EP0643145A1 - Hochfeste Werkstoffe auf Legierungen auf Magnesiumbasis und Verfahren zur Herstellung dieser Werkstoffe - Google Patents
Hochfeste Werkstoffe auf Legierungen auf Magnesiumbasis und Verfahren zur Herstellung dieser Werkstoffe Download PDFInfo
- Publication number
- EP0643145A1 EP0643145A1 EP94111190A EP94111190A EP0643145A1 EP 0643145 A1 EP0643145 A1 EP 0643145A1 EP 94111190 A EP94111190 A EP 94111190A EP 94111190 A EP94111190 A EP 94111190A EP 0643145 A1 EP0643145 A1 EP 0643145A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- matrix
- high strength
- based alloy
- alloy material
- general formula
- 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.)
- Granted
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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
- C22C23/06—Alloys based on magnesium with a rare earth metal 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
- C22C23/04—Alloys based on magnesium with zinc or cadmium as the next major constituent
Definitions
- the present invention relates to high strength magnesium-based alloy materials having superior mechanical properties and a method for producing the same.
- Mg-Al, Mg-Al-Zn, Mg-Th-Zr, Mg-Th-Zn-Zr, Mg-Zn-Zr, Mg-Zn-Zr-RE rare earth element
- these known alloys have been extensively used as light-weight structural component materials in a wide variety of applications, according to their properties.
- rapidly solidified materials there are known alloys disclosed in Japanese Patent Laid-open No. 3-47,941.
- magnesium-based alloy materials which have an advantageous combination of properties of high hardness, strength and thermal resistance and which are useful as lightweight and high strength materials (i.e., high specific strength materials) and have a superior ductility.
- a high strength magnesium-based alloy material having a microcrystalline composite structure, the alloy material consisting of a composition represented by the general formula (I): Mg a Nd b Zn c , wherein a, b and c are, in atomic %, 80 ⁇ a ⁇ 99, 1 ⁇ b ⁇ 12 and 0 ⁇ c ⁇ 12.
- the present invention also provides a high strength magnesium-based alloy material having a microcrystalline composite structure, the alloy material consisting of a composition represented by the general formula (II): Mg a' Nd b' Zn c' , wherein a', b' and c' are, in atomic %, 95 ⁇ a' ⁇ 99, 1 ⁇ b' ⁇ 3 and 0 ⁇ c' ⁇ 3.
- a', b' and c' are, in atomic %, 95 ⁇ a' ⁇ 99, 1 ⁇ b' ⁇ 3 and 0 ⁇ c' ⁇ 3.
- the aforesaid high strength magnesium-based alloy materials are produced by a method comprising: rapidly solidifying a molten alloy so as to form a fine-grained matrix phase, the molten alloy consisting of the composition represented by the above-defined general formula (I) or (II); and subjecting the resultant rapidly solidified alloy to plastic working at a prescribed heating temperature for work hardening, thereby forming a microcrystalline composite structure having a uniform dispersion of very fine intermetallic compounds in the matrix.
- the matrix in the composite structure consists of an Mg matrix having a hexagonal close-packed (hcp) structure and intermetallic compounds consisting of a non-equilibrium phase having a face-centered cubic (hcp) structure and/or other intermetallic compound phases, such as an Mg12Nd phase, are finely and uniformly dispersed throughout the matrix .
- the present invention provides the above-defined high strength magnesium-based alloy materials consisting of a composition represented by the general formula (I) or (II).
- the ranges of a, b and c are so limited that the above-defined alloy can be obtained with the aforesaid microcrystalline composite structure by industrial rapid cooling techniques, such as liquid quenching.
- fine hcp-Mg precipitates as a host matrix, and finer intermetallic compounds of a non-equilibrium fcc phase formed from, at least, Mg and Nd and/or Mg12Nd phase, etc. are uniformly and finely distributed throughout the hcp-Mg matrix.
- the intermetallic compounds comprising the non-equilibrium fcc phase which is formed from, at least, Mg and Nd and which has a good compatibility with the matrix of hcp-Mg, are uniformly and finely dispersed in the matrix, the Mg matrix is strengthened and the strength of the alloy is outstandingly improved.
