture in which the degree of integration in the Brass orientation, which is the Brass orientation and expressed by ODF (crystal orientation distribution function), is 10 times or more of the random orientation.

JP 2011-144396 A JP 2010-275611 A JP-A-9-125184 JP 2009-144190 A JP 2001-335874 A Japanese Patent Laid-Open No. 2002-241882 JP 2009-114514 A

  As described above, proposals such as composition control of 7000 series aluminum alloy excellent in both strength and SCC resistance and structure control such as precipitates or textures have conventionally been made with special materials such as extruded materials and warm rolling. There are a variety of rolling fields. However, there are few proposals for rolled plates produced by conventional methods, such as hot rolling and cold rolling of the ingot after soaking, except for special rolling that repeats the warm rolling. Is real.

  And, the extruded material is completely different from the rolled plate in its manufacturing process such as a hot working process, and the resulting structure of crystal grains and precipitates is, for example, a fibrous form in which the crystal grains are elongated in the extrusion direction. , The crystal grains are basically different from a rolled plate having equiaxed grains. For this reason, proposals such as composition control in the extruded material and structure control of precipitates can be applied to 7000 series aluminum alloy plates and also to automobile structural members made of this 7000 series aluminum alloy plates. It is unclear whether it is effective in improving both strength and SCC resistance. In other words, unless it is actually confirmed, it does not leave the expected range.

  Therefore, there is still no effective means for the structure control technology excellent in both strength and SCC resistance of the 7000 series aluminum alloy plate produced by the above-mentioned conventional method, and there are many unclear points and room for clarification. is the current situation.

  In view of the above-described problems, an object of the present invention is to provide a 7000 series aluminum alloy plate for automobile members, which is manufactured by the conventional method and is excellent in both strength and SCC resistance.

In order to achieve this object, the gist of the aluminum alloy sheet for automobile members of the present invention is, by mass, Zn: 3.8 to 7.5%, Mg: 0.7 to 3.5%, and the balance being An Al—Zn—Mg-based aluminum alloy plate having a composition of Al and inevitable impurities and having a plate thickness of 1 to 3 mm, an average crystal grain size of 6.0 to 14.5 μm, and an inclination of 5 to 5 mm. The average ratio when calculated as [(total length of 5-15 ° grain boundary) / (full length of 2-180 ° grain boundary)] × 100 of the low-angle grain boundary of 15 ° is 16 to 36%. , And an average when calculated as [(total length of crystal grain boundary of more than 15 ° and 180 ° or less) / (full length of crystal grain boundary of 2-180 °)] × 100 of the large tilt grain boundary exceeding the tilt angle of 15 °. The ratio is 18 to 37%.

  The aluminum alloy sheet referred to in the present invention is a cold-rolled sheet that is hot-rolled and then cold-rolled after soaking the ingot, and is further subjected to tempering such as solution treatment. This refers to the manufactured 7000 series aluminum alloy plate. In other words, it does not include a plate manufactured by a special rolling method such as Patent Documents 5 and 6 in which an ingot is forged and then warm rolling is repeated many times. And such a raw material aluminum alloy plate is processed into a motor vehicle member.

  In the present invention, the structure of the 7000 series aluminum alloy plate manufactured by such a conventional method is not a normal equiaxed recrystallized structure, but a fibrous structure as a processed structure similar to the extruded material. Then, the average grain size is 15 μm or less, the average ratio of small-angle grain boundaries with an inclination angle of 5 to 15 ° is 15% or more, and the average ratio of large-angle grain boundaries with an inclination angle of 15 ° or more is 15 It is defined as an organization that is ~ 50%. By setting it as such a structure | tissue, when distortion | strain enters into a board, it can be set as the structure | tissue which dislocation | distributes uniformly, without concentrating locally. As a result, even a 7000 series aluminum alloy plate manufactured by a conventional method has a high strength such that the 0.2% proof stress is 350 MPa or more, and the elongation is increased to ensure the formability. Moreover, although it is such high intensity | strength, it can be set as what suppressed the fall of SCC resistance.

  Hereinafter, embodiments of the present invention will be specifically described for each requirement.

Aluminum alloy composition:
First, the chemical component composition of the aluminum alloy sheet of the present invention will be described below, including reasons for limiting each element. In addition,% display of content of each element means the mass% altogether.

