[go: up one dir, main page]

CN102978541B - Shape-memory crystalline-phase strengthened and toughened Ti-base amorphous composite material and preparation method thereof - Google Patents

Shape-memory crystalline-phase strengthened and toughened Ti-base amorphous composite material and preparation method thereof Download PDF

Info

Publication number
CN102978541B
CN102978541B CN201210539119.7A CN201210539119A CN102978541B CN 102978541 B CN102978541 B CN 102978541B CN 201210539119 A CN201210539119 A CN 201210539119A CN 102978541 B CN102978541 B CN 102978541B
Authority
CN
China
Prior art keywords
phase
composite material
vacuum
amorphous composite
alloy
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.)
Expired - Fee Related
Application number
CN201210539119.7A
Other languages
Chinese (zh)
Other versions
CN102978541A (en
Inventor
赵燕春
寇生中
袁小鹏
李春燕
蒲永亮
李超
蒋维科
徐娇
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.)
LANZHOU POLYTECHNIC ALLOY POWDER CO Ltd
Original Assignee
Lanzhou 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 Lanzhou University of Technology filed Critical Lanzhou University of Technology
Priority to CN201210539119.7A priority Critical patent/CN102978541B/en
Publication of CN102978541A publication Critical patent/CN102978541A/en
Application granted granted Critical
Publication of CN102978541B publication Critical patent/CN102978541B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Manufacture And Refinement Of Metals (AREA)

Abstract

形状记忆晶相强韧化Ti基非晶复合材料及其制备方法,按原子百分比计,该复合材料成分为(Ti0.50Ni0.50-yMy)100-xCux,其中:M为Fe、Co、Nb、Al、Zr、Si元素的一种或者几种,x=5~33,y=0~0.25,该成分具有一定形状记忆效应和高非晶形成能力,由非晶基体中原位析出塑性相-过冷奥氏体相增韧,利用形状记忆合金中过冷奥氏体在形变诱导下发生热弹性马氏体相变使非晶产生加工硬化这一特性对基体增强,该复合材料表现出优异的综合力学性能,压缩屈服强度为1000~1800MPa,断裂强度为1400~2800MPa,塑性变形为10%~20%,并表现出强烈的加工硬化。

A Ti-based amorphous composite material strengthened and toughened by a shape-memory crystalline phase and a preparation method thereof. The composition of the composite material is (Ti 0.50 Ni 0.50-y M y ) 100-x Cux , wherein: M is Fe, One or several elements of Co, Nb, Al, Zr, Si, x=5~33, y=0~0.25, this composition has a certain shape memory effect and high amorphous forming ability, and is precipitated in situ from the amorphous matrix The plastic phase-supercooled austenite phase is toughened, and the supercooled austenite in the shape memory alloy undergoes thermoelastic martensitic phase transformation under deformation induction to make the amorphous work hardening to strengthen the matrix. The composite material It exhibits excellent comprehensive mechanical properties, the compressive yield strength is 1000~1800MPa, the fracture strength is 1400~2800MPa, the plastic deformation is 10%~20%, and it shows strong work hardening.

Description

形状记忆晶相强韧化Ti基非晶复合材料及其制备方法Shape memory crystalline phase toughened Ti-based amorphous composite material and preparation method thereof

技术领域 technical field

 本发明涉及Ti基非晶复合材料领域,具体为一种形状记忆晶相增强增韧Ti基非晶复合材料的成分及其制备方法。 The invention relates to the field of Ti-based amorphous composite materials, in particular to a composition of a shape-memory crystal phase reinforced and toughened Ti-based amorphous composite material and a preparation method thereof.

背景技术 Background technique

钛基非晶具有密度低、强度高、良好的耐磨耐蚀性和生物相容性等的优势,在航天航空、机械、建筑、能源和生物医学等方面具有很大应用前景。但是,由于非晶合金原子排列呈现长程无序、短程有序结构,变形时缺乏常规晶体金属材料的位错和滑移等加工硬化机制,高度局域化的剪切行为使得其室温塑性和断裂韧性低,限制了非晶合金作为结构材料在工程中的广泛应用。近年来,人们提出了多种对非晶合金增韧的方法,其中引入第二相可根据各种性能指标选择,BMG基复合材料结构和性能具有可设计性,是一种有效的BMG增韧方法。 Titanium-based amorphous has the advantages of low density, high strength, good wear resistance and corrosion resistance, and biocompatibility, and has great application prospects in aerospace, machinery, construction, energy, and biomedicine. However, due to the long-range disordered and short-range ordered structure of the atomic arrangement of amorphous alloys, the lack of work hardening mechanisms such as dislocations and slips of conventional crystalline metal materials during deformation, the highly localized shear behavior makes its plasticity and fracture at room temperature Low toughness limits the wide application of amorphous alloys as structural materials in engineering. In recent years, people have proposed a variety of methods for toughening amorphous alloys. The introduction of the second phase can be selected according to various performance indicators. The structure and properties of BMG-based composites can be designed, and it is an effective BMG toughening method. method.

如2008年,W. L. Johnson课题组通过调整合金成分和半固态处理,在钛基非晶合金系中开发出具有显著塑性的β相枝晶增韧的复合材料,其室温拉伸总变形率分别为10.8%和13.1%,断面收缩率分别为50%和46%,该材料的塑韧性指标达到了传统金属材料的指标范围,但其变形屈服后仍表现出应变软化,使得工程推广受到了一定限制。 For example, in 2008, W. L. Johnson’s research group developed a β-phase dendrite-toughened composite material with significant plasticity in the titanium-based amorphous alloy system by adjusting the alloy composition and semi-solid treatment. The total tensile deformation at room temperature The ratios are 10.8% and 13.1%, respectively, and the reduction of area is 50% and 46%. The plasticity and toughness index of this material has reached the index range of traditional metal materials, but it still shows strain softening after deformation and yielding, which makes engineering popularization. certain restrictions.

发明内容 Contents of the invention

本发明的目的是提供一种形状记忆晶相强韧化Ti基非晶复合材料及其制备方法。 The object of the present invention is to provide a Ti-based amorphous composite material strengthened and toughened by a shape memory crystal phase and a preparation method thereof.

本发明是形状记忆晶相强韧化Ti基非晶复合材料及其制备方法,形状记忆晶相强韧化Ti基非晶复合材料,Ti基非晶合金和能够产生形变诱导相变的过冷奥氏体相B2-TiNi以及马氏体相B19’-TiNi复合而成。 The invention relates to a Ti-based amorphous composite material strengthened and toughened by a shape-memory crystalline phase and a preparation method thereof, a Ti-based amorphous composite material strengthened and toughened by a shape-memory crystalline phase, a Ti-based amorphous alloy and a supercooled material capable of producing deformation-induced phase transitions It is composed of austenite phase B2-TiNi and martensite phase B19'-TiNi.

 状记忆晶相强韧化Ti基非晶复合材料的制备方法,其步骤为: The preparation method of the Ti-based amorphous composite material strengthened and toughened by the shape memory crystal phase comprises the following steps:

(1)配料: (1) Ingredients:

按权利要求1所示的(Ti0.50Ni0.50-yMy)100-xCux名义成分称取各组分; Each component is weighed by (Ti 0.50 Ni 0.50-y M y ) 100-x Cu x nominal composition shown in claim 1;

(2)熔炼制(Ti0.50Ni0.50-yMy)100-xCux母合金: (2) Melting (Ti 0.50 Ni 0.50-y M y ) 100-x Cu x master alloy:

将步骤(1)称得的所需原料放入真空高频电磁感应加热炉中; Put the required raw materials weighed in step (1) into the vacuum high-frequency electromagnetic induction heating furnace;

调节真空磁悬浮熔炼炉的真空度2×10-3~5×10-3Pa,然后充高纯氩气使真空室的真空度至0.1×10-3~0.8×10-3Pa熔炼,合金锭反复熔炼至少三次; Adjust the vacuum degree of the vacuum magnetic levitation melting furnace to 2×10 -3 ~ 5×10 -3 Pa, and then fill the high-purity argon to make the vacuum degree of the vacuum chamber to 0.1×10 -3 ~ 0.8×10 -3 Pa to melt the alloy ingot repeated smelting at least three times;

(3)铜模吸铸法制备非晶复合材料试样: (3) Preparation of amorphous composite material samples by copper mold suction casting method:

将步骤(2)制备的(Ti0.50Ni0.50-yMy)100-xCux母合金放入悬浮熔炼水冷坩埚中重熔,调节真空磁悬浮熔炼炉的真空度2×10-3~5×10-3Pa,然后充高纯氩气使真空室的真空度至0.1×10-3~0.8×10-3Pa; Put the (Ti 0.50 Ni 0.50-y M y ) 100-x Cu x master alloy prepared in step (2) into a suspension melting water-cooled crucible for remelting, and adjust the vacuum degree of the vacuum magnetic levitation melting furnace to 2×10 -3 ~5× 10 -3 Pa, and then filled with high-purity argon to make the vacuum of the vacuum chamber to 0.1×10 -3 ~0.8×10 -3 Pa;

在感应电压5~10kV下熔炼时间1~3min后,通过负压铜模吸铸法将母合金吸铸成棒材。 After smelting for 1-3 minutes under the induction voltage of 5-10kV, the master alloy is suction-cast into rods by negative-pressure copper mold suction casting.

 本发明与现有技术相比,有显著优点:所发明的复合材料以Ti基非晶合金作为基体材料,相比于单相非晶合金和以往的内生Ti基非晶复合材料,基体中原位析出具有形变诱导相变性质形状记忆晶相作为强韧相,达到显著提高强度和塑性的目的,并表现出强烈的加工硬化。 Compared with the prior art, the present invention has significant advantages: the invented composite material uses Ti-based amorphous alloy as matrix material, compared with single-phase amorphous alloy and previous endogenous Ti-based amorphous composite material, the matrix has The shape memory crystalline phase with deformation-induced phase transition properties is precipitated as a strong and tough phase, achieving the purpose of significantly improving strength and plasticity, and exhibiting strong work hardening.

附图说明 Description of drawings

图1为直径3mm的Ti基非晶复合材料的铸态XRD图,图2为直径3mm的Ti基非晶复合材料应力加载断裂后XRD图,图3为直径3mm的Ti基非晶复合材料的室温压缩应力应变曲线。 Figure 1 is the as-cast XRD pattern of a Ti-based amorphous composite material with a diameter of 3 mm, Figure 2 is the XRD pattern of a Ti-based amorphous composite material with a diameter of 3 mm after stress loading and fracture, and Figure 3 is the XRD pattern of a Ti-based amorphous composite material with a diameter of 3 mm Compressive stress-strain curves at room temperature.

具体实施方式 Detailed ways

 本发明是形状记忆晶相强韧化Ti基非晶复合材料及其制备方法,形状记忆晶相强韧化Ti基非晶复合材料,Ti基非晶合金和能够产生形变诱导相变的过冷奥氏体相B2-TiNi以及马氏体相B19’-TiNi复合而成。 The invention relates to a Ti-based amorphous composite material strengthened and toughened by a shape-memory crystalline phase and a preparation method thereof, a Ti-based amorphous composite material strengthened and toughened by a shape-memory crystalline phase, a Ti-based amorphous alloy and a supercooled material capable of producing deformation-induced phase transitions It is composed of austenite phase B2-TiNi and martensite phase B19'-TiNi.

 状记忆晶相强韧化Ti基非晶复合材料的制备方法,其步骤为: The preparation method of the Ti-based amorphous composite material strengthened and toughened by the shape memory crystal phase comprises the following steps:

(1)配料: (1) Ingredients:

按权利要求1所示的(Ti0.50Ni0.50-yMy)100-xCux名义成分称取各组分; Each component is weighed by (Ti 0.50 Ni 0.50-y M y ) 100-x Cu x nominal composition shown in claim 1;

(2)熔炼制(Ti0.50Ni0.50-yMy)100-xCux母合金: (2) Melting (Ti 0.50 Ni 0.50-y M y ) 100-x Cu x master alloy:

将步骤(1)称得的所需原料放入真空高频电磁感应加热炉中; Put the required raw materials weighed in step (1) into the vacuum high-frequency electromagnetic induction heating furnace;

调节真空磁悬浮熔炼炉的真空度2×10-3~5×10-3Pa,然后充高纯氩气使真空室的真空度至0.1×10-3~0.8×10-3Pa熔炼,合金锭反复熔炼至少三次; Adjust the vacuum degree of the vacuum magnetic levitation melting furnace to 2×10 -3 ~ 5×10 -3 Pa, and then fill the high-purity argon to make the vacuum degree of the vacuum chamber to 0.1×10 -3 ~ 0.8×10 -3 Pa to melt the alloy ingot repeated smelting at least three times;

(3)铜模吸铸法制备非晶复合材料试样: (3) Preparation of amorphous composite material samples by copper mold suction casting method:

将步骤(2)制备的(Ti0.50Ni0.50-yMy)100-xCux母合金放入悬浮熔炼水冷坩埚中重熔,调节真空磁悬浮熔炼炉的真空度2×10-3~5×10-3Pa,然后充高纯氩气使真空室的真空度至0.1×10-3~0.8×10-3Pa; Put the (Ti 0.50 Ni 0.50-y M y ) 100-x Cu x master alloy prepared in step (2) into a suspension melting water-cooled crucible for remelting, and adjust the vacuum degree of the vacuum magnetic levitation melting furnace to 2×10 -3 ~5× 10 -3 Pa, and then filled with high-purity argon to make the vacuum of the vacuum chamber to 0.1×10 -3 ~0.8×10 -3 Pa;

在感应电压5~10kV下熔炼时间1~3min后,通过负压铜模吸铸法将母合金吸铸成棒材。 After smelting for 1-3 minutes under the induction voltage of 5-10kV, the master alloy is suction-cast into rods by negative-pressure copper mold suction casting.

下面通过具体的实施例详述本发明。 The present invention is described in detail below through specific examples.

实施例1: Example 1:

Ti基非晶复合材料的成分为(Ti0.5Ni0.5)80Cu20,选用纯度大于99.99%的Ti和Cu、99.9%的Zr和Al,按原子百分比配好一定质量的原料后,放入真空高频电磁感应加热炉中,调节真空磁悬浮熔炼炉的真空度2×10-3~5×10-3Pa,然后充高纯氩气使真空室的真空度至0.1×10-3~0.8×10-3Pa熔炼,合金锭反复熔炼至少三次。再将母合金放入悬浮熔炼水冷坩埚中重熔,调节真空磁悬浮熔炼炉的真空度2×10-3~5×10-3Pa,然后充高纯氩气使真空室的真空度至0.1×10-3~0.8×10-3Pa。在感应电压5~10kV下熔炼时间1~3min后,通过负压铜模吸铸法将母合金吸铸成直径3mm棒材。 The composition of the Ti-based amorphous composite material is (Ti 0.5 Ni 0.5 ) 80 Cu 20 , select Ti and Cu with a purity greater than 99.99%, and Zr and Al with a purity of 99.9%. In the high-frequency electromagnetic induction heating furnace, adjust the vacuum degree of the vacuum magnetic levitation melting furnace to 2×10 -3 ~5×10 -3 Pa, and then fill the high-purity argon to make the vacuum degree of the vacuum chamber to 0.1×10 -3 ~0.8× Melting at 10 -3 Pa, the alloy ingot was smelted repeatedly at least three times. Then put the master alloy into the suspension smelting water-cooled crucible for remelting, adjust the vacuum degree of the vacuum magnetic levitation melting furnace to 2×10 -3 ~ 5×10 -3 Pa, and then fill the high-purity argon to make the vacuum degree of the vacuum chamber to 0.1× 10 -3 ~ 0.8×10 -3 Pa. After melting for 1-3 minutes at an induced voltage of 5-10 kV, the master alloy is suction-cast into a rod with a diameter of 3 mm by a negative-pressure copper mold suction casting method.

图1为吸铸试样的铸态XRD图,除了典型的非晶漫散射峰之外,还有明锐的晶体衍射峰叠加在漫散射峰之上,表明试样为非晶和晶体的复合结构。析出的主要晶体相为B2-TiNi,Pearson符号为cP2 (ClCs),点阵常数a0=0.301nm,为过冷奥氏体相;同时检测到B19’-TiNi相,晶体结构参数a0=0.2892,b0=0.4108,c0=0.4646,β=97.78o为马氏体相,由于铜模高的冷却速度快存在于铸态组织中。 Figure 1 is the as-cast XRD pattern of the suction casting sample. In addition to the typical amorphous diffuse scattering peaks, there are sharp crystal diffraction peaks superimposed on the diffuse scattering peaks, indicating that the sample is a composite structure of amorphous and crystalline. The main crystal phase precipitated is B2-TiNi, the Pearson symbol is cP2 (ClCs), and the lattice constant a 0 =0.301nm, which is a supercooled austenite phase; B19'-TiNi phase is detected at the same time, and the crystal structure parameter a 0 = 0.2892, b 0 =0.4108, c 0 =0.4646, β=97.78 o is the martensitic phase, which exists in the as-cast structure due to the high cooling rate of the copper mold.

图2为吸铸试样应力加载断裂后XRD图,除了典型的非晶漫散射峰之外,析出的主要晶体相B19’-TiNi相,与断裂前相比,应力加载后部分奥氏体向马氏体转变,马氏体析出量明显增加。 Figure 2 is the XRD pattern of the suction casting sample after stress loading and fracture. In addition to the typical amorphous diffuse scattering peak, the main crystal phase B19'-TiNi phase precipitated. Tensitic transformation, the amount of martensite precipitation increased significantly.

图3为吸铸试样的室温压缩应力应变曲线,该合金的的压缩屈服强度为 1384MPa,断裂强度为 2256MPa,压缩应变为 12.2%,并表现出强烈的加工硬化。 Figure 3 is the room temperature compressive stress-strain curve of the suction casting sample. The compressive yield strength of the alloy is 1384MPa, the fracture strength is 2256MPa, the compressive strain is 12.2%, and it shows strong work hardening.

实施例2: Example 2:

采用与实施例1相同的制备方法,Ti基非晶复合材料合金的成分为: Using the same preparation method as in Example 1, the composition of the Ti-based amorphous composite material alloy is:

原子百分比为(Ti0.5Ni0.48Zr0.02)80Cu20The atomic percentage is (Ti 0.5 Ni 0.48 Zr 0.02 ) 80 Cu 20 ,

如图1所示,吸铸试样的铸态组织为非晶基复合结构,析出主要晶体相为过冷奥氏体相B2-TiNi和马氏体相B19’ -TiNi。 As shown in Figure 1, the as-cast structure of the suction casting sample is an amorphous matrix composite structure, and the main crystal phases are supercooled austenite phase B2-TiNi and martensite phase B19’-TiNi.

如图2所示,与断裂前相比,应力加载后部分奥氏体向马氏体转变,马氏体析出量明显增加。 As shown in Figure 2, compared with before fracture, part of the austenite transformed into martensite after stress loading, and the amount of martensite precipitation increased significantly.

如图3,该合金的的压缩屈服强度为 1295MPa,断裂强度为 2360MPa,压缩应变为 11.6%,并表现出强烈的加工硬化。 As shown in Figure 3, the alloy has a compressive yield strength of 1295 MPa, a fracture strength of 2360 MPa, a compressive strain of 11.6%, and exhibits strong work hardening.

实施例3: Example 3:

采用与实施例1相同的制备方法,Ti基非晶复合材料合金的成分为: Using the same preparation method as in Example 1, the composition of the Ti-based amorphous composite material alloy is:

原子百分比为(Ti0.5Ni0.48Co0.02)80Cu20The atomic percentage is (Ti 0.5 Ni 0.48 Co 0.02 ) 80 Cu 20 ,

如图1所示,吸铸试样的铸态组织为非晶基复合结构,析出主要晶体相为过冷奥氏体相B2-TiNi和马氏体相B19’ -TiNi。 As shown in Figure 1, the as-cast structure of the suction casting sample is an amorphous matrix composite structure, and the main crystal phases are supercooled austenite phase B2-TiNi and martensite phase B19’-TiNi.

与断裂前相比,应力加载后部分奥氏体向马氏体转变,马氏体析出量明显增加。 Compared with before fracture, part of the austenite transforms into martensite after stress loading, and the amount of martensite precipitation increases significantly.

如图3所示,该合金的的压缩屈服强度为 1504MPa,断裂强度为 2582MPa,塑性应变为15%,并表现出强烈的加工硬化。 As shown in Fig. 3, the alloy has a compressive yield strength of 1504 MPa, a fracture strength of 2582 MPa, a plastic strain of 15%, and exhibits strong work hardening.

Claims (1)

1. a preparation method for shape memory crystalline phase highly malleablized Ti base amorphous composite, the steps include:
(1) prepare burden:
By atomic percentage, the composition of described Ti base amorphous composite is: (Ti 0.50ni 0.50-ym y) 100-xcu x, wherein: M is Co or Zr element, x=5 ~ 33, y=0 ~ 0.25 takes each component;
(2) melting system (Ti 0.50ni 0.50-ym y) 100-xcu xmother alloy:
The desired raw material that step (1) claims is put into vacuum high-frequency electromagnetic induction heating furnace;
Regulate the vacuum tightness 2 × 10 of vacuum magnetic suspension smelting furnace -3~ 5 × 10 -3pa, then fills vacuum tightness to 0.1 × 10 that high-purity argon gas makes vacuum chamber -3~ 0.8 × 10 -3pa melting, alloy pig melt back at least three times;
(3) copper mold casting prepares amorphous composite sample:
By (Ti prepared by step (2) 0.50ni 0.50-ym y) 100-xcu xwater-cooled suspension smelting crucible remelting put into by mother alloy, regulates the vacuum tightness 2 × 10 of vacuum magnetic suspension smelting furnace -3~ 5 × 10 -3pa, then fills vacuum tightness to 0.1 × 10 that high-purity argon gas makes vacuum chamber -3~ 0.8 × 10 -3pa;
(4) under induction voltage 5 ~ 10kV, after smelting time 1 ~ 3min, by negative pressure copper mold casting, bar is cast in mother alloy suction;
Described shape memory crystalline phase highly malleablized Ti base amorphous composite is that Ti base noncrystal alloy and the supercooled austenite phase B2-TiNi that can produce deformation induced trans-formation and martensitic phase B19 '-TiNi are composited; In preparation method, by doping and the composition adjustment acquisition different volumes mark supercooled austenite phase B2-TiNi and martensitic phase B19 '-TiNi of alloy, and there is strong amorphous formation ability; The compression yield strength of described matrix material is 1000 ~ 1800MPa, and breaking tenacity is 1400 ~ 2800MPa, and compressive strain is 10% ~ 20%, and shows strong work hardening.
CN201210539119.7A 2012-12-14 2012-12-14 Shape-memory crystalline-phase strengthened and toughened Ti-base amorphous composite material and preparation method thereof Expired - Fee Related CN102978541B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210539119.7A CN102978541B (en) 2012-12-14 2012-12-14 Shape-memory crystalline-phase strengthened and toughened Ti-base amorphous composite material and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210539119.7A CN102978541B (en) 2012-12-14 2012-12-14 Shape-memory crystalline-phase strengthened and toughened Ti-base amorphous composite material and preparation method thereof

Publications (2)

Publication Number Publication Date
CN102978541A CN102978541A (en) 2013-03-20
CN102978541B true CN102978541B (en) 2015-01-07

Family

ID=47852875

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210539119.7A Expired - Fee Related CN102978541B (en) 2012-12-14 2012-12-14 Shape-memory crystalline-phase strengthened and toughened Ti-base amorphous composite material and preparation method thereof

Country Status (1)

Country Link
CN (1) CN102978541B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103361501B (en) * 2013-07-18 2015-08-05 兰州理工大学 The preparation method of shape memory crystalline phase highly malleablized Ti base amorphous composite
CN104789910B (en) * 2015-03-06 2017-01-25 张临财 Ti-based amorphous alloy and method for making bone drill from the same
CN105177470B (en) * 2015-06-05 2017-04-19 北方民族大学 Titanium-based amorphous fiber and preparation method thereof
KR101752976B1 (en) * 2015-10-07 2017-07-11 서울대학교산학협력단 Fabricating method for metallic glass composite with controlling work hardening capacity and composites fabricated by the method
CN114109752B (en) * 2021-11-08 2023-07-28 上海交通大学 A shape memory alloy driving element
CN116949314B (en) * 2023-08-28 2025-06-27 哈尔滨工业大学 Multi-principal element shape memory alloy with high cycle stability and high-temperature linear super-elasticity, and preparation method and application thereof

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6682608B2 (en) * 1990-12-18 2004-01-27 Advanced Cardiovascular Systems, Inc. Superelastic guiding member

Also Published As

Publication number Publication date
CN102978541A (en) 2013-03-20

Similar Documents

Publication Publication Date Title
CN104498844B (en) A kind of large scale TRIP amorphous composite material and preparation method thereof
CN102978541B (en) Shape-memory crystalline-phase strengthened and toughened Ti-base amorphous composite material and preparation method thereof
CN107034383B (en) One kind is containing high-strength low mould β-Type Titanium Alloys of Si and the preparation method and application thereof
CN103789598B (en) A kind of directed TiAl-base alloy and preparation method thereof
Zhu et al. Microstructure and compressive properties of multiprincipal component AlCoCrFeNiCx alloys
CN103741080B (en) (Ti-Zr-Nb-Cu-Be)-O system amorphous composite and preparation method thereof
CN105986322B (en) A kind of magnetic phase transition material
CN106086713A (en) High entropy amorphous composite material and preparation method thereof
CN107287535A (en) A kind of big plastic high-strength degree zirconium-based bulk amorphous alloy and preparation method
CN115070052B (en) A new two-state structure nickel-titanium shape memory alloy and its 4D printing preparation method and application
CN100529130C (en) High-hardness titanium alloy and method for producing same
CN113637885B (en) Multicomponent FeNiCoAlTiZr super elastic alloy and preparation method thereof
CN106834942A (en) A kind of copper-containing nano-phase strengthened medium manganese steel and preparation method thereof
Chen et al. Hot deformation behavior of novel high-strength Mg-0.6 Mn-0.5 Al-0.5 Zn-0.4 Ca alloy
CN102912259B (en) Zirconium-based metal glass endogenic composite material and preparation method thereof
Wang et al. Hydrogen induced softening and hardening for hot workability of (TiB+ TiC)/Ti-6Al-4V composites
CN101654753A (en) TiNiNb/NbTi memory alloy composite material and preparation method thereof
CN113564441A (en) Fe-Ni-Co-Al-W alloy with super elasticity and preparation method thereof
CN105506517A (en) (Ti-Zr-Nb-Cu-Be)-N series amorphous composite material and preparation method thereof
Li et al. Ultrafine-grained Ti66Nb13Cu8Ni6. 8Al6. 2 composites fabricated by spark plasma sintering and crystallization of amorphous phase
Jiang et al. Effect of the cooling rate on the mechanical properties of Ti-Ni-Cu-Zr-based crystal/glassy alloys
CN100494437C (en) A method for dendrite spheroidization in bulk metallic glass composites
CN107164658B (en) A kind of dental pulp needle material and preparation method
CN106756646B (en) A kind of Strengthening and Toughening metal glass composite material and preparation method thereof
Matsugi et al. Compositional optimization of β type titanium alloys with shape memory ability and their characteristics

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20170526

Address after: 730050 Lanzhou City, Gansu Province Lan Ping, No. 287

Patentee after: LANZHOU POLYTECHNIC ALLOY POWDER Co.,Ltd.

Address before: 730050 Lanzhou City, Gansu Province Lan Ping, No. 287

Patentee before: Lanzhou University Of Technology

CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20150107

CF01 Termination of patent right due to non-payment of annual fee