- Nd makes it possible to form the above-mentioned composite structure having a dispersion of intermetallic compounds consisting of a non-equilibrium fcc phase, which is formed from, at least, Nd and Mg, and/or other intermetallic compounds, such as an Mg12Nd phase, while suppressing the grain growth of the matrix phase. Since the intermetallic compounds can be formed in large quantities in the presence of a small amount of Nd, it is possible to obtain alloys having a high strength on an Mg-rich side so that high specific-strength materials can be obtained.
- Another alloying element Zn transforms the non-equilibrium phase to a more stable non-equilibrium phase of fcc structure so that the intermetallic compounds having a good compatibility with the magnesium matrix ( ⁇ phase) uniformly and finely disperse in the matrix.
- the hardness and strength of the resultant alloys are improved and a high thermal resistance is imparted to the alloys by suppressing coarsening of the microcrystalline structure of the alloys at high temperatures.
- a molten alloy having the above-defined composition is rapidly solidified so as to obtain a fine-grained matrix phase.
- a cooling rate of 102-106 K/sec is particularly effective.
- the resultant rapidly solidified alloy is heated to a prescribed temperature and subjected to plastic working.
- magnesium alloy materials having a microcrystalline composite structure composed of an hcp Mg matrix and, homogeneously distributed in the matrix, intermetallic compounds consisting of a non-equilibrium fcc phase and/or other intermetallic compound phases, such as an Mg12Nd phase formed of Mg and Nd.
- the non-equilibrium fcc phase may be formed either during rapid solidification or during plastic working.
- the plastic working is preferably performed at a temperature of 50 to 500°C.
- a temperature lower than 50°C cannot provide a sound material due to an excessive deformation resistance.
- a temperature exceeding 500°C causes a considerable grain growth, thereby lowering the strength.
- the magnesium matrix and the intermetallic compounds formed by the above production method have a grain size ranging from 200 nm to 600 nm and a particle size ranging from 10 nm to 400 nm, respectively.
- the alloys may have superior properties as superplastic working materials.
- a molten alloy having a given composition was prepared using a high-frequency melting furnace.
- the molten alloy was subjected to a single-roller melt-spinning technique, which is one of the rapid solidification techniques, at a cooling of 102-106 K/sec and a rapidly solidified material comprising a fine-grained matrix phase.
- the thus obtained rapidly solidified material was subjected to hot-extrusion at a temperature of 320°C under an applied pressure of 1240-1628 MPa, while suppressing the grain growth of the matrix phase.
- the thus obtained extruded material had a microcrystalline composite structure having a dispersion of fine intermetallic compounds.
- test samples having the compositions (by atomic %) given in Table 1 were produced.
- Comparative extruded materials having compositions falling outside the compositional range of the present invention were produced under the same processing conditions as described above.
- the comparative materials are disclosed in Japanese Patent Application Laid-Open No. 3-47,941 hereinbefore described.
- test sample was subjected to X-ray diffraction and measured for its mechanical properties, i.e., tensile strength ( ⁇ B ), plastic elongation ( ⁇ f ), Young's modulus (E), specific strength ( ⁇ B / ⁇ ). The results are shown on the right-hand column of Table 1. The specific strength was obtained by dividing tensile strength by density for each sample. Further, the test samples were observed by a transmission electron microscope (TEM).
- TEM transmission electron microscope
- Mg97Nd3 comprised an hcp-Mg matrix having a grain size of 200 nm to 600 nm and, homogeneously distributed in the matrix, an intermetallic compound of Mg12Nd formed of Mg and Nd and having a particle size of 250 nm to 400 nm.
- Mg96Nd3Zn1 was composed of an hcp-Mg matrix having a grain size of 200 nm to 300 nm and, homogeneously distributed in the matrix, non-equilibrium fcc phase intermetallic compounds formed of Mg and Nd and/or Zn with a particle size of 10 nm to 200 nm.
- every test sample of the present invention exhibited superior mechanical properties, i.e., a tensile strength of not less than 500 MPa, a plastic elongation of not less than 0.4%, a Young's modulus of at least 37 GPa and a specific strength of not less than 280 MPa.
- the magnesium-based alloys of the present invention are superior in plastic elongation over the comparative test samples, they can be successfully subjected to various working operations and exhibit a sufficient durability to permit a high degree of working (plastic working).
- the Mg content exceeded 95 atomic % in the Mg-Nd-Zn alloys, the plastic elongation surprisingly increased, although any significant change was hardly detected in the tensile strength, Young's modulus and specific strength.
