US20160153075A1 - Magnesium alloy - Google Patents
Magnesium alloy Download PDFInfo
- Publication number
- US20160153075A1 US20160153075A1 US14/882,433 US201514882433A US2016153075A1 US 20160153075 A1 US20160153075 A1 US 20160153075A1 US 201514882433 A US201514882433 A US 201514882433A US 2016153075 A1 US2016153075 A1 US 2016153075A1
- Authority
- US
- United States
- Prior art keywords
- magnesium alloy
- solidus
- liquidus
- magnesium
- temperature range
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 229910000861 Mg alloy Inorganic materials 0.000 title claims abstract description 54
- 239000011777 magnesium Substances 0.000 claims abstract description 16
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims abstract description 10
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 10
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract description 9
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 9
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 9
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 9
- 239000011575 calcium Substances 0.000 claims description 9
- 230000005484 gravity Effects 0.000 claims description 9
- 239000011572 manganese Substances 0.000 claims description 8
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 claims description 5
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 5
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 5
- 229910052791 calcium Inorganic materials 0.000 claims description 5
- 229910052710 silicon Inorganic materials 0.000 claims description 5
- 239000010703 silicon Substances 0.000 claims description 5
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 4
- 229910052748 manganese Inorganic materials 0.000 claims description 4
- JBQYATWDVHIOAR-UHFFFAOYSA-N tellanylidenegermanium Chemical compound [Te]=[Ge] JBQYATWDVHIOAR-UHFFFAOYSA-N 0.000 claims description 4
- 230000000052 comparative effect Effects 0.000 description 12
- 238000000034 method Methods 0.000 description 9
- 238000010116 semi-solid metal casting Methods 0.000 description 9
- 229910045601 alloy Inorganic materials 0.000 description 7
- 239000000956 alloy Substances 0.000 description 7
- 238000005266 casting Methods 0.000 description 5
- 239000001989 lithium alloy Substances 0.000 description 4
- 239000011701 zinc Substances 0.000 description 4
- 229910000733 Li alloy Inorganic materials 0.000 description 3
- 238000001938 differential scanning calorimetry curve Methods 0.000 description 3
- 229910052725 zinc Inorganic materials 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 239000002075 main ingredient Substances 0.000 description 2
- DHKVCYCWBUNNQH-UHFFFAOYSA-N 2-[5-[2-(2,3-dihydro-1H-inden-2-ylamino)pyrimidin-5-yl]-1,3,4-oxadiazol-2-yl]-1-(1,4,5,7-tetrahydropyrazolo[3,4-c]pyridin-6-yl)ethanone Chemical compound C1C(CC2=CC=CC=C12)NC1=NC=C(C=N1)C1=NN=C(O1)CC(=O)N1CC2=C(CC1)C=NN2 DHKVCYCWBUNNQH-UHFFFAOYSA-N 0.000 description 1
- 229910019064 Mg-Si Inorganic materials 0.000 description 1
- 229910019400 Mg—Li Inorganic materials 0.000 description 1
- 229910019406 Mg—Si Inorganic materials 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000000113 differential scanning calorimetry Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- GCICAPWZNUIIDV-UHFFFAOYSA-N lithium magnesium Chemical compound [Li].[Mg] GCICAPWZNUIIDV-UHFFFAOYSA-N 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000005058 metal casting Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
- C22C23/02—Alloys based on magnesium with aluminium as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
Definitions
- This disclosure relates in general to an alloy, and more particularly to a magnesium alloy.
- Semi-solid metal casting is one of the casting technologies. In comparison to the conventional casting technology, the semi-solid metal casting process provides smaller grains and superior mechanical properties.
- One of the prerequisites of the semi-solid metal casting process is that the temperature range between the solidus and the liquidus of the metal/alloy used in the semi-solid metal casting process must be large enough. That is, a temperature range from the temperature at which the alloy starts to melt to the temperature at which the alloy completely melts, i.e., the solid-liquid co-existence region, must large enough for the control easiness of the casting temperature. As such, casting pieces with complicated shapes and excellent mechanical properties can be produced.
- Magnesium alloys have been widely used due to the feature of lightweight.
