CN115109959B - Titanium alloy with double-scale equiaxial structure and preparation method and application thereof - Google Patents
Titanium alloy with double-scale equiaxial structure and preparation method and application thereof Download PDFInfo
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- 229910001069 Ti alloy Inorganic materials 0.000 title claims abstract description 62
- 238000002360 preparation method Methods 0.000 title claims abstract description 19
- 239000010936 titanium Substances 0.000 claims abstract description 75
- 238000000034 method Methods 0.000 claims abstract description 37
- 239000000843 powder Substances 0.000 claims description 108
- 229910045601 alloy Inorganic materials 0.000 claims description 72
- 239000000956 alloy Substances 0.000 claims description 72
- 238000005245 sintering Methods 0.000 claims description 60
- 239000002994 raw material Substances 0.000 claims description 39
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 26
- 229910000883 Ti6Al4V Inorganic materials 0.000 claims description 25
- 229910052799 carbon Inorganic materials 0.000 claims description 25
- -1 titanium hydride Chemical compound 0.000 claims description 23
- 229910000048 titanium hydride Inorganic materials 0.000 claims description 23
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 21
- 238000003825 pressing Methods 0.000 claims description 20
- 238000000498 ball milling Methods 0.000 claims description 18
- 239000000203 mixture Substances 0.000 claims description 17
- 239000000463 material Substances 0.000 claims description 16
- 229910052719 titanium Inorganic materials 0.000 claims description 16
- HGCIXCUEYOPUTN-UHFFFAOYSA-N cyclohexene Chemical compound C1CCC=CC1 HGCIXCUEYOPUTN-UHFFFAOYSA-N 0.000 claims description 12
- 238000002156 mixing Methods 0.000 claims description 11
- 239000003153 chemical reaction reagent Substances 0.000 claims description 10
- 239000013078 crystal Substances 0.000 claims description 10
- 229920000642 polymer Polymers 0.000 claims description 8
- XDTMQSROBMDMFD-UHFFFAOYSA-N Cyclohexane Chemical compound C1CCCCC1 XDTMQSROBMDMFD-UHFFFAOYSA-N 0.000 claims description 7
- 229910052739 hydrogen Inorganic materials 0.000 claims description 5
- 229910052751 metal Inorganic materials 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims description 3
- 239000007788 liquid Substances 0.000 claims description 2
- 239000000126 substance Substances 0.000 claims description 2
- 239000013081 microcrystal Substances 0.000 claims 2
- 238000004321 preservation Methods 0.000 claims 2
- 229910001040 Beta-titanium Inorganic materials 0.000 claims 1
- 238000005275 alloying Methods 0.000 claims 1
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 22
- 230000000052 comparative effect Effects 0.000 description 15
- 229910052786 argon Inorganic materials 0.000 description 11
- 238000001272 pressureless sintering Methods 0.000 description 11
- 238000010438 heat treatment Methods 0.000 description 10
- 239000011159 matrix material Substances 0.000 description 9
- 239000007787 solid Substances 0.000 description 8
- 239000010935 stainless steel Substances 0.000 description 8
- 229910001220 stainless steel Inorganic materials 0.000 description 8
- 238000001816 cooling Methods 0.000 description 7
- 239000007789 gas Substances 0.000 description 5
- 238000000227 grinding Methods 0.000 description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 4
- 238000009694 cold isostatic pressing Methods 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 238000000465 moulding Methods 0.000 description 4
- 238000007712 rapid solidification Methods 0.000 description 4
- 238000001953 recrystallisation Methods 0.000 description 4
- 238000007711 solidification Methods 0.000 description 4
- 230000008023 solidification Effects 0.000 description 4
- 238000001291 vacuum drying Methods 0.000 description 4
- 229910000967 As alloy Inorganic materials 0.000 description 3
- 239000000047 product Substances 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 238000006356 dehydrogenation reaction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000000713 high-energy ball milling Methods 0.000 description 2
- 238000001000 micrograph Methods 0.000 description 2
- 230000006911 nucleation Effects 0.000 description 2
- 238000010899 nucleation Methods 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 239000011148 porous material Substances 0.000 description 2
- 238000006467 substitution reaction Methods 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000000280 densification Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000004821 distillation Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005324 grain boundary diffusion Methods 0.000 description 1
- 239000012761 high-performance material Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 239000013067 intermediate product Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000002159 nanocrystal Substances 0.000 description 1
- 238000012805 post-processing Methods 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000003584 silencer Effects 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 230000000930 thermomechanical effect Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/045—Alloys based on refractory metals
- C22C1/0458—Alloys based on titanium, zirconium or hafnium
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- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/02—Compacting only
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- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/02—Compacting only
- B22F3/04—Compacting only by applying fluid pressure, e.g. by cold isostatic pressing [CIP]
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/10—Sintering only
- B22F3/1003—Use of special medium during sintering, e.g. sintering aid
- B22F3/1007—Atmosphere
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/02—Making metallic powder or suspensions thereof using physical processes
- B22F9/04—Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C14/00—Alloys based on titanium
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- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/02—Making metallic powder or suspensions thereof using physical processes
- B22F9/04—Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling
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Abstract
本发明公开了一种双尺度等轴结构的钛合金及其制备方法与应用。该钛合金微观结构包括10‑30μm的等轴结构区域及其边界1‑2μm宽、7‑40μm长的连续微米晶β‑Ti板条相。其中,10‑30μm的等轴结构区域包括100‑400nm的等轴超细晶α‑Ti相,及其晶界100‑150nm宽、280‑900nm长的超细晶β‑Ti板条相。所述连续微米晶β‑Ti板条相和超细晶β‑Ti板条相构成双尺度结构,等轴超细晶α‑Ti相及其组成的微米级等轴结构区域构成等轴结构。本发明方法所得钛合金的力学性能较传统无压烧结钛合金具有极大提升,相比现有制备双尺度结构钛合金方法具有工艺简单、成本低和制品尺寸、结构自由度高等优势。
The invention discloses a titanium alloy with a dual-scale equiaxed structure and its preparation method and application. The titanium alloy microstructure includes a 10-30μm equiaxed structure region and its boundary is a continuous micron-crystalline β-Ti lath phase of 1-2μm wide and 7-40μm long. Among them, the 10-30μm equiaxed structure region includes the 100-400nm equiaxed ultra-fine-grained α-Ti phase and its grain boundary 100-150nm wide and 280-900nm long ultra-fine-grained β-Ti lath phase. The continuous micron-crystalline β-Ti lath phase and the ultra-fine-grain β-Ti lath phase constitute a dual-scale structure, and the equiaxed ultra-fine-grain α-Ti phase and the micron-scale equiaxed structural regions thereof constitute an equiaxed structure. The mechanical properties of the titanium alloy obtained by the method of the present invention are greatly improved compared with the traditional pressureless sintered titanium alloy. Compared with the existing method of preparing dual-scale structure titanium alloy, it has the advantages of simple process, low cost and high degree of freedom in product size and structure.
Description
技术领域Technical field
本发明属于钛合金技术领域,特别涉及一种双尺度等轴结构的钛合金及其制备方法与应用。The invention belongs to the technical field of titanium alloys, and particularly relates to a titanium alloy with a dual-scale equiaxed structure and its preparation method and application.
背景技术Background technique
钛及钛合金作为重要的金属结构材料之一,是国家和相关研究者重点的发展对象,其广泛应用于航空航天的压力机,阻流板,发动机舱、化工领域的反应器,电解槽,蒸馏塔、海洋工程领域的管道,钻探用泵、汽车领域的排气和消音系统、弹簧、连杆。依据微观组织决定宏观性能的材料理论,通过调控钛合金的微观结构(晶粒尺寸、相分布和形态)可以有效地优化其力学性能,并实现高强钛合金的制备。As one of the important metal structural materials, titanium and titanium alloys are the focus of development by the country and relevant researchers. They are widely used in aerospace presses, baffles, engine nacelles, reactors in the chemical industry, and electrolytic cells. Distillation towers, pipelines in the offshore engineering field, pumps for drilling, exhaust and silencer systems, springs, connecting rods in the automotive field. According to the material theory that microstructure determines macroscopic properties, by regulating the microstructure (grain size, phase distribution and morphology) of titanium alloys, its mechanical properties can be effectively optimized and the preparation of high-strength titanium alloys can be achieved.
细化晶粒至纳米晶(<100nm)和超细晶范畴(100-1000nm)可以有效地提高钛合金块体的强度,但是由于其缺少应变硬化能力而通常具有较低的塑性。通过在钛合金基体中引入多尺度的晶粒搭配(如超细晶和微米晶)可以实现钛合金强度与塑性的搭配。目前,制备双尺度结构钛合金的方法包括块体合金塑性变形-热处理诱发再结晶,不同尺寸原料粉末的混合固结,非晶晶化-固态烧结和半固态烧结,铜模快速凝固方法。然而,上述方法均存在工序复杂,制备的块体材料尺寸受限,制备成本高等问题,使得上述高性能材料难以推广应用。Refining the grains to nanocrystals (<100nm) and ultra-fine grains (100-1000nm) can effectively improve the strength of titanium alloy blocks, but they usually have low plasticity due to their lack of strain hardening ability. By introducing multi-scale grain matching (such as ultra-fine grains and micron grains) into the titanium alloy matrix, the strength and plasticity of titanium alloys can be matched. At present, methods for preparing dual-scale structure titanium alloys include plastic deformation of bulk alloys-heat treatment induced recrystallization, mixed solidification of raw material powders of different sizes, amorphous crystallization-solid sintering and semi-solid sintering, and copper mold rapid solidification methods. However, the above methods all have problems such as complicated processes, limited size of the prepared bulk materials, and high preparation costs, making it difficult to popularize and apply the above high-performance materials.
以氢化钛粉末代替纯钛粉末成形钛材料是降低粉末冶金钛材料的重要方法。氢化钛是氢化脱氢钛粉的中间产物,其成本较纯钛粉低。此外,氢化钛烧结过程中的脱氢效应有效地加速致密化,使得不需要后处理便可制备高致密度的钛合金块体。然而,目前无压烧结制备的钛合金通常具有尺寸大于100μm的α集束尺寸,使得无压烧结的钛合金抗拉强度难以突破1000MPa。现报道的无压烧结Ti-6Al-4V合金块体抗拉强度为830-970MPa,拉伸塑性为12.5-5%。(Metallurgical and Materials Transactions A,48(2017)2301–2319)。一般采用热机械处理、热氢处理进一步提高其力学性能,但同样提高了高性能钛合金的制备成本并限制了合金的尺寸、形状自由度。有鉴于此,如果能通过氢化钛或纯钛粉末烧结的工艺调控,获得超细晶β-Ti板条相,微米晶β-Ti板条相和超细等轴晶α-Ti共存的双尺度结构钛合金,将可低成本地制备出高强度的钛合金,并实现其在航空航天、装甲车、兵器、船舶、汽车领域等高强结构件或耐磨结构件中的低成本应用,将具有重要的理论和工程意义。Using hydrogenated titanium powder instead of pure titanium powder to form titanium materials is an important method to reduce the cost of powder metallurgy titanium materials. Titanium hydride is an intermediate product of hydrogenated and dehydrogenated titanium powder, and its cost is lower than that of pure titanium powder. In addition, the dehydrogenation effect during the titanium hydride sintering process effectively accelerates densification, making it possible to prepare high-density titanium alloy blocks without post-processing. However, titanium alloys currently prepared by pressureless sintering usually have α cluster sizes larger than 100 μm, making it difficult for the tensile strength of pressureless sintered titanium alloys to exceed 1000MPa. The reported tensile strength of the pressureless sintered Ti-6Al-4V alloy block is 830-970MPa, and the tensile plasticity is 12.5-5%. (Metallurgical and Materials Transactions A, 48 (2017) 2301–2319). Thermomechanical treatment and thermal hydrogen treatment are generally used to further improve its mechanical properties, but this also increases the preparation cost of high-performance titanium alloys and limits the freedom of size and shape of the alloy. In view of this, if the sintering process of titanium hydride or pure titanium powder can be controlled, a dual-scale coexistence of ultra-fine crystal β-Ti lath phase, micron crystal β-Ti lath phase and ultra-fine equiaxed α-Ti can be obtained. Structural titanium alloy will be able to prepare high-strength titanium alloy at low cost and realize its low-cost application in high-strength structural parts or wear-resistant structural parts in aerospace, armored vehicles, weapons, ships, automobiles and other fields, which will be of great importance. theoretical and engineering significance.
发明内容Contents of the invention
为了克服上述现有技术的缺点与不足,本发明的首要目的在于提供一种双尺度等轴结构的钛合金。In order to overcome the above-mentioned shortcomings and deficiencies of the prior art, the primary purpose of the present invention is to provide a titanium alloy with a dual-scale equiaxed structure.
本发明另一目的在于上述双尺度等轴结构的钛合金的制备方法。Another object of the present invention lies in the preparation method of the titanium alloy with the above-mentioned dual-scale equiaxed structure.
本发明再一目的在于提供上述双尺度等轴结构的钛合金航空航天、装甲车、兵器、船舶、汽车领域等高强结构件或耐磨结构件中的低成本应用。Another object of the present invention is to provide the low-cost application of the above-mentioned dual-scale equiaxed structure titanium alloy in high-strength structural parts or wear-resistant structural parts in the fields of aerospace, armored vehicles, weapons, ships, and automobiles.
本发明的目的通过下述方案实现。The object of the present invention is achieved through the following solutions.
一种双尺度等轴结构的钛合金的制备方法,包括以下制备步骤:A method for preparing a titanium alloy with a dual-scale equiaxed structure, including the following preparation steps:
(1)合金粉末含碳处理:将目标钛合金成分的合金元素粉末与含碳高分子试剂共混,再进行球磨;所述含碳高分子试剂为只含C和H的高分子液体;(1) Carbon-containing treatment of alloy powder: blend the alloy element powder of the target titanium alloy composition with a carbon-containing polymer reagent, and then perform ball milling; the carbon-containing polymer reagent is a polymer liquid containing only C and H;
(2)烧结原料混合:将步骤(1)所得混合物与钛原料粉末按照目标钛合金成分混合均匀,得到烧结原料;(2) Mixing of sintering raw materials: Mix the mixture obtained in step (1) and titanium raw material powder evenly according to the target titanium alloy composition to obtain sintering raw materials;
(3)无压烧结成形:将步骤(2)所得烧结原料进行压制和烧结成形,得到双尺度等轴结构的钛合金。(3) Pressureless sintering forming: The sintered raw material obtained in step (2) is pressed and sintered to form a titanium alloy with a dual-scale equiaxed structure.
