CN102021392B

CN102021392B - Co-Li-RE high-strength heat-resistant aluminium alloy material with C as modifier and preparation method thereof

Info

Publication number: CN102021392B
Application number: CN 200910307166
Authority: CN
Inventors: 张中可; 车云; 陈新孟; 门三泉; 胥光酉; 李祥
Original assignee: Guizhou Huake Aluminium Material Engineering Technology Research Co Ltd
Current assignee: Guizhou Huake Aluminium Material Engineering Technology Research Co Ltd
Priority date: 2009-09-17
Filing date: 2009-09-17
Publication date: 2012-07-25
Anticipated expiration: 2029-09-17
Also published as: CN102021392A

Abstract

The invention discloses a Co-Li-RE high-strength heat-resistant aluminium alloy material with C as a modifier. The aluminium alloy material comprises the following components by weight: 1.0-10.0% of Cu, 0.05-1.5% of Mn, 0.01-0.5% of Cd, 0.01-0.5% of Ti, 0.0001-0.15% of C, 0.01-1.0% of Zr, 0.01-1.0% of Co, 0.1-3.0% of Li, 0.05-5% of RE and the balance Al. The invention finally develops the high-strength heat-resistant aluminium alloy material by taking the high-quality melt, solid solution and phase diagram theory as the guidance, taking C as the efficient modifier, giving preference to the main alloying elements Cu, Mn and RE as formulas, reducing the temperature range of the quasi-solid phase of the alloys, solving the problems of great hot cracking tendency, low high temperature strength of the products and the like during casting and giving preference to multiple microalloying elements with low cost as formulas.

Description

With rotten Co-Li-RE high strength heat resistant alloy material of C and preparation method thereof

Technical field

The present invention relates to a kind of aluminum alloy materials and preparation method thereof, particularly a kind of with rotten Co-Li-RE high strength heat resistant alloy material of C and preparation method thereof.

Background technology

Duraluminum is a kind of younger metallic substance, just begins industrial application in 20 beginnings of the century.During the World War II, aluminium is mainly used in the manufacturing military aircraft.After the war; Because war industry is die-offed to the demand of aluminium; The aluminium industry member is just started to develop civil aluminum alloy; Make its range of application expand to construction industry, container package industry, transportation, electric power and national economy all departments such as electronic industry, machinery manufacturing industry and petrochemical complex, be applied in the middle of the daily life by aircraft industry.Now, more than the consumption of aluminium, scope is wide, is only second to iron and steel, becomes second largest metallic substance.

From the angle of production and Al-alloy products, be divided into two types of wrought aluminium alloy and y alloy ys to aldural traditionally; Divide from goods available temperature condition, aldural is divided into common aluminum alloy and high temperature (or heat-resisting) duraluminum again.Up to the present, can satisfy the high strength at high temperature needs, have only the Al-Cu line aluminium alloy, say from trade mark series that Al-Cu is that alloy comprises y alloy y and wrought aluminium alloy, no matter and casting still is out of shape, all belong to 2 line aluminium alloys; And can satisfy the high-temp and high-strength duraluminum that good casting property is carried out deformation processing easily simultaneously, also do not see the public reported mistake.

1, high strength cast aluminum alloys and wrought aluminium alloy

General y alloy y comprises that AlSi system, AlCu system, AlMg system and AlZn are 4 series; Wherein the intensity with AlCu system and AlZn line aluminium alloy is the highest; But it is most between 200Mpa～300Mpa; A few trade mark that has only AlCu system that is higher than 400Mpa, but because of adopting the refined aluminium matrix and adding noble element, manufacturing cost is very high; AlZn is that the resistance toheat of casting alloy is very poor.Therefore, general y alloy y is compared with wrought aluminium alloy because of obdurability is inferior slightly and is made its range of application receive bigger restriction.Many important use such as extraordinary traction engine bogie wheel, aviation alloyed aluminium etc. adopts wrought aluminium alloy, rather than y alloy y.Wrought aluminium alloy has reduced defective through means such as extruding, rolling, forgings, refinement crystal grain, improved density, thereby had very high intensity, good toughness and good use properties.But, equipment and moulds of industrial equipment are required height, operation is many, so the wrought aluminium alloy production cycle is long, cost is very high.Compare plurality of advantages such as that y alloy y has is cheap, organize isotropy, can obtain special organization, be easy to produce complex-shaped part, can small serial production also can produce in enormous quantities with wrought aluminium alloy.Therefore; Develop the high-toughness casting aluminum alloy material and the casting forming process thereof that can substitute the part wrought aluminium alloy; Can reach the purpose of casting and forging, shortening manufacturing cycle, reduction manufacturing cost, have important significance for theories and great actual application value.

In the evolution of high-toughness casting aluminum alloy, the A-U5GT that succeeds in developing in 20 beginnings of the century of France occupies an important position, at present representative high-toughness casting aluminum alloy its history at most, use the most extensive.China does not have the trade mark corresponding with it at present.

On the A-U5GT basis, transform behind the U.S. aluminium association trade mark 201.0 (1986) and 206.0 (1967) and form, have good mechanical property and stress corrosion resistant ability.But owing to contain 0.4%～1.0% silver, material cost is very high, only is used for military affairs or other demanding fields, has limited its range of application.

In the high-toughness casting aluminum alloy field, China has obtained the achievement of attracting attention in the world.The sixties, the Beijing Research Inst. of Aeronautic Material succeeded in developing the ZL205A alloy to the seventies.The ZL205A alloying constituent is complicated, contains Cu, Mn, Zr, V, Cd, Ti, 7 kinds of alloying elements such as B.The tensile strength of ZL205A (T6) is 510MPa, is that the cast aluminium alloy material intensity of the existing at present registration trade mark is the highest.The obdurability of ZL205A (T5) is best, and unit elongation can reach 13%; But the maximum defective of ZL205A is that castability is poor, hot cracking tendency is big, and because of formulation cost is high, range of application is little simultaneously.

Above-mentioned 3 kinds of high-toughness casting aluminum alloys belong to Al-Cu system.This series alloy intensity is high, and plasticity and toughness are also better.But castability is relatively poor, is embodied in that hot cracking tendency is big, flowability is relatively poor, feeding is difficult.In addition, this series alloy etch resistant properties is relatively poor, and the intergranular corrosion tendency is arranged.The qualified casting of this series alloy is very low.

In addition; Disclosed application number is that 4 patent names of 200810302670.3,200810302668.6,200810302669.0 and 200810302671.8 are in the document of " a kind of high-strength cast aluminium alloy material " and have introduced a kind of high-strength cast aluminium alloy material of being made up of Cu, Mn, Ti, Cr, Cd, Zr, B and REE; This aluminum alloy materials has advantages of higher tensile strength and unit elongation; Tensile strength has reached 440Mpa, and unit elongation is greater than 6%; But this type of high-strength cast aluminium alloy material in use still fails to solve the particularly thorny of the big problem of hot cracking tendency, alloy strength and castability; Its major cause is at alloy principal element Cu, Mn composition range; The accurate solid-state temperature a wider range of alloy; Grow sufficient condition is provided for having anisotropic dendrite during casting solidification, form powerful internal contraction stress solidifying the later stage, so it is big to shrink hot cracking tendency.