- Magnesium lithium alloy (Mg—Li alloy) is the lightest among the commonly used magnesium alloys.
- LZ91 Mg-9% Li-1% Zn
- AZ91 Mg-9% Al-1% Zn
- the temperature range between the solidus and the liquidus of M—Li alloy is small.
- the temperature range between the solidus and the liquidus of the Mg-6 wt % Li alloy is only 4° C. Such alloy is not suitable to be used in the semi-solid metal casting process.
- the disclosure is directed to a magnesium alloy.
- the temperature range between a solidus and a liquidus of the magnesium alloy is expanded through the addition of several kinds of elements.
- the magnesium alloy is suitable to be used in a semi-solid metal casting process.
- the magnesium alloy has a feature of lightweight.
- the magnesium alloy includes magnesium (Mg), 6-12 wt % of lithium (Li) and 1-10 wt % of aluminum (Al).
- a temperature range between a solidus and a liquidus of the magnesium alloy is equal to or larger than 50° C.
- the magnesium alloy includes magnesium (Mg), 6-12 wt % of lithium (Li), 1-10 wt % of aluminum (Al), 0.2-3 wt % of zinc (Zn), 0.3 wt % of manganese (Mn), 0.2 wt % of silicon (Si), 1.0 wt % of calcium (Ca) and 1.0 wt % of tin (Sn).
- FIG. 1 shows a differential scanning calorimetry (DSC, SDT Q600 V20.9 Build 20) curve of one example of the disclosure.
- FIG. 2 shows a DSC curve of one example of the disclosure.
- FIG. 3 shows a characteristic collection of examples and comparative examples of the present invention.
- the disclosure is directed to a magnesium alloy.
- the temperature range between a solidus and a liquidus of the magnesium alloy can be adjusted through the addition of several kinds of elements.
- the magnesium alloy includes magnesium (Mg), 6 to 12 wt % of lithium (Li) and 1 to 10 wt % of aluminum (Al).
- a temperature range between the solidus and the liquidus of the magnesium alloy is equal to or larger than 50° C. Since the magnesium alloy has a larger temperature range between the solidus and the liquidus, the magnesium alloy is suitable to be used in a semi-solid metal casting process.
- the temperature range between the solidus and the liquidus of the magnesium alloy is equal to or larger than 95° C.
- the magnesium alloy has a specific gravity smaller than 1.65. In general, a metal casting piece with a smaller density will have a larger strength-to-weight ratio (the ratio of strength to density), and is suitable to be used in a mobile device.
- Magnesium is the main ingredient of said magnesium alloy. That is, the magnesium alloy is mainly formed of magnesium apart from other disclosed ingredients. Since magnesium is the main ingredient, the magnesium alloy has the feature of lightweight.
- the addition of lithium reduces the density of the magnesium alloy to be smaller than 1.65 g/cm 3 but at the same time reduces the temperature range between the solidus and the liquidus of the magnesium alloy. In general, when 1 wt % of lithium is added to the magnesium alloy, the liquidus will drop by about 10° C. but the solidus will drop by only about 5° C., therefore the temperature range between the solidus and the liquidus will become smaller.
- the temperature range between the solidus and the liquidus of the magnesium alloy will expand, but the density of the magnesium will slightly increase.
- the magnesium alloy can include other ingredients.
- zinc (Zn) can be added to the magnesium alloy to enhance its corrosion resistance and reduce its melting point.
- Mn manganese
- Si silicon
- the heat released by the Mg—Si compound improves the casting property of the magnesium alloy.
- a small amount of calcium (Ca) can be added to the magnesium alloy to prevent combustion during the semi-solid metal casting process.
- a small amount of tin (Sn) can be added to the magnesium alloy to enhance the strength of the alloy at a high temperature.
- the magnesium alloy can further include 0.2 to 3 wt % of zinc, ⁇ 3 wt % of manganese, ⁇ 2 wt % of silicon, ⁇ 1.0 wt % of calcium and ⁇ 1.0 wt % of tin.
- FIG. 1 shows a DSC curve of Example 4.
- FIG. 2 shows a DSC curve of Example 5.
- the temperature range between the solidus and the liquidus is equal to or larger than 50° C. in both cases.
