CA2213550A1 - Creep resistant magnesium alloys for die casting - Google Patents
Creep resistant magnesium alloys for die castingInfo
- Publication number
- CA2213550A1 CA2213550A1 CA 2213550 CA2213550A CA2213550A1 CA 2213550 A1 CA2213550 A1 CA 2213550A1 CA 2213550 CA2213550 CA 2213550 CA 2213550 A CA2213550 A CA 2213550A CA 2213550 A1 CA2213550 A1 CA 2213550A1
- Authority
- CA
- Canada
- Prior art keywords
- alloy
- magnesium
- calcium
- aluminum
- less
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
Classifications
-
- 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
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Continuous Casting (AREA)
Abstract
A magnesium based alloy contains from about 2 to about 6 wt.% aluminum and from about 0.1 to about 0.8 wt.% calcium, the balance comprising magnesium.
The alloy includes the intermetallic compound Al2Ca at the grain boundaries of the magnesium crystals. The alloy according to this invention may have a creep extension of less than about 0.5 % at about 150 ~C.
The alloy includes the intermetallic compound Al2Ca at the grain boundaries of the magnesium crystals. The alloy according to this invention may have a creep extension of less than about 0.5 % at about 150 ~C.
Description
CA 02213~0 1997-08-21 Title: CREEP RESISTANT MAGNESrUM ALLOYS FOR DIE CASTING
FIELD OF THE INVENTION
This invention relates to magnesium based alloys. In particular, the invention relates to magnesium based alloys containing 5 aluminum and calcium. The alloys of this invention are particularly useful in die casting applications.
BACKGROUND TO THE INVENTION
Magnesium is the lightest of the structural metals and may readily be fabricated by standard processes. Variolls magnesium alloys have been 10 developed for use in various applications including, for example, the die casting of parts for automobiles. An example of a magnesium alloy which may be used in the fabrication of automobile parts is AZ91. This magnesium alloy contains about 8.5% aluminum and trace amount of other elements. AZ91 is an economically priced alloy for various 15 applications including the fabrication of automobile parts. One disadvantage of this alloy is that it has a creep extension of about 2.5%
(at 150 ~C) as measured by ASTM Tect No. E139-83. Due to its high creep extension, AZ91 is unattractive in various applications such as components for automobile transmissions where fabricated parts must 20 fit together with high tolerances andL remain dimensionally stable during the operating life of the part.
A second magnesium based alloy which is available for use is designated AE42. This alloy comprises about 3.8% aluminum and about 2.4% rare earths together with trace amounts of other 25 elements. This product has a desirable creep extension (about 0.3% or less at 150 ~C). Accordingly, while this alloy may be used to fabricate parts having a high degree of dimensional stability. However, due to the use of rare earth elements in fabricating this al:Loy, the alloy is uneconomical.
CA 02213~0 1997-08-21 SUMMARY OF THE INVENTION
In accordance with the instant invention, there is r provided a magnesium based alloy comprising from about 2 to about 6 wt. % aluminum and from about 0.1 to about 0.8 wt. % calcium, the 5 alloy having a creep extension less than about 0.5 %.
Preferably, the amount of aluminum varies from about 2 to about 5 wt. % and, more t,re~ldbly from about 4 to about 5 wt. %. In addition, the amount of calcium present in the alloy preferably varies from about 0.4 to about 0.8 wt. % calcium and, more preferably, from 10 about 0.5 to about 0.7 wt. % calcium.
As is appreciated from the forgoing, the main constituent elements of the alloy are magnesium, aluminum and calcium. The alloy may also contain other elements (e.g. up to about 0.05 wt. %
silicon, up to about 0.2 wt. % zinc, up to about 0.25 wt. % manganese) 15 and impurities (e.g. less than about 0.004 wt. % iron, less than about 0.008 wt. % copper and less than about 0.002 wt. % nickel).
It has surprisingly been found that the addition of the specified amount of aluminum and calcium result in the formation of the intermetallic compound Al2Ca at the grain boundaries of the 20 magnesium. Without being limited by theory, it is believed that the intermetallic compound Al2Ca results in high metallurgical stability (due to its high melting point) and strengthens the boundaries of the magnesium grains in the alloy.
Preferably, the alloy comprises from about 1 to about 24 25 volume % of the intermetallic compound A12Ca, more preferably from about 12 to about 24 volume % and, most preferably from about 15 to about 20 volume %.
The alloys of this invention are particularly useful as die casting alloys due to their decreased tendencies of hot-cracking and die-CA 022l3~0 l997-08-2l WO 96(25529 PCT/CA96100091 sticking, their high creep extension and their relative low cost. The alloys may be produced by any standard process used in the industry.
BRIEF DESCRIPTION OF THE DRAWINGS
These and other advantages of the instant invention will 5 be more fully and particularly explaLined in association with the following discussion of the preferred embodiment a,f the invention and the following drawings in which:
Figure 1 is a enlargement of the a section of a die cast alloy according to the instant invention;
Figure 2 is a second section of a die cast alloy according to the instant invention;
Figure 3 is a third section of a die cast alloy according to the instant invention; and Figure 4 is a drawing of an industrial die casting part used 15 in Example 2;
DESCRIPTION OF THE PREFERRED EMBODIMENT
The alloy of this invention comprises magnesium, aluminum and calcium. Calcium and aluminum comprise the main constituent elements in the magnesiu.m based alloy. As discussed 20 below, the alloy may also include other elements as additives or impurities.
The magnesium based a]loy preferably contains from about 0.1 to about 0.8 wt. % calcium, more ~re~eLably, f:rom about 0.4 to about 0.8 wt. % calcium and, most preferably, from about 0.5 to about 25 0.7 wt. % calcium. The use of more than about 0.8 wt. % calcium adversely affects the die castability of the alloy due to extensive hot-cracking and die sticking. In addition, if the alloy contains more than CA 02213~0 1997-08-21 WO 96t25529 PCT/CA96/00091 about 0.8 wt. % calcium, the corrosion resistance of the alloy tends to decrease.
The alloy preferably contains from about 2 to about 6 wt.
% aluminum, more preferably from about 2 to about 5 wt. %
5 aluminum and, most preferably from about 4 to about 5 wt. %
aluminum. If the alloy contains less than about 2 wt. % aluminum, then all of the aluminum will tend to be dissolved in the magnesium.
If the alloy contains more than about 6 wt. % aluminum, then the aluminum tends to combine with the magnesium to form significant 10 amounts of the intermetallic compound Mgl7All2. This intermetallic compound has a low melting point and accordingly has a deleterious affect on the properties of the magnesium based alloy. The balance of the alloy comprises magnesium.
The magnesium alloy may also include lesser amounts of 15 other additives and impurities. For example, up to about 0.5 wt. %
manganese, more preferably from about 0.25 to about 0.5 wt. %
manganese may be included in the alloy to improve corrosion resistance. Silicon and zinc are typical impurities which are contained in the magnesium which is used to prepare magnesium alloys. The 20 alloy may contain up to about 0.05 wt. % silicon and up to about 0.2 wt.
% zinc. Other elements may be present in amounts up to about 0.01 %
each.
Iron, copper and nickel have deleterious affects on the corrosion resistance of magnesium alloys. Accordingly, the alloy 25 preferably contains less than about 0.004 wt. % iron, and more preferably less than about 0.003 wt. % iron, preferably less than 0.008 wt. % copper and preferably less than about 0.002 wt. % nickel and, more preferably, less than about 0.001 wt. % nickel.
It has surprisingly been found that the addition of 30 calcium and aluminum in the weight percents set out herein results in the production of the intermetallic compound Al2Ca. This intermetallic compound is generally positioned along the grain CA 02213~0 1997-08-21 W~ 96125529 PCTJCA96JI)DD9I
boundaries of the magnesium crystals in the alloy. Preferably, the intermetallic continuously surrounds the grains of magnesium.
Figures 1 - 3 show micrographs of t]aree different alloys prepared according to the instant invention. The alloy in Figure 1, designated 5 AC50.6 is an alloy according to the inc;tant invention containing 4.5%
aluminum and 0.6% calcium. The al!Loy of Figure 2 is designated AC50.8 and contains 4.5% aluminum and 0.8% calcium. The alloy of Figure 3 is designated AC51 and contains 4.5% alurminum and 1.0%
~ calcium. These micrographs demons,trate the positioning of the 10 intermetallic substantially along the grain bow~daries of the magnesium crystals.
The magnesium based alloy of the instant invention has good creep resistance at temperatures commonly lencountered by components for cars (e.g. temperatures up to about 150~C). The alloy 15 preferably has a creep extension less than about 2.5%, more preferably less than about 0.5% and, most preferably less than about 0.35%. It will be appreciated that the greater the amount of Al2Ca which is formed, the lower the creep extension of the alla,y. Preferably, the alloy contains from about 1 to about 24 volume % of intermetallic Al2Ca, more 20 preferably from about 12 to about 24 volume % and"most preferably, from about 15 to about 20 volume %.
The alloy is particularly well adapted for use as a die casting alloy and may be made by any standard die casting process. For example, the alloy may be prepared by charging the constituent 25 elements to a suitable furnace and elevating the constituent elements to a temperature above their melting point. The mixture may be mixed as is known in the art and then poured into a suitable die and cooled to produced the die cast elem~ent. Alternately, a magnesium aluminum alloy such as AM50 may be charged to a furnace.
30 Subsequently, after the magnesium aluminum alloy has been melted or substantially melted, calcium, such ilS in the form of 70/30 Mg-Ca master alloy, may be charged to the furnace. Once this charge has been CA 02213~i~i0 1997-08-21 melted and mixed, the charge may be poured into a suitable die and cooled to produce the die cast element.
The alloys according to the instant invention have good tensile strength at temperatures up to about 150~C, as measured by 5 ASTM Test No. E8M-9OA, and yield strength, as measured by ASTM
Test No. E8M-9OA. The alloys of the instant invention preferably have a tensile strength greater than about 21 ksi, more preferably greater than about 22 ksi and, most preferably, greater than about 23 ksi. The yield strength is preferably greater than about 12 ksi, more preferably 10 greater than about 13 ksi and, most preferably greater than about 15 ksi.
The invention will be further understood by the following examples which are not to be construed as a limitation of the invention. Those skilled in the art will appreciate that other and further embodiments are obvious and within the spirit and scope of 15 this invention from the teachings of the present examples taken with the accompanying specifications.
Example 1 Several alloys were produced from a magnesium aluminum alloy (AM50) and a calcium magnesium alloy (Mg-Ca 20 master alloy). The composition of these alloys are set out in Table 1:
MA'lkl~lAL Al Ca Cu l~e Mn Ni Si Zn Wt. % Wt. % ppm PDm Wt. % DDm DDm DDm AM50 (1) 5.0 0.0002 10 20 0.32 10 70 200 30/70 Mg-Ca (1) ---- 30.2 0.08% 0.01% 0.01% 0.001% 0.015% 0 . 0 0 6 %
MASTER ALLOY
(1) balance is magnesium These alloys were charged to a 250 tonne frech hot-chamber die casting machine. The feed alloys were raised to a temperature in the range 620~C to about 635~C and mixed. This liquid 30 mixture was then charged into a die to form a test specimen. When CA 022l3~i~i0 l997-08-2l WO 96125529 ~ PCT~CA96~0~1~91 cooled, the die was removed and the test specimens were subjected to tests. The amounts of alloy AM50 and Mg-Ca Master Alloy used in each run, and the composition of the resulting alloys are set out in Table No. 2.
ALLOY AM50 Ca-Mg Al CaCu Fe Mn Ni Si Zn kg. Master Wt. % Wt. % ppm ppm Wt. % ppm ppm ppm Alloy AC50.6 180 . 4.53 0.61 2 10 0.24 l 16 31 AC50.8 180 . 4.53 0.85 2 13 0.25 l 20 29 AC51 180 ., 4.56 1.02 2 20 0.24 :Z 18 30 Various properties of the alloys where then tested and compared against other magnesium based alloys, namely AZ91 and AE42. The creep resistance of the alloys, was measured according to ASTM Test No. E139-83. The results of the 150~C creep performance tests are set out in Table No. 3.
TABLE 3 - CREEP PERl~ORMANCE
AZ91AE42 AC50.6AC50.8 ~C51 S--~ SS (MPa) ' 5 5 T ,' PERATURE (~C) ~ -~ 5~ 5 I .TION (HOURS) ' ~ 0~ ~ 0 % '~/0 ' ' C/o ~%
~ " % % - % ~ %
~ -- ' ~ % % . o ~0 . ,%
,~ ,' . AGE _. ~~ . /o .. h .~6 6 .. ~O
The results demonstrate that the alloys prepared according to the instant invention, namely AC50.6 AC50.8 and AC51 25 have a creep extension comparable to t]:Lose of AE42 at 150~C. With a creep extension of only about 0.3%, only slight cleformation of structural elements prepared using the~,e alloys will occur over time.
The creep extension was one order of magnitude less than the creep extension of standard magnesium based alloy AZ91.
CA 022l35~0 l997-08-2l The tensile properties of each of these alloys were also evaluated at 150~C according to ASTM Test No. E8M-90. The results are set out in Table No. 4.
PROPERTYi AC50.6 AC50.8 AC51 AE42 AZ91 YIELD STRENGTh 13,754 14,844 16,266 15,513 15,965 psi(MPa) (95) (102) (112) (107) (110) TENSILE STRENGTH 22,686 23,369 23,973 23,234 23,197 psi(MPa) (156) (161) (165) (160) (159) 10 ELONGAT'lON % 8.4 7.4 8.4 3~ 6.7 ~average of three specimens Table 4 shows that the 150~C tensile strength and yield strength of the alloys prepared according to the instant invention are equal to or better than those of magnesium based alloy AE42.
However, the elongation is substantially lower than the elongation of magnesium based alloy AE42.
The salt spray corrosion performance of each of these alloys was then measured pursuant to ASTM Test No. B117. The results are set out in Table No. 5.
RUN NO. AE42 AZ91 AC50.6 AC50.8 AC51 n~'cn2/dav n~/cm2/dav ~ ~n2/dav ~Is~/cn2/dav ~/cm2/dav : .un ~ o. ~ z~- 7 .un ~ o. :.' O :. :.: ' ~ .:: .' 1 un\o. :.-- :. ( ~. :.: :.
25 :.un ~ o. ~ ' ~ :.U ~
:.un~o. :.' :.~ :.1, :. :.. __ : .un \ o. . , ~ 0, ~ , _ ,~vera~e . :.l :.1 ;.:. :
As can be seen from the forgoing table, the alloys of the instant invention have similar corrosion resistance to magnesium based alloy AZ91 and AE42. In fact, alloy AC50.6, which contains only about 0.6% calcium, has a corrosion resistance which is twice that of alloy AE42. Accordingly, by selecting an alloy according to the instant invention having a lower level of calcium, the corrosion resistance of the resulting alloy may be substantially improved.
CA 022l3~0 l997-08-2l WO 96l25529 PCT/CA9GJDOD9I
Example 2 Two alloys with different c alcium levels ~ere prepared by the procedure of Example 1 and cast into an industrial die for die castability study.
The alloys were charged to a 600 tonne Prince cold-chamber die casting machine. The feed alloys were raised to a temperature of 660~C and mixed. This liquid mixture was then charged into an industrial die having five zones numbered 1 - 5 through a siphon tube to form an industrial die casting as shown in Figure 4. When cooled, the casting was removed from the die. One hundred (100) castings of each alloy were produced andL subjected to die castability evaluation and mechanical testing. Both visual and real-time X-ray inspections were used to detect the castin~; defects such as cracks and incomplete filling. Test specimens for tensile and creep testing were then machined from zone 3 of the die castings as shown in Figure 4.
The amounts of alloy A~50 and Mg-C a Master Alloy used in each run, and the composition of the resulting alloys are set out in Table No. 6.
TABLE 6 - COMPOSITION O:F DIE CAST ALLOYS
Alloy AM50 Mg-Ca Al Ca Cu Fe Mn Ni Si Zn kg. Master Wt. % Wt. % ppm ppm Wt. % ppm ppm ppm Alloy kg AC50.7 780 18.6 4.40 0.68 4 16 0.26 ,! 10 200 AC51 780 29.0 4.40 0.99 4 18 0.25 2 10 200 The die castability evaluation results obtained from the visual real-time X-ray inspections demonstrate that the alloy AC50.7 is readily die castable with very few casting defects. However, in the production of die castings using alloy AC51, substantial die-sticking 25 problems occurred, and significantly more casting defects such as cold shots, cracks and sink marks were observed in the castings.
CA 022l3~0 l997-08-2l The results show that the use of more than about 0.8 wt.
% calcium adversely affects the die castability due to the increased tendencies of hot-cracking and die-sticking during die casting productions. The magnesium based alloys of this invention preferably 5 contain up to 0.7 wt. % of calcium.
The creep and tensile properties of the alloys were tested and compared against other magnesium based alloys, namely AZ91 and AM50. The results of the 150~C creep performance tests are set out in Table No. 7.
TABLE NO. 7 - CREEP PERFORMANCE
AZ91 AM50 AC50.7 AC51 Stress (MPa) 35 35 35 35 T~ (~C) 150 150 150 150 Duration (Hours) 200 200 200 200 RUN 1 2.34% 1.58% 0.159% 0.145%
RI~N 2 1.88% 1.67% 0.146% 0.145%
RUN 3 2.34% 3.21% 0.218% 0.217%
AVERAGE 2.19% 2.15% 0.17% 0.17%
The results show that the creep extension of the alloys prepared according to the instant invention is about one order of magnitude less than those of standard magnesium based alloys AZ91 and AM50. The results also demonstrate that the creep resistance of 15 the alloys of this invention can be obtained with a calcium content as low as 0.6 to 0.7 wt. %.
The tensile properties of these alloys were also tested at 150~C, and the results are set out in Table No. 8.
CA 022l3550 l997-08-2l TABLE 8 - TENSILE I'ROPERll~:S
PROPERTY~ AC50.7 AC51 AZ91 AM50 YIELD STRENGTH 15,100 (104.1) 16,700 (115.4) 15,100 (104.3) 11,700 (80.4) psi (MPa) TENSILE 25,900 (178.8) 26,000 (179.3) 27,800 (191.9) 23,200 (159.9)STRENGTH
psi(MPa) ELONGATION % 16.7 18.3 13.3 24.0 ~ average of three specimens Table 8 shows that the 150~C tensile strength and yield strength of the alloys prepared accordi:ng to the instant invention are 5 equal to or better than those of magnesium based alloy AZ91 or AE42.
The elongation is higher than that of AZ91, but substantially lower than that of AM50.
FIELD OF THE INVENTION
This invention relates to magnesium based alloys. In particular, the invention relates to magnesium based alloys containing 5 aluminum and calcium. The alloys of this invention are particularly useful in die casting applications.
BACKGROUND TO THE INVENTION
Magnesium is the lightest of the structural metals and may readily be fabricated by standard processes. Variolls magnesium alloys have been 10 developed for use in various applications including, for example, the die casting of parts for automobiles. An example of a magnesium alloy which may be used in the fabrication of automobile parts is AZ91. This magnesium alloy contains about 8.5% aluminum and trace amount of other elements. AZ91 is an economically priced alloy for various 15 applications including the fabrication of automobile parts. One disadvantage of this alloy is that it has a creep extension of about 2.5%
(at 150 ~C) as measured by ASTM Tect No. E139-83. