CN109097624A - A kind of casting Two Liquid Phases solidification and high damping properties titanium alloy and technique - Google Patents

A kind of casting Two Liquid Phases solidification and high damping properties titanium alloy and technique Download PDF

Info

Publication number
CN109097624A
CN109097624A CN201811135566.XA CN201811135566A CN109097624A CN 109097624 A CN109097624 A CN 109097624A CN 201811135566 A CN201811135566 A CN 201811135566A CN 109097624 A CN109097624 A CN 109097624A
Authority
CN
China
Prior art keywords
alloy
casting
titanium alloy
solidification
titanium
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
Application number
CN201811135566.XA
Other languages
Chinese (zh)
Inventor
杨长江
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.)
Guangzhou Xianzhi Technology Co Ltd
Guangzhou Yuzhi Technology Co Ltd
Original Assignee
Guangzhou Xianzhi Technology Co Ltd
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 Guangzhou Xianzhi Technology Co Ltd filed Critical Guangzhou Xianzhi Technology Co Ltd
Priority to CN201811135566.XA priority Critical patent/CN109097624A/en
Publication of CN109097624A publication Critical patent/CN109097624A/en
Pending legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C14/00Alloys based on titanium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22BPRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
    • C22B9/00General processes of refining or remelting of metals; Apparatus for electroslag or arc remelting of metals
    • C22B9/16Remelting metals
    • C22B9/20Arc remelting
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/16Changing 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
    • C22F1/18High-melting or refractory metals or alloys based thereon
    • C22F1/183High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon

Abstract

The invention discloses a kind of casting Two Liquid Phases solidification and high damping properties titanium alloys and technique.According to weight percent, the ingredient of the alloy are as follows: Sn:6.0-8.0wt.%, Nd:0.5-0.8wt.%, Yb:0.4-0.6wt.%, Bi:3.0-3.5wt.%, Al:10.0-12.0wt.%, Sb:1.4-1.6wt.%, Si:2.0-3.0wt.%, Fe:4.0-5.0wt.%, surplus are titanium.The material is requires light-weighted structural material applications field to provide a kind of technical solution different from common titanium alloy, that is, provides a kind of titanium alloy with excellent casting character.The implementation and industrialization of the alloy can push significantly China to the new material update of high-end titanium alloy and business upgrade requirement.

Description

A kind of casting Two Liquid Phases solidification and high damping properties titanium alloy and technique
Technical field
The present invention relates to technical field of alloy, specifically, being related to a kind of titanium alloy.
Background technique
Titanium is a kind of important structural metal to grow up the 1950s, and because having, intensity is high, corrosion resistance is good, resistance to The features such as hot high and be widely used in every field.Alloying element appropriate is added in titanium, makes its phase transition temperature and is mutually contained Amount, which gradually changes, obtains the titanium alloy of different tissues.Titanium alloy has a series of excellent physics, mechanics and chemical property, main Show: (1) specific strength is high.The density of titanium alloy is generally in 4.5g/cm3Left and right, only the 60% of steel, the intensity of pure titanium connect The intensity of nearly ordinary steel, some high strength titanium alloys have been more than the intensity of many structural alloy steels.Therefore the specific strength of titanium alloy (strength/density) is much larger than other structural metallic materials, can produce the parts and components that unit strength is high, rigidity is good, light.(2) hot Intensity is high., can be in 450-500 DEG C of at a temperature of long-term work using temperature than aluminium alloy Gao Ji Baidu, and the work of aluminium alloy Temperature is then at 200 DEG C or less.(3) corrosion stability is good.Titanium alloy works in humid atmosphere and seawater medium, and corrosion stability is far excellent In stainless steel.It is especially strong to the resistance of spot corrosion, acid etching, stress corrosion.
Titanium alloy is widely used in civil and military aviation field.The advantage of titanium alloy is: (1) mitigating knot Structure weight improves structure efficiency.Titanium alloy has the characteristics that intensity strong steel but density is small in, closes instead of structural steel and high temperature Construction weight can be greatly reduced in gold, while can also save money.(2) meet the requirement of high temperature position.In the height of aircraft Warm position (such as rear body) may replace the aluminium alloy that cannot be met the requirements by applied at elevated temperature performance.(3) meet highly resistance corrosion and The requirement of long-life.Titanium alloy fatigue life with higher and excellent corrosion resistance, can be improved the anticorrosive of structure Ability and service life meet the requirement of Advanced Aircraft, engine high reliability and long-life.
In general, all due to become solid-state from liquid volume receipts can occur for metal or alloy when solidification Contracting, this is because solid density is greater than caused by liquid.It will be apparent that the difference of these density will lead in process of setting Cast hole and loose formation.In addition, alloy in process of setting since first precipitated phase forms dendrite trunk and side shoot and Prevent later melt from effectively filling up interdendritic gap, can also promote hole and loose generation.Thus, polynary conjunction Gold casting compactness of casting in solidification is always the difficult point in materialogy.For casting alloy, people can be selected The ingredient near multi-element eutectic point is selected, so that having fixed and single phase transition temperature in the process of setting of alloy, because of eutectic Temperature is fixed.Not only make casting alloying component in a wide range of uniform in this way, but also mutually coordinated due to eutectic phase It generates and makes the hole of casting and loose reached minimum.
Due to titanium alloy physical property, the extremely superiority of mechanical property and chemical property, domestic and international researcher and machine Structure has made extensive and intensive studies titanium alloy, and has developed a series of wrought titanium alloy and cast titanium conjunction Gold.These titanium alloys not only make it possible the industrial upgradings of relevant industries after popularization, also greatly promoting property related fields Technology development.It but is based on designing the ingredients of these alloys polynary to the optimization of the casting character of cast titanium alloy Near alloy eutectic point, thus the alloy near these eutectic points can greatly reduce in casting process in casting process Hole and loose formation.Due to the limitation of the design concept, alloying component has been limited near multicomponent alloy eutectic point, still Have a superior physical properties, the alloying component point of mechanical property and chemical property may not necessarily be near multi-element eutectic point.Thus exist Causing casting titanium alloy in actual use is not poor mechanical property, is exactly that heat transfer property or electric conductivity cannot expire The requirement used enough.
With the development of the world today and the raising of living standards of the people, to Ti alloy with high performance material and it is used in The demand of extreme environment advanced titanium alloys material is also more and more.Predictably titanium-base alloy can be in industrial circle and national defence Field shows more extensive application prospect.The innovation for carrying out Alloy Materials be unable to do without alloy structure and ingredient design, and The thermodynamics and kinetics of material are the main methods for solving the problems, such as such.It is true by the screening and ingredient of optimized alloy element It is fixed, it not only can achieve required various performance indicators, can also reduce the production cost of alloy smelting and processing and to equipment Requirement.Not only service life has further raising to such product, is also convenient for industrialization large-scale production.
Summary of the invention
The purpose of the present invention is to overcome the deficiency in the prior art, provides a kind of solidification of casting Two Liquid Phases and high damping properties Titanium alloy and technique.
To achieve the goals above, the present invention adopts the following technical scheme:
A kind of casting Two Liquid Phases solidification and high damping properties titanium alloy and technique.By weight percentage, the group of alloy becomes Sn:6.0-8.0wt.%,Nd:0.5-0.8wt.%,Yb:0.4-0.6wt.%,Bi:3.0-3.5wt.%,Al:10.0-12.0wt.%, Sb:1.4-1.6wt.%, Si:2.0-3.0wt.%, Fe:4.0-5.0wt.%, surplus are titanium.
A kind of above-mentioned casting Two Liquid Phases solidification and high damping properties titanium alloy and technique, include the following steps: raw material Using titanium sponge, alloying element is added in the form of pure metal or intermediate alloy.Alloy raw material uses press after ingredient and mixing It is pressed into small electrode.Several small electrode groups are welded together, melting 3 times in consumable electrode vacuum furnace are put into.Last primary molten During refining, melts of titanium alloy is cast in vacuum drying oven and is come out of the stove;Alloy casting uses the punching block of diameter 100-150mm, and adopts Cooled down with the mode of water cooling.Casting rod is heated in 810-840 degree, is forged using precise forging machine, drafts per pass is 5- 6%.An intermediate annealing is carried out between every 3 passage, temperature is 520-560 degree, 1.4 hours.It can be forged using multiple, until Stick diameter is forged between 40-60mm.Last heat treating regime are as follows: 350-380 degree solution treatment 1.2 hours, it is then air-cooled.
Compared with prior art, the invention has the following beneficial effects:
(1) liquid can be passed through in the design field of multicomponent alloy with the raising of the development of new technology and design of material ability The spinodal decomposition effect of phase generates two different melts, and both melts is made to have very big fusing point difference.It is this Design method is that another eliminate casts hole and loose novel method.Since the liquid phase spinodal decomposition of alloy can be suitable It is realized in big composition range, thus material designer can be further increased by constantly adjusting alloying element and content The other performance of material.This design method is undoubtedly very advanced, and in practice more compared to the design of eutectic point alloy It can solve practical problem.But regrettably, in titanium alloy field, there is no based on the design concept both at home and abroad at present New product occurs.Increasingly developed with science and technology and industry, the use environment and condition of titanium alloy are also increasingly harsher.Thus, It develops not near eutectic point and the casting with superior physical properties and mechanical property with titanium alloy is current heat both domestic and external Point direction.This patent provides a kind of titanium of novel elimination casting hole and rarefaction defect based on liquid phase spinodal decomposition characteristic Alloy and its technique.
(2) the novel casting titanium alloy of this patent design, during solidification, the liquid phase and richness Nd and Yb of rich Ti Liquid phase constantly separated from initial alloy melt.The melt of these richnesses Ti is due to richness Nd and Yb melt phase of getting along well It is molten, thus gradually squeezed in the gap of dendrite in process of setting along with the generation of dendrite, and narrow at these It is finally solidified in gap, plays the role of supplement solidification hole.Thus, the alloy for having liquid phase spinodal decomposition characteristic is most suitable for Prepare the casting of no solidification shrinkage hole because this material generate solidification hole the defects of it is few.With technical term come It says, liquid alloy generates two kinds of mutually insoluble liquid phases during solidification, and the liquid phase of low melting point can be in process of setting The dendrite hole that generates when compensation high-melting-point liquid phase solidification, thus physical property for casting and mechanical property have and extremely have The effect of benefit.
(3) the novel casting titanium alloy of present patent application protection has wide solidification temperature range (950-1420 degree). Wherein the solidification temperature range of main richness Ti melt is 1250-1420 degree, and the melt solidification temperature range of rich Nd and Yb are 950-1060 degree.The temperature range that the solidification temperature range of two kinds of liquid phases is covered from 1420 degree to 950 degree, thus with the conjunction When gold is cast, the cast member consistency that can be obtained is high, can achieve 98% or more and goes out without apparent hole It is existing.In addition, the alloy has extremely excellent reuse performance, the appearance profile of cast member is clear after 4 reuses, surface light It is clean.Thus, yield rate not only can be improved in the industrialization of the material, can also substantially reduce production cost by multiple reuse.
(4) with the continuous development of modern science and technology, vibration and noise problem oneself cause more and more extensive concern.In army Thing field, vibration and noise not only influence the normal work of Submarine Navigation instrument, can also improve submarine and be arrived by enemy's sonar detection Probability;The vibration and noise generated during the work time in civil field, precision instrument, lathe and household electrical appliance etc. is also stranded Disturb the production and living of people.Current high damping alloy is mainly iron-based, manganese base, and copper-based and acieral enters application The titanium-based damping alloy in field is fewer.The titanium alloy of present patent application protection has excellent due to the optimization for carrying out materialogy Different damping capacity.The material has excellent mechanical property: yield strength 600-620MPa, tensile strength 840- 850MPa, elongation percentage 4-6%.The mechanics that can achieve common titanium alloy is horizontal, but do not have with conventional titanium alloy High damping properties: SDC=20-30%, conventional titanium alloy material are SDC=8-12% or so.The present invention can be used for manufacturing using temperature Degree is 300 degree or less structural members and has highly significant lightweight and effectiveness in vibration suppression, has huge market prospects.
Specific embodiment
Embodiment 1
A kind of casting Two Liquid Phases solidification and high damping properties titanium alloy and technique.By weight percentage, the group of alloy becomes Sn:6.0wt.%,Nd:0.5wt.%,Yb:0.4wt.%,Bi:3.0wt.%,Al:10.0wt.%,Sb:1.4wt.%,Si: 2.0wt.%, Fe:4.0wt.%, surplus are titanium.A kind of above-mentioned casting Two Liquid Phases solidification and high damping properties titanium alloy and technique, Include the following steps: raw material using titanium sponge, alloying element is added in the form of pure metal or intermediate alloy.Alloy raw material warp After ingredient and mixing, small electrode is pressed into press.Several small electrode groups are welded together, melting in consumable electrode vacuum furnace is put into 3 times.During last melting once, melts of titanium alloy is cast in vacuum drying oven and is come out of the stove;Alloy casting uses diameter The punching block of 100-150mm, and cooled down by the way of water cooling.Casting rod is heated in 810-840 degree, is forged using precise forging machine It makes, drafts per pass is 5-6%.An intermediate annealing is carried out between every 3 passage, temperature is 520-560 degree, 1.4 hours. It can be using repeatedly forging, until forging stick diameter is between 40-60mm.Last heat treating regime are as follows: at 350-380 degree solid solution Reason 1.2 hours, it is then air-cooled.
The alloy has wide solidification temperature range (950-1420 degree).The wherein setting temperature of main richness Ti melt Range is 1250-1420 degree, and the melt solidification temperature range of rich Nd and Yb are 950-1060 degree.The setting temperature model of two kinds of liquid phases The temperature range covered from 1420 degree to 950 degree is enclosed, thus when being cast with the alloy, the casting that can be obtained Part consistency is high, can achieve 98% or more and occurs without apparent hole.The material has excellent mechanical property: surrender Intensity is 600MPa, tensile strength 840MPa, elongation percentage 4%.The mechanics that can achieve common titanium alloy is horizontal, still The high damping properties not having with conventional titanium alloy: SDC=25%, conventional titanium alloy material are SDC=8-12% or so.The present invention It can be used for manufacturing and the use of temperature be 300 degree or less structural members and there is highly significant lightweight and effectiveness in vibration suppression have huge Big market prospects.
Embodiment 2
A kind of casting Two Liquid Phases solidification and high damping properties titanium alloy and technique.By weight percentage, the group of alloy becomes Sn:8.0wt.%,Nd:0.8wt.%,Yb:0.6wt.%,Bi:3.5wt.%,Al:12.0wt.%,Sb:1.6wt.%,Si: 3.0wt.%, Fe:5.0wt.%, surplus are titanium.A kind of above-mentioned casting Two Liquid Phases solidification and high damping properties titanium alloy and technique, Include the following steps: raw material using titanium sponge, alloying element is added in the form of pure metal or intermediate alloy.Alloy raw material warp After ingredient and mixing, small electrode is pressed into press.Several small electrode groups are welded together, melting in consumable electrode vacuum furnace is put into 3 times.During last melting once, melts of titanium alloy is cast in vacuum drying oven and is come out of the stove;Alloy casting uses diameter The punching block of 100-150mm, and cooled down by the way of water cooling.Casting rod is heated in 810-840 degree, is forged using precise forging machine It makes, drafts per pass is 5-6%.An intermediate annealing is carried out between every 3 passage, temperature is 520-560 degree, 1.4 hours. It can be using repeatedly forging, until forging stick diameter is between 40-60mm.Last heat treating regime are as follows: at 350-380 degree solid solution Reason 1.2 hours, it is then air-cooled.
The alloy has wide solidification temperature range (950-1420 degree).The wherein setting temperature of main richness Ti melt Range is 1250-1420 degree, and the melt solidification temperature range of rich Nd and Yb are 950-1060 degree.The setting temperature model of two kinds of liquid phases The temperature range covered from 1420 degree to 950 degree is enclosed, thus when being cast with the alloy, the casting that can be obtained Part consistency is high, can achieve 98% or more and occurs without apparent hole.The material has excellent mechanical property: surrender Intensity is 610MPa, tensile strength 842MPa, elongation percentage 5%.The mechanics that can achieve common titanium alloy is horizontal, still The high damping properties not having with conventional titanium alloy: SDC=24%, conventional titanium alloy material are SDC=8-12% or so.The present invention It can be used for manufacturing and the use of temperature be 300 degree or less structural members and there is highly significant lightweight and effectiveness in vibration suppression have huge Big market prospects.
Embodiment 3
A kind of casting Two Liquid Phases solidification and high damping properties titanium alloy and technique.By weight percentage, the group of alloy becomes Sn:6.2wt.%,Nd:0.6wt.%,Yb:0.6wt.%,Bi:3.2wt.%,Al:10.5wt.%,Sb:1.4wt.%,Si: 2.4wt.%, Fe:4.8wt.%, surplus are titanium.A kind of above-mentioned casting Two Liquid Phases solidification and high damping properties titanium alloy and technique, Include the following steps: raw material using titanium sponge, alloying element is added in the form of pure metal or intermediate alloy.Alloy raw material warp After ingredient and mixing, small electrode is pressed into press.Several small electrode groups are welded together, melting in consumable electrode vacuum furnace is put into 3 times.During last melting once, melts of titanium alloy is cast in vacuum drying oven and is come out of the stove;Alloy casting uses diameter The punching block of 100-150mm, and cooled down by the way of water cooling.Casting rod is heated in 810-840 degree, is forged using precise forging machine It makes, drafts per pass is 5-6%.An intermediate annealing is carried out between every 3 passage, temperature is 520-560 degree, 1.4 hours. It can be using repeatedly forging, until forging stick diameter is between 40-60mm.Last heat treating regime are as follows: at 350-380 degree solid solution Reason 1.2 hours, it is then air-cooled.
The alloy has wide solidification temperature range (950-1420 degree).The wherein setting temperature of main richness Ti melt Range is 1250-1420 degree, and the melt solidification temperature range of rich Nd and Yb are 950-1060 degree.The setting temperature model of two kinds of liquid phases The temperature range covered from 1420 degree to 950 degree is enclosed, thus when being cast with the alloy, the casting that can be obtained Part consistency is high, can achieve 98% or more and occurs without apparent hole.The material has excellent mechanical property: surrender Intensity is 615MPa, tensile strength 846MPa, elongation percentage 5%.The mechanics that can achieve common titanium alloy is horizontal, still The high damping properties not having with conventional titanium alloy: SDC=28%, conventional titanium alloy material are SDC=8-12% or so.The present invention It can be used for manufacturing and the use of temperature be 300 degree or less structural members and there is highly significant lightweight and effectiveness in vibration suppression have huge Big market prospects.

Claims (3)

1. a kind of casting Two Liquid Phases solidification and high damping properties titanium alloy and technique;According to weight percent, the alloy at It is divided into: Sn:6.0-8.0wt.%, Nd:0.5-0.8wt.%, Yb:0.4-0.6wt.%, Bi:3.0-3.5wt.%, Al:10.0- 12.0wt.%, Sb:1.4-1.6wt.%, Si:2.0-3.0wt.%, Fe:4.0-5.0wt.%, surplus are titanium.
2. a kind of casting is existed with Two Liquid Phases solidification and high damping properties titanium alloy and technique, feature according to claim 1 In including following smelting step: raw material use titanium sponge, and alloying element is added in the form of pure metal or intermediate alloy;Alloy Raw material is pressed into small electrode after ingredient and mixing, with press;Several small electrode groups are welded together, consumable electrode vacuum furnace is put into Middle melting 3 times;During last melting once, melts of titanium alloy is cast in vacuum drying oven and is come out of the stove;Alloy casting uses The punching block of diameter 100-150mm, and cooled down by the way of water cooling.
3. a kind of casting is existed with Two Liquid Phases solidification and high damping properties titanium alloy and technique, feature according to claim 1 In including following procedure of processing: casting rod being heated in 810-840 degree, is forged using precise forging machine, drafts per pass is 5-6%;An intermediate annealing is carried out between every 3 passage, temperature is 520-560 degree, 1.4 hours;It can be using repeatedly forging, directly To forging stick diameter between 40-60mm;Last heat treating regime are as follows: 350-380 degree solution treatment 1.2 hours, it is then air-cooled.
CN201811135566.XA 2018-09-28 2018-09-28 A kind of casting Two Liquid Phases solidification and high damping properties titanium alloy and technique Pending CN109097624A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811135566.XA CN109097624A (en) 2018-09-28 2018-09-28 A kind of casting Two Liquid Phases solidification and high damping properties titanium alloy and technique

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811135566.XA CN109097624A (en) 2018-09-28 2018-09-28 A kind of casting Two Liquid Phases solidification and high damping properties titanium alloy and technique

Publications (1)

Publication Number Publication Date
CN109097624A true CN109097624A (en) 2018-12-28

Family

ID=64867446

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811135566.XA Pending CN109097624A (en) 2018-09-28 2018-09-28 A kind of casting Two Liquid Phases solidification and high damping properties titanium alloy and technique

Country Status (1)

Country Link
CN (1) CN109097624A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109778008A (en) * 2019-03-24 2019-05-21 杭州辰卓科技有限公司 A kind of two facies pattern of alpha+beta and there is high-damping and thermal stability titanium alloy and technique
CN109778011A (en) * 2019-03-25 2019-05-21 杭州辰卓科技有限公司 A kind of single-phase β high-damping high thermal conductivity titanium alloy of novel dislocation atmosphere mechanism and technique

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070049418A1 (en) * 2005-08-26 2007-03-01 Jiin-Huey Chern Lin Method of making a golf club head from bismuth-containing titanium alloy and golf club head
CN107779667A (en) * 2016-08-30 2018-03-09 天工爱和特钢有限公司 A kind of titanium alloy plate
CN107824227A (en) * 2015-12-17 2018-03-23 秦川 A kind of catalyst carrier for purifying vehicle tail gas
CN108559872A (en) * 2018-06-05 2018-09-21 中国航发北京航空材料研究院 A kind of TiAl alloy and preparation method thereof

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070049418A1 (en) * 2005-08-26 2007-03-01 Jiin-Huey Chern Lin Method of making a golf club head from bismuth-containing titanium alloy and golf club head
CN107824227A (en) * 2015-12-17 2018-03-23 秦川 A kind of catalyst carrier for purifying vehicle tail gas
CN107779667A (en) * 2016-08-30 2018-03-09 天工爱和特钢有限公司 A kind of titanium alloy plate
CN108559872A (en) * 2018-06-05 2018-09-21 中国航发北京航空材料研究院 A kind of TiAl alloy and preparation method thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109778008A (en) * 2019-03-24 2019-05-21 杭州辰卓科技有限公司 A kind of two facies pattern of alpha+beta and there is high-damping and thermal stability titanium alloy and technique
CN109778011A (en) * 2019-03-25 2019-05-21 杭州辰卓科技有限公司 A kind of single-phase β high-damping high thermal conductivity titanium alloy of novel dislocation atmosphere mechanism and technique

Similar Documents

Publication Publication Date Title
CN104630578B (en) High plasticity alloy cast aluminum and its gravitational casting preparation method
CN104561690B (en) High-plasticity cast aluminum alloy and extrusion casting preparation method thereof
CN104630556B (en) High anti-corrosion CuNiSiNbSn series elastic copper alloy of a kind of ultra-high-strength/tenacity and preparation method thereof
CN104278171B (en) A kind of CuTi series elastic copper alloy and preparation method thereof
CN100445019C (en) Al-Mg-Sc series solder wire
CN100396806C (en) Nickel base casting high temperature alloy for high temperature mould
CN104561688A (en) Heat-resistant cast aluminum alloy and gravity casting method thereof
CN110512116A (en) A kind of high Nb-TiAl intermetallic compound of multicomponent high-alloying
CN104561691A (en) High-plasticity cast aluminum alloy and pressure casting preparation method thereof
CN101348874A (en) High performance copper-based alloy material and preparation thereof
CN104630577A (en) Heat-resistant cast aluminum alloy and pressure casting method thereof
CN109266901A (en) A kind of preparation method of Cu15Ni8Sn high-strength wearable rod of metal alloy/silk
CN108411169A (en) Al-mg-si alloy and preparation method thereof
CN109097624A (en) A kind of casting Two Liquid Phases solidification and high damping properties titanium alloy and technique
CN107723517A (en) A kind of Ti Al based alloys and its application with good increasing material manufacturing forming property
CN101407880A (en) Mg-Zn-Zr-Nd magnesium alloy and preparation thereof
CN110804712A (en) Magnesium-containing high-entropy alloy and preparation method thereof
CN104099494A (en) Air conditioner aluminum foil material and surface treatment method thereof
CN105648445A (en) Aluminum-zinc-indium-erbium sacrificial anode and preparation method thereof
CN109136644A (en) A kind of ultralight titanium alloy for having excellent hot workability energy and high-temperature stability
CN111118356A (en) Aluminum alloy material, aluminum alloy molded part, preparation method of aluminum alloy molded part and terminal equipment
CN109280831A (en) A kind of fire-retardant Tough magnesium alloy and preparation method thereof
CN109112374A (en) A kind of high-strength magnesium-tin-zinc-lithium-sodium alloy and preparation method thereof
CN108277385A (en) A kind of titanium alloy plate and processing method
CN107739888A (en) A kind of Ti V based alloys and its application with good increasing material manufacturing forming property

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20181228

RJ01 Rejection of invention patent application after publication