- the temperature range between the solidus and the liquidus in Example 5 is even equal to or larger than 95° C.
- the specific gravity (SG) and the temperature range between the solidus and the liquidus (S-L range) of the examples and the comparative examples are shown in blocks 061 to 0101, 0121, 181, 191, 661, 671, 761, 771, 861 and 881 of FIG. 3 .
- each of the example according to this disclosure provides a larger temperature range between the solidus and the liquidus.
- each of the examples according to this disclosure provides a specific gravity 1.65, which is lower than 1.8, the specific gravity of a typical magnesium alloy.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Continuous Casting (AREA)
- Manufacture And Refinement Of Metals (AREA)
Abstract
Description
- This application claims the benefit of Taiwan application Serial No. 103141813, filed on Dec. 2, 2014, the subject matter of which is incorporated herein by reference.
- This disclosure relates in general to an alloy, and more particularly to a magnesium alloy.
- Semi-solid metal casting is one of the casting technologies. In comparison to the conventional casting technology, the semi-solid metal casting process provides smaller grains and superior mechanical properties. One of the prerequisites of the semi-solid metal casting process is that the temperature range between the solidus and the liquidus of the metal/alloy used in the semi-solid metal casting process must be large enough. That is, a temperature range from the temperature at which the alloy starts to melt to the temperature at which the alloy completely melts, i.e., the solid-liquid co-existence region, must large enough for the control easiness of the casting temperature. As such, casting pieces with complicated shapes and excellent mechanical properties can be produced.
- Magnesium alloys have been widely used due to the feature of lightweight. Magnesium lithium alloy (Mg—Li alloy) is the lightest among the commonly used magnesium alloys. For example, LZ91 (Mg-9% Li-1% Zn) has a specific gravity only about 1.5, which is much lower than 1.81, the specific gravity of the magnesium alloy AZ91 (Mg-9% Al-1% Zn) currently used for commercial purpose. However, the temperature range between the solidus and the liquidus of M—Li alloy is small. For example, the temperature range between the solidus and the liquidus of the Mg-6 wt % Li alloy is only 4° C. Such alloy is not suitable to be used in the semi-solid metal casting process.
- The disclosure is directed to a magnesium alloy. The temperature range between a solidus and a liquidus of the magnesium alloy is expanded through the addition of several kinds of elements. As such, the magnesium alloy is suitable to be used in a semi-solid metal casting process. Further, the magnesium alloy has a feature of lightweight.
- According to some embodiments of the disclosure, the magnesium alloy includes magnesium (Mg), 6-12 wt % of lithium (Li) and 1-10 wt % of aluminum (Al). A temperature range between a solidus and a liquidus of the magnesium alloy is equal to or larger than 50° C.
- According to some embodiments of the disclosure, the magnesium alloy includes magnesium (Mg), 6-12 wt % of lithium (Li), 1-10 wt % of aluminum (Al), 0.2-3 wt % of zinc (Zn), 0.3 wt % of manganese (Mn), 0.2 wt % of silicon (Si), 1.0 wt % of calcium (Ca) and 1.0 wt % of tin (Sn).
-
FIG. 1 shows a differential scanning calorimetry (DSC, SDT Q600 V20.9 Build 20) curve of one example of the disclosure. -
FIG. 2 shows a DSC curve of one example of the disclosure. -
FIG. 3 shows a characteristic collection of examples and comparative examples of the present invention. - In the following detailed description, for purposes of explanation, numerous specific details are set forth in order to provide a thorough understanding of the disclosed embodiments. It will be apparent, however, that one or more embodiments may be practiced without these specific details. In other instances, well-known structures and devices are schematically shown in order to simplify the drawing.
- The disclosure is directed to a magnesium alloy. The temperature range between a solidus and a liquidus of the magnesium alloy can be adjusted through the addition of several kinds of elements. The magnesium alloy includes magnesium (Mg), 6 to 12 wt % of lithium (Li) and 1 to 10 wt % of aluminum (Al). A temperature range between the solidus and the liquidus of the magnesium alloy is equal to or larger than 50° C. Since the magnesium alloy has a larger temperature range between the solidus and the liquidus, the magnesium alloy is suitable to be used in a semi-solid metal casting process. In a preferred embodiment, the temperature range between the solidus and the liquidus of the magnesium alloy is equal to or larger than 95° C. In some embodiments, the magnesium alloy has a specific gravity smaller than 1.65. In general, a metal casting piece with a smaller density will have a larger strength-to-weight ratio (the ratio of strength to density), and is suitable to be used in a mobile device.
