JP2009197258A - Molded article by high temperature pressurized gas molding - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide a molded article molded by high temperature pressurized gas molding and a method for producing the molded article by high temperature pressurized gas molding achieving the stable feed of a molded article having excellent corrosion resistance and high strength at high productivity. <P>SOLUTION: An aluminum alloy sheet obtained by adding Mn to an Al-Mg based alloy is, in a state where crystal grain sizes before molding is regulated to <20 μm and the area ratio of cavitation at an elongation of 100% in a tensile test is regulated to ≤1.5%, is heated at 300 to 450°C and is molded under the pressure of 1 to 4 MPa for ≤3 min, thus working strain introduced at a high speed is accumulated, and spot recrystallization occurs. In this way, a molded article having extremely fine crystal grains with the crystal grain size of ≤10 μm can be obtained. <P>COPYRIGHT: (C)2009,JPO&INPIT

Description

  The present invention relates to a high-temperature pressurized gas molded article molded by high-temperature pressurized gas molding and a method for producing the high-temperature pressurized gas molded article.

Superplastic forming is known as a method for forming an aluminum alloy sheet using high-temperature pressurized gas. In general, in superplastic forming of an aluminum alloy sheet, it is necessary to form slowly at a temperature range of 350 ° C. to 550 ° C., a pressure of less than 1 MPa, and a strain rate of about 10 ⁻³ / sec to 10 ⁻⁴ / sec. By forming under such conditions, a superplastic phenomenon appears in the aluminum alloy sheet, and the aluminum alloy sheet is formed by deformation mainly composed of grain boundary sliding.

According to this superplastic forming, an elongation exceeding 150% can be obtained by superplastic deformation. Therefore, it becomes possible to integrally form a complicated shape, and it is used for various applications such as aircraft and automobile parts. However, when it is formed into a complicated shape by this superplastic forming, a large elongation is given locally, and the plate thickness becomes too thin at that portion, resulting in a structurally insufficient strength.
In response to the problem that the good properties of aluminum alloy sheets, which are lightweight and excellent in strength, are impaired, not only material proposals but also proposals from processing technology such as cold preforming Has been made.

In general, there are many examples in which an Al—Mg alloy that is inexpensive and excellent in strength is used for superplastic forming of an aluminum alloy sheet.
Patent Document 1 shows that if an aluminum alloy is preformed in advance in a cold state and then superplastic forming is performed, local thinning can be avoided and an excellent molded product can be obtained in terms of strength. Yes.
Patent Document 2 proposes securing the strength of a molded product by using a chemical component composition in which a specific amount of both Mn and Cu is contained in this Al—Mg-based alloy.

However, the cause of the strength reduction is not only the local thickness reduction, but also cavitation in superplastic forming causes the strength reduction.
That is, in superplastic forming, with a large deformation exceeding 200%, there are cases where the matrix is not filled in the vicinity of the triple point of crystal grain boundaries or crystallized matter, and the cavitation is not only reduced in strength, In applications such as structural materials, it also causes a decrease in fatigue strength.
This cavitation can be suppressed by making the crystal grains finer.

With respect to this cavitation, Patent Document 3 discloses the amount of Fe and Si as the impurities that cause cavitation, and the amount of addition of Cu that suppresses cavitation while improving superplastic forming of an Al-Mg alloy. A method for suppressing cavitation by investigating the physical balance and adding Cu has been proposed.

Further, as described above, in superplastic forming, it is necessary to form slowly in order to develop a superplastic phenomenon, and specifically, a forming time of about 20 minutes to 30 minutes is required. This causes deterioration of productivity in industrial scale production, and development of a processing method capable of forming at a higher forming speed is desired.
In response to such a demand, Patent Document 4 and Patent Document 5 propose a molding technique at a higher molding speed than in the past.

In patent document 4, it is a temperature range of 400 to 510 ° C., 250 PSI (about 1.8 MPa) to 500 PSI (about 3.6 MPa), and it takes 2 to 12 minutes depending on the complexity of the shape.
Temperature range below Patent Document 5 at 0.99 ° C. or higher 450 ° C., at 15 kg / cm ² (about 1.5PMa) ~150kg / cm ² (about 15PMa), be formed in less than 2 minutes has been proposed.