优选的,所述含碳高分子试剂为环己烷和环己烯的一种。Preferably, the carbon-containing polymer reagent is one of cyclohexane and cyclohexene.
优选的,所述含碳高分子试剂的用量相对于每100g合金元素粉末的用量为20-40mL。Preferably, the amount of the carbon-containing polymer reagent is 20-40 mL relative to the amount per 100 g of alloy element powder.
优选的,所述目标钛合金为α+β双相钛合金;对应的,目标钛合金成分的合金元素粉末为相应的中间合金粉末或金属单质粉末;所述合金元素粉末的粒径为10-45μm。Preferably, the target titanium alloy is an α+β dual-phase titanium alloy; correspondingly, the alloy element powder of the target titanium alloy component is the corresponding intermediate alloy powder or metal elemental powder; the particle size of the alloy element powder is 10- 45μm.
优选的,所述球磨的设备为QM-2SP20,球磨的转速为250-400rpm、球料比为5:1-20:1、球磨时间30h-50h;或其他型号球磨设备及等效工艺参数。Preferably, the ball milling equipment is QM-2SP20, the ball milling speed is 250-400rpm, the ball-to-material ratio is 5:1-20:1, and the ball milling time is 30h-50h; or other types of ball milling equipment and equivalent process parameters.
优选的,所述钛原料粉末为纯钛粉末或氢化钛粉末TiHx,其中0<x<2,粒径为25-150μm。Preferably, the titanium raw material powder is pure titanium powder or titanium hydride powder TiH x , where 0<x<2, and the particle size is 25-150 μm.
优选的,所述压制和烧结成形的方式为模压-真空烧结或冷等静压-真空烧结。Preferably, the pressing and sintering forming method is molding-vacuum sintering or cold isostatic pressing-vacuum sintering.
优选的,Preferably,
所述压制和烧结成形的方式为模压-真空烧结;其中,模压压力为400-1000MPa,保压时间为1-120s,真空烧结温度为800-1500℃,保温时间为1-5h;The pressing and sintering forming method is molding-vacuum sintering; wherein, the molding pressure is 400-1000MPa, the holding time is 1-120s, the vacuum sintering temperature is 800-1500°C, and the holding time is 1-5h;
所述压制和烧结成形的方式为冷等静压-真空烧结;其中,压制压力为100-350MPa,保压时间为1-600s,真空烧结温度为800-1500℃,保温时间为1-5h。The pressing and sintering forming method is cold isostatic pressing-vacuum sintering; wherein the pressing pressure is 100-350MPa, the holding time is 1-600s, the vacuum sintering temperature is 800-1500°C, and the holding time is 1-5h.
由以上任一项所述的制备方法制得的一种双尺度等轴结构的钛合金。A titanium alloy with a dual-scale equiaxed structure prepared by any of the above preparation methods.
优选的,钛合金微观结构包括10-30μm的等轴结构区域及其边界1-2μm宽、7-40μm长的连续微米晶β-Ti板条相。其中,10-30μm的等轴结构区域包括100-400nm的等轴超细晶α-Ti相,及其晶界100-150nm宽、280-900nm长的超细晶β-Ti板条相。连续微米晶β-Ti板条相和超细晶β-Ti板条相构成双尺度结构,等轴超细晶α-Ti相及其组成的微米级等轴结构区域构成等轴结构。Preferably, the titanium alloy microstructure includes an equiaxed structure region of 10-30 μm and a continuous micron-crystalline β-Ti lath phase with a boundary of 1-2 μm wide and 7-40 μm long. Among them, the 10-30 μm equiaxed structure region includes an equiaxed ultra-fine grain α-Ti phase of 100-400 nm, and an ultra-fine grain β-Ti lath phase with a grain boundary of 100-150 nm wide and 280-900 nm long. The continuous micron-crystalline β-Ti lath phase and the ultra-fine-grain β-Ti lath phase constitute a dual-scale structure, and the equiaxed ultra-fine-grain α-Ti phase and its composed micron-scale equiaxed structural regions constitute an equiaxed structure.
以上所述的一种双尺度等轴结构的钛合金在航空航天、装甲车、兵器、船舶、汽车领域中高强耐磨结构件的应用。The above-mentioned dual-scale equiaxed structure titanium alloy is used in high-strength and wear-resistant structural parts in the fields of aerospace, armored vehicles, weapons, ships, and automobiles.
本发明将含碳高分子试剂与合金元素粉末混合后进行高能球磨,是为了在高能球磨过程中,含碳高分子试剂在磨球的碰撞及高温条件下分解出游离的C和H,并固溶至合金元素粉末中;含C、H的合金粉末与钛原料粉末(纯钛或氢化钛粉末)混合烧结过程中,游离的H以及氢化钛脱氢产生的H元素在真空条件下挥发,而固溶的C扩散至钛基体中,阻碍β-Ti高温时的晶界扩散,并为冷却时的β→α相变提供形核点,从而形成微米晶和超细晶共存的双尺度等轴结构钛合金。In the present invention, the carbon-containing polymer reagent is mixed with the alloy element powder and then subjected to high-energy ball milling, so that during the high-energy ball milling process, the carbon-containing polymer reagent decomposes free C and H under the collision of the grinding balls and high temperature conditions, and solidifies them. Dissolved into the alloy element powder; during the mixing and sintering process of the alloy powder containing C and H and the titanium raw material powder (pure titanium or titanium hydride powder), the free H and the H element generated by the dehydrogenation of titanium hydride volatilize under vacuum conditions, and The solid solution of C diffuses into the titanium matrix, hindering the grain boundary diffusion of β-Ti at high temperatures and providing nucleation points for the β→α phase transformation during cooling, thus forming a dual-scale equiaxed structure in which micron and ultra-fine grains coexist. Structural titanium alloy.
与现有技术相比,本发明具有如下优点与技术效果:Compared with the existing technology, the present invention has the following advantages and technical effects:
(1)通过本发明的方法能够制备超细晶β-Ti板条相,微米晶β-Ti板条相和超细等轴晶α-Ti构成双尺度等轴结构的钛合金。(1) The method of the present invention can prepare ultrafine-grained β-Ti lath phase, and micron-crystalline β-Ti lath phase and ultrafine equiaxed-crystal α-Ti constitute a titanium alloy with a dual-scale equiaxed structure.
(2)本发明的双尺度等轴结构钛合金具有优异的力学性能和较低的制备成本,可应用于航空航天、装甲车、兵器、船舶、汽车等领域中的高强或耐磨结构件。(2) The dual-scale equiaxed structure titanium alloy of the present invention has excellent mechanical properties and low preparation cost, and can be used in high-strength or wear-resistant structural parts in aerospace, armored vehicles, weapons, ships, automobiles and other fields.
附图说明Description of drawings
图1为实施例1得到的双尺度等轴结构钛合金的扫描电镜图。Figure 1 is a scanning electron microscope image of the dual-scale equiaxed structure titanium alloy obtained in Example 1.
图2为对比例1得到的常规无压烧结Ti-6Al-4V合金的扫描电镜图。Figure 2 is a scanning electron microscope image of the conventional pressureless sintered Ti-6Al-4V alloy obtained in Comparative Example 1.
图3为实施例1和对比例1得到Ti-6Al-4V合金的力学性能曲线图。Figure 3 is a graph showing the mechanical properties of the Ti-6Al-4V alloy obtained in Example 1 and Comparative Example 1.
具体实施方式Detailed ways
下面结合实施例对本发明作进一步详细的描述,但本发明的实施方式不限于此。下列实施例中涉及的物料若无特殊说明均可从商业渠道获得。所述方法若无特别说明均为常规方法。以下的“质量份”、“体积份”对应的单位分别是g、mL。The present invention will be described in further detail below with reference to examples, but the implementation of the present invention is not limited thereto. The materials involved in the following examples can be obtained from commercial sources unless otherwise specified. The methods described are conventional methods unless otherwise stated. The corresponding units of "parts by mass" and "parts by volume" below are g and mL respectively.
以下实施例的具体测试方法如下:试样致密度由阿基米德排水法测得;试样的微观组织由扫描电镜进行观察;试样的屈服强度、抗拉强度、断裂应变按照国际标准(ChineseGB/T 228-2002)进行拉伸性能测试。The specific test methods of the following examples are as follows: the density of the sample is measured by the Archimedean drainage method; the microstructure of the sample is observed by a scanning electron microscope; the yield strength, tensile strength, and fracture strain of the sample are in accordance with international standards ( ChineseGB/T 228-2002) for tensile property testing.
实施例1:Example 1:
一种双尺度等轴结构的钛合金的制备方法,包括以下步骤:A method for preparing a titanium alloy with a dual-scale equiaxed structure, including the following steps:
本实施例所用原料如下:环己烷、氢化钛粉末(75μm)、60Al40V中间合金粉末(45μm)。The raw materials used in this example are as follows: cyclohexane, titanium hydride powder (75 μm), and 60Al40V master alloy powder (45 μm).
(1)合金粉末含碳处理:本实施例的目标合金成分为Ti-6Al-4V合金。首先将100质量份的60Al40V合金粉末和20体积份的环己烷一同倒入行星球磨机(QM-2SP20)不锈钢球磨罐中,选用的不锈钢磨球直径分别为15mm、10mm和6mm,质量比为1:3:1。球磨参数如下:气氛为1个大气压高纯氩气(99.999%),球料比10:1,转速400rpm,球磨时间为30h。之后取出粉末在真空干燥箱中烘干12h后过325目筛得到含碳60Al40V中间合金粉末。(1) Carbon-containing treatment of alloy powder: The target alloy composition of this embodiment is Ti-6Al-4V alloy. First, pour 100 parts by mass of 60Al40V alloy powder and 20 parts by volume of cyclohexane into the stainless steel ball mill tank of the planetary ball mill (QM-2SP20). The selected stainless steel grinding ball diameters are 15mm, 10mm and 6mm respectively, and the mass ratio is 1 :3:1. The ball milling parameters are as follows: the atmosphere is high-purity argon (99.999%) at 1 atmosphere, the ball-to-material ratio is 10:1, the rotation speed is 400 rpm, and the ball milling time is 30 hours. Afterwards, the powder was taken out, dried in a vacuum drying oven for 12 hours, and then passed through a 325 mesh sieve to obtain carbon-containing 60Al40V master alloy powder.
(2)烧结原料混合:根据Ti-6Al-4V的目标合金成分,称取10质量份步骤(1)制备的含碳60Al40V中间合金粉末和93.26质量份氢化钛粉末(由于氢化钛中的Ti含量为96.5wt.%,因此90质量份的Ti粉末需要90÷0.965=93.26质量份氢化钛粉末),之后将称量粉末一并倒入容器中,并将容器内气氛置换为高纯氩气。采用V型混粉机以350rpm的转速混合粉末24h得到烧结原料粉末。(2) Mixing of sintering raw materials: According to the target alloy composition of Ti-6Al-4V, weigh 10 parts by mass of the carbon-containing 60Al40V master alloy powder prepared in step (1) and 93.26 parts by mass of titanium hydride powder (due to the Ti content in titanium hydride is 96.5 wt.%, so 90 parts by mass of Ti powder requires 90÷0.965=93.26 parts by mass of titanium hydride powder). Afterwards, the weighed powder is poured into the container, and the atmosphere in the container is replaced with high-purity argon gas. The powder was mixed using a V-shaped powder mixer at a rotation speed of 350 rpm for 24 h to obtain the sintered raw material powder.
(3)无压烧结成形:称量20质量份步骤(2)混合的烧结原料粉末倒入冷压模具中,以600MPa的压制压力、30s的保压时间进行压制,缓慢脱模得到压坯;将压坯放置在真空烧结炉内后,用真空烧结炉自带真空系统将炉膛抽至5×10-3Pa;之后,以10℃/min的升温速率升温至1250℃保温4h;之后,以10℃/min的冷却速率冷却至650℃后随炉冷却至室温,取出样品得到双尺度等轴结构的钛合金。(3) Pressureless sintering forming: Weigh 20 parts by mass of the sintering raw material powder mixed in step (2) and pour it into the cold pressing mold, press it with a pressing pressure of 600MPa and a holding time of 30s, and slowly demold it to obtain a green compact; After placing the green compact in the vacuum sintering furnace, use the vacuum system provided by the vacuum sintering furnace to pump the furnace to 5×10 -3 Pa; then, raise the temperature to 1250°C at a heating rate of 10°C/min and keep it for 4 hours; then, Cool to 650°C at a cooling rate of 10°C/min and then cool to room temperature in the furnace. Take out the sample to obtain a titanium alloy with a dual-scale equiaxed structure.