- Magnesium is the main ingredient of said magnesium alloy. That is, the magnesium alloy is mainly formed of magnesium apart from other disclosed ingredients. Since magnesium is the main ingredient, the magnesium alloy has the feature of lightweight. The addition of lithium reduces the density of the magnesium alloy to be smaller than 1.65 g/cm3 but at the same time reduces the temperature range between the solidus and the liquidus of the magnesium alloy. In general, when 1 wt % of lithium is added to the magnesium alloy, the liquidus will drop by about 10° C. but the solidus will drop by only about 5° C., therefore the temperature range between the solidus and the liquidus will become smaller. When aluminum is added to the magnesium alloy, the temperature range between the solidus and the liquidus of the magnesium alloy will expand, but the density of the magnesium will slightly increase. In general, when 1 wt % of aluminum is added to the magnesium alloy, the liquidus will drop by about 2° C., but the solidus will drop be about 10° C., therefore the temperature range between the solidus and the liquidus of the magnesium alloy will expand. By adjusting the ratio between lithium and aluminum, a larger temperature range between the solidus and the liquidus and a smaller specific gravity can be achieved.
- The magnesium alloy can include other ingredients. For example, zinc (Zn) can be added to the magnesium alloy to enhance its corrosion resistance and reduce its melting point. A small amount of manganese (Mn) can be added to the magnesium alloy to enhance its strength and corrosion resistance. A small amount of silicon (Si) can be added to the magnesium alloy to enhance its strength. Moreover, during the solidification process, the heat released by the Mg—Si compound improves the casting property of the magnesium alloy. A small amount of calcium (Ca) can be added to the magnesium alloy to prevent combustion during the semi-solid metal casting process. A small amount of tin (Sn) can be added to the magnesium alloy to enhance the strength of the alloy at a high temperature. Specifically, the magnesium alloy can further include 0.2 to 3 wt % of zinc, ≦3 wt % of manganese, ≦2 wt % of silicon, ≦1.0 wt % of calcium and ≦1.0 wt % of tin.
- Now, the effects of the disclosure are presented with several examples and comparative examples. All of the examples and comparative examples are alloys of Mg-(X wt %)Li-(Y wt %)Al-(1 wt %)Zn, and the values of X and Y of the examples and comparative examples are listed in Table 1.
-
TABLE 1 X (wt %) Y (wt %) Comparative example 1 6 0 (CE1) Comparative example 2 7 0 (CE2) Comparative example 3 8 0 (CE3) Comparative example 4 9 0 (CE4) Comparative example 5 10 0 (CE5) Comparative example 6 12 0 (CE6) Example 1 (E1) 8 1 Example 2 (E2) 9 1 Example 3 (E3) 6 6 Example 4 (E4) 7 6 Example 5 (E5) 6 7 Example 6 (E6) 7 7 Example 7 (E7) 6 8 Example 8 (E8) 8 8 -
FIG. 1 shows a DSC curve of Example 4.FIG. 2 shows a DSC curve of Example 5. As shown inFIGS. 1 and 2 , the temperature range between the solidus and the liquidus is equal to or larger than 50° C. in both cases. The temperature range between the solidus and the liquidus in Example 5 is even equal to or larger than 95° C. The specific gravity (SG) and the temperature range between the solidus and the liquidus (S-L range) of the examples and the comparative examples are shown inblocks 061 to 0101, 0121, 181, 191, 661, 671, 761, 771, 861 and 881 ofFIG. 3 . In comparison to the comparative examples, each of the example according to this disclosure provides a larger temperature range between the solidus and the liquidus. Also, each of the examples according to this disclosure provides a specific gravity 1.65, which is lower than 1.8, the specific gravity of a typical magnesium alloy. - To summarize, by adjusting the varieties and amounts of the elements added to the magnesium alloy, the magnesium alloy having a larger temperature range between the solidus and the liquidus and suitable to be used in a semi-solid metal casting process can be obtained. Moreover, the magnesium alloy has the feature of lightweight, and is suitable to be used in a mobile device.