JP-A-7-26342 JP 2004-225114 A Japanese Patent Laid-Open No. 10-259441 JP 2001-71046 A JP 2002-11527 A

As seen in the above Patent Document 1 to Patent Document 5, superplastic forming that does not impair the good properties of the aluminum alloy sheet, which is a lightweight and excellent material, and has good productivity in industrial scale production. Consideration has been made to do this.
However, in actual processing steps, the conventional high-temperature pressurized gas molded product and the manufacturing method of the high-temperature pressurized gas molded product have poor productivity in superplastic forming using an Al-Mg-based aluminum alloy sheet. Has not yet been improved to a satisfactory degree.

Further, due to the complexity of the shape, breakage and cavitation often become a problem in practice, and the suppression of breakage and cavitation when high-speed molding of complex shapes is performed has not yet been fully solved.
Further, as shown in Patent Document 3, even if cavitation can be suppressed by adding Cu, there is a problem of the back surface that the addition of Cu deteriorates the corrosion resistance, and the strength of the molded product is improved. It is not a realistic solution to make it happen.

  Therefore, in such a current situation, the strength of the molded article in the superplastic forming using the Al-Mg-based aluminum alloy sheet is improved, the productivity is improved and the breakage when the high-speed forming of the complex shape is performed is further suppressed. Therefore, it is desired to develop a stable high-speed molding technique that can suppress cavitation without deteriorating corrosion resistance and can achieve further reduction in thickness and weight.

In view of the problems in the prior art described above, the present invention provides a high-temperature pressurized gas molded article and a high-temperature pressurized gas molded article capable of stably supplying a high-strength molded article excellent in corrosion resistance with high productivity. It aims at providing the manufacturing method of.

    As a result of repeated earnest experiments to achieve the above-mentioned problems, the present inventors have determined that a predetermined aluminum alloy sheet heated to a temperature of 300 ° C. to 450 ° C. has a crystal grain size of less than 20 μm and a tensile test. When the cavitation area ratio at an elongation of 100% is adjusted to 1.5% or less and molded within 3 minutes at a pressure of 1 to 4 MPa, processing strain introduced at high speed is accumulated, and in-situ recrystallization occurs. It has been found that a molded article having extremely fine crystal grains having a crystal grain size of 10 μm or less can be obtained.

  That is, the high-temperature pressurized gas molded product of the present invention has Mg 3.0-8.0% ((mass%, the same in the description of the component amount), Cr 0.3% or less (0% is not included), and Zr 0.3%. 1% or more of the following (not including 0%) and V 0.3% or less (not including 0%), and more than 1.0% and not more than 2.0% Mn Then, after the aluminum alloy sheet consisting of Al and inevitable impurities is homogenized, it is hot-rolled and cold-rolled so that the crystal grain size before forming is less than 20 μm, and the cavitation area ratio is 100% elongation in the tensile test. Is adjusted to 1.5% or less, heated to 300 ° C. or higher and 450 ° C. or lower, and molded with a pressurized gas having a pressure of 1 MPa or higher and 4 MPa or lower within 3 minutes.

  In addition, the method for producing a high-temperature pressurized gas molded product of the present invention includes Mg 3.0 to 8.0%, Cr 0.3% or less (not including 0%) and Zr 0.3% or less (not including 0%) and V contains 0.3% or less (0% is not included) and contains 1.0% or more and 2.0% or less of Mn, with the balance being Al and inevitable impurities. The resulting aluminum alloy sheet is subjected to homogenization treatment, hot rolling and cold rolling to adjust the crystal grain size before forming to less than 20 μm and the cavitation area ratio at an elongation of 100% in a tensile test to 1.5% or less. And a step of heating to 300 ° C. to 450 ° C. and molding within 3 minutes with a pressurized gas having a pressure of 1 MPa to 4 MPa.

  It is preferable that the 0.2% yield strength of the high-temperature pressurized gas molded product is 150 MPa or more. Moreover, it is preferable that the crystal grain size of the high-temperature pressurized gas molded product is 10 μm or less.

  According to the high-temperature pressurized gas molded product and the manufacturing method of the high-temperature pressurized gas molded product of the present invention, high-speed molding is possible, productivity is improved, there is no problem of fracture or cavitation, and a stable molded product is guaranteed. The Moreover, since the product molded by the high-temperature pressurized gas molding of the present invention has a very fine crystal structure, a higher strength can be obtained than in the prior art. As a result, it is possible to reduce the thickness and weight of the applied parts, and it is expected to bring about great effects on the economy and the environment, such as cost reduction and energy saving.

The detailed contents of the present invention will be described. First, the reasons for limiting the components of the aluminum alloy sheet used in the present invention will be described.
Mg: Mg refines the recrystallized grains to improve the formability, and has the effect of improving the strength without inhibiting the corrosion resistance and weldability of the material. Here, if the amount of Mg is less than 3.0%, the effect of improving the formability becomes insufficient, and if it exceeds 8.0%, the hot rolling property and the cold rolling property are deteriorated and the production becomes difficult. Therefore, the amount of Mg is set in the range of 3.0 to 8.0%.

Mn: Mn has an effect of making recrystallized grains fine and preventing abnormal coarsening of crystal grains during molding. It also has the effect of improving strength. If Mn is 1.0% or less, these effects are insufficient. On the other hand, if Mn exceeds 2.0%, a coarse intermetallic compound is formed and molding becomes difficult, so Mn exceeds 1.0%. Of 2.0% or less.
Refinement of crystal grains is important for suppressing the occurrence of cavitation.

  Cr, Zr, V: All of these elements have the effect of making the recrystallized grains finer and preventing abnormal coarsening of the grains during molding. Therefore, one or more selected from these elements are added. To do. Further, if any of Cr, Zr, and V exceeds 0.3%, a coarse intermetallic compound is generated and molding becomes difficult. Accordingly, one or more of Cr 0.3% or less (not including 0%) and Zr 0.3% or less (not including 0%) and V 0.3% or less (not including 0%) are included. It was supposed to contain.

Furthermore, in general aluminum alloys, Fe, Si, Cu, Zn, and the like are contained as impurities, but if the amount of Fe as impurities is large, coarse Al—Fe, Al—Fe—S, Al—Fe— Since Mn-based intermetallic compounds are easily crystallized and cavitation increases, Fe is preferably regulated to less than 0.3% as an impurity. If the amount of Si is large, coarse intermetallic compounds such as αAl-Mn (Fe) -Si phase and Mg ₂ Si phase are easily crystallized, and cavitation increases, so Si is less than 0.3% as an impurity. It is preferable to regulate. Moreover, if there is much Cu, not only corrosion resistance will deteriorate but hot rolling will become difficult, Therefore It is preferable to control Cu to less than 0.1%. In addition, if Zn as an impurity is 0.5% or less, the characteristics of the aluminum alloy sheet of the present invention are not particularly impaired.

Further, Be is generally added to prevent oxidation of Mg in the molten metal. Also in this invention, it is desirable to add Be because it forms a dense oxide film on the surface of the molten metal and prevents the mixing of hydrogen, thereby preventing the occurrence of cavitation in the rolled sheet.
Here, cavitation causes a decrease in elongation and also causes deterioration in mechanical properties and corrosion resistance of the molded product. Moreover, Be suppresses the oxidation of Mg on the surface of the rolled sheet and stabilizes the surface.

  Since the molding in the present invention is performed at a high temperature of 300 to 450 ° C., when the amount of Mg is large as in the alloy of the present invention, the surface is easily oxidized during the molding and the surface is easily blackened. Oxidation prevents the oxidation of the plate surface during molding and stabilizes the product surface. If the amount of Be is less than 0.0001% (1 ppm), the above effect is not exhibited, and if it exceeds 0.01% (100 ppm), not only the effect is saturated, but also a problem occurs in terms of toxicity and economy. The amount of Be is in the range of 0.0001 to 0.01%.

  Furthermore, in the production of the aluminum alloy sheet of the present invention, it is usual to add Ti alone or Ti in combination with B or C for refining the ingot structure before or during casting. In this case, if the Ti content exceeds 0.15%, coarse primary crystal particles of TiAl3 are crystallized and adversely affect the formability. Therefore, the Ti content is preferably within the range of 0.15% or less. Further, both B and C are added together with Ti to further promote the refinement and homogenization of crystal grains. However, if the amount of B exceeds 0.05%, TiB2 particles are formed, and the amount of C is 0. If it exceeds 0.05%, graphite is produced, and in any case, the moldability is adversely affected. Therefore, it is preferable that both B and C added together with Ti be in the range of 0.05% or less.

Next, the manufacturing method of the high temperature pressurization gas molded product of this invention is demonstrated.
First, a molten alloy having the composition described above is melted and cast. As the casting method, a semi-continuous casting method (DC casting method) is generally used, but a continuous casting method (for example, roll casting method) can also be used. In addition, before or during casting, Ti as described above may be added to the molten metal alone or together with B or C as an ingot structure refining agent.

  The ingot obtained by the DC casting method is chamfered as necessary, and then the ingot is heated (homogenized) usually at 400 to 560 ° C. for 0.5 to 24 hours. Below 400 ° C., the homogenization effect is insufficient, and above 560 ° C. eutectic melting occurs and cavitation increases. If it is less than 0.5 hours, the homogenizing effect is insufficient, and if it is 24 hours or more, the effect is saturated and uneconomical. This ingot heating may be performed in one stage for both homogenization and preheating before hot rolling, or may be performed in two stages by distinguishing these.

  After the ingot is heated, hot rolling is performed according to a conventional method, and cold rolling is further performed to obtain a required final thickness. In this case, intermediate annealing may be performed once or twice or more between hot rolling and cold rolling or in the middle of cold rolling. The conditions for the intermediate annealing are not particularly limited, but in the case of batch-type intermediate annealing, the temperature is 250 to 450 ° C. × 0.5 to 12 hours, and when continuous annealing is applied, the temperature is 400 to 560 ° C. × 0 to 30 seconds. It is preferable to do. When the batch type is 250 ° C. or lower and the continuous annealing is 400 ° C. or lower, the effect of softening is insufficient, and when the batch type is 450 ° C. or higher, the surface oxide film becomes thick and the rollability and surface quality are deteriorated. At continuous annealing at 560 ° C. or higher, eutectic melting occurs and cavitation increases. When the batch type is 0.5 hours or less, the effect of softening is insufficient, and when the time is 12 hours or more, the effect is saturated, which is uneconomical. Continuous annealing for 30 seconds or more is not preferable because the surface oxide film becomes thick and the rollability and surface quality deteriorate.

  On the other hand, a cast plate obtained by a continuous casting method is wound on a coil with or without hot rolling, and is normally homogenized at 400 to 560 ° C. for 0.5 to 24 hours in the coil state. After the heating, the required final plate thickness is obtained only by cold rolling without performing hot rolling. In this case, intermediate annealing may be performed once or twice or more under the same conditions as described above during the cold rolling.

Here, the rolling rate in the cold rolling before reaching the final plate thickness (that is, in the case of cold rolling to the final plate thickness without intermediate annealing, the entire rolling rate, or one or more intermediate times) In the case of cold rolling to the final sheet thickness with annealing, the cold rolling rate after the final intermediate annealing is particularly preferably 50% or more, and more preferably 70% or more.
If the cold rolling ratio before the final plate thickness is less than 50%, the recrystallized grains become coarse and sufficient characteristics cannot be obtained. If the cold rolling ratio before the final plate thickness is 50% or more, the crystal grain size before forming can be made to be a fine recrystallized structure of less than 20 μm without causing coarsening of recrystallized grains. When the crystal grain size is 20 μm or more, sufficient performance in strength and moldability cannot be obtained.
In order to obtain a recrystallized structure before forming, as a final manufacturing process of the aluminum alloy sheet, the cold rolled sheet may be annealed, but the sheet is heated to 300 ° C. to 450 ° C. for forming. It is preferable to recrystallize.

Next, the molding conditions will be described in detail.
An aluminum alloy plate material is set in a pre-heated pressurized gas forming machine and heated to 300 ° C to 450 ° C. Below 300 ° C., the aluminum alloy sheet cannot be sufficiently recrystallized. Heating above 450 ° C. is not preferable because the recrystallized grains may become coarse. In order to suppress the release of strain and make the crystal grains of the molded product finer, it is desirable that the temperature be less than 450 ° C. Therefore, the molding temperature is set to 300 ° C. to 450 ° C., desirably 380 ° C. or higher and lower than 420 ° C.
The plate can also be heated in advance before being set in the molding machine. By heating the plate in advance, the molding cycle time can be shortened. In that case, when the temperature is lowered during the conveyance of the plate material, heating may be performed in advance at a temperature allowing for the lowered temperature. As the high-pressure gas for molding, N ₂ gas is suitable at a relatively low cost, but argon gas or the like can be used when an inert gas is required. Further, air may be used if a compressor is provided.

The molding pressure is 1 to 4 MPa and the molding time is within 3 minutes.
If the pressure is less than 1 MPa at a molding temperature of 300 ° C. to 450 ° C., it is difficult to complete the molding within 3 minutes. On the other hand, molding at a pressure exceeding 4 MPa may cause breakage. Although the molding time is set to be within 3 minutes, if the molding is performed for a time exceeding 3 minutes, there is a possibility that the crystal grains are partially coarsened. Desirably within 2 minutes.
If the pressure is less than 1 MPa, although depending on the plate thickness, a sufficient strain rate cannot be obtained, and the accumulation of processing strain sufficient to cause in-situ recrystallization will be insufficient. As a result, the crystal grains may remain in the state before molding or may be partially coarsened, and a high-temperature pressurized gas molded product having a high strength targeted by the present invention cannot be obtained.

In the present invention, an aluminum alloy plate material having a cavitation area ratio at an elongation of 100% in a tensile test of 1.5% or less, preferably 1.0% or less is used.
High temperature pressing often involves a large reduction in thickness, and cavitation is often a problem. When the cavitation area ratio is large, there is a risk that the static strength and fatigue strength of the molded product may be deteriorated. From the examination results of the present inventors, it has been found that there is no practical problem if the cavitation area ratio at an elongation of 100%, which is an indication of large deformation, is 1.5% or less. Desirably, it is 1.0% or less.
Here, the cavitation area ratio is to specifically measure the amount of cavitation generated in the material by polishing the cross section of the molded plate material and observing it with an image analyzer.
The measurement of the cavitation area ratio at an elongation of 100% is to measure a plate material (molded product) in which the plate thickness of the formed plate material is ½ the thickness of the base plate.

The high-temperature pressurized gas molded article of the present invention is characterized by having a strength of 150 MP or more with a 0.2% proof stress.
It is generally known that the strength is improved by making the crystal grains fine. In the aluminum alloy sheet having the composition of the present invention, 150 MP or more can be achieved with a 0.2% proof stress by setting the crystal grain size to 10 μm or less. For this purpose, all conditions of the alloy composition specified in the present invention, a forming temperature of 300 ° C. to 450 ° C., a forming pressure of 1 to 4 MPa, a forming time of 3 minutes or less, and a crystal grain size of 10 μm or less must be satisfied. When the 0.2% proof stress exceeds 150 MPa, for example, it is possible to reduce the thickness and weight, and it is expected to bring about great effects on the economy and the environment such as cost reduction and energy saving.

[Example]
Eleven kinds of alloys having the component compositions shown in Table 1 were cast by a DC casting method according to a conventional method.
Alloy No. 1 to Alloy No. 8 are alloys that conform to the component ranges defined in the present invention, and Alloy No. 9 to Alloy No. 11 are alloys that deviate from the component ranges defined in the present invention.
After chamfering each ingot, homogenization treatment was performed at 530 ° C. for 10 hours. Next, it heated to 500 degreeC and hot-rolled and obtained the hot-rolled sheet of 6 mm in thickness. Thereafter, it was cold-rolled to finish a plate thickness of 1.5 mm. For some products, intermediate annealing was performed during cold rolling. The intermediate annealing was batch annealing at 390 ° C. × 2 hours.

In the molding experiment, square tube molding of 350 mm × 350 mm and height 80 mm was performed by a pressure molding method using N ₂ gas. Table 2 shows the molding conditions. The molding time was set to 30 sec, and the holding time after the pressure increase was added to form the molding time. A sample was cut out from the vicinity of the center of the rectangular tube forming, and the crystal grain size after forming was measured by observing the microstructure of the cross section perpendicular to the rolling direction. The 0.2% proof stress was measured by a tensile test parallel to the rolling.
For the crystal grains before molding, the crystal grain size was measured by observing the microstructure of a sample separately heated to the molding temperature. Further, a tensile test was conducted at a temperature of 350 ° C. and a strain rate of 1 × 10 ⁻² / sec, and the cavitation area ratio at an elongation of 100% was measured.

  The present invention example of production number 1, production number 2, production number 3, production number 4 and the comparative example of production number 5 to production number 8 were produced using the present invention alloy number 1. Further, production number 9 as a comparative example was produced using alloy number 4 of the present invention example.

  In addition, the present invention example of production number 1 and production number 2 and the comparative example of production number 5 and production number 7 to production number 9 have a molding time of 100 sec using a pressurized gas at a pressure of 3 MPa, while the present invention of production number 3 In the example, the molding time is set to 80 sec with a pressurized gas at a pressure of 4 MPa, and in the example of the present invention of production number 4, the molding time is set to 150 sec with a pressurized gas at a pressure of 3 MPa. It was molded under conditions suitable for the conditions to be molded within.

  Furthermore, in the present invention example of production number 1, production number 2, production number 3, production number 4 and the comparative example of production number 8 and production number 9, the molding temperature is set to a temperature range of 320 ° C. to 420 ° C., and the temperature is 300 ° C. or more. Molding was performed under conditions suitable for heating to 450 ° C. or lower.

Further, in the present invention examples of production number 1, production number 2, production number 3 and production number 4, the crystal grain size before molding is less than 8 μm, the crystal grain size after molding is 4 to 7 μm, and the crystal grain size before molding Is less than 20 μm and the crystal grain size after molding is 10 μm or less.
Furthermore, in the present invention examples of production number 1, production number 2, production number 3, and production number 4, the molded product has a 0.2% proof stress of 155 to 190 MPa and a 0.2% proof stress of 150 MPa or more. .
In addition, in the inventive example of production number 1, production number 2, production number 3, production number 4 and comparative example of production number 7, the cavitation area ratio at an elongation of 100% in the tensile test is 0.5 to 0.7%. Yes, to meet the condition of 1.5% or less.

  As described above, the present invention examples of production number 1, production number 2, production number 3, and production number 4 are examples that satisfy all the conditions defined in the present invention, and showed good moldability and molded product strength. .

  However, the production number 5 is 520 ° C., which exceeds the provision of the present invention, and molding is possible, but the crystal grain size after molding is 12 μm, which exceeds the provision of the present invention of 10 μm or less. As a result, the 0.2% yield strength after molding was 145 MPa which did not satisfy the condition of 150 MPa or more.

The production number 6 is a 3.0% plate material in which the cavitation area ratio of the aluminum alloy plate material before forming exceeds 1.5%, and the forming temperature is set to 520 ° C. like the production number 5 and, unlike the production number 5, the pressure is 1 MPa or more. The molding pressure was 0.85 MPa which did not reach the condition of molding with the pressurized gas, and the molding time was extended to 300 seconds exceeding 3 minutes, thereby allowing molding.
However, the crystal grain diameter after processing exceeded 10 μm and was slightly large as 20 μm as in the case of production number 5, and the 0.2% proof stress was 138 MPa which is 150 MPa or less.

Production number 7 did not reach 300 ° C. and was too low at 280 ° C., so that sufficient deformability could not be obtained, and fracture occurred during the molding.
In production numbers 8 and 9, the cavitation area ratio of the aluminum alloy sheet material before forming exceeded 1.5%, production number 8 was 2.3%, and production number 9 was 2.1%. Although such an aluminum alloy sheet was subjected to intermediate annealing in the middle of cold rolling, the cold rolling rate after annealing was less than 50%, so there was little accumulation of processing strain before recrystallization, and the crystal grain size before processing However, in the production number 8, it was 30 μm, and in the production number 9, it was 27 μm. The crystal grain size after molding of production number 8 was 15 μm exceeding the regulation of the present invention of 10 μm or less, and as a result, the 0.2% proof stress after molding was 143 MPa which did not satisfy the condition of 150 MPa or more. In addition, the crystal grain size after molding of production number 9 was 12 μm exceeding the provision of the present invention of 10 μm or less, and as a result, the 0.2% proof stress after molding was 145 MPa which did not satisfy the condition of 150 MPa or more.

The production numbers 10 to 19 were molded under the same conditions that met the conditions of the present invention by heating to a temperature of 360 ° C. and using a pressurized gas with a pressure of 3 MPa for a molding time of 100 sec.
Among them, production number 10 to production number 16, which are examples of the present invention, production number 10 is alloy number 2, production number 11 is alloy number 3, production number 12 is alloy number 4, production number 13 is alloy number 5, production No. 14 was manufactured using Alloy No. 6, Manufacturing No. 15 was manufactured using Alloy No. 7, and Manufacturing No. 16 was manufactured using Alloy No. 8, both of which were manufactured using alloys corresponding to the examples of the present invention. The strength of the molded product was shown.

  On the other hand, production number 17 uses alloy number 9 which is 0.50% which does not reach the condition that the Mn addition amount exceeds 1.0% and is not more than 2.0%. Cr is 0.3% or less and Zr is 0.3% or less, which is 0.70% which does not reach the condition that the addition amount exceeds 1.0% and is 2.0% or less, and further suppresses the coarsening of crystal grains during forming. , V 0.3% or less (none of which includes 0%), alloy number 10 containing none of Cr, Zr, and V was used, contrary to the condition of containing one or more of V 0.3% and below. Exceeding the condition that the crystal grain size is not more than 10 μm, the crystal grain size reaches 15 μm for the production number 17 and 16 μm for the production number 18 and the crystal grain size after the molding is not sufficiently refined. The condition that the 2% proof stress is 150 MPa or more is not satisfied.

  Production number 19 is Fe 0.3% or less as one of Cr 0.3% or less, Zr 0.3% or less, and V 0.3% or less (both not including 0%) that suppress the coarsening of crystal grains during molding. Since Alloy No. 11 having an Fe content of 0.35% was used beyond the condition of 3% or less, fracture occurred during the molding due to the coarse crystallized product generated during casting. Further, cavitation occurred around the crystallized product, and the condition that the cavitation area ratio was 1.5% or less was not satisfied, and the cavitation area ratio was 3.2%. For this reason, sufficient deformability was not obtained, and it broke in the middle of molding.

Claims (6)

Mg3.0-8.0% (mass%, the same in the description of component amounts below), containing 1.0% to 2.0% Mn, Cr0.3% or less (0% not included) ) And Zr 0.3% or less (not including 0%) and V0.3% or less (not including 0%), and the balance is aluminum composed of Al and inevitable impurities Cavitation at 100% elongation under conditions of homogenization treatment, hot rolling and cold rolling, crystal grain size before forming less than 20 μm, temperature of 350 ° C., strain rate of 1 × 10 ⁻² / sec The aluminum alloy plate prepared to have an area ratio of 1.5% or less is heated to 300 ° C. or higher and 450 ° C. or lower and is molded within 3 minutes by a pressurized gas having a pressure of 1 MPa or higher and 4 MPa or lower. High temperature pressurized gas Form product.   The high-temperature pressurized gas molded article according to claim 1, wherein the 0.2% proof stress is 150 MPa or more.   The high-temperature pressurized gas molded article according to claim 1 or 2, wherein the crystal grain size of the molded article is 10 µm or less. Mg 3.0-8.0%, 2.0% or less of Mn, Cr 0.3% or less (not including 0%) and Zr 0.3% or less (not including 0%) and V 0.3% An aluminum alloy sheet containing one or more of the following (not including 0%) and more than 1.0% and the balance being Al and inevitable impurities, hot rolling after homogenization treatment, Prepared so that the cavitation area ratio at 100% elongation is 1.5% or less under conditions of cold rolling and forming a crystal grain size of less than 20 μm, a temperature of 350 ° C., and a strain rate of 1 × 10 ⁻² / sec. And a step of heating to 300 ° C. or higher and 450 ° C. or lower and molding with a pressurized gas having a pressure of 1 MPa or higher and 4 MPa or lower within 3 minutes.   The method for producing a high-temperature pressurized gas molded article according to claim 4, wherein the 0.2% yield strength of the obtained high-temperature pressurized gas molded article is 150 MPa or more. The method for producing a high-temperature pressurized gas molded article according to claim 4 or 5, wherein the crystal grain size of the obtained high-temperature pressurized gas molded article is 10 µm or less.