WO2004106577A1 - Method for producing high strength ultra plastic material - Google Patents
Method for producing high strength ultra plastic material Download PDFInfo
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- WO2004106577A1 WO2004106577A1 PCT/JP2004/007370 JP2004007370W WO2004106577A1 WO 2004106577 A1 WO2004106577 A1 WO 2004106577A1 JP 2004007370 W JP2004007370 W JP 2004007370W WO 2004106577 A1 WO2004106577 A1 WO 2004106577A1
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- Prior art keywords
- metal material
- alloy
- temperature
- strength
- ultrasonic
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- 239000000463 material Substances 0.000 title claims abstract description 49
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 17
- 239000007769 metal material Substances 0.000 claims abstract description 56
- 238000010438 heat treatment Methods 0.000 claims abstract description 41
- 238000013016 damping Methods 0.000 claims abstract description 27
- 238000002844 melting Methods 0.000 claims abstract description 17
- 230000008018 melting Effects 0.000 claims abstract description 17
- 229910000861 Mg alloy Inorganic materials 0.000 claims abstract description 10
- 238000001953 recrystallisation Methods 0.000 claims description 9
- 238000000034 method Methods 0.000 abstract description 38
- 239000013078 crystal Substances 0.000 abstract description 35
- 229910052751 metal Inorganic materials 0.000 abstract description 4
- 239000002184 metal Substances 0.000 abstract description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 20
- 229910045601 alloy Inorganic materials 0.000 description 17
- 239000000956 alloy Substances 0.000 description 17
- 238000005096 rolling process Methods 0.000 description 16
- 229910052742 iron Inorganic materials 0.000 description 11
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 10
- 230000008859 change Effects 0.000 description 10
- 238000010008 shearing Methods 0.000 description 9
- 239000011777 magnesium Substances 0.000 description 8
- 230000003287 optical effect Effects 0.000 description 8
- 230000010287 polarization Effects 0.000 description 8
- 239000004519 grease Substances 0.000 description 7
- 229910001069 Ti alloy Inorganic materials 0.000 description 6
- 229910001297 Zn alloy Inorganic materials 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 6
- NWIPPCMREQXKRU-UHFFFAOYSA-N ethanol nitrate Chemical compound CCO.[O-][N+]([O-])=O NWIPPCMREQXKRU-UHFFFAOYSA-N 0.000 description 6
- 230000007246 mechanism Effects 0.000 description 6
- 230000002093 peripheral effect Effects 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 229910052782 aluminium Inorganic materials 0.000 description 4
- 229910052749 magnesium Inorganic materials 0.000 description 4
- 229920001296 polysiloxane Polymers 0.000 description 4
- 239000000843 powder Substances 0.000 description 4
- 238000003825 pressing Methods 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
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- 238000001125 extrusion Methods 0.000 description 3
- 229910052761 rare earth metal Inorganic materials 0.000 description 3
- 150000002910 rare earth metals Chemical group 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 230000009466 transformation Effects 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 229910000881 Cu alloy Inorganic materials 0.000 description 2
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 2
- 229910000990 Ni alloy Inorganic materials 0.000 description 2
- 229910000691 Re alloy Inorganic materials 0.000 description 2
- 229910001093 Zr alloy Inorganic materials 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 239000012535 impurity Substances 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 239000003960 organic solvent Substances 0.000 description 2
- 238000005185 salting out Methods 0.000 description 2
- 230000000930 thermomechanical effect Effects 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000599 Cr alloy Inorganic materials 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 229910019656 Mg2 Ni Inorganic materials 0.000 description 1
- 229910000914 Mn alloy Inorganic materials 0.000 description 1
- 229910001182 Mo alloy Inorganic materials 0.000 description 1
- 229910000676 Si alloy Inorganic materials 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- QZPSXPBJTPJTSZ-UHFFFAOYSA-N aqua regia Chemical compound Cl.O[N+]([O-])=O QZPSXPBJTPJTSZ-UHFFFAOYSA-N 0.000 description 1
- 239000012300 argon atmosphere Substances 0.000 description 1
- 239000012298 atmosphere Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000002238 attenuated effect Effects 0.000 description 1
- 238000005097 cold rolling Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005238 degreasing Methods 0.000 description 1
- 238000004512 die casting Methods 0.000 description 1
- 235000013399 edible fruits Nutrition 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- HQFCOGRKGVGYBB-UHFFFAOYSA-N ethanol;nitric acid Chemical compound CCO.O[N+]([O-])=O HQFCOGRKGVGYBB-UHFFFAOYSA-N 0.000 description 1
- 235000013305 food Nutrition 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- KHYBPSFKEHXSLX-UHFFFAOYSA-N iminotitanium Chemical compound [Ti]=N KHYBPSFKEHXSLX-UHFFFAOYSA-N 0.000 description 1
- 230000002427 irreversible effect Effects 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 238000004898 kneading Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 229910000734 martensite Inorganic materials 0.000 description 1
- 239000012768 molten material Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 1
- 229910001000 nickel titanium Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 238000011165 process development Methods 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000008707 rearrangement Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 230000003252 repetitive effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
- 230000002195 synergetic effect Effects 0.000 description 1
- 238000010119 thixomolding Methods 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/06—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of magnesium or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F3/00—Changing the physical structure of non-ferrous metals or alloys by special physical methods, e.g. treatment with neutrons
Definitions
- the present invention relates to the refinement of crystal grains of a metal material using ultrasonic waves, and relates to a method for producing a metal material having high-strength superplastic characteristics.
- the general definition of superplasticity is a phenomenon in which the tensile stress of a polycrystalline material shows a high strain dependence of the deformation stress and a huge elongation of several hundred percent or more without local shrinkage.
- a material with equiaxed small crystal grains of 10 ⁇ or less deformed at a temperature of 1/2 or more of the melting point expressed in absolute temperature and a strain rate of ⁇ -4 / s. At times, it is said that a large deformation is developed with a low deformation stress of lOMPa or less.
- Grain refining methods for iron and steel materials and non-ferrous metal materials include a method of adding an element that suppresses the growth of crystal grains, a method of utilizing transformation, precipitation, and recrystallization due to thermomechanical treatment, and a method of strong shearing. (See, for example, JP-A-2003-041331, JP-A-2002-194472, JP-A-2002-105568, and JP-A-2000-271693).
- Magnesium which has a structure, has a drawback that high-quality parts and casings cannot be produced unless molded by die casting or thixomolding, which is difficult for secondary calories due to low stretchability at room temperature. This limitation of the manufacturing method is also a reason for narrowing the applications of magnesium alloys.
- Extrusion and roll-rolling are common methods for metal materials.
- the ECAP method (Equal Channel Angular Pressing method) has recently been studied.
- Extrusion is a method in which a billet or slab is literally extruded from a die having a hole of a predetermined shape, and a direct method of extruding through an orifice of the die is generally used.
- pure magnesium extrudes billets or slabs at a temperature of 350-400 ° C and extrudes it.
- ⁇ Compared to aluminum, it is difficult to balance the billet temperature and extrusion speed.
- Roll rolling is a method in which a metal material is fed in one direction while being pressed by upper and lower rolls.
- the repetitive joining rolling is a method in which a rolled plate is halved in a length direction, subjected to a surface treatment such as degreasing, and then two plates are overlapped and rolled again.
- This method has the characteristic that it can be strongly sheared without changing the plate thickness, but it has a high manufacturing cost and disadvantages.
- Cryogenic rolling is a method of rolling at a temperature of liquid nitrogen that does not recover as much as possible the strain introduced by rolling, and then rapidly heating to form fine recrystallized grains. No fruit has been obtained.
- Different peripheral speed rolling is a method of applying a strong shearing force to the material by changing the peripheral speed of the upper and lower rolls.However, since the rolling is performed without lubrication, the surface condition that is easily subjected to uneven shearing force is roughened. is there.
- Melt rolling is a method of rapidly cooling, for example, by pouring a molten metal in which an additive element is supersaturated into a water-cooled roll, and has the effect of suppressing the grain growth while promoting the generation of recrystallization nuclei.
- metal materials that are easily oxidized are not suitable for mass production because sufficient atmosphere adjustment is required.
- Warm rolling is a method of rolling at a temperature equivalent to the middle point between hot rolling at a temperature higher than the recrystallization temperature and cold rolling at normal temperature.
- an appropriate amount of Zr is added to an A1-Zn-Mg_Cu alloy The effect of some of the alloys has been confirmed, such as obtaining a fine grain structure.
- the ECAP method is a method in which a billet or slab is put into a die having a hole with a certain angle, and a high shear force is applied to the billet or slab by pressing and extruding to obtain a fine grain structure.
- a high shear force is applied to the billet or slab by pressing and extruding to obtain a fine grain structure.
- billets or slabs that have been subjected to strong shearing force are very tough, so secondary processing such as rolling is difficult to improve workability.
- hot rolling is performed, crystal grains grow and do not satisfy sufficient strength, toughness and high ductility at practical levels.
- Either method is a method in which a billet or the like that has been melted is subjected to a strong shearing process, and a very large stress is required for the shearing process, or the initial shape of the metal material cannot be maintained. Disclosure of the invention
- the present invention solves the above-mentioned problems of the prior art, and has a high strength in which the structure of the metal material is fine crystal grain force. It is intended to provide a method for producing a material.
- the metal material is heated at a temperature obtained by multiplying its melting point expressed in absolute temperature by 0.35 to 0.6. The above problem is solved by processing.
- the metal material is attenuated when vibration is applied, and finally the vibration stops.
- the other is internal friction, a mechanism by which vibration energy is converted into heat or strain inside a metal material. Internal friction is also called damping capacity.
- the damping ability is classified into the following four types depending on the difference in vibration energy conversion mechanism. (1) By viscous or plastic flow at the interface between the parent phase and the second phase.
- the dislocation is caused by the detachment from the fixing point by the impurity atom.
- the force is consumed as heat in any of the conversion mechanisms in the category of 4), or accumulated as strain. Since a large strain equal to or greater than mechanical shearing is introduced into the metal material in which the strain is accumulated, the metal material has a melting point expressed in absolute temperature of 0.35 to 0.35. When heat treatment is carried out at a temperature multiplied by 1.6, it is considered that the lattice defects change to a recrystallized structure consisting of equiaxed fine crystal grains in the process of energy release due to rearrangement or mutual annihilation.
- a metal material having a large damping capacity generally means a specific damping capacity (specific damping capacity).
- SDC is 10% or more, and is collectively referred to as high attenuation metal materials.
- pure gold Mg, Ni, and Fe have a large specific damping capacity, and alloys such as Mg alloy, Mn-Cu alloy, Mn-Cu-A1 alloy, Cu-Zn-A1 alloy, Cu-Al_Ni alloy, Fe_Cr alloy (12Cr steel ), Fe_Cr-A1 alloy, Fe_Cr-Mo alloy, Co_Ni alloy, Fe_Cr-Al_Mn alloy, Ni-Ti alloy, Cu_Zn_Al alloy, Al_Zn alloy, intergranular corrosion treatment 18-8 stainless steel, Fe_C_Si alloy (flake graphite-iron) Or, spheroidal graphite (iron rolled iron) has a large specific damping capacity and is called a high damping alloy, a vibration damping alloy or a vibration damping alloy.
- the intrinsic damping capacity is represented by a vibration energy loss rate per cycle of a vibrating object as follows.
- W is the vibrational energy and is the energy lost in one cycle.
- Mg or Mg alloy force is most suitable for applying this method.
- Mg has the largest damping ability among all metallic materials and has a specific damping ability of 60% or more.Therefore, it is easy to accumulate vibration energy as strain, and heat treatment at an appropriate temperature makes it possible to regenerate fine crystal grains. It is possible to have a crystal structure. Mg is relatively low in strength and corrosion resistance.This problem has been solved.A Mg alloy added with Al, Zn, Zr, etc., has a lower damping capacity than Mg, but some of the ultrasonic vibration energy is lost. It accumulates as strain and becomes a recrystallized structure composed of fine crystal grains by the heat treatment due to the synergistic effect with the effect of the added element, and it is possible to achieve both higher strength and superplasticity.
- Mg alloy includes Mg-A1 alloy, Mg-A1-Zn alloy, Mg-Zr alloy, Mg-Zn-Zr alloy, Mg_Mg2 Ni alloy, Mg— RE— Zn alloy (RE is rare earth), Mg— Ag-RE alloys (RE is rare earth), Mg_Y_RE alloys (RE is rare earth), etc. are known as practical alloys.
- Mg-A1 alloy and Mg-A1-Zn Among alloys, Mg_10% Al alloy (A1100), Mg_9% Al_l% Zn alloy (AZ91), Mg_6% ⁇ 1_3. / 0
- the specific damping capacity of ⁇ alloy (AZ63) is 10. less than / o.
- the ultrasonic vibration energy applied to Mg or the Mg alloy is, as described in the above-mentioned vibration energy conversion mechanism (3), the dislocation is detached from the anchoring point by the impurity atom. It is believed that it is consumed or consumed to form deformation twins.
- the metal material to which ultrasonic waves are applied undergoes recrystallization by heat treatment at a temperature obtained by multiplying the melting point expressed in absolute temperature by 0.35 to 0.6. If the temperature is higher than 0.6 multiplied by the melting point expressed in absolute temperature, which is difficult to control because there is energy loss to suppress the growth of recrystallized grains, and if the temperature is lower than 0.35 multiplied by metal, Only the recovery, which is a phenomenon in which the strain inside the material partially disappears, is performed, and no recrystallized grains are generated.
- the recrystallization temperature is a temperature at which the metal structure subjected to cold working is practically completely changed to a structure having new recrystallized grains by a heat treatment for 1 hour in practice. It is a specific value that changes depending on the purity, the degree of internal strain, etc., but tends to converge to a certain temperature as the internal strain increases. That is, in a metal material that has undergone a large internal strain, it is considered that grain growth is suppressed by setting the above temperature range as one guide, and a desired high-strength superplastic material can be easily obtained.
- the shape of the metal material There is no particular limitation on the shape of the metal material.
- a plate material, a rod material, a pipe which is a powder solidified molded product or a molten material, or a molded product which is press-molded into a target shape can be used.
- the powder solidified compact is a powder sintered compact or a solid compact formed by compressive shearing of a powder
- the ingot material is a molded product or a metal material that has been melted and solidified after being pressed or extruded into a desired shape.
- stuffed food Such as stuffed food.
- a method of applying ultrasonic waves to the metal material for example, a method in which a horn connected to an ultrasonic vibrator is brought into close contact with the metal material and ultrasonic waves are applied for a certain period of time is used.
- Grease or the like can be inserted between the horn and the metal material to efficiently transmit vibration from the horn to the metal material.
- grease is difficult to be deteriorated or ignited by vibrations, and safe grease must be used.
- silicone grease can be used.
- the ultrasonic frequency, output and application time must be determined by taking into account the melting point, intrinsic damping capacity, size, etc. of metallic materials, and optimal values must be determined.
- a 200W ultrasonic wave with a frequency of 19KHz is output using a 22mm diameter titanium alloy horn for 5-60 seconds. It is good to apply.
- the metal material to which the ultrasonic wave is applied is heated at the recrystallization temperature for one hour.
- AZ31 is expected to have a recrystallization temperature of 180 230 ° C, and is heated at 230 ° C in vacuum for lh. If it is other than vacuum, it is preferable to heat under an argon atmosphere. When heated in nitrogen, hydrogen or oxygen, it forms compounds with these and deteriorates surface and mechanical properties. It should be noted that any oxidation-resistant metal material may be heated in the air.
- the recrystallized metal material maintains its initial shape, and its crystal grain size becomes 1 / 10-1 / 150 of that before ultrasonic waves were applied.
- the size of the material does not change, and the crystal structure with a crystal grain size of 150-200 / im is an equiaxed crystal structure of 11/15 / m.
- a pure A1 wrought material for industrial use CFIS alloy number 1100
- a test piece of 20 mm X 50 mm X 1.25 mm was cut out with a peripheral blade cutter, and the surface was quickly washed with ethanol.
- an ultrasonic homogenizer as an ultrasonic application means, an appropriate amount of silicone grease was applied to the end face of a horn made of titanium alloy and having a diameter of 22mm, and the above-mentioned industrial pure A1 wrought material test piece was jacked there.
- the operation of applying ultrasonic vibration of 300 W at 19 KHz for 60 seconds was performed three times while pressing.
- the commercial pure Al wrought specimen to which ultrasonic waves were applied was inserted into a vacuum heating furnace and subjected to lh heat treatment at a degree of vacuum of 5 Pa and a heating temperature of 468 K, ie, a heating temperature / melting point of 0.50.
- the tensile strength of the heat-treated industrial pure A1 wrought material was 180 MPa, the elongation at break was 473 K, and the strain rate was 10_4Zs. The tensile strength was 150%, indicating that the superplastic phenomenon had occurred. all right.
- a lOmm X IOmm XI .25mm microstructure observation test piece was cut out, etched with 0.5% aqua regia, and then subjected to simple polarization observation with an optical microscope.
- the crystal grain size was found to be about 15 ⁇ m.
- the crystal grain size before application of ultrasonic waves was 1/10 of 150 xm.
- test piece of 20 mm ⁇ 50 mm ⁇ I.25 mm was cut out from a cold rolled material of industrial pure iron with an outer peripheral cutter, and the surface was quickly washed with ethanol.
- an ultrasonic homogenizer as an ultrasonic application means, an appropriate amount of silicone grease was applied to the end face of a horn made of a titanium alloy and having a diameter of 22 mm, and the above-mentioned industrial pure iron cold-rolled material test piece was jacked there. Ultrasonic vibration of 300 K at 19 KHz was applied for 60 seconds while pressing with.
- test piece of cold rolled industrial pure iron to which ultrasonic waves were applied was inserted into a vacuum heating furnace and subjected to lh heat treatment at a vacuum of 5 Pa and a heating temperature of 923 K, that is, a heating temperature / melting point of 0.51.
- the tensile strength of the heat-treated industrial pure iron cold-rolled material was 700 MPa, and the elongation at break was 923 K and the strain rate was 10_3Zs. all right.
- a 20 mm X 50 mm X 1.25 mm test piece was cut out from AZ31 wrought material with an outer edge cutter, and the surface was quickly washed with ethanol.
- an ultrasonic homogenizer as an ultrasonic application means, an appropriate amount of silicone grease was applied to the end surface of a horn made of a titanium alloy and having a diameter of 22mm, and the above-mentioned AZ31 expanded specimen was pressed with a jack. While applying 200W ultrasonic vibration at 19KHz for 15 seconds
- the AZ31 wrought specimen to which the ultrasonic wave was applied was introduced into a vacuum heating furnace, and subjected to lh heat treatment at a degree of vacuum of 5 Pa and a heating temperature of 503 K, that is, a heating temperature / melting point of 0.54.
- the tensile strength of the heat-treated AZ31 wrought material was 300 MPa, the elongation at break was 503K, and the strain rate was ⁇ -2 / s. The strain rate was 100%, indicating that the superplastic phenomenon occurred.
- the strain rate was 100%, indicating that the superplastic phenomenon occurred.
- the AZ31 wrought specimen with the ultrasonic wave applied was inserted into a vacuum heating furnace and subjected to lh heat treatment at a degree of vacuum of 5 Pa and a heating temperature of 463 K, that is, a heating temperature / melting point of 0.50. A similar operation was performed.
- the tensile strength of the heat-treated AZ31 wrought material was 310 MPa, and the elongation at break was measured at 503 K and the strain rate was ⁇ -2 / s. I understand.
- a lOmm X IOmm XI .25 mm microstructure observation test piece was cut out, etched with a 1% ethanol nitrate solution, and subjected to simple polarization observation with an optical microscope.
- the crystal grain size was about 3 ⁇ m, It was 1/50 of the crystal grain size of 150 ⁇ m before the application of sound waves.
- the tensile strength of the heat-treated AZ31 wrought material was 300 MPa, the elongation at break was 503K, and the strain rate was ⁇ -2 / s. The strain rate was 100%, indicating that the superplastic phenomenon occurred.
- the strain rate was 100%, indicating that the superplastic phenomenon occurred.
- a lOmmXIOmmXI. 25mm microstructure observation test piece was cut out, etched with a 1% ethanol nitrate solution, and then subjected to simple polarization observation with an optical microscope.
- the crystal grain size was found to be about 5 ⁇ m. It was 1/30 of the crystal grain size of 150 ⁇ m before sound wave application.
- test piece of 20 mm ⁇ 50 mm ⁇ 1.25 mm was cut out from AZ31 wrought material with an outer cutter, and the surface was quickly washed with ethanol.
- An ultrasonic homogenizer was used as an ultrasonic application means, and a horn end face made of a titanium alloy and having a diameter of 22mm was installed at a distance of 2cm from an AZ31 wrought material test piece submerged in pure water. Then, ultrasonic vibration of 240 W at 19 KHz was applied for 300 seconds.
- test piece of AZ31 material to which the ultrasonic wave was applied was inserted into a vacuum heating furnace and subjected to lh heat treatment at a vacuum degree of 5 Pa and a heating temperature of 453 K, ie, a heating temperature / melting point of 0.49.
- the tensile strength of the heat-treated AZ31 wrought material was 375MPa, and the elongation at break was 233K when examined at 503K and the strain rate ⁇ ⁇ -2 / s, indicating that the superplastic phenomenon occurred.
- a lOmmXIOmmXI 25mm tissue observation specimen was cut out, etched with a 1% ethanol nitrate solution, and then subjected to simple polarization observation with an optical microscope. As a result, the crystal grain size was about lxm. The crystal grain size before application was 1/150 of 150 zm.
- An ultrasonic homogenizer was used as a means for applying ultrasonic waves, and the horn end face made of a titanium alloy and having a diameter of 22mm was set at a distance of 2cm from an AZ31 wrought material specimen submerged in pure water. Then, ultrasonic vibration of 240 W at 19 KHz was applied for 300 seconds.
- test piece of AZ31 material to which ultrasonic waves were applied was introduced into a vacuum heating furnace, and subjected to lh heat treatment at a vacuum degree of 5 Pa and a heating temperature of 303 K, that is, a heating temperature / melting point of 0.33.
- the tensile strength of the heat-treated AZ31 wrought material was 260 MPa, the elongation at break was 503K, and the strain rate was ⁇ -2 / s.When measured at 50%, it was confirmed that the superplastic phenomenon did not occur. Was done.
- a lOmm X IOmm XI .25mm microstructure observation test piece was cut out, etched with a 1% ethanol nitrate solution, and then subjected to simple polarization observation with an optical microscope.
- the crystal grain size was found to be about 150 ⁇ . There was no change with respect to the crystal grain size of 150 / im before the application of ultrasonic waves.
- the tensile strength of the heat-treated AZ31 wrought material was 280 MPa, the elongation at break was measured at 503 K and the strain rate was ⁇ -2 / s, indicating 80%, confirming that no superplastic phenomenon had occurred.
- the tensile strength of the heat-treated AZ31 wrought material was 280 MPa, the elongation at break was measured at 503 K and the strain rate was ⁇ -2 / s, indicating 80%, confirming that no superplastic phenomenon had occurred.
- a lOmm X IOmm XI. 25mm microstructure observation specimen was cut out, etched with a 1% ethanol nitrate solution, and then subjected to simple polarization observation with an optical microscope.
- the crystal grain size was found to be about 30 ⁇ m. And 15 with a crystal grain size of 150 ⁇ m before the application of ultrasonic waves.
- a large internal strain can be given to a metal material, and a high-strength superplastic material in which the structure of the metal material is composed of fine crystal grains can be easily obtained. Obtainable.
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- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
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Abstract
Description
Claims
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE112004000826T DE112004000826T5 (en) | 2003-05-30 | 2004-05-28 | Method for producing high-strength, superplastic material |
JP2005506503A JPWO2004106577A1 (en) | 2003-05-30 | 2004-05-28 | Manufacturing method of high strength and superplastic material |
AU2004243728A AU2004243728A1 (en) | 2003-05-30 | 2004-05-28 | Method for producing high strength ultra plastic material |
GB0521161A GB2414952B (en) | 2003-05-30 | 2004-05-28 | Method for producing high strength superplastic material |
US10/553,882 US20060231174A1 (en) | 2003-05-30 | 2004-05-28 | Method for producing high-strength superplastic material |
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JP2003-155450 | 2003-05-30 | ||
JP2003155450 | 2003-05-30 |
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WO2004106577A1 true WO2004106577A1 (en) | 2004-12-09 |
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PCT/JP2004/007370 WO2004106577A1 (en) | 2003-05-30 | 2004-05-28 | Method for producing high strength ultra plastic material |
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US (1) | US20060231174A1 (en) |
JP (1) | JPWO2004106577A1 (en) |
CN (1) | CN1795282A (en) |
AU (1) | AU2004243728A1 (en) |
DE (1) | DE112004000826T5 (en) |
GB (1) | GB2414952B (en) |
TW (1) | TW200510553A (en) |
WO (1) | WO2004106577A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2007169674A (en) * | 2005-12-19 | 2007-07-05 | Furukawa Co Ltd | Method for producing superplastic magnesium alloy material |
JP2007169675A (en) * | 2005-12-19 | 2007-07-05 | Furukawa Co Ltd | Method for producing superplastic magnesium alloy material |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102006057762A1 (en) * | 2006-12-07 | 2008-06-19 | Technische Universität Chemnitz | Making screws by adding head to shaft, presses more ductile head onto pre-formed, profiled shaft, to produce closed, interlocking bond between them |
DE102007009996B4 (en) * | 2007-03-01 | 2014-03-27 | Minebea Co., Ltd. | electric motor |
CN102220527B (en) * | 2011-05-27 | 2012-09-12 | 重庆大学 | Method for improving damping performance of extruded Mg-Cu-Mn series alloy |
US9458534B2 (en) | 2013-10-22 | 2016-10-04 | Mo-How Herman Shen | High strain damping method including a face-centered cubic ferromagnetic damping coating, and components having same |
US10023951B2 (en) | 2013-10-22 | 2018-07-17 | Mo-How Herman Shen | Damping method including a face-centered cubic ferromagnetic damping material, and components having same |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5322843A (en) * | 1976-08-13 | 1978-03-02 | Nippon Steel Corp | Method of improving solidification structure of weld zone by use of ultrasonic oscillatory radiation |
JP2000073152A (en) * | 1998-08-28 | 2000-03-07 | Univ Osaka | Production of superfine structure high strength metallic sheet by repeated lap joint rolling |
JP2003113418A (en) * | 2001-10-04 | 2003-04-18 | Nippon Steel Corp | Method for improving fatigue life and long-life metal material |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1209031A (en) * | 1967-01-25 | 1970-10-14 | Pressed Steel Fisher Ltd | A method of refining the structure of alloys |
JP2866917B2 (en) * | 1994-10-05 | 1999-03-08 | 工業技術院長 | Superplasticity Development Method for Ceramic Particle Reinforced Magnesium Matrix Composite by Melt Stirring Method |
-
2004
- 2004-05-21 TW TW093114465A patent/TW200510553A/en unknown
- 2004-05-28 DE DE112004000826T patent/DE112004000826T5/en not_active Ceased
- 2004-05-28 CN CNA2004800144394A patent/CN1795282A/en active Pending
- 2004-05-28 US US10/553,882 patent/US20060231174A1/en not_active Abandoned
- 2004-05-28 WO PCT/JP2004/007370 patent/WO2004106577A1/en active Application Filing
- 2004-05-28 JP JP2005506503A patent/JPWO2004106577A1/en not_active Withdrawn
- 2004-05-28 AU AU2004243728A patent/AU2004243728A1/en not_active Abandoned
- 2004-05-28 GB GB0521161A patent/GB2414952B/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5322843A (en) * | 1976-08-13 | 1978-03-02 | Nippon Steel Corp | Method of improving solidification structure of weld zone by use of ultrasonic oscillatory radiation |
JP2000073152A (en) * | 1998-08-28 | 2000-03-07 | Univ Osaka | Production of superfine structure high strength metallic sheet by repeated lap joint rolling |
JP2003113418A (en) * | 2001-10-04 | 2003-04-18 | Nippon Steel Corp | Method for improving fatigue life and long-life metal material |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2007169674A (en) * | 2005-12-19 | 2007-07-05 | Furukawa Co Ltd | Method for producing superplastic magnesium alloy material |
JP2007169675A (en) * | 2005-12-19 | 2007-07-05 | Furukawa Co Ltd | Method for producing superplastic magnesium alloy material |
Also Published As
Publication number | Publication date |
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AU2004243728A1 (en) | 2004-12-09 |
US20060231174A1 (en) | 2006-10-19 |
JPWO2004106577A1 (en) | 2006-07-20 |
CN1795282A (en) | 2006-06-28 |
DE112004000826T5 (en) | 2006-03-02 |
GB2414952B (en) | 2006-05-31 |
TW200510553A (en) | 2005-03-16 |
GB0521161D0 (en) | 2005-11-23 |
GB2414952A (en) | 2005-12-14 |
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