CN106319286A - Low-cost titanium alloy and preparation method thereof - Google Patents
Low-cost titanium alloy and preparation method thereof Download PDFInfo
- Publication number
- CN106319286A CN106319286A CN201610985168.1A CN201610985168A CN106319286A CN 106319286 A CN106319286 A CN 106319286A CN 201610985168 A CN201610985168 A CN 201610985168A CN 106319286 A CN106319286 A CN 106319286A
- Authority
- CN
- China
- Prior art keywords
- alloy
- titanium
- titanium alloy
- low
- cost
- 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.)
- Pending
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C14/00—Alloys based on titanium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/03—Making non-ferrous alloys by melting using master alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
- C22F1/18—High-melting or refractory metals or alloys based thereon
- C22F1/183—High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Manufacture And Refinement Of Metals (AREA)
Abstract
本申请提供了一种低成本钛合金及其制备方法,所述钛合金以钛为主体元素,以α稳定元素B和β稳定元素Fe为合金元素,所述钛合金的各成分含量为:Fe:0.5‑5wt.%,B:0.05‑0.2wt.%,余量为钛和不可避免的杂质。制备方法为:按设计的合金成分比例将原材料加入到通入氩气的冷坩埚悬浮熔炼炉中,反复熔炼后得到铸锭,铸锭在相变点以上开坯锻造,对锻造合金取样进行热处理,最后进行结构及性能表征。本申请所提供的钛合金,合金成分均匀,组织细小,抗拉强度达到750MPa~850MPa,延伸率10‑15%,合金具有低成本的优势,在某些领域可以替代部分价格较昂贵的钛合金。
The application provides a low-cost titanium alloy and a preparation method thereof. The titanium alloy uses titanium as the main element, and the α-stable element B and the β-stable element Fe as alloy elements. The content of each component of the titanium alloy is: Fe : 0.5‑5wt.%, B: 0.05‑0.2wt.%, the balance is titanium and unavoidable impurities. The preparation method is as follows: according to the designed alloy composition ratio, the raw materials are added to the cold crucible suspension melting furnace with argon gas, and the ingot is obtained after repeated melting. The ingot is opened and forged above the phase transition point, and the forged alloy is sampled for heat treatment. , and finally carry out structure and performance characterization. The titanium alloy provided by this application has a uniform alloy composition, a fine structure, a tensile strength of 750MPa-850MPa, and an elongation of 10-15%. The alloy has the advantage of low cost and can replace some more expensive titanium alloys in some fields .
Description
技术领域technical field
本申请涉及一种低成本钛合金及其制备方法,属于钛合金材料技术领域。The application relates to a low-cost titanium alloy and a preparation method thereof, belonging to the technical field of titanium alloy materials.
背景技术Background technique
钛及钛合金因具有低密度、高比强度、耐高温、耐腐蚀、无磁、生物兼容等优异性能,在航空、航天、舰船等领域得到大量的应用,然而钛的高成本限制了钛及钛合金的应用范围,尤其在民用领域。目前工业钛合金中合金化元素多数使用V、Mo、Nb、Zr、Sn和Ta等贵重金属,使钛合金的成本居高不下,影响了钛合金的使用范围。Due to their low density, high specific strength, high temperature resistance, corrosion resistance, non-magnetic, biocompatibility and other excellent properties, titanium and titanium alloys have been widely used in aviation, aerospace, ships and other fields. However, the high cost of titanium limits the use of titanium. And the application scope of titanium alloy, especially in the civil field. At present, most of the alloying elements in industrial titanium alloys use precious metals such as V, Mo, Nb, Zr, Sn and Ta, which makes the cost of titanium alloys remain high and affects the scope of use of titanium alloys.
目前降低钛合金成本的途径有:通过改进原材料(海绵钛)的生产方式来降低原材料成本、采用廉价合金化元素、优化钛合金加工工艺、优化钛制品加工技术等各种方法。如公开号为CN102828058A,发明名称为《一种低成本钛合金的制备方法》的中国发明专利,利用Mo-Fe中间合金粉末与钛粉末均匀混合,压制后真空烧结,其中合金成分按质量分数计:Fe:1.5wt.%,Mo:2.5wt.%,提高了合金的塑性和疲劳性能,抗拉强度达到850MPa以上,延伸率不小于15%,断面收缩率不小于20%;然而Mo的价格仍然较贵,因此成本降低有限,只有Fe、Al、Si、Cr、C、O、N和B等资源丰富的廉价元素才能达到大幅度降低钛合金成本的目的。At present, the ways to reduce the cost of titanium alloys include: reducing the cost of raw materials by improving the production method of raw materials (titanium sponge), using cheap alloying elements, optimizing the processing technology of titanium alloys, and optimizing the processing technology of titanium products. For example, the publication number is CN102828058A, and the invention title is "A Preparation Method of Low-cost Titanium Alloy". The Chinese invention patent uses Mo-Fe master alloy powder and titanium powder to be evenly mixed, pressed and then vacuum sintered. The alloy composition is calculated by mass fraction. : Fe: 1.5wt.%, Mo: 2.5wt.%, improve the plasticity and fatigue properties of the alloy, the tensile strength reaches more than 850MPa, the elongation is not less than 15%, and the reduction of area is not less than 20%; however, the price of Mo It is still expensive, so the cost reduction is limited. Only cheap elements such as Fe, Al, Si, Cr, C, O, N and B can achieve the purpose of greatly reducing the cost of titanium alloys.
发明内容Contents of the invention
根据本申请的一个方面,提供了一种低成本钛合金,该钛合金采用Fe元素及B元素作为合金化元素,使得该钛合金的成本明显降低,同时,该钛合金的抗拉强度达到750MPa~850MPa,延伸率10-15%,其综合性能可以满足某些工程领域的要求。According to one aspect of the present application, a low-cost titanium alloy is provided, which uses Fe and B elements as alloying elements, so that the cost of the titanium alloy is significantly reduced, and at the same time, the tensile strength of the titanium alloy reaches 750MPa ~850MPa, elongation 10-15%, its comprehensive performance can meet the requirements of some engineering fields.
为了实现上述目的,本申请采用如下技术方案:In order to achieve the above object, the application adopts the following technical solutions:
一种低成本钛合金,其特征在于,所述钛合金以钛为主体元素,以α稳定元素B和β稳定元素Fe为合金元素,所述钛合金的各成分含量为:Fe:0.5-5wt.%,B:0.05-0.2wt.%,余量为钛和不可避免的杂质。A low-cost titanium alloy, characterized in that the titanium alloy uses titanium as the main element, the α-stable element B and the β-stable element Fe as alloy elements, and the content of each component of the titanium alloy is: Fe: 0.5-5wt .%, B: 0.05-0.2wt.%, the balance is titanium and unavoidable impurities.
优选地,所述钛合金的各成分含量为:Fe:2-5wt.%,B:0.1-0.2wt.%,余量为钛和不可避免的杂质。Preferably, the content of each component of the titanium alloy is: Fe: 2-5wt.%, B: 0.1-0.2wt.%, and the balance is titanium and unavoidable impurities.
优选地,所述钛合金的各成分含量为:Fe:3-4wt.%,B:0.1-0.15wt.%,余量为钛和不可避免的杂质。Preferably, the content of each component of the titanium alloy is: Fe: 3-4wt.%, B: 0.1-0.15wt.%, and the balance is titanium and unavoidable impurities.
优选地,所述钛合金中的钛由海绵钛提供,硼由Fe-B中间合金提供,铁由Fe-B中间合金和工业纯铁提供。Preferably, titanium in the titanium alloy is provided by sponge titanium, boron is provided by Fe-B master alloy, and iron is provided by Fe-B master alloy and industrial pure iron.
