US20090116993A1 - ae series heat resistant compression casting magnesium alloy containing cerium and lanthanum - Google Patents
ae series heat resistant compression casting magnesium alloy containing cerium and lanthanum Download PDFInfo
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- US20090116993A1 US20090116993A1 US12/133,229 US13322908A US2009116993A1 US 20090116993 A1 US20090116993 A1 US 20090116993A1 US 13322908 A US13322908 A US 13322908A US 2009116993 A1 US2009116993 A1 US 2009116993A1
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- lanthanum
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- 229910000861 Mg alloy Inorganic materials 0.000 title claims abstract description 40
- 229910052684 Cerium Inorganic materials 0.000 title claims abstract description 39
- 229910052746 lanthanum Inorganic materials 0.000 title claims abstract description 35
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 title claims abstract description 26
- 238000005266 casting Methods 0.000 title claims abstract description 25
- 230000006835 compression Effects 0.000 title claims abstract description 23
- 238000007906 compression Methods 0.000 title claims abstract description 23
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 title claims abstract description 22
- 239000000203 mixture Substances 0.000 claims abstract description 30
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical group [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims abstract description 14
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 14
- 239000011777 magnesium Substances 0.000 claims abstract description 14
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 13
- 239000004615 ingredient Substances 0.000 claims abstract description 8
- 239000012535 impurity Substances 0.000 claims description 12
- 229910052742 iron Inorganic materials 0.000 claims description 12
- 229910052802 copper Inorganic materials 0.000 claims description 10
- 229910052759 nickel Inorganic materials 0.000 claims description 10
- 239000000956 alloy Substances 0.000 abstract description 54
- 229910045601 alloy Inorganic materials 0.000 abstract description 53
- 229910052761 rare earth metal Inorganic materials 0.000 abstract description 25
- 150000002910 rare earth metals Chemical class 0.000 abstract description 13
- WMOHXRDWCVHXGS-UHFFFAOYSA-N [La].[Ce] Chemical compound [La].[Ce] WMOHXRDWCVHXGS-UHFFFAOYSA-N 0.000 abstract description 9
- 239000002994 raw material Substances 0.000 abstract description 2
- -1 aluminum manganese Chemical compound 0.000 description 12
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 9
- 230000000694 effects Effects 0.000 description 7
- 239000011572 manganese Substances 0.000 description 7
- 238000011161 development Methods 0.000 description 6
- 229910052779 Neodymium Inorganic materials 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 5
- 229910052777 Praseodymium Inorganic materials 0.000 description 4
- OTCUTGXFWFYJDP-UHFFFAOYSA-N [La].[Ce].[Mn] Chemical compound [La].[Ce].[Mn] OTCUTGXFWFYJDP-UHFFFAOYSA-N 0.000 description 4
- 239000000155 melt Substances 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 239000002075 main ingredient Substances 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 238000007670 refining Methods 0.000 description 3
- 229910052727 yttrium Inorganic materials 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 229910052688 Gadolinium Inorganic materials 0.000 description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- 229910003023 Mg-Al Inorganic materials 0.000 description 2
- 229910000914 Mn alloy Inorganic materials 0.000 description 2
- 238000003723 Smelting Methods 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 229910001385 heavy metal Inorganic materials 0.000 description 2
- 230000007774 longterm Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 238000000746 purification Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910052691 Erbium Inorganic materials 0.000 description 1
- 229910052689 Holmium Inorganic materials 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 229910021323 Mg17Al12 Inorganic materials 0.000 description 1
- 229910000691 Re alloy Inorganic materials 0.000 description 1
- RKLPWYXSIBFAJB-UHFFFAOYSA-N [Nd].[Pr] Chemical compound [Nd].[Pr] RKLPWYXSIBFAJB-UHFFFAOYSA-N 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- 239000003513 alkali Substances 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000008014 freezing Effects 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- 230000009931 harmful effect Effects 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000002085 persistent effect Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 229910001404 rare earth metal oxide Inorganic materials 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000004227 thermal cracking Methods 0.000 description 1
- 238000004627 transmission electron microscopy Methods 0.000 description 1
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 description 1
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Classifications
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
- C22C23/02—Alloys based on magnesium with aluminium as the next major constituent
Definitions
- the present invention relates to a magnesium alloy material, and more particularly, to an AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum.
- the light compression casting magnesium alloys mainly in Mg—Al based alloys have found extended application in automobiles.
- the application of magnesium alloys still drops behind greatly and one of the reasons thereof is being short of sufficient high temperature property.
- the long-term service temperatures of the AZ, AM series compression casting magnesium alloys used widely can not excess 120° C., which makes them can not be used in manufacturing automobile driving assemblies that requires high creep resistant performance at high temperature, therefore the further application of magnesium alloys is blocked greatly.
- AE series alloys The rare earths used in Mg—Al—Re alloys (herein, referred to as “AE series alloys”) developed are cerium rich mixture of rare earths (including La, Ce, Pr and Nd), however, the prices of Pr, Nd keep rising at present which makes the costs of this kind of AE series alloys increased. Additionally, the mechanical performances of the heat resistance magnesium alloys developed presently still need to be improved.
- rare earths have been recognized by the scientific research departments and manufacturers in China and abroad, and the rare earths used include single pure rare earth (such as Nd, Y, Gd) and mixture of rare earths.
- the mixture of rare earths used mostly are: cerium rich mixture of rare earths with La, Ce, Pr, Nd as the main ingredients thereof, yttrium rich mixture of rare earths with Y, Ho, Er, Gd as the main ingredients thereof, praseodymium neodymium mixture with Pr and Nd as the main ingredients thereof.
- cerium lanthanum mixture which is cheaper than the rare earths described above. Therefore, developing an application market of the cerium lanthanum mixture is pressing and significant for the complex utilization and equilibrium development of the rare earths.
- cerium and lanthanum Due to the specific chemical activity of cerium and lanthanum, after being added into magnesium alloys, both of them can produce the following four effects: purification, activation, fining and alloying/microalloying effects. As compared with other rare earth elements, lanthanum has better impurity removing (remove the hydrogen and oxides inclusions) and purification effects on alloys. Comparing with lanthanum, cerium has a higher solid dissolving degree and a better effect of fining the alloy texture in magnesium alloys. It has been recognized widely by researchers that lanthanum and cerium can elevate the allround performance of magnesium alloys.
- cerium lanthanum rare earths By utilizing cerium lanthanum rare earths in combination, exerting their respective advantages and developing new rare earths magnesium alloys with high performance, it can help to solve the problem of overstocking abundantly rare earth resource of cerium lanthanum mixture, to alleviate the contradiction of the resource between production and demand and to solve the problem of imbalance between production and distribution.
- this invention provides an AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum. This alloy has a low cost, a good heat resistant performance and a long-term service temperature up to 200° C.
- the ingredients and their mass percentage proportions of the AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum are as follows: Al: 3% ⁇ 5%, Ce: 0.4% ⁇ 2.6%, La: 0.4% ⁇ 2.6%, Mn: 0.2% ⁇ 0.6%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium.
- the preparation method of the AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum of this invention is as follows:
- pure magnesium, aluminum, aluminum manganese intermediate alloy and manganese-cerium lanthanum intermediate alloy are pre-heated to 200° C.
- pure magnesium, aluminum, aluminum manganese intermediate alloy are put into a crucible preheated to 300° C. and a protective gas with a SF 6 /CO 2 volume ratio of 1:100 is introduced.
- a protective gas with a SF 6 /CO 2 volume ratio of 1:100 is introduced.
- Said cerium and lanthanum as raw material used in the manganese-cerium lanthanum intermediate alloy can take the form of residual and cheap cerium lanthanum mixture obtained by separating Nd and Rr with high value from the common cerium rich mixture of rare earths.
- FIG. 1 shows the scanning electron microscope and transmission electron microscopy microtexture scheme for AlCeLa 4, 2.4, 1.6 alloy in Example 4. It can be seen that the main reason that the alloy has good mechanical performance lies in a fine grain strengthen of the alloy produced by fined alloy grains and a dispersion strengthen (mainly grain boundary strengthen) of the alloy produced by the abundant fine high melting Al-RE at the grain boundary.
- FIG. 2 shows curve 1 and curve 2 as the creep curves of AlCeLa 4, 2.4, 1.6 alloy in Example 4 of this invention and AE 44 alloy under the condition of 200° C. and 70 MPa, respectively.
- the mass percentage proportions of the AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum are as follows: Al: 3%, Ce: 0.6%, La: 0.4%, Mn: 0.2%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium.
- the performance of the alloy is shown in FIG. 1 and FIG. 2 .