- It will be apparent to those skilled in the art that various modifications and variations can be made to the disclosed embodiments. It is intended that the specification and examples be considered as exemplary only, with a true scope of the disclosure being indicated by the following claims and their equivalents.
Claims (7)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW103141813A TWI537395B (en) | 2014-12-02 | 2014-12-02 | Magnesium alloy |
| TW103141813 | 2014-12-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20160153075A1 true US20160153075A1 (en) | 2016-06-02 |
Family
ID=56078810
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US14/882,433 Abandoned US20160153075A1 (en) | 2014-12-02 | 2015-10-13 | Magnesium alloy |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20160153075A1 (en) |
| JP (1) | JP6404803B2 (en) |
| CN (1) | CN105838950B (en) |
| TW (1) | TWI537395B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109763046A (en) * | 2019-03-29 | 2019-05-17 | 重庆大学 | A kind of high-strength and high-plastic magnesium-zinc-manganese-tin-calcium alloy and preparation method thereof |
| PL424338A1 (en) * | 2018-01-22 | 2019-07-29 | Instytut Metalurgii I Inżynierii Materiałowej Im. Aleksandra Krupkowskiego Polskiej Akademii Nauk | Ultra-light magnesium alloy for thixotropic casting |
| US20220298609A1 (en) * | 2018-04-23 | 2022-09-22 | Canon Kabushiki Kaisha | Magnesium-lithium-based alloy |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106148786B (en) * | 2016-08-22 | 2018-12-18 | 上海交通大学 | High-strength casting magnesium lithium alloy and preparation method thereof |
| JP7078839B2 (en) * | 2017-12-12 | 2022-06-01 | 富士通株式会社 | Magnesium alloy, its manufacturing method, and electronic equipment |
| CN112442620B (en) * | 2020-10-29 | 2021-10-01 | 航天材料及工艺研究所 | A 300MPa grade magnesium-lithium alloy material and preparation method thereof |
| CN112593132B (en) * | 2020-12-30 | 2022-03-01 | 郑州轻研合金科技有限公司 | High-strength semi-solid two-phase die-casting magnesium-lithium alloy and preparation method thereof |
| CN113502422B (en) * | 2021-06-11 | 2022-06-07 | 清华大学 | High-strength-toughness magnesium-lithium alloy and preparation method thereof |
| CN115161527B (en) * | 2022-07-28 | 2023-02-24 | 郑州轻研合金科技有限公司 | High-strength weldable magnesium-lithium alloy and preparation method thereof |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5059390A (en) * | 1989-06-14 | 1991-10-22 | Aluminum Company Of America | Dual-phase, magnesium-based alloy having improved properties |
| WO2000059760A1 (en) * | 1999-04-03 | 2000-10-12 | Volkswagen Aktiengesellschaft | Deformation element comprised of a ductile metallic lightweight material and the use thereof |
| US20040241036A1 (en) * | 2001-06-11 | 2004-12-02 | Andrea Meyer-Lindenberg | Medical implant for the human or animal body |
| US6846451B2 (en) * | 2001-08-23 | 2005-01-25 | The Japan Steel Works, Ltd. | Magnesium alloy and magnesium alloy member superior in corrosion resistance |
| CN101121981A (en) * | 2007-09-20 | 2008-02-13 | 哈尔滨工程大学 | A high-strength magnesium-lithium alloy |
| CN103031474A (en) * | 2011-09-29 | 2013-04-10 | 比亚迪股份有限公司 | Magnesium lithium alloy |
| US10280496B2 (en) * | 2016-01-07 | 2019-05-07 | Amli Materials Technology Co., Ltd. | Light magnesium alloy and method for forming the same |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4130500A (en) * | 1977-12-14 | 1978-12-19 | The United States Of America As Represented By The United States Department Of Energy | Lithium-aluminum-magnesium electrode composition |
| JPS5926160B2 (en) * | 1983-03-01 | 1984-06-25 | 松下電器産業株式会社 | Diaphragm for speaker |