The 2XXX of official registration is that the wrought aluminium alloy trade mark has more than 70 at present; The overwhelming majority is a U.S. Register; Wherein have only 2001,2004,2011,14 trades mark such as 2011A, 2111,2219,2319,2419,2519,2021,2A16,2A17,2A20,2B16 be copper content at the high xaloy more than 5%, and wherein copper content is having only 2A16,2A17,2A20, these 4 trades mark of 2B16 more than 6%.All contain compositions such as more Si, Mg, Zn in these wrought aluminium alloy prescriptions; And there is not rare earth (RE) etc. to play the element of microalloying effect; Therefore its prescription composition is that y alloy y differs greatly with 2, reflects the duraluminum different production technology and the deep processing technology of two kinds of attributes.

2, high temperature aluminium alloys

Superalloy is claimed heat-resistance high-strength alloy, the strong alloy of heat or superalloy again; It is a kind of important meals material that grows up along with the appearance of aero-turbine in the forties in 20th century; Can under high temperature oxidation atmosphere and exhaust gas corrosion condition, bear bigger working load for a long time; Being mainly used in the hot-end component of internal combustion turbine, is the important structure material of aerospace, naval vessel, generating, petrochemical complex and communications and transportation industry.Wherein some alloy also can be used for biotechnology and makes orthopaedics and dental material.

That superalloy commonly used comprises is Ni-based, iron-based and cobalt base alloy, can under 600～1100 ℃ of hot environments, work; Heat-resisting aluminium alloy then is to grow up during the cold war.The heat-resistance high-strength duraluminum is suitable for bearing bigger working load in the thermal environment midium or long term below 400 ℃, obtains increasing application in fields such as aerospace, heavy industry machineries.Except that aero-turbine, internal combustion turbine etc. directly with parts that high-temperature fuel gas contacts, all the other HTHP strong power parts all can adopt the heat-resistance high-strength aluminium alloy casting.

Because the duraluminum ratio is easier to processing, along with the raising of processing technology level, under the situation that intensity meets the demands, how People more and more adopts wrought aluminium alloy to substitute y alloy y.Therefore the heat-resistance high-strength duraluminum is divided into Ajax alloy again and is out of shape with two big types of alloys.

Generally speaking, the heat-resistance high-strength alloy all contains multiple alloy element, many reach ten surplus kind.The element that is added plays effects such as solution strengthening, dispersion-strengthened, grain-boundary strengthening and surface stabilization respectively in alloy, make alloy can at high temperature keep high mechanical property and environmental performance.

The factor of considered when selecting casting for use with superalloy:

(1) normal working temperature of foundry goods, the highest and minimum working temperature and the frequency of temperature variation.

(2) expansion character of the temperature range of foundry goods itself and alloy.

(3) load performance that bears of foundry goods, loading, supporting and external constraint mode.

(4) to life requirements and the deflection of allowing, Working environment and character, manufacturing process and the cost factor etc. of foundry goods.

Be used for the aluminum alloy materials of high temperature component casting at present, have only A201.0, ZL206, ZL207, ZL208, more than 206.0 kinds of trades mark in the national standard, comprise aluminum bronze Mn series alloy and aluminium rare earth-based alloy; Wherein, aluminum bronze Mn series alloy majority is an alloy material with high-purity grade of aluminium ingot, and cost is higher, and then at room temperature mechanical property is relatively poor relatively for the aluminium rare earth-based alloy.And; At present heat-resistance high-strength duraluminum ubiquity hot strength low (instantaneous tensile strength is less than 200Mpa more than 250 ℃; Creep rupture strength is less than 100Mpa), defectives such as formulation cost is high, castability is poor, casting qualified rate is low, waste product material and slag charge reuse property difference, cause problems such as casting quality is poor, cost high, the slag charge treatment scheme is long.In addition, also all contain noble element in the new prescription of most heat-resisting aluminium alloy patents of declaring in recent years, and castability is poor, quality can't satisfy the requirement of aeronautical technology progressive, is inappropriate for the industrialization production application.

And the heat-resistance high-strength wrought aluminium alloy that in national economy and the modernization of national defense and development, has extensive use and the bright prospect of aurora; Report is less in the domestic and foreign literature; 2XXX such as known 2219,2A02,2A04,2A06,2A10,2A11,2A12,2A14,2A16,2A17,2A50,2A70,2A80 are that 7XXX such as wrought aluminium alloy and 7A04 are wrought aluminium alloy; The intensity majority is less than 100Mpa under temperature more than 250 ℃; And its main alloy element is except that Cu, Mn; All be with Si, Mg, Zn as main micro alloying element, and do not add these several kinds of elements and more than 250 ℃ under the temperature heat-resistance high-strength wrought aluminium alloy material of intensity more than 150Mpa be not reported.

3, the rotten processing of duraluminum

The high materialization processing of melt is the core link of aluminium alloy smelting and pursues one's goal, is basis and the prerequisite that obtains the fine aluminum alloy material simultaneously.High materialization is handled and is mainly comprised two aspects: the one, and pureization, the 2nd, structural unit refinement and homogenizing.The former takes the method for an impurity solid state filtering and " with the gas degasification " to reduce melt impurity and hydrogen richness, and technological process can produce waste residue and waste gas; The latter is commonly referred to rotten the processing; Be with additive or machinery, physical method make the size of the elementary cell xln that constitutes aluminium alloy melt and sosoloid become as far as possible little, distribute even as far as possible; Because of additive gets into alloy melt; Become the effective ingredient of alloy, thereby do not produce waste residue and waste gas in the process.It is the fundamental means of adjustment duraluminum as-cast structure that efficient alterant is particularly used in rotten processing.

Theoretical according to melt crystallization, the additive that adds as alterant should satisfy following requirement:

(1) at high temperature chemical ingredients is constant, and enough stability is arranged in molten aluminium;

(2) fusing point of additive should be than the height of aluminium;

(3) lattice of additive and aluminium should adapt on scantlings of the structure;

(4) form powerful adsorption bond with the melt atom that is processed.

Generally adopt the processing of going bad of wire rod or pie additive in the wrought aluminium alloy field of materials at present; Comprise titanium, boron, rare earth compound alterant etc.; Facts have proved, adopt suitable alterant that the performance of wrought aluminium alloy material is had good improvement effect.And in the y alloy y field; Mostly the alterant that adopts is pulverous alkali metal halide composite salt; This type of alterant exist modification effect limited, increase foreign matter content in the duraluminum, produce shortcomings such as a large amount of obnoxious flavoures; In melt treatment, realize having increased trace elements again in the whole Water purification, improved the environmental protection cost simultaneously.Usually, the alkali metal halide composite salt is that the alterant of y alloy y has modification effect preferably as Al-Si, but is the alterant of alloy as Al-Cu, and modification effect is not enough.

In sum; Can know that the problem that in the research of heat-resistance high-strength degree field of aluminum alloys, exists at present has both at home and abroad: lack rotten efficiently the processing in the fusion process; Hot strength and weather resistance are not enough, and the high temperature instantaneous strength is all less than 250Mpa more than 250 ℃, and creep rupture strength is all less than 100Mpa; The materials processed poor performance; Waste disposal long flow path, cost height can't satisfy aeronautical technology progressive requirement etc.

Summary of the invention

Technical problem to be solved by this invention is; The melt treatment that exists to present aldural field is extensive, of poor quality, hot cracking tendency big, castability is poor; Technical barriers such as the goods yield rate is low, hot strength is low, waste product material and slag charge reuse property difference; With high-quality melt, sosoloid and phase diagram theory is guidance, with the C element as efficient alterant, through preferred alloy principal element Cu, Mn and REE prescription; Reduce the accurate solid-state temperature scope of alloy, the problem that is ubiquitous of big, the goods hot strength low (comprising instantaneous strength and creep rupture strength) of hot cracking tendency when solving casting; Preferred low-cost multicomponent microalloying element formula is for material base condition is created in the cultivation and the grain refining effect of high temperature phase and strengthening phase in the sosoloid; And optimize melting, thermal treatment process technology, realize high temperature phase and the enough culture of strengthening phase and giving full play to of grain refining effect in the sosoloid.The AlCu that finally develops a kind of rare earth multicomponent micro-alloying is novel high-strength heat-resisting (castibility and deformability) aluminum alloy materials.

Technical scheme of the present invention is that by weight percentage, this alloying constituent is Cu:1.0～10.0%; Mn:0.05～1.5%, Cd:0.01～0.5%, Ti:0.01～0.5%; C:0.0001～0.15%, Zr:0.01～1.0%, Co:0.01～1.0%; Li:0.1～3.0%, RE:0.05～5%, all the other are Al.

Above-mentioned rare earth elements RE is single rare earth element or more than one mixed rare-earth elements.

Above-mentioned rare earth elements RE comprises La, Ce, Pr, Nd, Er, Eu and Y.

The preparation method of this novel high-strength heat-resistant aluminium alloy material comprises the steps:

(1) in above-mentioned element ratio scope; Selected one group of feasible element ratio, the alloy total amount of preparation is as required again extrapolated the quality of every kind of required elemental metals; The perhaps quality of master alloy; Perhaps the quality of hybrid metal additive (comprising salt compounds) is worked out the alloy production allocation sheet, and gets the raw materials ready by allocation sheet choosing foot.

(2) in smelting furnace, add an amount of aluminium ingot or molten aluminum liquid, heating makes it to melt fully and is incubated down at 700～800 ℃; For preventing that melt from sucking too much air, melting process should be accomplished as far as possible at short notice with in the enclosed environment.

(3) add Mn, Ti, Zr, Co, Li pure metal or Al-Mn, Al-Ti, Al-Zr, Al-Co, Al-Li master alloy or hybrid metal additive (comprising salt compounds) earlier by formula rate again; Add Cu, Cd pure metal or Al-Cu, Al-Cd master alloy or hybrid metal additive (comprising salt compounds) after stirring again; Add C and rare earth elements RE again, stir.

Wherein, the hybrid metal additive is meant pie or the block non-coking property sintered metal product that interpolation, adjustment alloy constituent element are used.Sintered metal product comprises that manganese, copper, zirconium, cobalt, lithium or titanium metal powder and flux mix; Flux is meant that the mixture of basic metal or earth alkali metal halogen salt is (like NaCl, KCl, Na ₃AlF ₆Deng).C is meant compound or aluminium carbon master alloy, comprises binary master alloy, ternary master alloy and polynary master alloy.

(4) then above-mentioned alloy melt is carried out furnace refining; In alloy melt, add refining agent (can adopt chlorine, Sesquichloratum, Manganous chloride tetrahydrate etc. as refining agent according to different operating modes), and stir, for preventing that melt from sucking moisture content and scaling loss, the melt refining should be operated in enclosed environment as far as possible simultaneously.

(5) slag hitting after the refining, leave standstill, temperature adjustment to 630～850 ℃, alloy liquid is toppled over and is come out of the stove, online degasification, slagging-off are handled.

(6) casting (crystallization and freezing in mold).

(7), confirm foundry goods is carried out 470～560 ℃, 30 hours with interior solution treatment in order to prevent the material burning.

Compared with prior art, the present invention has following major advantage:

To adopt refined aluminium mostly be matrix material and add the above noble element of per mille to have solved present Al-Cu and be high tough duraluminum (ZL201A, ZL 204A, ZL 205A etc.); Cost is higher; Causing Al-Cu is that high tough duraluminum can only be used for leading-edge fields such as aerospace, defence and military, and civil area is because of the not high restricted application problems of cost performance.

Along with the continuous expansion in China of China and the quick growth of world aluminum output and aluminium industry size, " with aluminium for steel " day by day becomes the trend and the trend of industry development, and also presses for the high high tough duraluminum of cost performance at civil area; The present invention is a matrix material through adopting general aluminium; Do not add (or adding less) noble element; Preferred feature micro alloying element prescription, and adopt technologies such as intensive, terse founding, purification, add efficient alterant; Develop the novel high-strength heat-resistant aluminium alloy material, overcome the threshold on cost of current material.

Particularly, the present invention has following eight advantages.

1, HS and high firmness.See from the strength of materials, require under the prerequisite satisfying plasticity, can be through Technology means such as thermal treatments, make various strengthening phases in as-cast structure fully, evenly, rationally separate out and distribute, make the strength of materials reach 480～540MPa, hardness >=HB140.

2, the double attribute of material.See from the material applications attribute; It belongs to the both sexes duraluminum; The characteristic of existing y alloy y has the characteristic of wrought aluminium alloy again, both can directly be used to cast all kinds of light powerful spares and structural part, also can cast bar earlier and be hot extruded into the section bar into various sections again.

In essence, this material belongs to the y alloy y of multicomponent microalloying, but because material has excellent flowing property and intergranular self-lubricating property, makes it possess the easy processing characteristics of wrought aluminium alloy simultaneously.

3, the advance of technology.See from production technique; On smelting technique, changed traditional extensive technology, can use electric furnace to carry out tight protectiveness melting, thereby avoid melt to sneak into too much impurity and gas; Complicated follow-up melt treatment flow process has also been simplified and shortened to the purity that had both kept alloy; Simultaneously, fusion process has improved energy utilization rate greatly and has reduced the pollution to environment than the conventional reflective melting technology, belongs to environment protecting and power-saving type technology.

(1) the protectiveness melting has significantly reduced energy consumption, pollution, has simplified Production Flow Chart, has improved the intensification degree

Because aluminium and aluminium alloy melt have extremely strong air-breathing tendency, so in the bad stove of open type or closure when thawing and melting, fused alloy liquid can absorb airborne O in large quantities ₂, gas such as moisture, generate insoluble Al ₂O ₃With H with excellent activity ₂, in melt, form impurity and gas, if untimely removing can form the slag inclusion, pore of foundry goods, defective such as loose when casting, cause goods to be scrapped; Wherein especially with H in the melt ₂Harm maximum because H ₂Solubleness when aluminium and duraluminum molten state is much higher than the solubleness when solid-state, therefore when solidifying, has a large amount of H ₂From alloy, overflow and cause a large amount of defectives.Insoluble slag then relatively is prone to remove.Therefore, avoiding melt air-breathing is the important measures that keep melt quality and castability.

Common large scale industry aluminium alloy smelting stove is to be the reflector oven or the holding furnace of the energy with liquid or geseous fuel, needs a large amount of air-breathings, contains a large amount of water vapors and CO in the products of combustion simultaneously ₂, NO _XDeng material, at high temperature very easily generate various detrimental impurity, simultaneously the same H that very easily adsorbs of these impurity itself with aluminium liquid with aluminium generation chemical reaction ₂, make melt receive severe contamination, before casting, melt must experience together or the special cleaning section in a few road, and the casting flow process of after the sampling detection is qualified, being allowed for access, and this has prolonged work flow undoubtedly, and energy consumption and contamination index all are difficult to reduce; Because the continuity requirement of producing must make equipment maximize, increase investment simultaneously, improved technological access threshold; To form multiplication long and the overhaul cost of equipment, start-up cost are all along with the maximization of equipment and long flow process.

And general aluminium alloy casting spare production plant, because production scale is little, equipment is simply extensive, and aluminium alloy melt is seldom taked airtight sfgd., causes melt quality and castability not high equally.

The preparation method that the present invention requires; Its melting mode is to adopt the Induction Heating Equipment of with closure; Air, water vapor and various products of combustion are to the pollution of melt when having eradicated fuel combustion; In fusion process, can adopt protective gas to carry out the protective atmosphere melting, farthest the invasion and attack of secluding air simultaneously; Owing to kept the high purity of melt, can take very simple through type degasification, deslagging device in cast sections thereafter, and needn't add special stop formula soaking equipment, thereby simplify technical process greatly.

(2) optimize the thermal treatment process of foundry goods, avoided the generation that material mechanical performance reduces, goods are scrapped that causes because of " burning "

Application number is that 4 patent names of 200810302670.3,200810302668.6,200810302669.0 and 200810302671.8 are in the invention of " a kind of high-strength cast aluminium alloy material "; The heat treatment process parameter of prescribed material is " below 620 ℃, 72 hours in ", in the material application test, when temperature surpasses 560 ℃ when finding solution treatment; " burning " phenomenon usually can take place; Cause the destruction of material microstructure, its characteristic feature is that leading indicators such as intensity and ductility significantly reduce, and foundry goods becomes fragile; The surface blackening obfuscation, even in heat treatment process, promptly crack, be out of shape and scrap.And when solid solubility temperature was lower than 470 ℃, because cultivation, the precipitation strength effect of strengthening phase are insufficient, the intensity of material was difficult to reach the desired destination value; Simultaneously,, find that heat treatment time surpasses 30 hours, the raising of material property is not had unusual effect through after test of many times gropes.Therefore, in order to improve effect and efficient, with heat treatment process parameter optimize and revise into: 470～560 ℃, 30 hours with interior solution treatment.

4, the science and the economy of prescription.See that from raw material sources advanced prescription has been created advantage--the body material advantage and the alloying element advantage of two aspects.On the one hand; The matrix alloy of novel material series can adopt general industry fine aluminium (promptly two zero aluminium; Comprise that aluminium liquid and remelting use aluminium ingot); Must adopt refined aluminium or the high-purity grade of prescription model that aluminium is matrix alloy than existing aldural, have advantages such as raw material supply abundance, cost is low, buying is convenient; Simultaneously, this material can adopt refined aluminium or high-purity grade of aluminium as matrix alloy equally, and the material of this prescription has higher ductility than the general alumina-base material of this kind.On the other hand, the contribution rate that cost of alloy is raise because of noble element is the tens of of common element and even more than hundred times, majority does not adopt noble element in the alloying element combination of novel material series, even adopt, ratio is also very little, all below per mille; And the ratio of existing aldural noble element is all more than per mille, and the advantage of two aspects is that serial novel material opens up a market and laid in great potential.

The present invention is the polynary prescription of characteristic micro alloying element through preferred alloy principal element copper (Cu), manganese (Mn) with cobalt (Co), lithium (Li), for material base condition is created in the cultivation and the grain refining effect of high temperature phase and strengthening phase in the sosoloid; With carbon (C) is the efficient alterant of alloy; Because the lattice parameter of the carbide that forms approaches the lattice parameter of aluminium sosoloid most; These carbide particles group is as crystallization nuclei very tiny (its size is less than 1 μ m) and can stable existence in aluminium liquid under suitable refining temperature; In the ingot solidification process, α-Al is had fabulous stable refinement nucleation ability basically, be superior to other alterants thereby do its antidamping ability of alterant with carbon; At utmost improve the alloy organizing dispersity, realize best modification effect; Select high temperature element cobalt (Co), lithium (Li) and the rare earth elements RE trace additives as complex alloysization for use, Co forms AlCo, Al in alloy ₉Co ₂Deng 8 kinds of dispersivity High-Temperature Strengthening phases, Co is the trace additives of the high strength cast aluminum alloys of complex alloysization, when it and Mn coexist, forms Al ₄(CoFeMn) etc. very complicated strengthening phase hinders dislocation, stops grain sliding in the interdendritic, has improved alloy at room temperature and high temperature (under 400 ℃) intensity effectively; Li forms AlLi in alloy ₃～Al ₁₂13 kinds of metallic compound dispersivitys such as Li High-Temperature Strengthening phase, rare earth elements RE can form multiple metallic compound in duraluminum (Rare-Earth Ce forms α-Ce in alloy ₃Al ₁₁～β-Ce ₃7 kinds of metallic compounds such as Al; Rare earth La forms α-Al in alloy ₁₁La ₃～β Al ₁₁La ₃Deng 6 kinds of metallic compounds; Rare earth Pr forms α-Al in alloy ₁₁Pr ₃～β-Al ₁₁Pr ₃Deng 6 kinds of metallic compounds; Rare earth Nd forms α-Al in alloy ₁₁Nd ₃～β-Al ₁₁Nd ₃Deng 6 kinds of metallic compounds; Rare earth Er forms ErAl in alloy ₃, ErAl ₂, ErAl, Er ₃Al ₂, Er ₂5 kinds of metallic compounds such as Al; Rare Earth Y forms Al in alloy ₃Y, Al ₂Y, AlY, Al ₂Y ₃, AlY ₂Deng 5 kinds of metallic compounds; Rare earth Dy forms α-DyAl in alloy ₃～β-DyAl ₃Deng 6 kinds of metallic compounds; Rare earth Eu forms EuAl in alloy ₄, EuAl ₂, 3 kinds of metallic compounds such as EuAl; Rare-earth Sm forms Al in alloy ₁₁Sm ₃, Al ₃Sm, Al ₂Sm, AlSm, AlSm ₂Deng 5 kinds of metallic compounds; Rare earth Pm forms Al in alloy ₁₁Pm ₃, AlPm ₂Deng 5 kinds of infusibility active metallic compounds; Rare-earth Gd forms Al in alloy ₄Gd, Al ₁₇Gd ₂Deng 7 kinds of infusibility active metallic compounds; Rare earth Tb forms Al in alloy ₃Tb, AlTb ₂Deng 5 kinds of infusibility active metallic compounds; Rare earth Ho forms Al in alloy ₃Ho, AlHo ₂Deng 5 kinds of infusibility active metallic compounds; Rare earth Tm forms Al in alloy ₃3 kinds of infusibility active metallic compounds such as Tm, AlTm; Rare Earth Y b forms Al in alloy ₃Yb, Al ₂2 kinds of infusibility active metallic compounds such as Yb; Rare earth Lu forms Al in alloy ₃Lu, AlLu ₂Deng 5 kinds of infusibility active metallic compounds or the like), all significantly improved alloy at room temperature intensity, high-temperature capability and fluidity of molten.

The main alloying element mechanism of action of the present invention is following.

1. this material allows copper (Cu) content in 1～10% scope, is that y alloy y cupric (Cu) amount is that 3～11% scope is slightly different than Al-Cu, but in theory then has earthshaking innovative significance.

On the one hand; At copper (Cu) content is 5.65～5.7% o'clock; Just in time equal the eutectic solubleness of Cu in the Al-Cu alloy; In heat treatment process,, form more rich Cu strengthening phase (comprising Al according to the turn model and mechanism of action variation of " fully solid solution-evenly separate out-grain-boundary strengthening phase-brilliant crack weighting agent (bond, inlay, anti-skidding) " ₂Cu is the θ phase), thus the room temperature of duraluminum and mechanical behavior under high temperature are all improved greatly, also improved processing characteristics; But because the solubility with temperature of Cu in Al reduces and sharply descend, in the crystallization and freezing process, the degree of supersaturation of Cu in α-Al sosoloid improves fast; On one side α-Al dendrite is grown up,, cause structural stress huge between intracrystalline and crystal boundary Yi Bian increase the tendency of outside crystal boundary, discharging rich Cu strengthening phase strongly; Alloy monolithic is in the solidification shrinkage stage simultaneously; String stress and structural stress are superimposed, and the instant actual strength when surpassing alloy then forms thermal crack; Therefore in the certain limit of copper (Cu) content≤5.65%, the castability of duraluminum is the poorest, hot cracking tendency is maximum.But total trend is that along with the reduction of copper content, the hot cracking tendency of alloy also reduces; When Cu content＜1%; Its strengthening phase is not enough; The turn model of strengthening phase and the mechanism of action are difficult to give full play to, and when temperature variation, the separating out and can form crystal boundary from more defective between crystal boundary to dissolving in of intracrystalline, reduce alloy at room temperature and hot strength; So it is Cu content is low excessively, nonsensical concerning simple Al-Cu alloy; If but added more REE (RE) in the alloy, then could play remedying the low excessively special-effect of Cu content.

On the other hand; At Cu content >=5.7% o'clock; Rich Cu can not all be absorbed by matrix when thermal treatment, then is distributed in crystal boundary with border rich Cu metallic compound form disperse, has reduced the concentration difference of the inside and outside Cu particle of α-Al sosoloid; Mild α-Al sosoloid dendrite is discharged the intensity of rich Cu phase to crystal boundary in process of setting, has promptly reduced structural stress and hot cracking tendency.Obviously, when Cu content >=5.7%, rich Cu is many more mutually, and the structural stress and the hot cracking tendency of alloy inside are more little during crystallization; Simultaneously, the rich Cu of the thin brilliant disperse of HMP forms active heterogeneous nucleus when melt crystallization, quicken the melt crystallization reaction but stop nuclei growth, refinement crystal grain, also reduced the alloy hot cracking tendency; And make between the matrix crystal boundary filling fuller; Rich Cu can also form the refractory metal compound with multiple element such as Al, Mn mutually.All these effects, the surface tension of the melt that weakened has significantly reduced melt viscosity, thereby has significantly improved the castability of fluidity of molten and alloy.

When Cu content is in 5.7% left and right sides; After heat treatment, more rich Cu phase (dissolving in-precipitated phase) and the less thin brilliant disperse phase of (about 0.5%) Cu based metallization compound are arranged, make the alloy strength under the room temperature state keep higher level at the matrix crystal boundary; But when being in hot environment; Because of a large amount of rich Cu dissolve in the matrix mutually again, will cause more intergranular space and defective, this can make the hot strength of alloy significantly descend.Along with Cu content continue to increase, the degree of alloy strength temperature influence reduces, and when disperse phase and precipitated phase were in the equivalent state basically, it is minimum that the strength of materials is acted upon by temperature changes, and Cu content should be 11～12% in the alloy at this moment.

But when Cu content in the alloy＞10%; Superfluous Cu has preferential crystallization character mutually and forms huge network structure during because of crystallization; Alloy viscosity strengthens greatly; Surplus replaces the principal element that aluminum substrate becomes crystallization control in crystallisation process, original disperse phase is all shielded the good effect of aluminum substrate phase, so the various performances of alloy decline to a great extent again.

According to the checking of above theoretical basis and practice, confirm that the zone of reasonableness of main alloying element Cu content is: 1～10% (wt%).

2. this material improves corrosion stability with manganese (Mn) element, shields impurity F e simultaneously, reduces the deleterious effect of Fe.

MnAl because of manganese (Mn) element and matrix effect generation ₆Have identical current potential with fine aluminium, can improve the corrosion stability and the weldableness of alloy effectively; While, Mn was as the High-Temperature Strengthening phase, had the effect that improves recrystallization temperature, suppresses the recrystal grain alligatoring, can realize the solution strengthening to alloy, additional reinforcement, raising resistance toheat; Under the grain-refining agent effect, can generate the Al of pelletizing shape with the Fe element ₃(Fe, Mn) effectively eliminated the deleterious effect of Fe to alloy, so the present invention can allow the scope (Fe≤0.5%) of Fe content at broad, and the benefit of bringing like this is: realize general aluminium substitution refined aluminium, reduce cost, enlarge raw material sources and material Application Areas.

3. mainly use rare earth RE as basic micro alloying element; And its content range is big; Reach as high as 5%, can give full play to degasification, slagging-off, Water purification, crystal grain thinning and the metamorphism of REE in alloy, the mechanical property and the solidity to corrosion effect of raising alloy.

The mechanism of REE degasification, slagging-off, Water purification is: the REE activity is very strong, and oxygen, hydrogen, sulphur, nitrogen etc. are had stronger avidity, and its deoxidizing capacity surpasses the strongest existing reductor aluminium, can be content 50 * 10 ^-6Oxygen takes off to 10 * 10 ^-6Below, its desulfidation can be 20 * 10 containing the S amount ^-6Take off to 1～5 * 10 ^-6Therefore, the duraluminum that contains rare earth when melting, be easy to aluminium liquid in above-mentioned substance generation chemical reaction, reaction product is insoluble to aluminium and gets in the slag, thereby the gas content in the alloy is reduced, the tendency that makes alloy product produce pore and shrinkage porosite reduces greatly.

REE can significantly improve the mechanical property of alloy.REE can form stable high melting point metal compound such as Al in duraluminum ₄RE, Al ₈CuRE, Al ₈Mn ₄RE, Al ₂₄RE ₃Mn etc.These high melting point metal compound disperses are distributed in intergranular and the interdendritic that is netted or skeleton shape, and with the matrix mortise, played and strengthened and the effect of stable crystal boundary.Simultaneously, also form the AlSiRE phase of some amount in the alloy,, therefore thermotolerance and the wear resistance that improves alloy all had good effect because its fusing point and hardness are very high.In addition, also can in molten metal in lower melting point impurity element Sn, Pb, Sb etc., form dystectic compound with them or make they from the interdendritic in whole crystal uniform distribution, eliminated dendritic structure.

REE has crystal grain thinning and metamorphism.REE is a surface active element, can concentrate to be distributed on the crystal boundary face, reduces melt viscosity, strengthens flowability, reduces pulling force between phase and phase, because the merit that forms the critical size nucleus is reduced, nuclei of crystallization quantity increases, thereby makes grain refining.Rare earth has long-lasting and remelting stability to the metamorphism of duraluminum, and most ofs single or mishmetals add then has very strong refinement and metamorphism to α-Al mutually.

In addition, REE can also improve the electroconductibility of alloy.Because rare earth ability refinement aluminium grain also can form stable compound (like CeFe by impurity such as Fe, Si in alloy ₅, CeSi, CeSi ₂Deng) and separate out from intracrystalline, add the Water purification of rare earth to alloy, make the resistivity of aluminium be reduced, electroconductibility improves (about 2%).

The rare earth elements RE of very small amount can produce significantly rotten improving effect to alloy property; Therefore; The rare earth adding quantity of general duraluminum is below 1%; In 200810302670.3,200810302668.6,200810302669.0 and 200810302671.8 patented claims, content of rare earth confirms as 0.05～0.3%.Analyze from the Al-RE alloy phase diagram, because the solubleness of most of rare earth in aluminium very little (being about 0.01% like Ce), it exists, and form is many to be distributed in crystal boundary or basic intracrystalline portion with high melting point metal compound.Because activity is very high, in cleaning molten, serve as scavenging agent and consume a part, if add-on is very little, then its metamorphism to α-Al phase just is difficult to give full play to.Be the metamorphic long-lasting and remelting stability of maintenance rare earth, and give full play to its High-Temperature Strengthening characteristic, the present invention is special to be considered copper content with content of rare earth, confirm that its content range is 0.05～5%.

4. cobalt (Co) element adds element as the characteristic of complex alloysization, in alloy, can form AlCo, Al ₉Co ₂Deng 8 kinds of dispersivity High-Temperature Strengthening phases, Co is the trace additives of the high strength cast aluminum alloys of complex alloysization, when it and Mn coexist, forms Al ₄(CoFeMn) etc. very complicated strengthening phase hinders dislocation, stops grain sliding in the interdendritic, has improved alloy at room temperature and high temperature (under 400 ℃) intensity effectively; Lithium (Li) element adds element as the characteristic of complex alloysization, in melt, can form High-Temperature Strengthening phase Al ₁₂Li～AlLi ₃Between 13 kinds of metallic compounds, be disperse phase and be distributed in the matrix crystal boundary, improve alloy at room temperature and hot strength.

5. be the efficient alterant of alloy with carbon (C); Because the lattice parameter of the carbide that forms approaches the lattice parameter of aluminium sosoloid most; These carbide particles group is as crystallization nuclei very tiny (its size is less than 1 μ m) and can stable existence in aluminium liquid under suitable refining temperature; In the ingot solidification process, α-Al is had fabulous stable refinement nucleation ability basically, be superior to other alterants thereby do its antidamping ability of alterant with carbon; At utmost improve the alloy organizing dispersity, realize best modification effect.

5, the castability of excellence.Through the foundry goods that uses at several fields such as high-tech structure, Aeronautics and Astronautics, civilian heavy industrys foundry trial repeatedly; Verified the excellent properties of this novel material: castability is higher than present A201.0, ZL206, ZL207, ZL208, high strength cast aluminum alloys such as 206.0, the significant problem that hot cracking tendency is big, casting qualified rate is low when having solved above-mentioned aluminium alloy casting; The present invention old material melt down remelting; Also can realize the arbitrary proportion batching with virgin material; And new and old material mixed melt casting performance does not have change; And the good action of stable material intensity, raising ductility is arranged, and the situation that more original aldural waste material reuse property is poor, circulation route is long has utmost point remarkable economical property and intensivism.

The principle that novel material is eliminated hot cracking tendency is: form rich Cu phase because of copper content in the alloy increases; Rich Cu is distributed in crystal boundary as the thin brilliant disperse phase of HMP with the disperse of metallic compound form; The strong tendency that spreads to crystal boundary of having offset effectively when melt crystallization that the rich Cu solute of intragranular forms because of degree of supersaturation sharply raises, thereby the structural stress when having slowed down crystallization; The multiple disperse phase of elements such as rich Cu disperse phase and Co, Li characteristic micro alloying element, RE microalloying of rare earth element and Mn, Zr, Ti, C on the while crystal boundary; The multiple effect that all has crystal grain thinning, filling matrix crystal boundary, the nearly aluminium current potential metallic compound of formation; All these act on the surface tension of the melt that weakened significantly; Reduced melt viscosity, thereby significantly improved the castability of fluidity of molten and alloy, made cast article have higher qualification rate.

The good principle of old material reuse property is: the multicomponent microalloying effect has long-lasting stable with remelting among the present invention; During remelting; The structural performance of melt has kept the atom bloc framework and the fine crystalline structure of an alloy melt formation; A large amount of active nucleus can be given full play to the effect of cohesion, assimilation microlitic structure in melt, and can keep original flowability.Therefore, the good action of allocating stable material intensity, raising ductility into of old material.

This specific character of old material can be implemented in the instant reuse of production scene fully, no matter is slag charge, processing clout or rejected casting, all can with together melting or directly add in the melt of virgin material.

This specific character of the present invention; 1XXX system and the 2XXX series high strength aluminum alloy materials qualified casting widely applied at present significantly improve; Greatly reduce rejection number; Therefore do not need big waste product stockyard (in the actual production, very big scrapground ground often will be cooked up in the aluminium alloy casting workshop) in the production scene; Existing simultaneously a lot of y alloy ys do not possess remelting stability, and therefore direct reuse needs group to criticize and focus at the scene, occupies very big manufacturing cost, derives a series of processing links and fruitless labour; And use novel material provided by the invention, all these extra links, cost and fruitless labour all can be saved.

6, processing, the surface anticorrosion handling property of excellence.Through novel material being processed into the test of the finished parts of different shapes such as axle, ball, pipe, angle section, bolt, testimonial material has fabulous processability, and the surface can reach the fine and clean degree of nearly minute surface degree, and luminous reflectance factor is higher than fine aluminium; Surface oxidation and coated test show that thickness can reach the standard-required grade after the surperficial anodic oxidation, surface color does not have change, and the tack of coating and oxidized surface reaches the standard class of resistance to rupture test fully.

7, the high-temperature behavior of excellence.This material has the characteristic of high temperature aluminium alloys; Can reach that intensity is higher than more than the 200Mpa under 400 ℃ of conditions; Be higher than traditional high temperature (heat-resisting) aluminum alloy materials, this characteristic makes novel material can substitute other each the position heat-resistant part material except that aircraft engine casket body directly bears the parts of high-temperature fuel gas calcination.(thermotolerance principle referring in the characteristic 4 " science of prescription and economy " about the content of copper-rich phase, rare earth RE, refractory alloy Elements C o, Li etc.).

8, typical original.This series type material is that the applicant develops after obtaining alloying theory innovation breakthrough fast; The checking of material excellent properties is exactly to the theoretical checking of new alloyization simultaneously; Therefore and this theoretical breakthrough was not all clearly put down in writing on all documents and materials at present, should the series novel material belongs to primitiveness, basic great innovation in the world.

Innovative point of the present invention

Table one has been listed close 31 kinds of duraluminums elementary composition in a certain respect performance and purposes with the present invention.Can find out that compare with existing various high copper content wrought aluminium alloies, heat-resistant deforming duraluminum, birmastic, the present invention mainly contains following innovative content.

The one, copper (Cu) content allowed band is big, 1～10%; Cooperate with manganese (Mn) element simultaneously and form multiple High-Temperature Strengthening phase.

The 2nd, mainly use rare earth RE as basic micro alloying element; And its content range is big; Reach as high as 5%, can give full play to degasification, slagging-off, Water purification, crystal grain thinning and the metamorphism of rare earth RE in alloy, the mechanical property and the solidity to corrosion effect of raising alloy; Rare earth elements RE is all very strong to the avidity of oxygen, sulphur, nitrogen, hydrogen, thereby the effect of its deoxidation, desulfurization, removal hydrogen and nitrogen is all very strong, in addition; RE is a surface active element; Can concentrate to be distributed on the crystal boundary face, reduce pulling force between phase and phase, because the merit that forms the critical size nucleus is reduced; Nuclei of crystallization quantity increases, thereby makes grain refining.

The 3rd, looser to the restriction ratio of ferro element, allow its content maximum can reach 0.5%, this is for to use general aluminium to open up the space as the founding that matrix carries out alloy.

The 4th, do not use low melting point elements such as magnesium, zinc as the material that produces strengthening phase, avoid the decomposition and the conversion of material reinforcement phase under the high temperature, thereby significantly improved the hot strength of material.

The 5th, add element with cobalt (Co) element as the characteristic of complex alloysization, in alloy, can form AlCo, Al ₉Co ₂Deng 8 kinds of dispersivity High-Temperature Strengthening phases, when Co and Mn coexistence, form Al ₄(CoFeMn) etc. very complicated strengthening phase hinders dislocation, stops grain sliding in the interdendritic, has improved alloy at room temperature and high temperature (under 400 ℃) intensity effectively; Dispersivity High-Temperature Strengthening phase, lithium (Li) element adds element as the characteristic of complex alloysization, in melt, can form High-Temperature Strengthening phase Al ₁₂Li～AlLi ₃Between 13 kinds of metallic compounds, be disperse phase and be distributed in the matrix crystal boundary, improve alloy at room temperature and hot strength.Be used in combination titanium (Ti), zirconium (Zr) element as comprehensive grain-refining agent, make alloy material possessed high-strength and high ductility heat-resisting with whole basic substance of premium propertiess such as melt high workability.

The 6th, be the efficient alterant of alloy with carbon (C); Because the lattice parameter of the carbide that forms approaches the lattice parameter of aluminium sosoloid most; These carbide particles group is as crystallization nuclei very tiny (its size is less than 1 μ m) and can stable existence in aluminium liquid under suitable refining temperature; In the ingot solidification process, α-Al is had fabulous stable refinement nucleation ability basically, be superior to other alterants thereby do its antidamping ability of alterant with carbon; At utmost improve the alloy organizing dispersity, realize best modification effect.

More than be the most tangible several aspects in the characteristic formula of the present invention.

The various aluminum alloy chemically compositions that table one is relevant with the present invention

Mechanical property relatively

The applicant compares the present invention with the mechanical property of existing several kinds of high tough duraluminums, see table two.

The mechanical property of table two the present invention and several kinds of high-toughness casting aluminum alloys

The alloy code name	Castmethod	As-heat-treated condition	Tensile strength sigma _b?MPa	Unit elongation δ ₅％	Hardness HBS
						ZL201A	S	T4	365～370	?17～19	?100
	S	T5	440～470	?8～15	?120
						ZL205A	S	T5	480	?13	?120
	S	T6	510	?7	?140
							S	T7	495	?3.4	?130
High-ductility 205A	J	T5	385～405	?19～23
						206.0①	S	T7	435	?11.7	?90
KO-1	S	T6	460	?5.0	?135
							J	T6	460	?9.0
	R	T5	358～450	?4.0～7.0
						ZL107A	J	T5	420～470	?4～6
The present invention	J、S	T6	480～540	?3～8	?140

1. institute's column data is 206.0 high-purity alloys, i.e. W (Si)≤0.05%, W (Fe)≤0.10%.S-sand mold casting, J-permanent mold casting, R-investment cast

Can find out that from table two tensile strength of the present invention reaches 480～540MPa, hardness obviously is superior to the mechanical property of existing high tough duraluminum greater than HB140.

High-temperature behavior

The applicant tests the intensity high temperature endurance performance of the present invention under all temps condition, and contrasts with the existing high temperature endurance performance of using heat-resisting aluminium alloy always, sees table three.

The high temperature endurance performance of table three the present invention and heat-resisting aluminium alloy commonly used

Can find out that from table three room temperature strength of the present invention is greater than 450Mpa, more than 300Mpa, during 300 ℃ of hot strengths, high temperature endurance performance obviously is superior to the high-temperature and durable property of existing heat-resistance high-strength alloy greater than 200Mpa during 250 ℃ of hot strengths.

In sum; The present invention has the Application Areas of high-tech content, the length and breadth of land and splendid market outlook with the rotten Co-Li-RE high strength heat resistant alloy material of C; Its extremely excellent cost performance makes it can substitute present nearly all aldural and high temperature aluminium alloys, has represented the developing direction of the light strong structured material in the China and even the world.

Embodiment

Embodiment 1:Cu-1.0%, characteristic micro alloying element-Co, Li, basic microalloying REE-lanthanum La, efficient alterant element-C

(1) by the good required various alloying element of charge calculation table weighing, as follows.

(2) in smelting furnace, add an amount of aluminium ingot, heating makes it to melt fully and is incubated down at 700～800 ℃; For preventing that melt from sucking too much air, melting process should be accomplished as far as possible at short notice with in the enclosed environment.

(3) add Al-Mn, Al-Ti, Al-Co, Al-Li, Al-Zr master alloy or hybrid metal additive (comprising salt compounds) earlier by formula rate again; Add Cu pure metal and Al-Cd master alloy or hybrid metal additive after stirring again; Add C and rare-earth elements La again, stir.

The hybrid metal additive is meant pie or the block non-coking property sintered metal product that interpolation, adjustment alloy constituent element are used, and comprises that manganese, copper, zirconium, cobalt, lithium or titanium metal powder and flux mix.Flux is meant the mixture of basic metal or earth alkali metal halogen salt, comprises NaCl, KCl and Na ₃AlF ₆C is meant compound or aluminium carbon master alloy, comprises binary master alloy, ternary master alloy and polynary master alloy.

(6) casting (crystallization and freezing in mold).

(7) foundry goods is carried out 470～560 ℃, 30 hours with interior solution treatment.

(8) sample index: tensile strength 485Mpa, unit elongation 7.5%.

Embodiment 2:Cu-4.2%, characteristic micro alloying element-Co, Li, basic microalloying rare-earth elements La, Ce mishmetal, efficient alterant element-C

(3) add Al-Mn, Al-Ti, Al-Co, Al-Li, Al-Zr master alloy or hybrid metal additive (comprising salt compounds) earlier by formula rate again; Add Cu pure metal and Al-Cd master alloy or hybrid metal additive after stirring again; Add C and rare-earth elements La, Ce mishmetal again, stir.

(6) casting (crystallization and freezing in mold).

(8) sample index: tensile strength 538Mpa, unit elongation 7.4%.

Embodiment 3:Cu-5.1%, characteristic micro alloying element-Co, Li, basic microalloying REE Eu, efficient alterant element-C

(1) by the good required various alloying element of following charge calculation table weighing, as follows.

(3) add Al-Mn, Al-Ti, Al-Co, Al-Li, Al-Zr master alloy or hybrid metal additive (comprising salt compounds) earlier by formula rate again; Add Cu pure metal and Al-Cd master alloy or hybrid metal additive after stirring again; Add C and REE Eu again, stir.

(6) casting (crystallization and freezing in mold).

(8) sample index: tensile strength 503Mpa, unit elongation 6.1%.

Embodiment 4:Cu-6.01%, characteristic micro alloying element-Co, Li, basic microalloying REE-La, Ce, Pr mishmetal, efficient alterant element-C

(3) add Al-Mn, Al-Ti, Al-Co, Al-Li, Al-Zr master alloy or hybrid metal additive (comprising salt compounds) earlier by formula rate again; Add Cu pure metal and Al-Cd master alloy or hybrid metal additive after stirring again; Add C and rare-earth elements La, Ce, Pr mishmetal again, stir.

(6) casting (crystallization and freezing in mold).

(8) sample index: tensile strength 533Mpa, unit elongation 7.1%

Embodiment 5:Cu-6.5%, characteristic micro alloying element-Co, Li, basic microalloying rare earth element er Er, efficient alterant element-C

(3) add Al-Mn, Al-Ti, Al-Co, Al-Li, Al-Zr master alloy or hybrid metal additive (comprising salt compounds) earlier by formula rate again; Add Cu pure metal and Al-Cd master alloy or hybrid metal additive after stirring again; Add C and rare earth element er again, stir.

(6) casting (crystallization and freezing in mold).

(8) sample index: tensile strength 527Mpa, unit elongation 6.9%.

Embodiment 6:Cu-7%, characteristic micro alloying element-Co, Li, basic microalloying rear earth element nd Nd, efficient alterant element-C

(3) add Al-Mn, Al-Ti, Al-Co, Al-Li, Al-Zr master alloy or hybrid metal additive (comprising salt compounds) earlier by formula rate again; Add Cu pure metal and Al-Cd master alloy or hybrid metal additive after stirring again; Add C and rare earth element nd again, stir.

(6) casting (crystallization and freezing in mold).

(8) sample index: tensile strength 517Mpa, unit elongation 5.2%.

Embodiment 7:Cu-8%, characteristic micro alloying element-Co, Li, basic microalloying rare-earth element cerium Ce, efficient alterant element-C

(3) add Al-Mn, Al-Ti, Al-Co, Al-Li, Al-Zr master alloy or hybrid metal additive (comprising salt compounds) earlier by formula rate again; Add Cu pure metal and Al-Cd master alloy or hybrid metal additive after stirring again; Add C and rare earth element ce again, stir.

(6) casting (crystallization and freezing in mold).

(8) sample index: tensile strength 501Mpa, unit elongation 4.8%.

Embodiment 8:Cu-10%, characteristic micro alloying element-Co, Li, basic microalloying rare earth element yttrium Y, efficient alterant element-C

(3) add Al-Mn, Al-Ti, Al-Co, Al-Li, Al-Zr master alloy or hybrid metal additive (comprising salt compounds) earlier by formula rate again; Add Cu pure metal and Al-Cd master alloy or hybrid metal additive after stirring again; Add C and rare earth element y again, stir.

(6) casting (crystallization and freezing in mold).

(8) sample index: tensile strength 487Mpa, unit elongation 4.3%.

Claims

1. one kind with the rotten Co-Li-RE high strength heat resistant alloy material of C, and it is characterized in that: this alloy is a raw material with the general industry fine aluminium, and by weight percentage, this alloying constituent is Cu:1.0～10.0%; Mn:0.05～1.5%, Cd:0.01～0.5%, Ti:0.01～0.5%, C:0.0001～0.15%; Zr:0.01～1.0%, Co:0.01～1.0%, Li:0.1～3.0%; Rare earth elements RE: 0.05～5%, Si :≤0.1%, Fe≤0.5%; The single content of other impurity element is not more than 0.05%, and summation is not more than 0.15%, and all the other are Al.

2. according to claim 1 with the rotten Co-Li-RE high strength heat resistant alloy material of C, it is characterized in that: rare earth elements RE is single rare earth element or mishmetal.

3. according to claim 1 and 2 with the rotten Co-Li-RE high strength heat resistant alloy material of C, it is characterized in that: rare earth elements RE comprises La, Ce, Pr, Nd, Er, Eu and Y.

4. a Co-Li-RE high strength heat resistant alloy preparation methods that goes bad with C as claimed in claim 3 is characterized in that: comprise the steps:

(1) in above-mentioned element ratio scope; A selected group element ratio, the alloy total amount of preparation is as required again extrapolated the quality of every kind of required elemental metals; The perhaps quality of master alloy; Perhaps the quality of hybrid metal additive is worked out the alloy production allocation sheet, and gets the raw materials ready by allocation sheet choosing foot;

(2) in smelting furnace, add an amount of aluminium ingot or molten aluminum liquid, heating makes it to melt fully and is incubated down at 700～800 ℃; Melting process is accomplished in enclosed environment;

(3) press formula rate again and add Mn, Ti, Zr, Co, Li pure metal or Al-Mn, Al-Ti, Al-Zr, Al-Co, Al-Li master alloy or hybrid metal additive earlier; Add Cu, Cd pure metal or Al-Cu, Al-Cd master alloy or hybrid metal additive after stirring again; Add C and rare earth elements RE again, stir;

(4) then above-mentioned alloy melt is carried out furnace refining; In alloy melt, add refining agent, and stir, the melt refining is operated in enclosed environment;

(5) slag hitting after the refining, leave standstill, temperature adjustment to 630～850 ℃, alloy liquid is toppled over and is come out of the stove, online degasification, slagging-off are handled;

(6) casting;

5. according to claim 4 with the rotten Co-Li-RE high strength heat resistant alloy preparation methods of C, it is characterized in that: the hybrid metal additive is meant pie or the block non-coking property sintered metal product that interpolation, adjustment alloy constituent element are used.

6. according to claim 5 with the rotten Co-Li-RE high strength heat resistant alloy preparation methods of C, it is characterized in that: sintered metal product comprises that manganese, copper, zirconium, cobalt, lithium or titanium metal powder and flux mix.

7. according to claim 6 with the rotten Co-Li-RE high strength heat resistant alloy preparation methods of C, it is characterized in that: flux is meant the mixture of basic metal or earth alkali metal halogen salt.

8. according to claim 4 with the rotten Co-Li-RE high strength heat resistant alloy preparation methods of C, it is characterized in that: in step (3), C is meant compound or aluminium carbon master alloy, comprises binary master alloy and polynary master alloy.

9. according to claim 4 with the rotten Co-Li-RE high strength heat resistant alloy preparation methods of C, it is characterized in that: in step (4), refining agent is meant chlorine, Sesquichloratum, Manganous chloride tetrahydrate.