- the mass percentage proportions of the AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum are as follows: Al: 5%, Ce: 1.2%, La: 0.8%, Mn: 0.4%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium.
- the performance of the alloy is shown in FIG. 1 and FIG. 2 .
- the mass percentage proportions of the AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum are as follows: Al: 4%, Ce: 1.8%, La: 1.2%, Mn: 0.4%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium.
- the performance of the alloy is shown in FIG. 1 and FIG. 2 .
- the mass percentage proportions of the AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum are as follows: Al: 4%, Ce: 2.4%, La: 1.6%, Mn: 0.6%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium.
- the performance of the alloy is shown in FIG. 1 , FIG. 2 and FIG. 3 .
- Example 1 The mechanical performances of Example 1, 2, 3 and 4 of this invention at room temperature Tensile Yield Percentage Alloy No. strength (MPa) strength (MPa) elongation (%) Example 1 228 130 15 Example 2 245 135 10 Example 3 257 148 13 Example 4 271 160 14 AE44 248 140 11 AZ91 222 145 3
- Example 1 The mechanical performances at high temperature of Example 1, 2, 3 and 4 in this invention 150° C. 200° C.
- Tensile Yield Percentage Tensile Yield Percentage strength strength elongation strength strength elongation Alloy No. (MPa) (MPa) (%) (MPa) (MPa) (%)
- Example 1 134 94 26 105 80 23
- Example 2 140 103 21 108 87 20
- Example 3 145 111 24 112 96 21
- Example 4 147 120 31 120 107 26 AE44 140 109 27 115 100 19 AZ91 150 105 13 99 84 15
- Example 4 TABLE 3 the creep resistant performance at high temperature of AlCeLa 4, 2.4, 1.6 alloy in Example 4 of this invention 200° C., 70 MPa Percentage Minimum Persistent elongation creep life over 100 hrs rate Alloy No. (hours) (%) ( ⁇ 10 ⁇ 9 s ⁇ 1 )
- Example 4 >100 0.17 1.82 AE44 >100 0.18 3.42
- Table 1 shows the mechanical performances of the alloys in Example 1, 2, 3 and 4 of this invention and AE 44, AZ 91 at room temperature.
- Table 2 shows the mechanical performances at high temperature of Example 1, 2, 3 and 4 in this invention and AE 44, AZ 91.
- Table 3 shows the creep resistant performance at high temperature of AlCeLa 4, 2.4, 1.6 alloy in Example 4 of this invention and AE 44.
- AE 44 is a new high temperature creep resistant compression casting magnesium alloy developed by Hydro Magnesium Industry Company in Norway in 2005 and has been applied to produce automobile parts, such as the cradle for engine in automobile.
- AZ 91 is a magnesium alloy with a standard trademark and is also one of the magnesium alloys with the most use level in industry at present, however the service temperature thereof can not excess 120° C.
- the data of AE 44 and AZ 91 in FIG. 1 , FIG. 2 and FIG. 3 are the data obtained by preparing the samples at the same condition and testing them at the same condition
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- Manufacture And Refinement Of Metals (AREA)
Abstract
This invention relates to an AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum and the composition ingredients and the weight percentage thereof are as follows: Al: 3%˜5%, Ce: 0.4%˜2.6%, La: 0.4%˜2.6%, Mn: 0.2%˜0.6%, and the remainder is magnesium. The raw material of cerium lanthanum mixture of rare earth used is the residual, cheap and overstocked cerium lanthanum mixture of rare earth obtained from common cerium rich mixture of rare earth after the Nd, Rr with high value and good market have been separated. The mechanical performance of this invention at room temperature and high temperature excels that of AE 44 and AZ 91 alloys, and the minimum creep rate of 1.82×10-9 S-1 and the creep percentage elongation in 100 h of 0.17% at the condition of 200° C. and 70 MPa excel these of AE 44 alloy.
Description
- The present invention relates to a magnesium alloy material, and more particularly, to an AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum.
- In recent years, due to the pressure of environment protection and the enhancement of energy saving consciousness, the light compression casting magnesium alloys mainly in Mg—Al based alloys have found extended application in automobiles. However, as compared with aluminum alloys, the application of magnesium alloys still drops behind greatly and one of the reasons thereof is being short of sufficient high temperature property. At present, the long-term service temperatures of the AZ, AM series compression casting magnesium alloys used widely can not excess 120° C., which makes them can not be used in manufacturing automobile driving assemblies that requires high creep resistant performance at high temperature, therefore the further application of magnesium alloys is blocked greatly. On the basis of that, the rare earth and alkali earth elements have been introduced into Mg-Al based alloys to develop a magnesium alloy with a creep resistant performance at high temperature, however, there are still some problems existing in this kind of heat resistant magnesium alloys developed recently. The main disadvantages existing in Mg—Al—Ca (AX) and Mg—Al—Sr (AJ) alloys are that thermal cracking occurs easily and the inferior plastic property of the alloys, and the like. The rare earths used in Mg—Al—Re alloys (herein, referred to as “AE series alloys”) developed are cerium rich mixture of rare earths (including La, Ce, Pr and Nd), however, the prices of Pr, Nd keep rising at present which makes the costs of this kind of AE series alloys increased. Additionally, the mechanical performances of the heat resistance magnesium alloys developed presently still need to be improved.
- As the alloying (microalloying) elements for improving the heat resistant performance of the traditional magnesium alloys and developing new heat resistant magnesium alloys, rare earths have been recognized by the scientific research departments and manufacturers in China and abroad, and the rare earths used include single pure rare earth (such as Nd, Y, Gd) and mixture of rare earths. At present, the mixture of rare earths used mostly are: cerium rich mixture of rare earths with La, Ce, Pr, Nd as the main ingredients thereof, yttrium rich mixture of rare earths with Y, Ho, Er, Gd as the main ingredients thereof, praseodymium neodymium mixture with Pr and Nd as the main ingredients thereof. However, at present what overstocked abundantly is another cerium lanthanum mixture which is cheaper than the rare earths described above. Therefore, developing an application market of the cerium lanthanum mixture is pressing and significant for the complex utilization and equilibrium development of the rare earths.
- Due to the specific chemical activity of cerium and lanthanum, after being added into magnesium alloys, both of them can produce the following four effects: purification, activation, fining and alloying/microalloying effects. As compared with other rare earth elements, lanthanum has better impurity removing (remove the hydrogen and oxides inclusions) and purification effects on alloys. Comparing with lanthanum, cerium has a higher solid dissolving degree and a better effect of fining the alloy texture in magnesium alloys. It has been recognized widely by researchers that lanthanum and cerium can elevate the allround performance of magnesium alloys. By utilizing cerium lanthanum rare earths in combination, exerting their respective advantages and developing new rare earths magnesium alloys with high performance, it can help to solve the problem of overstocking abundantly rare earth resource of cerium lanthanum mixture, to alleviate the contradiction of the resource between production and demand and to solve the problem of imbalance between production and distribution.
- For overcoming the shortcomings of the present compression casting magnesium alloys, this invention provides an AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum. This alloy has a low cost, a good heat resistant performance and a long-term service temperature up to 200° C.
- The ingredients and their mass percentage proportions of the AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum are as follows: Al: 3%˜5%, Ce: 0.4%˜2.6%, La: 0.4%˜2.6%, Mn: 0.2%˜0.6%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium.
- According to some embodiments, the preparation method of the AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum of this invention is as follows:
- Firstly, weighting according to the proportions, pure magnesium, aluminum, aluminum manganese intermediate alloy and manganese-cerium lanthanum intermediate alloy are pre-heated to 200° C., then pure magnesium, aluminum, aluminum manganese intermediate alloy are put into a crucible preheated to 300° C. and a protective gas with a SF6/CO2 volume ratio of 1:100 is introduced. After the materials added have been molten completely and when the temperature of the melt reaches 720° C.˜740° C., manganese-cerium lanthanum intermediate alloy is added and the introduction of the protective gas is continued. After the manganese-cerium lanthanum intermediate alloy added has been molten completely and when the temperature rises back to 720˜740° C., stirring for 5˜10 min, then refining for 5˜10 min with blowing argon. After the refining, settling for 28˜32 min and the melt is cooled to 680° C.˜700° C. A compression casting is performed on a cold chamber compression casting machine under a mould clamping force of 500 KN and an AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum is obtained. Said cerium and lanthanum as raw material used in the manganese-cerium lanthanum intermediate alloy can take the form of residual and cheap cerium lanthanum mixture obtained by separating Nd and Rr with high value from the common cerium rich mixture of rare earths.
- The features and beneficial effects of this invention are as follows:
-
- 1) Aluminum is a main alloy element in an alloy, and an adequate amount of aluminum can provide an alloy with balanced strength, plastic property and casting processing performance, and makes this invention be fit for mass production. 2) Cerium lanthanum rare earth mixture is an element of this invention for increasing the strength and the heat resistant property of an alloy in a strengthen mechanism as follows: on the one hand, as Al11RE3 and Al2RE are formed by the combination of rare earth and aluminum in the alloy, Mg17Al12 phase with poor thermal stability is reduced or restrained which helps to increase the high temperature performance of the alloy; on the other hand, the Al-RE compounds of Al11RE3 and the like produced have very high melting point (e.g., the melting point of Al11RE3 can be up to 1200° C.). These compounds disperse in grain boundary and show very high thermal stability which can nail the grain boundary effectively to block the slippage of the grain boundary and restrain the climb of dislocation in crystal. Additionally, during smelting, cerium lanthanum rare earth mixture can remove the impurities in manganese alloy melt to achieve the effects of degas refining and purifying the melt. Cerium lanthanum rare earth mixture is a surface-active element of manganese alloy. During the smelting of an alloy, the rare earths gather on the surface of the alloy liquid and a multiple composite dense oxide layer of MgO, RE2O3 and A1 2O3 is formed, which alleviates the oxidation phenomenon, elevates the initial burning temperature and favors the melt casting of the alloy. During the freezing of the alloy liquid, the rare earths gather at the advancing front of the solid and liquid to increase the supercoolling degree of the ingredients and help to fine the alloy texture. Therefore, cerium lanthanum mixture of rare earth benefits the improvement of the allround performance of an alloy. 3) The main effect of manganese is to increase the corrosion resistant performance of an alloy, and manganese can form a compound with iron or other heavy metal elements in magnesium alloy so as to remove them as a slag. As a result, the harmful effect of iron or other heavy metal elements on the corrosion resistance of the magnesium alloy can be eliminated. 4) The cerium lanthanum rare earth mixture is the residual and cheap cerium lanthanum rare earth mixture obtained by separating Nd, Rr with high value from common cerium rich mixture of rare earth. From 1990s up till now, the experts on rare earth in China and abroad have paid great attention to the problem of imbalance on the application of rare earths. At present, a difficult problem affecting the complex utilization and equilibrium development of the rare earths is the abundant overstock of cerium lanthanum rare earth mixture. Only in China, almost 12,0000 tons of cerium lanthanum rare earth with a value of one hundred million dollars is produced each year, however, this cerium lanthanum rare earth mixture is always kept overstocked and has not been widely utilized, which becomes a bottleneck for the complex utilization and equilibrium development of the rare earths. The reasons that this invention develops an AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum by utilizing cheap cerium lanthanum mixture of rare earth lie in: 1. utilizing the cerium lanthanum rare earth overstocked in magnesium alloy which has been referred to as “a green light engineering material of the 21th century”, which can alleviate the problem of imbalance between production and distribution for rare earth source and can benefit the harmonious development of the utilization of many rare earth elements; 2. reducing the costs of this kind of alloys and ensuring the continuable development of these alloys by the abundant cerium lanthanum rare earth resource, which can increase the competition of magnesium alloys and accelerate the development of rare earth magnesium alloys nicely and quickly.
-
FIG. 1 shows the scanning electron microscope and transmission electron microscopy microtexture scheme for AlCeLa 4, 2.4, 1.6 alloy in Example 4. It can be seen that the main reason that the alloy has good mechanical performance lies in a fine grain strengthen of the alloy produced by fined alloy grains and a dispersion strengthen (mainly grain boundary strengthen) of the alloy produced by the abundant fine high melting Al-RE at the grain boundary. -
FIG. 2 shows curve 1 andcurve 2 as the creep curves of AlCeLa 4, 2.4, 1.6 alloy in Example 4 of this invention and AE 44 alloy under the condition of 200° C. and 70 MPa, respectively. - The mass percentage proportions of the AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum are as follows: Al: 3%, Ce: 0.6%, La: 0.4%, Mn: 0.2%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium. The performance of the alloy is shown in
FIG. 1 andFIG. 2 . - The mass percentage proportions of the AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum are as follows: Al: 5%, Ce: 1.2%, La: 0.8%, Mn: 0.4%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium. The performance of the alloy is shown in
FIG. 1 andFIG. 2 . - The mass percentage proportions of the AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum are as follows: Al: 4%, Ce: 1.8%, La: 1.2%, Mn: 0.4%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium. The performance of the alloy is shown in
FIG. 1 andFIG. 2 . - The mass percentage proportions of the AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum are as follows: Al: 4%, Ce: 2.4%, La: 1.6%, Mn: 0.6%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium. The performance of the alloy is shown in
FIG. 1 ,FIG. 2 andFIG. 3 . -
TABLE 1 The mechanical performances of Example 1, 2, 3 and 4 of this invention at room temperature Tensile Yield Percentage Alloy No. strength (MPa) strength (MPa) elongation (%) Example 1 228 130 15 Example 2 245 135 10 Example 3 257 148 13 Example 4 271 160 14 AE44 248 140 11 AZ91 222 145 3 -
TABLE 2 The mechanical performances at high temperature of Example 1, 2, 3 and 4 in this invention 150° C. 200° C. Tensile Yield Percentage Tensile Yield Percentage strength strength elongation strength strength elongation Alloy No. (MPa) (MPa) (%) (MPa) (MPa) (%) Example 1 134 94 26 105 80 23 Example 2 140 103 21 108 87 20 Example 3 145 111 24 112 96 21 Example 4 147 120 31 120 107 26 AE44 140 109 27 115 100 19 AZ91 150 105 13 99 84 15 -
TABLE 3 the creep resistant performance at high temperature of AlCeLa 4, 2.4, 1.6 alloy in Example 4 of this invention 200° C., 70 MPa Percentage Minimum Persistent elongation creep life over 100 hrs rate Alloy No. (hours) (%) (×10−9 s−1) Example 4 >100 0.17 1.82 AE44 >100 0.18 3.42 - Table 1 shows the mechanical performances of the alloys in Example 1, 2, 3 and 4 of this invention and AE 44, AZ 91 at room temperature.
- Table 2 shows the mechanical performances at high temperature of Example 1, 2, 3 and 4 in this invention and AE 44, AZ 91.
- Table 3 shows the creep resistant performance at high temperature of AlCeLa 4, 2.4, 1.6 alloy in Example 4 of this invention and AE 44.
- AE 44 is a new high temperature creep resistant compression casting magnesium alloy developed by Hydro Magnesium Industry Company in Norway in 2005 and has been applied to produce automobile parts, such as the cradle for engine in automobile. AZ 91 is a magnesium alloy with a standard trademark and is also one of the magnesium alloys with the most use level in industry at present, however the service temperature thereof can not excess 120° C. The data of AE 44 and AZ 91 in
FIG. 1 ,FIG. 2 andFIG. 3 are the data obtained by preparing the samples at the same condition and testing them at the same condition
Claims (5)
1. An AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum, characterized in that the composition ingredients and the weight percentage thereof are as follows: Al: 3%˜5%, Ce: 0.4%˜2.6%, La: 0.4%˜2.6%, Mn: 0.2%˜0.6%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium.
2. The AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum according to claim 1 , characterized in that the composition ingredients and the weight percentage thereof are as follows: Al: 3%˜4%, Ce: 0.4%˜0.6%, La: 0.4%˜0.6%, Mn: 0.2%˜0.6%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium.
3. The AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum according to claim 1 , characterized in that the composition ingredients and the weight percentage thereof are as follows: Al: 4%˜5%, Ce: 1.0%˜1.2%, La: 0.8%˜1.0%, Mn: 0.2%˜0.6%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium.
4. The AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum according to claim 1 , characterized in that the composition ingredients and the weight percentage thereof are as follows: Al: 4%˜5%, Ce: 1.8%˜2.0%, La: 1.0%˜1.2%, Mn: 0.2%˜0.6%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium.
5. The AE series heat resistant compression casting magnesium alloy containing cerium and lanthanum according to claim 1 , characterized in that the composition ingredients and the weight percentage thereof are as follows: Al: 4%˜5%, Ce: 2.4%˜2.6%, La: 1.4%˜1.6%, Mn: 0.2%˜0.6%, the total amount of impurity elements of Fe, Cu and Ni is less than 0.03%, and the remainder is magnesium.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200710056279.5 | 2007-11-05 | ||
| CN2007100562795A CN101158002B (en) | 2007-11-06 | 2007-11-06 | AE series thermo-stable die-casting magnesium alloy containing cerium and lanthanide |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20090116993A1 true US20090116993A1 (en) | 2009-05-07 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US12/133,229 Abandoned US20090116993A1 (en) | 2007-11-05 | 2008-06-04 | ae series heat resistant compression casting magnesium alloy containing cerium and lanthanum |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US20090116993A1 (en) |
| CN (1) | CN101158002B (en) |
Cited By (4)
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| CN103451459A (en) * | 2013-09-14 | 2013-12-18 | 天津六合镁制品有限公司 | Preparation method of magnesium alloy |
| WO2016178204A1 (en) * | 2015-05-07 | 2016-11-10 | Dead Sea Magnesium Ltd. | Creep resistant, ductile magnesium alloys for die casting |
| WO2020221752A1 (en) * | 2019-04-29 | 2020-11-05 | Brunel University London | A casting magnesium alloy for providing improved thermal conductivity |
| CN115449682A (en) * | 2022-09-28 | 2022-12-09 | 广东汇天航空航天科技有限公司 | Magnesium-based alloy compounded by rare earth and alkaline earth elements and preparation method thereof |
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| CN100554466C (en) * | 2008-05-21 | 2009-10-28 | 中国科学院长春应用化学研究所 | A high-strength and corrosion-resistant Mg-Al-Mn die-casting magnesium alloy containing yttrium-rich rare earth |
| CN101255519B (en) * | 2008-05-21 | 2010-06-16 | 中国科学院长春应用化学研究所 | A kind of preparation method of high-strength and high-toughness Mg-Al-Mn die-casting magnesium alloy containing lanthanum-cerium mixed rare earth |
| CN101824571B (en) * | 2010-03-09 | 2011-12-07 | 扬州宏福铝业有限公司 | Mg-Al-Zn-RE wrought magnesium alloy containing Ce-La mixed rare earth and production method and application thereof |
| CN102134672A (en) * | 2011-03-22 | 2011-07-27 | 南昌大学 | Mg-Al-Mn-xCe rare earth die cast magnesium alloy |
| CN104073702A (en) * | 2014-07-02 | 2014-10-01 | 中国科学院长春应用化学研究所 | Rear-earth magnesium alloy and preparation method thereof |
| CN105525172A (en) | 2014-11-13 | 2016-04-27 | 比亚迪股份有限公司 | Magnesium alloy as well as preparation method thereof and application thereof |
| CN105543604B (en) | 2014-11-13 | 2017-07-04 | 比亚迪股份有限公司 | A kind of magnesium alloy and its preparation method and application |
| CN104388715A (en) * | 2014-12-15 | 2015-03-04 | 春兴精工(常熟)有限公司 | Preparation method of high-yield-strength magnesium alloy |
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Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BRPI0618517B1 (en) * | 2005-11-10 | 2018-01-09 | Magontec Gmbh | ALLOY AND MAGNESIUM FOUNDRY PROCESS |
-
2007
- 2007-11-06 CN CN2007100562795A patent/CN101158002B/en not_active Expired - Fee Related
-
2008
- 2008-06-04 US US12/133,229 patent/US20090116993A1/en not_active Abandoned
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103451459A (en) * | 2013-09-14 | 2013-12-18 | 天津六合镁制品有限公司 | Preparation method of magnesium alloy |
| WO2016178204A1 (en) * | 2015-05-07 | 2016-11-10 | Dead Sea Magnesium Ltd. | Creep resistant, ductile magnesium alloys for die casting |
| US20170129006A1 (en) * | 2015-05-07 | 2017-05-11 | Dead Sea Magnesium Ltd. | Creep resistant, ductile magnesium alloys for die casting |
| US10751793B2 (en) * | 2015-05-07 | 2020-08-25 | Dead Sea Magnesium Ltd. | Creep resistant, ductile magnesium alloys for die casting |
| WO2020221752A1 (en) * | 2019-04-29 | 2020-11-05 | Brunel University London | A casting magnesium alloy for providing improved thermal conductivity |
| CN115449682A (en) * | 2022-09-28 | 2022-12-09 | 广东汇天航空航天科技有限公司 | Magnesium-based alloy compounded by rare earth and alkaline earth elements and preparation method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101158002A (en) | 2008-04-09 |
| CN101158002B (en) | 2011-01-12 |
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