- the magnesium-based alloys of the present invention have high levels of strength and heat-resistance, they are very useful as high strength materials and high heat-resistant materials.
- the magnesium-based alloys are also useful as high specific-strength materials because of their high specific strength. Still further, since the alloys exhibit superior elongation at room temperature and Young's module at room temperature, they can be successfully subjected to various working operations and exhibit a sufficient durability to permit a high degree of working (plastic working).
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5193483A JP2807400B2 (ja) | 1993-08-04 | 1993-08-04 | 高力マグネシウム基合金材およびその製造方法 |
JP193483/93 | 1993-08-04 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0643145A1 true EP0643145A1 (de) | 1995-03-15 |
EP0643145B1 EP0643145B1 (de) | 1998-12-23 |
Family
ID=16308787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19940111190 Expired - Lifetime EP0643145B1 (de) | 1993-08-04 | 1994-07-18 | Hochfeste Werkstoffe auf Legierungen auf Magnesiumbasis und Verfahren zur Herstellung dieser Werkstoffe |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0643145B1 (de) |
JP (1) | JP2807400B2 (de) |
DE (1) | DE69415447T2 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2000060131A2 (de) * | 1999-04-03 | 2000-10-12 | Volkswagen Aktiengesellschaft | Magnesiumlegierungen hoher duktilität, verfahren zu deren herstellung und deren verwendung |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008016150A1 (fr) * | 2006-08-03 | 2008-02-07 | National Institute For Materials Science | Alliage de magnésium et son procédé de fabrication |
JP5721043B2 (ja) * | 2010-10-20 | 2015-05-20 | 住友電気工業株式会社 | マグネシウム合金、及び制振材 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1989011552A1 (en) * | 1988-05-23 | 1989-11-30 | Allied-Signal Inc. | Superplastic forming of rapidly solidified magnesium base metal alloys |
WO1991013181A1 (en) * | 1990-02-20 | 1991-09-05 | Allied-Signal Inc. | Method for superplastic forming of rapidly solidified magnesium base metal alloys |
EP0531165A1 (de) * | 1991-09-06 | 1993-03-10 | Tsuyoshi Masumoto | Hochfeste amorphe Magnesiumlegierung und Verfahren zu ihrer Herstellung |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4765954A (en) * | 1985-09-30 | 1988-08-23 | Allied Corporation | Rapidly solidified high strength, corrosion resistant magnesium base metal alloys |
JP2511526B2 (ja) * | 1989-07-13 | 1996-06-26 | ワイケイケイ株式会社 | 高力マグネシウム基合金 |
JP3238516B2 (ja) * | 1993-03-15 | 2001-12-17 | 健 増本 | 高強度マグネシウム合金及びその製造方法 |
-
1993
- 1993-08-04 JP JP5193483A patent/JP2807400B2/ja not_active Expired - Fee Related
-
1994
- 1994-07-18 DE DE1994615447 patent/DE69415447T2/de not_active Expired - Fee Related
- 1994-07-18 EP EP19940111190 patent/EP0643145B1/de not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1989011552A1 (en) * | 1988-05-23 | 1989-11-30 | Allied-Signal Inc. | Superplastic forming of rapidly solidified magnesium base metal alloys |
WO1991013181A1 (en) * | 1990-02-20 | 1991-09-05 | Allied-Signal Inc. | Method for superplastic forming of rapidly solidified magnesium base metal alloys |
EP0531165A1 (de) * | 1991-09-06 | 1993-03-10 | Tsuyoshi Masumoto | Hochfeste amorphe Magnesiumlegierung und Verfahren zu ihrer Herstellung |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2000060131A2 (de) * | 1999-04-03 | 2000-10-12 | Volkswagen Aktiengesellschaft | Magnesiumlegierungen hoher duktilität, verfahren zu deren herstellung und deren verwendung |
WO2000060131A3 (de) * | 1999-04-03 | 2001-01-11 | Volkswagen Ag | Magnesiumlegierungen hoher duktilität, verfahren zu deren herstellung und deren verwendung |
Also Published As
Publication number | Publication date |
---|---|
DE69415447D1 (de) | 1999-02-04 |
JP2807400B2 (ja) | 1998-10-08 |
JPH0748647A (ja) | 1995-02-21 |
DE69415447T2 (de) | 1999-07-08 |
EP0643145B1 (de) | 1998-12-23 |
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