优选地,所述低成本钛合金中不可避免的杂质包括O≤0.07wt.%,C≤0.03wt.%,N≤0.01wt.%,Si≤0.02wt.%,H≤0.004wt.%,其它杂质元素含量均≤0.01wt.%。Preferably, the inevitable impurities in the low-cost titanium alloy include O≤0.07wt.%, C≤0.03wt.%, N≤0.01wt.%, Si≤0.02wt.%, H≤0.004wt.%, The contents of other impurity elements are all ≤0.01wt.%.
根据本申请的又一个方面,提供了一种低成本钛合金的制备方法。According to still another aspect of the present application, a method for preparing a low-cost titanium alloy is provided.
为了实现上述目的,本申请采用如下技术方案:In order to achieve the above object, the application adopts the following technical solutions:
一种低成本钛合金的制备方法,其特征在于,所述方法包括如下步骤:A method for preparing a low-cost titanium alloy, characterized in that the method comprises the steps of:
(1)按所述钛合金各成分含量计算出所需海绵钛、Fe-B中间合金和工业纯铁的量,并按照计算结果进行称量;(1) Calculate the amount of required sponge titanium, Fe-B master alloy and industrial pure iron according to the content of each component of the titanium alloy, and weigh according to the calculation results;
(2)将称量后的海绵钛、Fe-B中间合金和工业纯铁放入冷坩埚悬浮熔炼炉的水冷铜坩埚中进行熔炼,得到铸锭;(2) put the weighed titanium sponge, Fe-B master alloy and industrial pure iron into the water-cooled copper crucible of the cold crucible suspension smelting furnace for smelting to obtain an ingot;
(3)将步骤(2)所得的铸锭在相变点以上50-150℃开坯锻造成后制成棒材;(3) making the ingot obtained in step (2) into a bar after being billeted and forged at 50-150° C. above the phase transformation point;
(4)对步骤(3)所得的棒材取样后进行热处理后进行结构和性能的表征。(4) Sampling the rod obtained in step (3) and performing heat treatment to characterize its structure and properties.
优选地,所述步骤(2)具体包括:Preferably, said step (2) specifically includes:
将称量后的海绵钛、Fe-B中间合金和工业纯铁放入冷坩埚悬浮熔炼炉的水冷铜坩埚中,对所述冷坩埚悬浮熔炼炉的炉体抽真空后通入高纯氩气,在高温下进行首次熔炼;等待铸锭充分冷却后,把铸锭上下倒置放入水冷铜坩埚中进行再次熔炼,如此反复3-4次后为止。Put the weighed sponge titanium, Fe-B intermediate alloy and industrial pure iron into the water-cooled copper crucible of the cold crucible suspension melting furnace, vacuumize the furnace body of the cold crucible suspension melting furnace, and then pass high-purity argon gas into it , at high temperature for the first smelting; after the ingot is fully cooled, turn the ingot upside down and put it into a water-cooled copper crucible for re-smelting, repeating this for 3-4 times until.
优选地,所述在高温下进行首次熔炼,是指在1500-1800℃时进行10-20min的首次熔炼,再次熔炼的温度和时间与首次熔炼相同;优选在1600℃下进行15min的首次熔炼。Preferably, the first smelting at high temperature refers to the first smelting at 1500-1800° C. for 10-20 minutes, and the temperature and time for re-smelting are the same as the first smelting; preferably the first smelting at 1600° C. for 15 minutes.
优选地,步骤(2)中,对炉体抽真空后通入高纯氩气,所述高纯氩气是指纯度为99.999%的氩气,通入量为0.5-0.7×105Pa。Preferably, in step (2), high-purity argon gas is introduced after the furnace body is evacuated, and the high-purity argon gas refers to argon gas with a purity of 99.999%, and the input volume is 0.5-0.7×10 5 Pa.
优选地,步骤(4)中所述的热处理,是指将棒材加热至800-850℃保温0.5-2h后空冷,再进行400-600℃保温0.5-2h后空冷;优选将棒材加热至810-840℃保温1-1.5h后空冷,再进行500℃保温1h后空冷。Preferably, the heat treatment described in step (4) refers to heating the bar to 800-850°C for 0.5-2h and air cooling, then air cooling at 400-600°C for 0.5-2h; preferably heating the bar to Keep warm at 810-840°C for 1-1.5h, then air cool, then keep warm at 500°C for 1h, then air cool.
本申请能产生的有益效果包括:The beneficial effect that this application can produce comprises:
1)本申请所提供的一种低成本的钛合金,各成分含量:Fe:0.5-5wt.%,B:0.05-0.2wt.%,余量为钛和不可避免的杂质;低成本钛合金中不可避免杂质含量为:O≤0.07wt.%,C≤0.03wt.%,N≤0.01wt.%,Si≤0.02wt.%,H≤0.004wt.%,其他杂质元素含量均≤0.01wt.%,总杂质含量≤0.2wt.%。1) A low-cost titanium alloy provided by this application, the content of each component: Fe: 0.5-5wt.%, B: 0.05-0.2wt.%, the balance is titanium and unavoidable impurities; low-cost titanium alloy The unavoidable impurity content is: O ≤ 0.07wt.%, C ≤ 0.03wt.%, N ≤ 0.01wt.%, Si ≤ 0.02wt.%, H ≤ 0.004wt.%, other impurity elements are ≤ 0.01wt. .%, total impurity content ≤ 0.2wt.%.
本申请所提供的钛合金,合金成分均匀,组织细小,抗拉强度达到750MPa~850MPa,延伸率10-15%,合金具有低成本的优势,在某些领域可以替代部分价格较昂贵的钛合金。The titanium alloy provided by this application has uniform alloy composition, fine structure, tensile strength of 750MPa-850MPa, and elongation of 10-15%. The alloy has the advantage of low cost and can replace some more expensive titanium alloys in some fields .
本申请中,Fe作为钛合金的β稳定元素,其市场价格低廉,Fe加入β钛合金中,可以加快合金时效响应速度,达到时效强度峰值所需时间也较短;Fe含量过多时,容易发生偏析形成“β斑”;而钛中加入B元素可以有效的细化铸态组织并阻碍后续加工过程中已细化晶粒的长大,从而减少变形火次,达到降低成本的目的。In this application, Fe is a β stable element of titanium alloy, and its market price is low. Adding Fe to β titanium alloy can speed up the aging response speed of the alloy, and the time required to reach the peak aging strength is also shorter; when the Fe content is too much, it is easy to occur Segregation forms "β spots"; adding B element to titanium can effectively refine the as-cast structure and hinder the growth of refined grains in the subsequent processing process, thereby reducing the number of deformation fires and achieving the purpose of reducing costs.
2)本申请所提供的一种低成本的钛合金的制备方法,其制备原料采用海绵钛、Fe-B中间合金、工业纯铁;中间合金成本如表1所示,Fe-B中间合金成本低于其他中间合金的成本,Fe-B中间合金的成本如表2所示。2) The preparation method of a kind of low-cost titanium alloy provided by the application, its preparation raw material adopts sponge titanium, Fe-B master alloy, industrial pure iron; Master alloy cost is as shown in table 1, and Fe-B master alloy cost Lower than the cost of other master alloys, the cost of Fe-B master alloy is shown in Table 2.
表1.近些年几种中间合金成本Table 1. Costs of several master alloys in recent years
表2.Fe-B中间合金成分Table 2. Fe-B master alloy composition
附图说明Description of drawings
图1为实施例1所得的低成本钛合金的微观结构图;Fig. 1 is the microstructure figure of the low-cost titanium alloy obtained in embodiment 1;
图2为实施例2所得的低成本钛合金的微观结构图;Fig. 2 is the microstructure figure of the low-cost titanium alloy obtained in embodiment 2;
图3为实施例3所得的低成本钛合金的微观结构图。FIG. 3 is a microstructure diagram of the low-cost titanium alloy obtained in Example 3.
具体实施方式detailed description
下面结合实施例详述本申请,但本申请并不局限于这些实施例。The present application is described in detail below in conjunction with the examples, but the present application is not limited to these examples.
如无特别说明,本申请的实施例中的原料均通过商业途径购买。Unless otherwise specified, the raw materials in the examples of the present application were purchased through commercial channels.
为使本申请的目的、技术方案和优点更加清楚明了,下面结合具体实施方式,对本发明进一步详细说明。应该理解,这些描述只是示例性的,而并非要限制本发明的范围。In order to make the purpose, technical solution and advantages of the present application clearer, the present invention will be further described in detail below in conjunction with specific embodiments. It should be understood that these descriptions are exemplary only, and are not intended to limit the scope of the present invention.
实施例1Example 1
1、本申请的合金成分设计的元素比例如表3所示。1. The element ratios of the alloy composition design of the present application are shown in Table 3.
2、将购买的海绵钛、Fe-B中间合金、工业纯铁按每铸锭1.5kg的比例进行配比,再放入冷坩埚悬浮熔炼炉的水冷铜坩埚中,对炉体抽真空后通入纯度为99.999%的氩气,通入量为0.5×105Pa的高纯氩气,在1500℃时进行20min的合金首次熔炼。2. Proportion the purchased sponge titanium, Fe-B intermediate alloy and industrial pure iron according to the ratio of 1.5kg per ingot, and then put them into the water-cooled copper crucible of the cold crucible suspension melting furnace, vacuumize the furnace body and pass Argon gas with a purity of 99.999% and high-purity argon gas with an amount of 0.5×10 5 Pa were injected, and the alloy was melted for the first time at 1500° C. for 20 minutes.
3、等待铸锭充分冷却后,把铸锭上下倒置放入水冷铜坩埚中进行再次熔炼使合金成分均匀化,如此反复3-4次后为止。3. After the ingot is fully cooled, turn the ingot upside down and put it into a water-cooled copper crucible for re-melting to homogenize the alloy composition, and repeat this for 3-4 times.
4、根据GB/T23605-2009钛合金β转变温度测定方法,测定制得合金的相变温度。4. According to the GB/T23605-2009 method for measuring the beta transition temperature of titanium alloys, the phase transition temperature of the obtained alloy was measured.
5、铸锭在相变点以上50-150℃开坯锻造成后制成棒材。5. The ingot is forged at 50-150°C above the phase transition point and then made into a bar.
6、对棒材取样后进行840℃保温1h后空冷,再进行500℃保温1h后空冷的热处理制度。6. After sampling the bar, heat it at 840°C for 1 hour and then air-cool it, then carry out the heat treatment system of holding it at 500°C for 1 hour and then air-cool it.
7、对热处理后合金进行微观结构表征,见图1,并按照国标GB/T228.1-2010的要求进行力学性能测试,性能见表4。7. Perform microstructure characterization of the alloy after heat treatment, as shown in Figure 1, and perform mechanical property tests in accordance with the requirements of the national standard GB/T228.1-2010, and see Table 4 for properties.
表3.实施例1中合金的配比成分Table 3. The proportioning composition of alloy in embodiment 1
表4.实施例1中棒材的力学性能Table 4. Mechanical properties of rods in Example 1
实施例2Example 2
(1)本申请的合金成分设计的元素比例如表5所示。(1) Table 5 shows the element ratios of the alloy composition design of the present application.
(2)将购买的海绵钛、Fe-B中间合金、工业纯铁按每铸锭1.5kg的比例进行配比,再放入冷坩埚悬浮熔炼炉的水冷铜坩埚中,对炉体抽真空后通入纯度为99.999%的氩气,通入量为0.6×105Pa的高纯氩气,在1800℃时进行10min的合金首次熔炼。(2) Proportion the purchased sponge titanium, Fe-B intermediate alloy, and industrial pure iron according to the ratio of 1.5kg per ingot, and then put them into the water-cooled copper crucible of the cold crucible suspension melting furnace, and vacuumize the furnace body Argon with a purity of 99.999% and high-purity argon with an amount of 0.6×10 5 Pa was introduced, and the alloy was melted for the first time at 1800° C. for 10 minutes.
(3)等待铸锭充分冷却后,把铸锭上下倒置放入水冷铜坩埚中进行再次熔炼使合金成分均匀化,如此反复3-4次后为止。(3) After the ingot is fully cooled, turn the ingot upside down and put it into a water-cooled copper crucible for re-melting to homogenize the alloy composition, and repeat this process for 3-4 times.
(4)根据GB/T 23605-2009钛合金β转变温度测定方法,测定制得合金的相变温度。(4) According to the GB/T 23605-2009 method for measuring the β-transition temperature of titanium alloys, the phase transition temperature of the obtained alloy was measured.
(5)铸锭在相变点以上50-150℃开坯锻造成后制成棒材。(5) The ingot is forged at 50-150°C above the phase transition point and then made into a bar.
(6)对棒材取样后进行810℃保温1h后空冷,再进行500℃保温1h后空冷的热处理制度。(6) After the bar is sampled, it is heat-treated at 810°C for 1 hour and then air-cooled, and then at 500°C for 1 hour and then air-cooled.
(7)对热处理后合金进行微观结构表征,见图2,并按照国标GB/T228.1-2010的要求进行力学性能测试,性能见表6。(7) Perform microstructure characterization of the alloy after heat treatment, as shown in Figure 2, and perform mechanical property tests in accordance with the requirements of the national standard GB/T228.1-2010, and see Table 6 for properties.
表5.实施例2中合金的配比成分Table 5. Proportioning composition of alloy in embodiment 2
表6.实施例2中棒材的力学性能Table 6. Mechanical properties of rods in Example 2
实施例3Example 3
(1)本申请的合金成分设计的元素比例如表7所示。(1) Table 7 shows the element ratios of the alloy composition design of the present application.
(2)将购买的海绵钛、Fe-B中间合金、工业纯铁按每铸锭1.5kg的比例进行配比,再放入冷坩埚悬浮熔炼炉的水冷铜坩埚中,对炉体抽真空后通入纯度为99.999%的氩气,通入量为0.5×105Pa的高纯氩气,在1600℃时进行15min的合金首次熔炼。(2) Proportion the purchased sponge titanium, Fe-B intermediate alloy, and industrial pure iron according to the ratio of 1.5kg per ingot, and then put them into the water-cooled copper crucible of the cold crucible suspension melting furnace, and vacuumize the furnace body Argon gas with a purity of 99.999% and high-purity argon gas with an amount of 0.5×10 5 Pa was introduced, and the alloy was melted for the first time at 1600° C. for 15 minutes.
(3)等待铸锭充分冷却后,把铸锭上下倒置放入水冷铜坩埚中进行再次熔炼使合金成分均匀化,如此反复3-4次后为止。(3) After the ingot is fully cooled, turn the ingot upside down and put it into a water-cooled copper crucible for re-melting to homogenize the alloy composition, and repeat this process for 3-4 times.
(4)根据GB/T 23605-2009钛合金β转变温度测定方法,测定制得合金的相变温度。(4) According to the GB/T 23605-2009 method for measuring the β-transition temperature of titanium alloys, the phase transition temperature of the obtained alloy was measured.
(5)铸锭在相变点以上50-150℃开坯锻造成后制成棒材。(5) The ingot is forged at 50-150°C above the phase transition point and then made into a bar.
(6)对棒材取样后进行810℃保温1h后空冷,再进行500℃保温1h后空冷的热处理制度。(6) After the bar is sampled, it is heat-treated at 810°C for 1 hour and then air-cooled, and then at 500°C for 1 hour and then air-cooled.
(7)对热处理后合金进行微观结构表征,见图3,并按照国标GB/T228.1-2010的要求进行力学性能测试,性能见表8。(7) Perform microstructural characterization of the alloy after heat treatment, as shown in Figure 3, and perform mechanical performance tests in accordance with the requirements of the national standard GB/T228.1-2010, and see Table 8 for the properties.
表7.实施例3中合金的配比成分Table 7. Proportioning composition of alloy in embodiment 3
表8.实施例3中棒材的力学性能Table 8. Mechanical properties of rods in Example 3
以上所述,仅是本申请的几个实施例,并非对本申请做任何形式的限制,虽然本申请以较佳实施例揭示如上,然而并非用以限制本申请,任何熟悉本专业的技术人员,在不脱离本申请技术方案的范围内,利用上述揭示的技术内容做出些许的变动或修饰均等同于等效实施案例,均属于技术方案范围内。The above are only a few embodiments of the application, and do not limit the application in any form. Although the application is disclosed as above with preferred embodiments, it is not intended to limit the application. Any skilled person familiar with this field, Without departing from the scope of the technical solution of the present application, any changes or modifications made using the technical content disclosed above are equivalent to equivalent implementation cases, and all belong to the scope of the technical solution.
Claims (10)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610985168.1A CN106319286A (en) | 2016-10-25 | 2016-10-25 | Low-cost titanium alloy and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610985168.1A CN106319286A (en) | 2016-10-25 | 2016-10-25 | Low-cost titanium alloy and preparation method thereof |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106319286A true CN106319286A (en) | 2017-01-11 |
Family
ID=57816315
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610985168.1A Pending CN106319286A (en) | 2016-10-25 | 2016-10-25 | Low-cost titanium alloy and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106319286A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108842095A (en) * | 2018-05-22 | 2018-11-20 | 南京工业大学 | low-cost high-strength α + β titanium alloy and preparation method thereof |
CN109097628A (en) * | 2018-10-10 | 2018-12-28 | 广州宇智科技有限公司 | A kind of novel fire resistant titanium alloy that the 500-600 degree under non-oxidizing atmosphere uses |
CN109732084A (en) * | 2019-03-21 | 2019-05-10 | 西京学院 | A kind of iron-titanium-molybdenum alloy and preparation method thereof |
CN115522101A (en) * | 2022-09-19 | 2022-12-27 | 河北科技大学 | Fe-containing double-phase titanium-based alloy and preparation method thereof |
CN115747569A (en) * | 2022-12-30 | 2023-03-07 | 昆明理工大学 | Novel Ti-Fe-B alloy and preparation method thereof |
CN118726793A (en) * | 2024-08-21 | 2024-10-01 | 惠州至精精密技术有限公司 | A kind of free-cutting titanium material and its preparation process |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060234800A1 (en) * | 2005-03-30 | 2006-10-19 | Honda Motor Co., Ltd. | Titanium alloy bolt and its manufacturing process |
CN104831122A (en) * | 2015-05-19 | 2015-08-12 | 南京工业大学 | Low-cost high-performance titanium alloy and preparation method thereof |
-
2016
- 2016-10-25 CN CN201610985168.1A patent/CN106319286A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060234800A1 (en) * | 2005-03-30 | 2006-10-19 | Honda Motor Co., Ltd. | Titanium alloy bolt and its manufacturing process |
ES2286936B2 (en) * | 2005-03-30 | 2009-10-30 | Honda Motor Co., Ltd. | TITANIUM ALLOY BOLT AND PROCESS TO MANUFACTURE IT. |
CN104831122A (en) * | 2015-05-19 | 2015-08-12 | 南京工业大学 | Low-cost high-performance titanium alloy and preparation method thereof |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108842095A (en) * | 2018-05-22 | 2018-11-20 | 南京工业大学 | low-cost high-strength α + β titanium alloy and preparation method thereof |
CN109097628A (en) * | 2018-10-10 | 2018-12-28 | 广州宇智科技有限公司 | A kind of novel fire resistant titanium alloy that the 500-600 degree under non-oxidizing atmosphere uses |
CN109732084A (en) * | 2019-03-21 | 2019-05-10 | 西京学院 | A kind of iron-titanium-molybdenum alloy and preparation method thereof |
CN109732084B (en) * | 2019-03-21 | 2021-05-11 | 西京学院 | A kind of iron-titanium-molybdenum alloy and preparation method thereof |
CN115522101A (en) * | 2022-09-19 | 2022-12-27 | 河北科技大学 | Fe-containing double-phase titanium-based alloy and preparation method thereof |
CN115747569A (en) * | 2022-12-30 | 2023-03-07 | 昆明理工大学 | Novel Ti-Fe-B alloy and preparation method thereof |
CN118726793A (en) * | 2024-08-21 | 2024-10-01 | 惠州至精精密技术有限公司 | A kind of free-cutting titanium material and its preparation process |
CN118726793B (en) * | 2024-08-21 | 2025-06-17 | 惠州至精精密技术有限公司 | A kind of free-cutting titanium material and its preparation process |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106319286A (en) | Low-cost titanium alloy and preparation method thereof | |
CN109576621B (en) | A precise heat treatment method for nickel-based deformed superalloy parts | |
CN104831122A (en) | Low-cost high-performance titanium alloy and preparation method thereof | |
CN106521236B (en) | Fe-containing low-cost near β type high-strength titanium alloy and preparation method thereof | |
CN108103381A (en) | A kind of high-strength F eCoNiCrMn high-entropy alloys and preparation method thereof | |
CN109706363B (en) | Eutectic high-entropy alloy and preparation method thereof | |
CN107287535A (en) | A kind of big plastic high-strength degree zirconium-based bulk amorphous alloy and preparation method | |
CN108842095A (en) | low-cost high-strength α + β titanium alloy and preparation method thereof | |
CN109536777B (en) | A kind of high temperature titanium alloy and preparation method thereof | |
CN107460370A (en) | A kind of low-cost high-strength high-ductility metastable β Titanium-alloy and preparation method thereof | |
CN108130444A (en) | The preparation method of Al-Ti-B-RE Grain Refiner | |
CN111826545B (en) | Copper-iron alloy material and preparation method and application thereof | |
CN110819873A (en) | High Nb-TiAl alloy added with nano yttrium oxide and preparation method thereof | |
CN106947887B (en) | A kind of high-temperature titanium alloy composition design and multiway forging technique | |
CN107858574A (en) | A kind of weak texture wrought magnesium alloy of multielement complex intensifying and preparation method thereof | |
CN108411156A (en) | A kind of nearly β types high strength titanium alloy and preparation method thereof | |
CN107164653A (en) | A kind of rich Ti content Ti-Ni alloy with negative expansion performance and preparation method thereof | |
CN107829004A (en) | A kind of zinc-magnesium alloy ingot and preparation method thereof | |
CN108130443A (en) | Rare earth Al-Ti-B alloy and preparation method thereof | |
CN107299250A (en) | As cast condition is tough Ti3Al intermetallic compounds and its manufacture method and application | |
CN104862567B (en) | Preparation method of high-Sn wrought magnesium alloy panel | |
CN104294064B (en) | Cu is based bulk amorphous-preparation method of nanometer crystal alloy composite | |
CN115386768B (en) | 600 ℃/1 GPa-grade high-temperature ultrahigh-strength titanium alloy and preparation method thereof | |
CN102644013A (en) | High-strength and high-elongation cast magnesium alloy and production method thereof | |
CN109536776B (en) | Heat-resistant titanium alloy and preparation method thereof |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170111 |