本实施例制备的双尺度等轴结构的钛合金的致密度达99.2%,其基体微观结构包括15μm的等轴结构区域及其边界平均1.5μm宽、7-40μm长的连续微米晶β-Ti板条相(如图1左所示)。其中,15μm的等轴结构区域包括尺寸约300nm的等轴超细晶α-Ti相,及其晶界平均140nm宽、280-900nm长的超细晶β-Ti板条相(如图1右所示)。连续微米晶β-Ti板条相和超细晶β-Ti板条相构成双尺度结构,等轴超细晶α-Ti相及其组成的微米级等轴结构区域构成等轴结构。室温拉伸屈服强度,抗拉强度和伸长率分别为1170MPa,1253MPa和5%(如图3所示)。本实施例制备的Ti-6Al-4V合金抗拉强度远高于传统无压烧结制备的Ti-6Al-4V块体合金的830-970MPa(Metallurgical and Materials Transactions A,48(2017)2301–2319),同时具有相当的拉伸塑性。此外,相比合金塑性变形-热处理诱发再结晶、不同尺寸原料粉末的混合固结、非晶晶化-固态烧结和半固态烧结、铜模快速凝固等方法,本实施例双尺度等轴结构钛合金的制备方法具有工艺简单,制备成本低,制品形状和尺寸不受限等优势。The dual-scale equiaxed structure titanium alloy prepared in this example has a density of 99.2%, and its matrix microstructure includes a 15 μm equiaxed structure region and its boundary is an average of 1.5 μm wide and 7-40 μm long continuous micron crystal β-Ti Lath phase (shown on the left in Figure 1). Among them, the 15 μm equiaxed structure region includes an equiaxed ultrafine-grained α-Ti phase with a size of about 300nm, and an ultrafine-grained β-Ti lath phase with an average grain boundary width of 140nm and a length of 280-900nm (right side of Figure 1 shown). The continuous micron-crystalline β-Ti lath phase and the ultra-fine-grain β-Ti lath phase constitute a dual-scale structure, and the equiaxed ultra-fine-grain α-Ti phase and its composed micron-scale equiaxed structural regions constitute an equiaxed structure. The room temperature tensile yield strength, tensile strength and elongation are 1170MPa, 1253MPa and 5% respectively (as shown in Figure 3). The tensile strength of the Ti-6Al-4V alloy prepared in this example is much higher than the 830-970MPa of the Ti-6Al-4V bulk alloy prepared by traditional pressureless sintering (Metallurgical and Materials Transactions A, 48 (2017) 2301–2319) , and has considerable tensile plasticity. In addition, compared with methods such as alloy plastic deformation-heat treatment induced recrystallization, mixed solidification of raw material powders of different sizes, amorphous crystallization-solid sintering and semi-solid sintering, rapid solidification of copper molds, the dual-scale equiaxed structure titanium in this embodiment The preparation method of the alloy has the advantages of simple process, low preparation cost, and unlimited shape and size of the product.
实施例2:Example 2:
一种双尺度等轴结构钛合金的制备方法,包括以下步骤:A method for preparing a dual-scale equiaxed structure titanium alloy, including the following steps:
本实施例所用原料如下:环己烯、纯钛粉末(45μm)、60Al40V中间合金粉末(10μm)。The raw materials used in this example are as follows: cyclohexene, pure titanium powder (45 μm), and 60Al40V master alloy powder (10 μm).
(1)合金粉末含碳处理:本实施例的目标合金成分为Ti-6Al-4V合金。首先将100质量份的60Al40V合金粉末和40体积份的环己烯一同倒入行星球磨机(QM-2SP20)不锈钢球磨罐中,选用的不锈钢磨球直径分别为15mm、10mm和6mm,质量比为1:3:1。球磨参数如下:气氛为1个大气压高纯氩气(99.999%),球料比5:1,转速250rpm,球磨时间为50h。之后取出粉末在真空干燥箱中烘干12h后过325目筛得到含碳60Al40V中间合金粉末。(1) Carbon-containing treatment of alloy powder: The target alloy composition of this embodiment is Ti-6Al-4V alloy. First, pour 100 parts by mass of 60Al40V alloy powder and 40 parts by volume of cyclohexene into the stainless steel ball mill tank of the planetary ball mill (QM-2SP20). The selected stainless steel grinding ball diameters are 15mm, 10mm and 6mm respectively, and the mass ratio is 1 :3:1. The ball milling parameters are as follows: the atmosphere is 1 atmospheric pressure high-purity argon (99.999%), the ball-to-material ratio is 5:1, the rotation speed is 250rpm, and the ball milling time is 50h. Afterwards, the powder was taken out, dried in a vacuum drying oven for 12 hours, and then passed through a 325 mesh sieve to obtain carbon-containing 60Al40V master alloy powder.
(2)烧结原料混合:根据Ti-6Al-4V的目标合金成分,称取10质量份步骤(1)制备的含碳60Al40V中间合金粉末和90质量份纯钛粉末,之后将称量粉末一并倒入容器中,并将容器内气氛置换为高纯氩气。采用V型混粉机以350rpm的转速混合粉末24h得到烧结原料粉末。(2) Mixing of sintering raw materials: According to the target alloy composition of Ti-6Al-4V, weigh 10 parts by mass of the carbon-containing 60Al40V master alloy powder prepared in step (1) and 90 parts by mass of pure titanium powder, and then weigh the powders together Pour it into a container and replace the atmosphere in the container with high-purity argon. The powder was mixed using a V-shaped powder mixer at a rotation speed of 350 rpm for 24 h to obtain the sintered raw material powder.
(3)无压烧结成形:称量20质量份步骤(2)混合的烧结原料粉末倒入冷等静压模具中,以350MPa的压制压力、30s的保压时间进行冷等静压压制,缓慢脱模得到压坯;将压坯放置在真空烧结炉内后,用真空烧结炉自带真空系统将炉膛抽至5×10-3Pa;之后,以10℃/min的升温速率升温至1500℃保温1h;之后,以10℃/min的冷却速率冷却至650℃后随炉冷却至室温,取出样品得到无柯肯达尔孔,高塑性的钛基复合材料。(3) Pressureless sintering molding: Weigh 20 parts by mass of the mixed sintering raw material powder in step (2) and pour it into the cold isostatic pressing mold, and perform cold isostatic pressing with a pressing pressure of 350MPa and a holding time of 30s. Slowly Demold the compact to obtain the compact; after placing the compact in the vacuum sintering furnace, use the vacuum system of the vacuum sintering furnace to pump the furnace to 5×10 -3 Pa; then, raise the temperature to 1500 °C at a heating rate of 10 °C/min. Keep warm for 1 hour; then, cool to 650°C at a cooling rate of 10°C/min and then cool to room temperature in the furnace. Take out the sample to obtain a titanium-based composite material with no Kirkendall pores and high plasticity.
本实施例制备的双尺度等轴结构钛合金的致密度达98.7%,其基体微观结构包括30μm的等轴结构区域及其边界平均2μm宽、9-35μm长的连续微米晶β-Ti板条相。其中,30μm的等轴结构区域包括尺寸约400nm的等轴超细晶α-Ti相,及其晶界平均150nm宽、300-850nm长的超细晶β-Ti板条相。连续微米晶β-Ti板条相和超细晶β-Ti板条相构成双尺度结构,等轴超细晶α-Ti相及其组成的微米级等轴结构区域构成等轴结构。室温拉伸屈服强度,抗拉强度和伸长率分别为1158MPa,1237MPa和6%。本实施例制备的Ti-6Al-4V合金抗拉强度远高于传统无压烧结制备的Ti-6Al-4V块体合金的830-970MPa(Metallurgical andMaterials Transactions A,48(2017)2301–2319),同时具有相当的拉伸塑性。此外,相比合金塑性变形-热处理诱发再结晶、不同尺寸原料粉末的混合固结、非晶晶化-固态烧结和半固态烧结、铜模快速凝固等方法,本实施例双尺度等轴结构钛合金的制备方法具有工艺简单,制备成本低,制品形状和尺寸不受限等优势。The dual-scale equiaxed structure titanium alloy prepared in this example has a density of 98.7%, and its matrix microstructure includes a 30 μm equiaxed structure region and its boundary is an average of 2 μm wide and 9-35 μm long continuous micron crystal β-Ti laths. Mutually. Among them, the 30 μm equiaxed structure region includes an equiaxed ultrafine-grained α-Ti phase with a size of about 400nm, and an ultrafine-grained β-Ti lath phase with an average grain boundary width of 150nm and a length of 300-850nm. The continuous micron-crystalline β-Ti lath phase and the ultra-fine-grain β-Ti lath phase constitute a dual-scale structure, and the equiaxed ultra-fine-grain α-Ti phase and its composed micron-scale equiaxed structural regions constitute an equiaxed structure. The room temperature tensile yield strength, tensile strength and elongation are 1158MPa, 1237MPa and 6% respectively. The tensile strength of the Ti-6Al-4V alloy prepared in this example is much higher than the 830-970MPa of the Ti-6Al-4V bulk alloy prepared by traditional pressureless sintering (Metallurgical and Materials Transactions A, 48 (2017) 2301–2319). It also has considerable tensile plasticity. In addition, compared with methods such as alloy plastic deformation-heat treatment induced recrystallization, mixed solidification of raw material powders of different sizes, amorphous crystallization-solid sintering and semi-solid sintering, rapid solidification of copper molds, the dual-scale equiaxed structure titanium in this embodiment The preparation method of the alloy has the advantages of simple process, low preparation cost, and unlimited shape and size of the product.
实施例3:Example 3:
一种双尺度等轴结构钛合金的制备方法,包括以下步骤:A method for preparing a dual-scale equiaxed structure titanium alloy, including the following steps:
本实施例所用原料如下:环己烯、纯钛粉末(45μm)、60Al40V中间合金粉末(10μm)。The raw materials used in this example are as follows: cyclohexene, pure titanium powder (45 μm), and 60Al40V master alloy powder (10 μm).
(1)合金粉末含碳处理:本实施例的目标合金成分为Ti-6Al-4V合金。首先将100质量份的60Al40V合金粉末和30体积份的环己烯一同倒入行星球磨机(QM-2SP20)不锈钢球磨罐中,选用的不锈钢磨球直径分别为15mm、10mm和6mm,质量比为1:3:1。球磨参数如下:气氛为1个大气压高纯氩气(99.999%),球料比20:1,转速300rpm,球磨时间为40h。之后取出粉末在真空干燥箱中烘干12h后过325目筛得到含碳60Al40V中间合金粉末。(1) Carbon-containing treatment of alloy powder: The target alloy composition of this embodiment is Ti-6Al-4V alloy. First, pour 100 parts by mass of 60Al40V alloy powder and 30 parts by volume of cyclohexene into the stainless steel ball mill tank of the planetary ball mill (QM-2SP20). The selected stainless steel grinding ball diameters are 15mm, 10mm and 6mm respectively, and the mass ratio is 1 :3:1. The ball milling parameters are as follows: the atmosphere is high-purity argon (99.999%) at 1 atmosphere, the ball-to-material ratio is 20:1, the rotation speed is 300 rpm, and the ball milling time is 40 hours. Afterwards, the powder was taken out, dried in a vacuum drying oven for 12 hours, and then passed through a 325 mesh sieve to obtain carbon-containing 60Al40V master alloy powder.
(2)烧结原料混合:根据Ti-6Al-4V的目标合金成分,称取10质量份步骤(1)制备的含碳60Al40V中间合金粉末和90质量份纯钛粉末,之后将称量粉末一并倒入容器中,并将容器内气氛置换为高纯氩气。采用V型混粉机以350rpm的转速混合粉末24h得到烧结原料粉末。(2) Mixing of sintering raw materials: According to the target alloy composition of Ti-6Al-4V, weigh 10 parts by mass of the carbon-containing 60Al40V master alloy powder prepared in step (1) and 90 parts by mass of pure titanium powder, and then weigh the powders together Pour it into a container and replace the atmosphere in the container with high-purity argon. The powder was mixed using a V-shaped powder mixer at a rotation speed of 350 rpm for 24 h to obtain the sintered raw material powder.
(3)无压烧结成形:称量20质量份步骤(2)混合的烧结原料粉末倒入冷等静压模具中,以100MPa的压制压力、600s的保压时间进行冷等静压压制,缓慢脱模得到压坯;将压坯放置在真空烧结炉内后,用真空烧结炉自带真空系统将炉膛抽至5×10-3Pa;之后,以10℃/min的升温速率升温至1000℃保温5h;之后,以10℃/min的冷却速率冷却至650℃后随炉冷却至室温,取出样品得到无柯肯达尔孔,高塑性的钛基复合材料。(3) Pressureless sintering molding: Weigh 20 parts by mass of the mixed sintering raw material powder in step (2) and pour it into a cold isostatic pressing mold, and perform cold isostatic pressing with a pressing pressure of 100MPa and a holding time of 600s. Slowly Demold the compact to obtain the compact; after placing the compact in the vacuum sintering furnace, use the vacuum system of the vacuum sintering furnace to pump the furnace to 5×10 -3 Pa; then, raise the temperature to 1000 °C at a heating rate of 10 °C/min. Keep warm for 5 hours; then, cool to 650°C at a cooling rate of 10°C/min and then cool to room temperature in the furnace. Take out the sample to obtain a titanium-based composite material with no Kirkendall pores and high plasticity.
本实施例制备的双尺度等轴结构钛合金的致密度达99.1%,其基体微观结构包括10μm的等轴结构区域及其边界平均1μm宽、7-32μm长的连续微米晶β-Ti板条相。其中,10μm的等轴结构区域包括尺寸约100nm的等轴超细晶α-Ti相,及其晶界平均115nm宽、200-780nm长的超细晶β-Ti板条相。连续微米晶β-Ti板条相和超细晶β-Ti板条相构成双尺度结构,等轴超细晶α-Ti相及其组成的微米级等轴结构区域构成等轴结构。室温拉伸屈服强度,抗拉强度和伸长率分别为1142MPa,1221MPa和6%。本实施例制备的Ti-6Al-4V合金抗拉强度远高于传统无压烧结制备的Ti-6Al-4V块体合金的830-970MPa(Metallurgical andMaterials Transactions A,48(2017)2301–2319),同时具有相当的拉伸塑性。此外,相比合金塑性变形-热处理诱发再结晶、不同尺寸原料粉末的混合固结、非晶晶化-固态烧结和半固态烧结、铜模快速凝固等方法,本实施例双尺度等轴结构钛合金的制备方法具有工艺简单,制备成本低,制品形状和尺寸不受限等优势。The dual-scale equiaxed structure titanium alloy prepared in this example has a density of 99.1%, and its matrix microstructure includes a 10 μm equiaxed structure region and its boundary is an average of 1 μm wide and 7-32 μm long continuous micron crystal β-Ti laths. Mutually. Among them, the 10 μm equiaxed structure region includes an equiaxed ultrafine-grained α-Ti phase with a size of about 100nm, and an ultrafine-grained β-Ti lath phase with an average grain boundary width of 115nm and a length of 200-780nm. The continuous micron-crystalline β-Ti lath phase and the ultra-fine-grain β-Ti lath phase constitute a dual-scale structure, and the equiaxed ultra-fine-grain α-Ti phase and its composed micron-scale equiaxed structural regions constitute an equiaxed structure. The room temperature tensile yield strength, tensile strength and elongation are 1142MPa, 1221MPa and 6% respectively. The tensile strength of the Ti-6Al-4V alloy prepared in this example is much higher than the 830-970MPa of the Ti-6Al-4V bulk alloy prepared by traditional pressureless sintering (Metallurgical and Materials Transactions A, 48 (2017) 2301–2319). It also has considerable tensile plasticity. In addition, compared with methods such as alloy plastic deformation-heat treatment induced recrystallization, mixed solidification of raw material powders of different sizes, amorphous crystallization-solid sintering and semi-solid sintering, rapid solidification of copper molds, the dual-scale equiaxed structure titanium in this embodiment The preparation method of the alloy has the advantages of simple process, low preparation cost, and unlimited shape and size of the product.
对比例1:Comparative example 1:
本对比例所用原料如下:氢化钛粉末(75μm)、60Al40V中间合金粉末(45μm)。The raw materials used in this comparative example are as follows: titanium hydride powder (75 μm), 60Al40V master alloy powder (45 μm).
(1)烧结原料混合:根据Ti-6Al-4V的目标合金成分,称取10质量份60Al40V中间合金粉末和93.26质量份氢化钛粉末(由于氢化钛中的Ti含量为96.5wt.%,因此90质量份的Ti粉末需要90÷0.965=93.26质量份氢化钛粉末),之后将称量粉末一并倒入容器中,并将容器内气氛置换为高纯氩气。采用V型混粉机以350rpm的转速混合粉末24h得到烧结原料粉末。(1) Mixing of sintering raw materials: According to the target alloy composition of Ti-6Al-4V, weigh 10 parts by mass of 60Al40V master alloy powder and 93.26 parts by mass of titanium hydride powder (since the Ti content in titanium hydride is 96.5wt.%, so 90 The mass parts of Ti powder require 90÷0.965=93.26 mass parts of titanium hydride powder), and then the weighed powder is poured into the container, and the atmosphere in the container is replaced with high-purity argon gas. The powder was mixed using a V-shaped powder mixer at a rotation speed of 350 rpm for 24 h to obtain the sintered raw material powder.
(2)无压烧结成形:称量20质量份步骤(1)混合的烧结原料粉末倒入冷压模具中,以600MPa的压制压力、30s的保压时间进行压制,缓慢脱模得到压坯;将压坯放置在真空烧结炉内后,用真空烧结炉自带真空系统将炉膛抽至5×10-3Pa;之后,以10℃/min的升温速率升温至1250℃保温4h;之后,以10℃/min的冷却速率冷却至650℃后随炉冷却至室温,取出样品得到高强双尺度等轴结构钛合金。(2) Pressureless sintering molding: Weigh 20 parts by mass of the mixed sintering raw material powder in step (1) and pour it into the cold pressing mold, press it with a pressing pressure of 600MPa and a holding time of 30s, and slowly demold it to obtain a green compact; After placing the green compact in the vacuum sintering furnace, use the vacuum system provided by the vacuum sintering furnace to pump the furnace to 5×10 -3 Pa; then, raise the temperature to 1250°C at a heating rate of 10°C/min and keep it for 4 hours; then, Cool to 650°C at a cooling rate of 10°C/min and then cool to room temperature in the furnace. Take out the sample to obtain a high-strength dual-scale equiaxed structure titanium alloy.
本对比例制备的Ti-6Al-4V合金基体为长条状的α-Ti(图2灰色相)及其边界β-Ti(图2白色相)组成,其中α-Ti集束的长度约为150μm。本对比例制备的Ti-6Al-4V的屈服强度约860MPa,抗拉强度为930MPa,伸长率为7%(如图3所示)。其综合力学性能弱于实施例1制备的高强双尺度等轴结构钛合金。The Ti-6Al-4V alloy matrix prepared in this comparative example is composed of long strips of α-Ti (gray phase in Figure 2) and its boundary β-Ti (white phase in Figure 2), in which the length of the α-Ti bundle is about 150 μm. . The yield strength of Ti-6Al-4V prepared in this comparative example is about 860MPa, the tensile strength is 930MPa, and the elongation is 7% (as shown in Figure 3). Its comprehensive mechanical properties are weaker than those of the high-strength dual-scale equiaxed structure titanium alloy prepared in Example 1.
对比例2:Comparative example 2:
本对比例所用原料如下:环己烷、氢化钛粉末(75μm)、60Al40V中间合金粉末(45μm)。The raw materials used in this comparative example are as follows: cyclohexane, titanium hydride powder (75 μm), and 60Al40V master alloy powder (45 μm).
(1)合金粉末混合:本对比例的目标合金成分为Ti-6Al-4V合金。首先将100质量份的60Al40V合金粉末和20体积份的环己烷一同倒入容器中,并将容器内气氛置换为高纯氩气。采用V型混粉机以350rpm的转速混合粉末24h得到中间合金原料粉末。(1) Alloy powder mixing: The target alloy composition of this comparative example is Ti-6Al-4V alloy. First, 100 parts by mass of 60Al40V alloy powder and 20 parts by volume of cyclohexane are poured into a container, and the atmosphere in the container is replaced with high-purity argon gas. A V-shaped powder mixer was used to mix the powder at a rotation speed of 350 rpm for 24 hours to obtain the master alloy raw material powder.
(2)烧结原料混合:根据Ti-6Al-4V的目标合金成分,称取10质量份步骤(1)制备的中间合金粉末和93.26质量份氢化钛粉末(由于氢化钛中的Ti含量为96.5wt.%,因此90质量份的Ti粉末需要90÷0.965=93.26质量份氢化钛粉末),之后将称量粉末一并倒入容器中,并将容器内气氛置换为高纯氩气。采用V型混粉机以350rpm的转速混合粉末24h得到烧结原料粉末。(2) Mixing of sintering raw materials: According to the target alloy composition of Ti-6Al-4V, weigh 10 parts by mass of the intermediate alloy powder prepared in step (1) and 93.26 parts by mass of titanium hydride powder (since the Ti content in titanium hydride is 96.5wt .%, so 90 parts by mass of Ti powder requires 90÷0.965=93.26 parts by mass of titanium hydride powder), and then the weighed powder is poured into the container, and the atmosphere in the container is replaced with high-purity argon gas. The powder was mixed using a V-shaped powder mixer at a rotation speed of 350 rpm for 24 h to obtain the sintered raw material powder.
(3)无压烧结成形:称量20质量份步骤(2)混合的烧结原料粉末倒入冷压模具中,以600MPa的压制压力、30s的保压时间进行压制,缓慢脱模得到压坯;将压坯放置在真空烧结炉内后,用真空烧结炉自带真空系统将炉膛抽至5×10-3Pa;之后,以10℃/min的升温速率升温至1250℃保温4h;之后,以10℃/min的冷却速率冷却至650℃后随炉冷却至室温,取出得到钛合金样品。(3) Pressureless sintering forming: Weigh 20 parts by mass of the sintering raw material powder mixed in step (2) and pour it into the cold pressing mold, press it with a pressing pressure of 600MPa and a holding time of 30s, and slowly demold it to obtain a green compact; After placing the green compact in the vacuum sintering furnace, use the vacuum system provided by the vacuum sintering furnace to pump the furnace to 5×10 -3 Pa; then, raise the temperature to 1250°C at a heating rate of 10°C/min and keep it for 4 hours; then, Cool to 650°C at a cooling rate of 10°C/min, then cool to room temperature in the furnace, and take out the titanium alloy sample.
未经球磨的环己烷在烧结过程直接挥发,无法为α-Ti提供形核质点。本对比例制备的Ti-6Al-4V合金基体为长条状的α-Ti及其边界β-Ti组成,其中α-Ti集束的长度约为162μm。本对比例制备的Ti-6Al-4V的屈服强度约857MPa,抗拉强度为918MPa,伸长率为8%。其综合力学性能弱于实施例1制备的高强双尺度等轴结构钛合金。Cyclohexane that has not been ball-milled directly volatilizes during the sintering process and cannot provide nucleation points for α-Ti. The Ti-6Al-4V alloy matrix prepared in this comparative example is composed of long strips of α-Ti and its boundary β-Ti, in which the length of the α-Ti bundle is about 162 μm. The yield strength of Ti-6Al-4V prepared in this comparative example is about 857MPa, the tensile strength is 918MPa, and the elongation is 8%. Its comprehensive mechanical properties are weaker than those of the high-strength dual-scale equiaxed structure titanium alloy prepared in Example 1.
对比例3:Comparative example 3:
本对比例所用原料如下:无水乙醇(C2H5OH)、氢化钛粉末(75μm)、60Al40V中间合金粉末(45μm)。The raw materials used in this comparative example are as follows: absolute ethanol (C 2 H 5 OH), titanium hydride powder (75 μm), and 60Al40V master alloy powder (45 μm).
(1)合金粉末含碳处理:本实施例的目标合金成分为Ti-6Al-4V合金。首先将100质量份的60Al40V合金粉末和20体积份的无水乙醇一同倒入行星球磨机(QM-2SP20)不锈钢球磨罐中,选用的不锈钢磨球直径分别为15mm、10mm和6mm,质量比为1:3:1。球磨参数如下:气氛为1个大气压高纯氩气(99.999%),球料比10:1,转速400rpm,球磨时间为30h。之后取出粉末在真空干燥箱中烘干12h后过325目筛得到含碳60Al40V中间合金粉末。(1) Carbon-containing treatment of alloy powder: The target alloy composition of this embodiment is Ti-6Al-4V alloy. First, pour 100 parts by mass of 60Al40V alloy powder and 20 parts by volume of absolute ethanol into the stainless steel ball mill tank of the planetary ball mill (QM-2SP20). The selected stainless steel grinding ball diameters are 15mm, 10mm and 6mm respectively, and the mass ratio is 1 :3:1. The ball milling parameters are as follows: the atmosphere is high-purity argon (99.999%) at 1 atmosphere, the ball-to-material ratio is 10:1, the rotation speed is 400 rpm, and the ball milling time is 30 hours. Afterwards, the powder was taken out, dried in a vacuum drying oven for 12 hours, and then passed through a 325 mesh sieve to obtain carbon-containing 60Al40V master alloy powder.
(2)烧结原料混合:根据Ti-6Al-4V的目标合金成分,称取10质量份步骤(1)制备的含碳60Al40V中间合金粉末和93.26质量份氢化钛粉末(由于氢化钛中的Ti含量为96.5wt.%,因此90质量份的Ti粉末需要90÷0.965=93.26质量份氢化钛粉末),之后将称量粉末一并倒入容器中,并将容器内气氛置换为高纯氩气。采用V型混粉机以350rpm的转速混合粉末24h得到烧结原料粉末。(2) Mixing of sintering raw materials: According to the target alloy composition of Ti-6Al-4V, weigh 10 parts by mass of the carbon-containing 60Al40V master alloy powder prepared in step (1) and 93.26 parts by mass of titanium hydride powder (due to the Ti content in titanium hydride is 96.5 wt.%, so 90 parts by mass of Ti powder requires 90÷0.965=93.26 parts by mass of titanium hydride powder). Afterwards, the weighed powder is poured into the container, and the atmosphere in the container is replaced with high-purity argon gas. The powder was mixed using a V-shaped powder mixer at a rotation speed of 350 rpm for 24 h to obtain the sintered raw material powder.
(3)无压烧结成形:称量20质量份步骤(2)混合的烧结原料粉末倒入冷压模具中,以600MPa的压制压力、30s的保压时间进行压制,缓慢脱模得到压坯;将压坯放置在真空烧结炉内后,用真空烧结炉自带真空系统将炉膛抽至5×10-3Pa;之后,以10℃/min的升温速率升温至1250℃保温4h;之后,以10℃/min的冷却速率冷却至650℃后随炉冷却至室温,取出样品得到双尺度等轴结构的钛合金。(3) Pressureless sintering forming: Weigh 20 parts by mass of the sintering raw material powder mixed in step (2) and pour it into the cold pressing mold, press it with a pressing pressure of 600MPa and a holding time of 30s, and slowly demold it to obtain a green compact; After placing the green compact in the vacuum sintering furnace, use the vacuum system provided by the vacuum sintering furnace to pump the furnace to 5×10 -3 Pa; then, raise the temperature to 1250°C at a heating rate of 10°C/min and keep it for 4 hours; then, Cool to 650°C at a cooling rate of 10°C/min and then cool to room temperature in the furnace. Take out the sample to obtain a titanium alloy with a dual-scale equiaxed structure.
本对比例制备的钛合金的致密度达99.2%,其基体微观结构包括15μm的等轴结构区域及其边界平均1.2μm宽、10-40μm长的连续微米晶β-Ti板条相。其中,15μm的等轴结构区域包括尺寸约500nm的等轴超细晶α-Ti相,及其晶界平均145nm宽、200-900nm长的超细晶β-Ti板条相。由于乙醇中含有的氧在球磨过程中固溶至粉末中,并残留在烧结制备的钛合金基体,导致本对比例制备钛合金氧含量达0.42wt.%。其抗拉强度为782MPa,无室温塑性。The titanium alloy prepared in this comparative example has a density of 99.2%, and its matrix microstructure includes a 15 μm equiaxed structure region and its boundary is an average 1.2 μm wide and 10-40 μm long continuous micron-crystalline β-Ti lath phase. Among them, the 15 μm equiaxed structure region includes an equiaxed ultrafine-grained α-Ti phase with a size of about 500nm, and an ultrafine-grained β-Ti lath phase with an average grain boundary width of 145nm and a length of 200-900nm. Since the oxygen contained in ethanol is dissolved into the powder during the ball milling process and remains in the titanium alloy matrix prepared by sintering, the oxygen content of the titanium alloy prepared in this comparative example reaches 0.42 wt.%. Its tensile strength is 782MPa and has no room temperature plasticity.
上述实施例为本发明较佳的实施方式,但本发明的实施方式并不受上述实施例的限制,其他的任何未背离本发明的精神实质与原理下所作的改变、修饰、替代、组合、简化,均应为等效的置换方式,都包含在本发明的保护范围之内。The above embodiments are preferred embodiments of the present invention, but the embodiments of the present invention are not limited to the above embodiments. Any other changes, modifications, substitutions, combinations, etc. may be made without departing from the spirit and principles of the present invention. All simplifications should be equivalent substitutions, and are all included in the protection scope of the present invention.
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