  The chemical component composition of the aluminum alloy plate of the present invention is determined as an Al—Zn—Mg—Cu based 7000 series aluminum alloy in order to guarantee the characteristics of the automotive member intended for the present invention such as strength and SCC resistance. . From this viewpoint, the chemical composition of the aluminum alloy sheet of the present invention is, by mass%, Zn: 4.0-8.0%, Mg: 0.5-2.0%, with the balance being Al and inevitable impurities. It shall consist of This composition may further optionally include one or two of Cu: 0.05 to 0.6% and Ag: 0.01 to 0.15%, in addition to or in addition to this. Separately, one or more of Mn: 0.05 to 0.3%, Cr: 0.03 to 0.2%, and Zr: 0.03 to 0.3% may be selectively included.

Zn: 3.0-8.0%:
Zn, which is an essential alloying element, forms fine precipitates together with Mg to improve the strength. If the Zn content is less than 3.0% by mass, the strength is insufficient, and if it exceeds 8.0% by mass, the grain boundary precipitate MgZn ₂ increases and the SCC sensitivity becomes sharp. Therefore, the Zn content is in the range of 3.0 to 8.0%, preferably in the range of 5.0 to 7.0%. In order to prevent the Zn content from increasing and the SCC sensitivity from becoming sharp, it is desirable to add Cu or Ag described later.

Mg: 0.5-4.0%
Mg, which is an essential alloy element, forms fine precipitates together with Zn to improve strength and elongation. If the Mg content is less than 0.5%, the strength is insufficient, and if it exceeds 4.0% by mass, the rollability of the plate is lowered and the SCC sensitivity becomes sharp. Therefore, the Mg content is in the range of 0.5 to 4.0%, preferably 0.5 to 1.5%.

One or two of Cu: 0.05 to 0.6% and Ag: 0.01 to 0.15%:
Cu and Ag have the effect of improving the SCC resistance of the Al—Zn—Mg alloy. When one or both of these are contained, the effect of improving SCC resistance is small when the Cu content is less than 0.05% and the Ag content is less than 0.01%. On the other hand, if the Cu content exceeds 0.6%, various properties such as rollability and weldability are reduced. Moreover, even if it contains Ag content exceeding 0.15%, the effect will be saturated and it will become expensive. Therefore, the Cu content is 0.05 to 0.6%, preferably 0.4% or less, and the Ag content is 0.01 to 0.15%.

One or more of Mn: 0.05 to 0.3%, Cr: 0.03 to 0.2%, Zr: 0.03 to 0.3%:
Mn, Cr and Zr contribute to strength improvement by refining the crystal grains of the ingot. When any one, two or three of these are contained, if the content of Mn, Cr, or Zr is less than the lower limit, the content is insufficient, recrystallization is promoted, and SCC resistance is improved. descend. On the other hand, when the contents of Mn, Cr, and Zr exceed the respective upper limits, a coarse crystallized product is formed and the elongation is lowered. Therefore, the ranges are Mn: 0.05 to 0.3%, Cr: 0.03 to 0.2%, and Zr: 0.03 to 0.3%.

Ti, B:
Ti and B are impurities in the rolled plate, but have the effect of refining the crystal grains of the aluminum alloy ingot, so that each content in the range specified by the JIS standard is allowed as a 7000 series alloy. The upper limit of Ti is 0.2%, preferably 0.1%, and the upper limit of B is 0.05% or less, preferably 0.03%.

Other elements:
In addition to these elements, other elements such as Fe and Si are inevitable impurities. As a melting raw material, in addition to pure aluminum ingots, the inclusion of these impurity elements due to the use of aluminum alloy scrap is assumed (allowed), and each content within the range specified by the JIS standard of 7000 series alloys is allowed. . For example, if Fe: 0.5% or less and Si: 0.5% or less, inclusion is permitted without affecting the characteristics of the aluminum alloy rolled sheet according to the present invention.

Organization:
In the 7000 series aluminum alloy sheet structure of the present invention, as a premise, as in the case of a normal 7000 series aluminum alloy sheet, a fine nano-level size precipitate is formed from the composition and the production method according to the conventional method. Many exist in the crystal grains to achieve basic properties such as strength and SCC resistance. This precipitate is an intermetallic compound of Mg and Zn (composition is MgZn ₂ or the like) that is generated in crystal grains, and further contains contained elements such as Cu and Zr according to the composition. It is a finely dispersed phase.

Average grain size and grain boundary ratio:
In addition, the 7000 series aluminum alloy sheet structure of the present invention is a fibrous microfabricated structure with an average crystal grain size of 15 μm or less in order to further enhance the properties such as higher strength and SCC resistance. . Further, in this fibrous finely processed structure, the average ratio of small-angle grain boundaries having an inclination of 5 to 15 ° is 15% or more, and the average ratio of large-angle grain boundaries exceeding 15 ° is 15 to 50%. It is an organization.

  As described above, a 7000 series aluminum alloy manufactured by a conventional method is obtained by forming a fibrous microfabricated structure in which a low-angle grain boundary exists at a certain ratio or more and is mixed with a large-angle grain boundary at a certain ratio. Even in the case of a plate, when the plate is distorted, the strain can be uniformly deformed without locally concentrating the strain. As a result, local breakage can be prevented, high strength such that 0.2% proof stress is 350 MPa or more, and elongation can be increased to ensure moldability. Moreover, although it is such high intensity | strength, it can be set as what suppressed the fall of SCC resistance.

  On the other hand, when these requirements are lacking, when the average crystal grain size exceeds 15 μm, the average proportion of the low-angle grain boundaries is less than 15%, or the average proportion of the large-angle grain boundaries is less than 15%, Higher strength cannot be achieved, elongation is lowered, and moldability is lowered.

  The small-angle grain boundary referred to in the present invention is a grain boundary between crystal grains having a small crystal orientation difference (tilt angle) of 5 to 15 ° among crystal orientations measured by the SEM / EBSP method described later. The large tilt grain boundary referred to in the present invention is a grain boundary between crystal grains having a difference in crystal orientation (tilt angle) of more than 15 ° and 180 ° or less. Here, crystal grain boundaries having an orientation difference of less than 2 to 5 ° are not considered and are not defined in the present invention because the effects and influences on increasing the strength are very small.

  As an average ratio of the low-angle grain boundaries, in the present invention, the total length of the grain boundaries of the measured small-angle grain boundaries (the total length of the grain boundaries of all the small-angle grains measured) was also measured. The ratio of the crystal orientation difference with respect to the total length of the crystal grain boundary of 2 to 180 ° (the total length of the measured crystal grain boundaries of all crystal grains) is defined as the ratio of the small tilt grain boundary with the tilt angle of 5 to 15 °. doing. That is, the ratio (%) of the specified low-angle grain boundaries with an inclination angle of 5 to 15 ° is [(total length of 5-15 ° crystal grain boundaries) / (total length of 2-180 ° crystal grain boundaries)] × 100. The average of these values is 15% or more. From the production limit, the upper limit of the proportion of the low-angle grain boundaries of 5 to 15 ° is about 60%.

  On the other hand, the average ratio of the large tilt grain boundary is also the same as the total crystal grain boundary of the measured large tilt grain boundary (the total length of the measured grain boundaries of all the small tilt grain). The ratio of the orientation difference to the total length of the crystal grain boundary having a difference of 2 to 180 ° (the total length of the measured crystal grain boundaries of all crystal grains) is defined as the ratio of the large tilt grain boundary exceeding the tilt angle of 15 °. That is, the ratio (%) of the specified large tilt grain boundary can be calculated as [(total length of crystal grain boundary of more than 15 ° and 180 ° or less) / (full length of crystal grain boundary of 2-180 °)] × 100. The average of these values is in the range of 15 to 50%.

Measurement of grain size and grain boundary ratio:
Each of these average crystal grain sizes and crystal grain boundaries (small-angle grain boundaries and large-angle grain boundaries) defined in the present invention are all measured by the SEM / EBSP method. The measurement site | part of the structure | tissue of the board in this case is taken as the cross section of this board in the width direction similarly to the measurement part of this normal structure | tissue. And what averaged each measured value of five measurement specimens (5 measurement locations) taken from any location of the cross section in the width direction of this plate, the average crystal grain size defined in the present invention, The average ratio of the low-angle grain boundary and the large-angle grain boundary (crystal grain boundary).

  The SEM / EBSP method is widely used as a texture measurement method, and is applied to a field emission scanning electron microscope (FESEM) in a backscattered electron diffraction image (EBSP: Electron Back Scattering (Scattered) Pattern) system. Is a crystal orientation analysis method. This measurement method has high measurement accuracy because of its high resolution as compared with other texture measurement methods. This method has an advantage that the average crystal grain size and the average ratio of crystal grain boundaries at the same measurement site of the plate can be simultaneously measured with high accuracy. Measurement of the average ratio of crystal grain boundaries and average crystal grain size of an aluminum alloy plate by this SEM / EBSP method has been conventionally performed, for example, in Japanese Patent Application Laid-Open No. 2009-173972, Patent Document 5, Patent Document 6, and the like. In the present invention, this method is also used.

  In these disclosed SEM / EBSP methods, an EBSP is projected onto a screen by irradiating an electron beam onto a sample of an Al alloy plate set in a lens barrel of the FESEM (FE-SEM). This is taken with a high-sensitivity camera and captured as an image on a computer. In the computer, the orientation of the crystal is determined by analyzing this image and comparing it with a pattern obtained by simulation using a known crystal system. Each calculated orientation of the crystal is recorded as a three-dimensional Euler angle together with position coordinates (x, y) and the like. Since this process is automatically performed for all measurement points, tens of thousands to hundreds of thousands of crystal orientation data can be obtained at the end of measurement.

  Thus, the SEM / EBSP method has a wider field of view than the electron diffraction method using a transmission electron microscope, and has an average crystal grain size and an average crystal grain size of hundreds of crystal grains. There is an advantage that information on standard deviation or orientation analysis can be obtained within a few hours. In addition, since the measurement is performed by scanning a specified region at an arbitrary fixed interval instead of measurement for each crystal grain, there is also an advantage that each of the above-described information on the numerous measurement points covering the entire measurement region can be obtained. is there. Details of the crystal orientation analysis method in which the EBSP system is mounted on these FESEMs are described in detail in Kobe Steel Engineering Reports / Vol.52 No.2 (Sep.2002) P66-70 and the like.

  Here, in the case of an aluminum alloy plate, it is usually called Cube orientation, Goss orientation, Brass orientation (hereinafter also referred to as B orientation), Cu orientation (hereinafter also referred to as Copper orientation), S orientation, etc. A texture composed of the orientation factors (crystal grains having these orientations) is formed, and there is a crystal plane corresponding to them. These facts are described in, for example, “Cross Texture” (published by Maruzen Co., Ltd.) edited by Shinichi Nagashima, “Light Metal”, Vol. 43, 1993, P285-293, etc.

The formation of these textures differs depending on the processing and heat treatment methods even in the case of the same crystal system. In the case of a texture of a plate material by rolling, it is expressed by a rolling surface and a rolling direction, the rolling surface is expressed by {ABC}, and the rolling direction is expressed by <DEF> (ABCDEF indicates an integer). Based on this expression, each direction is expressed as follows.
Cube orientation {001} <100>
Goss orientation {011} <100>
Rotated-Goss orientation {011} <011>
Brass orientation (B orientation) {011} <211>
Cu orientation (Copper orientation) {112} <111>
(Or D direction {4411} <11118>
S orientation {123} <634>
B / G direction {011} <511>
B / S orientation {168} <211>
P direction {011} <111>

  Then, the average crystal grain size was calculated by the following formula. Average crystal grain size = (Σx) / n (where n is the number of crystal grains measured and x is the respective crystal grain size).

  In these measurements, a sample having a surface prepared by mechanically polishing the cross-section in the width direction of the cold-rolled sheet after the solution treatment, and then electrolytically polishing following buffing was prepared. Thereafter, the crystal orientation measurement and the crystal grain size measurement by EBSP were performed using FESEM. As the EBSP measurement / analysis system, EBSP: manufactured by TSL (OIM) was used.

(Production method)
The manufacturing method of the 7000 series aluminum alloy rolled sheet in the present invention will be specifically described below.

  In this invention, it can manufacture with the manufacturing method by the normal manufacturing process of a 7000 series aluminum alloy rolled sheet. That is, an aluminum alloy hot-rolled sheet having a thickness of 1.5 to 5.0 mm is manufactured through normal manufacturing processes such as casting (DC casting or continuous casting), homogenization heat treatment, and hot rolling. The At this stage, a product plate may be used. Further, it is further cold-rolled while selectively performing intermediate annealing once or twice before cold rolling or in the middle of cold rolling to obtain a cold plate having a thickness of 3 mm or less. It is good also as a product board of a rolled sheet.

(Dissolution, casting cooling rate)
First, in the melting and casting process, an ordinary molten casting method such as a continuous casting method or a semi-continuous casting method (DC casting method) is appropriately selected for the aluminum alloy melt adjusted within the above-mentioned 7000-based component composition range. Cast.

(Homogenization heat treatment)
Next, the cast aluminum alloy ingot is subjected to a homogenization heat treatment prior to hot rolling. The purpose of this homogenization heat treatment (soaking) is to homogenize the structure, that is, eliminate segregation in crystal grains in the ingot structure. The homogenization heat treatment conditions are suitably selected from a range of homogenization time of 2 hours or more, preferably at a temperature of about 400 to 550 ° C.

(Hot rolling)
In the hot rolling, the hot rolling itself becomes difficult because burning occurs under conditions where the hot rolling start temperature exceeds the solidus temperature. On the other hand, when the hot rolling start temperature is less than 350 ° C., the load during hot rolling becomes too high, and the hot rolling itself becomes difficult. Therefore, the hot rolling start temperature is selected from the range of 350 ° C. to the solidus temperature and hot rolled to obtain a hot rolled sheet having a thickness of about 2 to 7 mm. Annealing (roughening) of the hot-rolled sheet before cold rolling is not necessarily required, but may be performed.

(Cold rolling)
In cold rolling, the hot rolled sheet is rolled to produce a cold rolled sheet (including a coil) having a desired final thickness of about 1 to 3 mm. Intermediate annealing may be performed between cold rolling passes.

(Solution treatment)
After cold rolling, solution treatment is performed as a tempering. The solution treatment is not particularly limited and may be heating and cooling using a normal continuous heat treatment line. However, in order to obtain a sufficient solid solution amount of each element or to refine crystal grains, it is desirable to set a solution treatment temperature of 450 to 550 ° C.

  The heating (temperature increase) rate during the solution treatment is desirably 0.01 ° C./s or more and 100 ° C./s or less on average. If the average heating rate is too small as less than 0.01 ° C./s, coarse crystal grains are formed, and the structure after the solution treatment cannot be made into a fibrous fine structure having an average crystal grain size of 15 μm or less. In addition, it is impossible to obtain a structure in which the average ratio of large tilt grain boundaries exceeding 15 ° is 15 to 50% and the average ratio of small tilt grain boundaries having a tilt angle of 5 to 15 ° is 15% or more. As a result, strength and SCC resistance are reduced. On the other hand, the average heating rate cannot exceed 100 ° C./s due to the limit of the equipment capacity of the solution treatment furnace.

  The average cooling (temperature decrease) rate after the solution treatment is desirably 1 ° C./s or more and 500 ° C./s or less. If the average cooling rate is too low, less than 1 ° C./s, coarse recrystallization occurs, and the structure after the solution treatment cannot be made into a fibrous fine structure having an average crystal grain size of 15 μm or less. In addition, it is impossible to obtain a structure in which the average ratio of large tilt grain boundaries exceeding 15 ° is 15 to 50% and the average ratio of small tilt grain boundaries having a tilt angle of 5 to 15 ° is 15% or more. And the coarse grain boundary precipitate which reduces intensity | strength and a moldability is also formed. As a result, strength and SCC resistance are reduced.

  On the other hand, the average cooling rate cannot exceed 500 ° C./s because of the limit of the equipment capacity of the solution treatment furnace. In order to ensure this cooling rate, for cooling after the solution treatment, forced cooling means and conditions such as air cooling such as a fan, water cooling means such as mist, spray, and immersion are selected and used. Incidentally, the solution treatment is basically only once, but when the room temperature aging is prolonged and the strength of the material is increased, the solution treatment is performed under the above-mentioned preferable conditions in order to ensure formability. It may be applied again, and this excessive room temperature age hardening may be canceled once.

  And the aluminum alloy plate of this invention is shape-processed into a motor vehicle member as a raw material, and is assembled as a motor vehicle member. Further, after being molded into an automobile member, it is subjected to a separate artificial age hardening treatment to obtain an automobile member or an automobile body.

Artificial age hardening treatment:
The 7000 series aluminum alloy plate of the present invention has a desired strength as an automobile member by the artificial age hardening treatment. The artificial age hardening treatment is preferably performed after forming the material 7000 series aluminum alloy plate into an automobile member. This is because the 7000 series aluminum alloy plate after the artificial age hardening treatment has high strength but has low formability, and may not be formed depending on the complexity of the shape of the automobile member.

  The temperature and time conditions of this artificial age hardening treatment are freely determined from the desired strength, the strength of the 7000 series aluminum alloy plate of the material, the progress of room temperature aging, and the like. By the way, exemplifying the conditions of artificial age hardening treatment, an aging treatment at 100 to 150 ° C. is performed for 12 to 36 hours (including an overaging region) in the case of one-stage aging treatment. In the two-stage process, the first-stage heat treatment temperature is in the range of 70 to 100 ° C. for 2 hours or longer, and the second-stage heat treatment temperature is in the range of 100 to 170 ° C. for five hours or longer (over-aged region). Select from).

  The relationship between the mechanical properties such as strength and the SCC resistance was evaluated for various 7000 series aluminum alloy cold-rolled steel structures having the composition shown in Table 1 below. These results are shown in Table 2 below.

  The structure of the cold rolled sheet mainly controlled the average heating rate and the average cooling rate during the solution treatment shown in Table 2. Specifically, in common with each example, a 7000 series aluminum alloy molten metal having each component composition shown in Table 1 below was DC cast to obtain an ingot of 45 mm thickness × 220 mm width × 145 mm length. The ingot was subjected to homogenization heat treatment at 470 ° C. for 4 hours, and then hot-rolled using this temperature as a starting temperature to produce a hot-rolled sheet having a thickness of 5.0 mm. This hot-rolled sheet was cold-rolled without being roughened (annealed) and without intermediate annealing between passes to obtain a cold-rolled sheet having a thickness of 2.0 mm in common.

  This cold-rolled sheet was subjected to a solution treatment of 500 ° C. × 30 seconds in common with each example, but the average heating (temperature increase) rate to this solution treatment temperature and the average cooling (temperature decrease) from this temperature ) The speed was variously adjusted as shown in Table 2. Test pieces were collected from the aluminum alloy plate after the solution treatment, and the structure was examined as follows. The results are shown in Table 2.

(Average ratio of grain boundaries, average grain size)
The measurement of the average crystal grain size and the average ratio of crystal grain boundaries of the test piece after the solution treatment was performed by the measurement method described above for the structure of the cross section in the width direction of the plate.

  And using JEM SEM (JEOL JSM 6500F) equipped with TSL EBSP measurement / analysis system (OIM), measurement of grain boundary ratio (%) and average grain size (μm) in this structure Went. In each example, as described above, this measurement was performed on each of five test pieces taken from arbitrary positions on the cross section in the width direction of the plate, and these measured values were averaged. The measurement area of each test piece is commonly an area of 400 μm in the rolling direction of the cross section parallel to the rolling direction × 100 μm in the plate thickness direction from the outermost layer, and the measurement step interval is also 0.4 μm in common.

  In addition, the artificial age hardening treatment after forming the automobile member was simulated, and the aluminum alloy plate after the solution treatment was subjected to an artificial age hardening treatment under the common conditions of 120 ° C. × 24 hours. Test specimens were collected from arbitrary locations on the aluminum alloy plate thus obtained, and the mechanical properties and corrosion resistance were investigated as follows. These results are also shown in Table 2.

(Mechanical properties)
In each example, a room temperature tensile test in the direction perpendicular to the rolling was performed after the artificial age hardening treatment, and tensile strength (MPa), 0.2% proof stress (MPa), and total elongation (%) were measured. The room temperature tensile test was performed at a room temperature of 20 ° C. based on JIS2241 (1980). The tensile speed was 5 mm / min, and the test was performed at a constant speed until the test piece broke.

(Fine precipitate)
In each example, as a reference, it was observed with a transmission electron microscope having a magnification of 300000 times, and the average number density (pieces / μm ² ) of precipitates having a size of 2.0 to 20 nm in the crystal grains was measured. This observation was performed on five test pieces, and the number density of precipitates having a size of 2.0 to 20 nm in the crystal grains was obtained and averaged (average number density). The number density of precipitates having a size of 20 nm was in the range of 2 to 9 × 10 ⁴ pieces / μm ^{3 on} average. Here, the size of the precipitate was measured in terms of the diameter of a circle having an equivalent area.

(SCC resistance)
In order to evaluate the SCC resistance of the test piece after the artificial age hardening treatment, a stress corrosion cracking test by a chromic acid acceleration method was performed. A 4% strain load was applied to the test piece in the direction perpendicular to the rolling, and after age-hardening treatment at 120 ° C. for 24 hours, the specimen was immersed in a test solution at 90 ° C. for a maximum of 10 hours, and SCC was visually observed. The stress load was determined by generating a tensile stress on the outer surface of the test piece by tightening the bolts and nuts of the jig, and the load strain was measured with a strain gauge adhered to the outer surface. A test solution was prepared by adding 36 g of chromium oxide, 30 g of potassium dichromate and 3 g of sodium chloride (per liter) to distilled water. The case where no SCC occurred was evaluated as ◯, and the case where SCC occurred within 10 hours was evaluated as x.

  As is clear from Tables 1 and 2, each invention example is within the composition range of the aluminum alloy of the present invention, and the cold rolling rate and the average heating rate and the average cooling rate during the solution treatment are produced within the above-described preferable ranges. Has been. As a result, as a structure after the solution treatment, a large-angle particle having an average crystal grain size of 15 μm or less and an average ratio of small-angle grain boundaries with an inclination angle of 5 to 15 ° of 15% or more and an inclination angle of more than 15 °. It has a structure in which the average ratio of the boundaries is 15 to 50%. As a result, the 0.2% yield strength after the artificial aging treatment is 350 MPa or more, preferably 400 MPa or more, and the SCC resistance is also excellent. Here, the total elongation is preferably 13.0% or more for automobile members.

On the other hand, each comparative example is outside the scope of the present invention as shown in Table 1. In Comparative Example 7, Zn falls outside the lower limit. In Comparative Example 8, Mg deviates from the lower limit. In Comparative Example 9, since Cu exceeds the upper limit, a large crack occurred during hot rolling, and the production was interrupted. Comparative Example 10 Zr is Ru out to the upper limit.

  In Comparative Examples 11 and 12, although the alloy composition is within the scope of the present invention as shown in Table 1, the average heating rate and the average cooling rate during the solution treatment are not appropriate, such as after the solution treatment. This structure deviates from the range defined in the present invention and is a normal equiaxed recrystallized structure. That is, the average crystal grain size exceeds 15 μm, the average ratio of small-angle grain boundaries with an inclination angle of 5 to 15 ° is less than 15%, and the average ratio of large-angle grain boundaries with an inclination angle of more than 15 ° is less than 15%. For this reason, the strength is not increased even after the artificial aging treatment.

  The above results support the critical significance of the requirements of the present invention for the aluminum alloy sheet of the present invention to have both high strength, high ductility and SCC resistance.

  As described above, the present invention can provide a 7000 series aluminum alloy plate for automobile members having both strength and stress corrosion cracking resistance. Therefore, the present invention is also suitable for automobile structural members such as frames and pillars that contribute to weight reduction of the vehicle body, and other automobile members.

Claims (3)

Al-mass composition containing Zn: 3.8-7.5%, Mg: 0.7-3.5%, the balance consisting of Al and inevitable impurities, with a plate thickness of 1-3 mm. A Zn—Mg-based aluminum alloy plate having an average crystal grain size of 6.0 to 14.5 μm and a small tilt grain boundary with a tilt angle of 5 to 15 ° [(the total length of a crystal grain boundary of 5 to 15 ° ) / (Total length of 2-180 ° grain boundary)] × 100 of an average ratio of 16 to 36% when calculated as 100 and a tilt angle of more than 15 ° [(over 15 ° to 180 ° According to a conventional method, characterized in that it has a structure with an average ratio of 18 to 37% when calculated as the following (full length of grain boundaries) / (full length of 2-180 ° grain boundaries) × 100 Aluminum alloy plate for automobile parts to be manufactured .   The aluminum for automobile members according to claim 1, wherein the aluminum alloy further contains one or two of Cu: 0.05 to 0.6% and Ag: 0.01 to 0.15% by mass%. Alloy plate.   The aluminum alloy is one or more of Mn: 0.05 to 0.3%, Cr: 0.03 to 0.2%, and Zr: 0.03 to 0.3% in mass%. The aluminum alloy plate for automobile members according to claim 1 or 2, comprising: