CN103160759A - Be-containing magnesium-based amorphous composite material - Google Patents

Be-containing magnesium-based amorphous composite material Download PDF

Info

Publication number
CN103160759A
CN103160759A CN2011104071322A CN201110407132A CN103160759A CN 103160759 A CN103160759 A CN 103160759A CN 2011104071322 A CN2011104071322 A CN 2011104071322A CN 201110407132 A CN201110407132 A CN 201110407132A CN 103160759 A CN103160759 A CN 103160759A
Authority
CN
China
Prior art keywords
alloy
composite material
magnesium
pure
atomic percent
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
Application number
CN2011104071322A
Other languages
Chinese (zh)
Other versions
CN103160759B (en
Inventor
尤俊华
邱克强
任英磊
李庆丰
王琳
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Yancheng Ruijia Automobile Service Co.,Ltd.
Original Assignee
Shenyang University of Technology
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Shenyang University of Technology filed Critical Shenyang University of Technology
Priority to CN201110407132.2A priority Critical patent/CN103160759B/en
Publication of CN103160759A publication Critical patent/CN103160759A/en
Application granted granted Critical
Publication of CN103160759B publication Critical patent/CN103160759B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Powder Metallurgy (AREA)

Abstract

The invention discloses a Be-containing magnesium-based amorphous composite material. An alloy is characterized by comprising the components in atomic percent shown in the formula of (Mg0.81Ni0.08Zn0.05Y0.06)100 - xBex (x ranges from 1 to 6), and comprising an impurity element O in atomic percent of not greater than 0.002%. According to the composite material disclosed by the invention, a long period phase is formed by adding element Ni, element Zn and element Y together; and the purpose of adding element Be is to increase the entropy of the alloy and change the internal atomic arrangement structure of the alloy. Compared with the existing magnesium-based amorphous composite material, the composite material disclosed by the invention is good in comprehensive mechanical property; the problem of brittle failure of magnesium-based amorphous alloy is solved; and a way with a great prospect is provided for the practicability of amorphous alloy composite material.

Description

A kind of magnesium base amorphous matrix material of Be that contains
Technical field
The invention belongs to the amorphous composite technical field, be specifically related to a kind of have a long-periodic structure contain the magnesium base amorphous matrix material of Be.
Background technology
Magnesium is the Patterns for Close-Packed Hexagonal Crystal structure, its stacking ordination number is the two-layer stacking provisions of AB, and so-called magnesium alloy long period stacking structure is exactly than the longer stacking order of two-layer atom stacking order, as 6H (ABCBCB '), 10H (ABACBCBCAC), 14H (ACBCBABABABCBC), (H represents six structures for 18R (its sequence is ABABABCACACABCBCBC) and 24R (ABABABABCACACACABCBCBCBC), R represents water chestnut face structure, and the numeral of front is stamped the number of plies for heap).
1994, Luo etc. in the Mg-Zn-Y alloy reported first 18R long-periodic structure.Calendar year 2001, Kawamura etc. have prepared yield strength by the method for rapid solidification/powder metallurgy and have surpassed 600MPa, the Mg97Zn1Y2(atomic percent of unit elongation 5%, lower same) alloy, and this alloy also has excellent high-temperature yield strength and the superplasticity under high strain rate, and this makes the research to long-periodic structure enhancing magnesium alloy become a focus.Kawamura in 2004 etc. prepare again yield strength and reach 375MPa, and unit elongation arrives 4% As-extruded long-periodic structure enhancing Mg97ZnY2.Matsuura in 2005 etc. are at the Mg of rapid solidification 98Cu 1Y 1Found the long-periodic structure of amorphous and 14H in band, there is the alloy system of long-periodic structure in this is to expand to Mg-Cu-Y system by Mg-Zn-Y.2006, it is base block amorphous that the use water-cooled copper mold casting methods such as Hui Xidong have successfully been prepared 6H long-periodic structure enhancing magnesium, its compressive strain arrival 18%, and compressed rupture strength arrives 1.2GPa.2008, the long-periodic structure of discovery 18R in the Mg-Ni-Y alloy of the water cooled copper moulds such as Itoi preparation.
Present research is found, long-periodic structure strengthens magnesium alloy can be divided into two classes according to macrocyclic formation condition, the first type comprises the alloy systems such as Mg-Y-Zn, Mg-Dy-Zn, Mg-Ho-Zn and Mg-Er-Zn, long-periodic structure in these alloy systems forms in process of setting, the type of long-periodic structure is 18R, but by high temperature annealing, its 18R structure fundamental transformation is 14H.The second type comprises the alloy systems such as Mg-Gd-Zn, Mg-Tb-Zn and Mg-Tm-Zn, does not have long-periodic structure or fewer in its as cast condition, separates out from matrix Mg supersaturated solid solution by 14H long-periodic structure after high temperature annealing.Also find in addition also to have formed these 5 kinds dissimilar LPSO structures of 6H, l0H, 14H, 18R and 24R in Mg-RE-Zn/Cu (Mg-Gd-Zn, Mg-Sm-Zn, Mg-Er-Zn etc.) alloy, thereby make this LPSO structure become the study hotspot problem of magnesium alloy research field.
The present invention intends disclosing a kind of Mg-Ni-Zn-Y-Be amorphous composite, changes the atomic arrangement structure of the magnesium base amorphous matrix material with long-periodic structure by adding element Be.Be and Mg solid-state or even liquid under do not dissolve each other, and the atomic size of Be is very little, can carry heavy alloyed entropy, thus the Be element add the structure that can change alloy, make the comprehensive mechanical property of alloy all obtain raising to a certain degree.
Summary of the invention
The invention provides the magnesium base amorphous matrix material of a kind of Be of containing, its objective is the comprehensive mechanical property that improves magnesium base amorphous matrix material, prepare and have compressive strength at room temperature 〉=657MPa, the amorphous composite of strain rate 〉=16.3%.
For achieving the above object, the present invention is by the following technical solutions:
A kind of Be magnesium-based amorphous alloy composite material that contains, it is characterized in that: the component of described alloy and atomic percent are (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 100-xBe x, x=1 ~ 6.
Impurity element and atomic percent are O≤0.002%.
Compressive strength at room temperature 〉=the 657MPa of magnesium base amorphous matrix material, strain rate 〉=16.3%.
The present invention changes the atomic structure of magnesium base amorphous matrix material by adding the Be element, has improved the comprehensive mechanical property of alloy.
Description of drawings:
Fig. 1 is (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 95Be 5The SEM photo that alloy is 2000 times;
Fig. 2 is Mg 81Ni 8Zn 5Y 6The SEM photo that alloy is 2000 times;
Fig. 3 is (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 95Be 5Alloy and Mg 81Ni 8Zn 5Y 6The diameter of alloy is the stress-strain(ed) curve of 2mm sample.
Embodiment:
The present invention discloses the magnesium base amorphous matrix material of a kind of Be of containing, and has higher intensity and good plasticity, thereby has solved magnesium base amorphous alloy brittle failure problem, for the application of amorphous composite provides a very promising approach.
The component of described alloy and atomic percent are (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 100-xBe x(x=1 ~ 6), impurity element and atomic percent are O≤0.002%.
The characteristics of above-mentioned amorphous composite are:
Compressive strength at room temperature 〉=657MPa, strain rate 〉=16.3%.
The present invention adds Ni, Zn and the Y element with strengthening effect by uniting, and makes they and Mg form Mg 12ZnY long period phase.Experiment shows, Mg 12ZnY phase long-periodic structure is the 6H structure of being stamped by ABCBCB ' heap, and wherein A and B ' are the atomic shells that is rich in Zn and Y, and its structure and desirable 6H type magnesium are variant, can improve the comprehensive mechanical property of amorphous alloy composite material.Add the purpose of Be element and carry heavy alloyed entropy, change the inner atomic arrangement structure of alloy, further put forward heavy alloyed mechanical property.
The above-mentioned Be of containing magnesium base long period amorphous alloy composite material prepares by following steps:
(1) batching: raw material is that purity is 99.9% pure Mg, 99.9% pure Ni, 99.9% pure Cu, 99.9% pure Y and 99.9% pure Be, and the atomic percent of each element is (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 100-xBe x(x=1 ~ 6), foreign matter content O≤0.002%;
(2) melting: at first with electric arc furnace, high-melting-point element Cu, Y, Ni and Be are smelted into master alloy, master alloy and element M g are carried out melting with boron nitride crucible in well formula resistance furnace, utilize N 2And SF 6Mixed gas is as shielding gas;
(3) casting: molten metal liquid is poured into cylinder sample.
Describe the present invention below in conjunction with specific embodiment, need to prove, protection scope of the present invention is not limited in following embodiment.
Embodiment 1:
A kind of Be magnesium-based amorphous alloy composite material that contains, it is characterized in that: the component of described alloy and atomic percent are (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 99Be 1
The preparation method is as follows:
(1) batching: raw material is that purity is 99.9% pure Mg, 99.9% pure Ni, 99.9% pure Cu, 99.9% pure Y and 99.9% pure Be, and the atomic percent of each element is (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 99Be 1, foreign matter content O≤0.002%;
(2) melting: at first with electric arc furnace, high-melting-point element Cu, Y, Ni and Be are smelted into master alloy, master alloy and element M g are carried out melting with boron nitride crucible in well formula resistance furnace, utilize N 2And SF 6Mixed gas is as shielding gas;
(3) casting: molten metal liquid is poured into the cylinder sample that diameter is 2mm.
Compressive strength at room temperature 〉=the 657MPa of magnesium base amorphous matrix material, strain rate 〉=16.3%.
Embodiment 2:
A kind of Be magnesium-based amorphous alloy composite material that contains, it is characterized in that: the component of described alloy and atomic percent are (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 98Be 2
The preparation method is as follows:
(1) batching: raw material is that purity is 99.9% pure Mg, 99.9% pure Ni, 99.9% pure Cu, 99.9% pure Y and 99.9% pure Be, and the atomic percent of each element is (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 98Be 2, foreign matter content O≤0.002%;
(2) melting: at first with electric arc furnace, high-melting-point element Cu, Y, Ni and Be are smelted into master alloy, master alloy and element M g are carried out melting with boron nitride crucible in well formula resistance furnace, utilize N 2And SF 6Mixed gas is as shielding gas;
(3) casting: molten metal liquid is poured into the cylinder sample that diameter is 2mm.
Compressive strength at room temperature 〉=the 661MPa of magnesium base amorphous matrix material, strain rate 〉=17%.
Embodiment 3:
A kind of Be magnesium-based amorphous alloy composite material that contains, it is characterized in that: the component of described alloy and atomic percent are (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 97Be 3
The preparation method is as follows:
(1) batching: raw material is that purity is 99.9% pure Mg, 99.9% pure Ni, 99.9% pure Cu, 99.9% pure Y and 99.9% pure Be, and the atomic percent of each element is (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 97Be 3, foreign matter content O≤0.002%;
(2) melting: at first with electric arc furnace, high-melting-point element Cu, Y, Ni and Be are smelted into master alloy, master alloy and element M g are carried out melting with boron nitride crucible in well formula resistance furnace, utilize N 2And SF 6Mixed gas is as shielding gas;
(3) casting: molten metal liquid is poured into the cylinder sample that diameter is 2mm.
Compressive strength at room temperature 〉=the 670MPa of magnesium base amorphous matrix material, strain rate 〉=17.2%.
Embodiment 4:
A kind of Be magnesium-based amorphous alloy composite material that contains, it is characterized in that: the component of described alloy and atomic percent are (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 96Be 4
The preparation method is as follows:
(1) batching: raw material is that purity is 99.9% pure Mg, 99.9% pure Ni, 99.9% pure Cu, 99.9% pure Y and 99.9% pure Be, and the atomic percent of each element is (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 96Be 4, foreign matter content O≤0.002%;
(2) melting: at first with electric arc furnace, high-melting-point element Cu, Y, Ni and Be are smelted into master alloy, master alloy and element M g are carried out melting with boron nitride crucible in well formula resistance furnace, utilize N 2And SF 6Mixed gas is as shielding gas;
(3) casting: molten metal liquid is poured into the cylinder sample that diameter is 2mm.
Compressive strength at room temperature 〉=the 675MPa of magnesium base amorphous matrix material, strain rate 〉=17.3%.
Embodiment 5:
A kind of Be magnesium-based amorphous alloy composite material that contains, it is characterized in that: the component of described alloy and atomic percent are (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 95Be 5
The preparation method is as follows:
(1) batching: raw material is that purity is 99.9% pure Mg, 99.9% pure Ni, 99.9% pure Cu, 99.9% pure Y and 99.9% pure Be, and the atomic percent of each element is (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 95Be 5, foreign matter content O≤0.002%;
(2) melting: at first with electric arc furnace, high-melting-point element Cu, Y, Ni and Be are smelted into master alloy, master alloy and element M g are carried out melting with boron nitride crucible in well formula resistance furnace, utilize N 2And SF 6Mixed gas is as shielding gas;
(3) casting: molten metal liquid is poured into the cylinder sample that diameter is 2mm.
Compressive strength at room temperature 〉=the 689MPa of magnesium base amorphous matrix material, strain rate 〉=18%.
Fig. 1 is (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 95Be 5The SEM photo that alloy is 2000 times;
Fig. 2 is Mg 81Ni 8Zn 5Y 6The SEM photo that alloy is 2000 times;
Fig. 3 is (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 95Be 5Alloy and Mg 81Ni 8Zn 5Y 6The diameter of alloy is the stress-strain(ed) curve of 2mm sample.
Embodiment 6:
A kind of Be magnesium-based amorphous alloy composite material that contains, it is characterized in that: the component of described alloy and atomic percent are (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 94Be 6
The preparation method is as follows:
(1) batching: raw material is that purity is 99.9% pure Mg, 99.9% pure Ni, 99.9% pure Cu, 99.9% pure Y and 99.9% pure Be, and the atomic percent of each element is (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 94Be 6, foreign matter content O≤0.002%;
(2) melting: at first with electric arc furnace, high-melting-point element Cu, Y, Ni and Be are smelted into master alloy, master alloy and element M g are carried out melting with boron nitride crucible in well formula resistance furnace, utilize N 2And SF 6Mixed gas is as shielding gas;
(3) casting: molten metal liquid is poured into the cylinder sample that diameter is 2mm.
Compressive strength at room temperature 〉=the 675MPa of magnesium base amorphous matrix material, strain rate 〉=17%.

Claims (3)

1. one kind contains the magnesium base amorphous matrix material of Be, and it is characterized in that: the component of described alloy and atomic percent are (Mg 0.81Ni 0.08Zn 0.05Y 0.06) 100-xBe x, x=1 ~ 6.
2. a kind of magnesium base amorphous matrix material of Be that contains according to claim 1, it is characterized in that: impurity element and mass percent are O≤0.002%.
3. a kind of magnesium base amorphous matrix material of Be that contains according to claim 1, is characterized in that: the compressive strength at room temperature 〉=657MPa of magnesium-based amorphous alloy composite material, strain rate 〉=16.3%.
CN201110407132.2A 2011-12-09 2011-12-09 Be-containing magnesium-based amorphous composite material Active CN103160759B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201110407132.2A CN103160759B (en) 2011-12-09 2011-12-09 Be-containing magnesium-based amorphous composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201110407132.2A CN103160759B (en) 2011-12-09 2011-12-09 Be-containing magnesium-based amorphous composite material

Publications (2)

Publication Number Publication Date
CN103160759A true CN103160759A (en) 2013-06-19
CN103160759B CN103160759B (en) 2015-04-22

Family

ID=48584289

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201110407132.2A Active CN103160759B (en) 2011-12-09 2011-12-09 Be-containing magnesium-based amorphous composite material

Country Status (1)

Country Link
CN (1) CN103160759B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103602930A (en) * 2013-12-03 2014-02-26 沈阳工业大学 Magnesium-matrix amorphous composite material containing high-melting point element

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101418423A (en) * 2008-12-01 2009-04-29 沈阳工业大学 Magnesium base amorphous alloy and composite material thereof
CN102129890A (en) * 2011-01-11 2011-07-20 北京航空航天大学 Amorphous alloy-based optical focusing lens and preparation method thereof

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101418423A (en) * 2008-12-01 2009-04-29 沈阳工业大学 Magnesium base amorphous alloy and composite material thereof
CN102129890A (en) * 2011-01-11 2011-07-20 北京航空航天大学 Amorphous alloy-based optical focusing lens and preparation method thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103602930A (en) * 2013-12-03 2014-02-26 沈阳工业大学 Magnesium-matrix amorphous composite material containing high-melting point element
CN103602930B (en) * 2013-12-03 2016-06-15 沈阳工业大学 Magnesium base amorphous composite containing high-melting-point element

Also Published As

Publication number Publication date
CN103160759B (en) 2015-04-22

Similar Documents

Publication Publication Date Title
CN103122431B (en) Preparation method for magnesium-lithium alloy with enhanced long-period structure phase
CN102409213B (en) Preparation method of high-strength magnesium alloy enhanced by heat treatment
CN102618758A (en) Cast magnesium alloy of low linear shrinkage
CN110284042B (en) Superplastic high-entropy alloy, sheet and preparation method thereof
CN102154580B (en) High-intensity heat-resistant magnesium alloy material and preparation process thereof
CN102230118A (en) Magnesium alloy of high intensity and high yield ratio and preparation method thereof
CN103498086A (en) High-strength high-ductility magnesium alloy and preparation process thereof
CN109957687A (en) A kind of diecasting aluminum-silicon alloy and preparation method thereof
CN101538671A (en) Rapid solidification superhigh strength magnesium alloy and preparation method thereof
CN101871066A (en) High-obdurability magnesium alloy comprising tin and zinc and preparation method thereof
CN102618762A (en) Heat-resisting magnesium alloy
CN102719716A (en) Heat conduction magnesium alloy and preparation method thereof
CN103589903A (en) High-strength and wear-resistant copper alloy and preparation method thereof
CN104946938A (en) Preparation method of Al-Ti-B-Y intermediate alloy and application thereof
CN102226244B (en) High-strength magnesium-zinc-manganese-yttrium magnesium alloy material
CN103305738A (en) Silicon-containing heat-resistant rare earth magnesium alloy and preparation method thereof
CN102242299A (en) Bi and Nd composite reinforced high-strength cast magnesium alloy and preparation method thereof
CN101871068B (en) High-strength high-plasticity magnesium alloy comprising tin and aluminium and preparation method thereof
CN102899592B (en) Plastic zirconium-based metal glass and preparation method thereof
CN103469039A (en) Magnesium-aluminum-zinc wrought magnesium alloy containing calcium and rare-earth samarium
CN101713034A (en) Method for refining LA141 magnesium-lithium alloy grains
CN100494437C (en) Method for branch crystal balling in large block metal glass composite
CN102912259B (en) Zirconium-based metal glass endogenic composite material and preparation method thereof
CN102719703B (en) Multi-component zinc-aluminium alloy capable of enhancing comprehensive chemical properties
CN104480361A (en) High-strength/toughness heat-resistant die casting magnesium alloy and preparation method thereof

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20201230

Address after: 224000 No.6 Xinhua Road, Yandu District, Yancheng City, Jiangsu Province

Patentee after: Yancheng Ruijia Automobile Service Co.,Ltd.

Address before: 110870 No. 111 Shenyang West Road, Shenyang economic and Technological Development Zone, Liaoning

Patentee before: SHENYANG University OF TECHNOLOGY

TR01 Transfer of patent right