| JP3387548B2 (en) * | 1993-03-29 | 2003-03-17 | 三井金属鉱業株式会社 | Manufacturing method of magnesium alloy molded product |
| JP3320037B2 (en) * | 1999-07-12 | 2002-09-03 | シャープ株式会社 | FORGED MOLDED PRODUCT AND ITS MANUFACTURING METHOD |
| CN101407898B (en) * | 2008-10-22 | 2010-06-23 | 仝仲盛 | Method for manufacturing magnesium alloy extrusion parts |
| CN101403064B (en) * | 2008-11-06 | 2010-09-08 | 哈尔滨工程大学 | A kind of magnesium-lithium alloy reinforced by adding Ag |
| JP2012021182A (en) * | 2010-07-12 | 2012-02-02 | Sumitomo Electric Ind Ltd | Magnesium alloy coil material and method for manufacturing the same |
| JP5757085B2 (en) * | 2010-12-22 | 2015-07-29 | 住友電気工業株式会社 | Magnesium alloy coil material, magnesium alloy coil material manufacturing method, magnesium alloy member, and magnesium alloy member manufacturing method |
| CN102505089B (en) * | 2011-12-26 | 2013-07-24 | 北京航空航天大学 | Biodegradable magnesium-lithium alloy material and preparation method thereof |
| CN102676894B (en) * | 2012-01-15 | 2014-09-17 | 河南科技大学 | Magnesium-based microcrystal alloy strip material and preparation method thereof |
| CN102618764A (en) * | 2012-04-13 | 2012-08-01 | 江汉大学 | Magnesium alloy with hot cracking resistance and low linear shrinkage |
| CN102618765B (en) * | 2012-04-13 | 2014-08-06 | 江汉大学 | Magnesium alloy with hot cracking resistance and low linear shrinkage |
| CN102618758B (en) * | 2012-04-13 | 2014-11-26 | 江汉大学 | Cast magnesium alloy of low linear shrinkage |
| CN102912203A (en) * | 2012-10-31 | 2013-02-06 | 重庆大学 | Grain-refined manganese-lithium alloy and method for manufacturing same |
| CN104004950B (en) * | 2014-06-05 | 2016-06-29 | 宁波高新区融创新材料科技有限公司 | Ease of solubility magnesium alloy materials and manufacture method thereof and application |
-
2014
- 2014-12-02 TW TW103141813A patent/TWI537395B/en active
-
2015
- 2015-01-13 CN CN201510016017.0A patent/CN105838950B/en active Active
- 2015-10-13 US US14/882,433 patent/US20160153075A1/en not_active Abandoned
- 2015-11-13 JP JP2015222590A patent/JP6404803B2/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5059390A (en) * | 1989-06-14 | 1991-10-22 | Aluminum Company Of America | Dual-phase, magnesium-based alloy having improved properties |
| WO2000059760A1 (en) * | 1999-04-03 | 2000-10-12 | Volkswagen Aktiengesellschaft | Deformation element comprised of a ductile metallic lightweight material and the use thereof |
| US20040241036A1 (en) * | 2001-06-11 | 2004-12-02 | Andrea Meyer-Lindenberg | Medical implant for the human or animal body |
| US6846451B2 (en) * | 2001-08-23 | 2005-01-25 | The Japan Steel Works, Ltd. | Magnesium alloy and magnesium alloy member superior in corrosion resistance |
| CN101121981A (en) * | 2007-09-20 | 2008-02-13 | 哈尔滨工程大学 | A high-strength magnesium-lithium alloy |
| CN103031474A (en) * | 2011-09-29 | 2013-04-10 | 比亚迪股份有限公司 | Magnesium lithium alloy |
| US10280496B2 (en) * | 2016-01-07 | 2019-05-07 | Amli Materials Technology Co., Ltd. | Light magnesium alloy and method for forming the same |
Non-Patent Citations (2)
| Title |
|---|
| NPL: Machine translation of CN 103031474A, 04/2013 * |
| WO 760 Haferkamp 2000059A1, with English machine translation, thereafter * |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| PL424338A1 (en) * | 2018-01-22 | 2019-07-29 | Instytut Metalurgii I Inżynierii Materiałowej Im. Aleksandra Krupkowskiego Polskiej Akademii Nauk | Ultra-light magnesium alloy for thixotropic casting |
| US20220298609A1 (en) * | 2018-04-23 | 2022-09-22 | Canon Kabushiki Kaisha | Magnesium-lithium-based alloy |
| CN109763046A (en) * | 2019-03-29 | 2019-05-17 | 重庆大学 | A kind of high-strength and high-plastic magnesium-zinc-manganese-tin-calcium alloy and preparation method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2016128603A (en) | 2016-07-14 |
| JP6404803B2 (en) | 2018-10-17 |
| CN105838950B (en) | 2018-09-14 |
| TW201621059A (en) | 2016-06-16 |
| CN105838950A (en) | 2016-08-10 |
| TWI537395B (en) | 2016-06-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US20160153075A1 (en) | Magnesium alloy | |
| KR101367892B1 (en) | Magnesium alloy for high temperature and manufacturing method thereof | |
| EP3219818B1 (en) | Magnesium alloy and preparation method and use thereof | |
| JP5113104B2 (en) | Spheroidal graphite cast iron pipe and manufacturing method thereof | |
| US10947609B2 (en) | Magnesium alloy having excellent mechanical properties and corrosion resistance and method for manufacturing the same | |
| WO2016186094A1 (en) | Method for processing molten cast iron | |
| CN105624494A (en) | Anti-corrosion wrought magnesium alloy containing rare earth elements and manufacturing method of anti-corrosion wrought magnesium alloy | |
| JP2010116620A (en) | Magnesium alloy and magnesium alloy casting | |
| WO2005003398A3 (en) | High strength aluminum alloys and process for making the same | |
| US10358703B2 (en) | Magnesium alloy and method of preparing the same | |
| US20210147963A1 (en) | Magnesium alloy with high thermal conductivity, inverter housing, inverter and vehicle | |
| CN104178672A (en) | High-strength magnesium alloy and preparation method thereof | |
| JPH06279905A (en) | Superplastic magnesium alloy | |
| US20170314101A1 (en) | Aluminum alloy for die casting, and aluminum alloy die-cast product using same | |
| CN102808117A (en) | Aluminum alloy | |
| CN105132743A (en) | Zn-Al alloy containing Ta and Te elements and preparation method thereof | |
| CN105132747A (en) | Casting zinc-aluminium alloy containing tantalum and preparation method thereof | |
| US20170073801A1 (en) | Radiating Fin Formed Of Aluminum Alloy And Method For Producing The Same | |
| JP6778675B2 (en) | Heat resistant magnesium alloy | |
| CN108642339A (en) | A kind of bat high-strength corrosion-resisting aluminium alloy and preparation method thereof | |
| JPH0823057B2 (en) | Superplastic magnesium alloy | |
| US20130269480A1 (en) | Method for Making a Strong Aluminum Alloy | |
| CN104789835A (en) | High-strength and high-toughness aluminum alloy for baseball bat | |
| RU2012140397A (en) | MAGNESIUM ALLOY ALLOWED FOR APPLICATION AT HIGH TEMPERATURE AND METHOD FOR PRODUCING IT | |
| KR102023802B1 (en) | High strength magnesium alloy |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: AMLI MATERIALS TECHNOLOGY CO., LTD., TAIWAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:WANG, JIAN-YIH;YEH, MING-TARNG;WU, CHENG-YUAN;SIGNING DATES FROM 20150818 TO 20150821;REEL/FRAME:036786/0333 |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: RESPONSE TO NON-FINAL OFFICE ACTION ENTERED AND FORWARDED TO EXAMINER |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: NON FINAL ACTION MAILED |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: RESPONSE TO NON-FINAL OFFICE ACTION ENTERED AND FORWARDED TO EXAMINER |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: FINAL REJECTION MAILED |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: ADVISORY ACTION MAILED |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: DOCKETED NEW CASE - READY FOR EXAMINATION |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: NON FINAL ACTION MAILED |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |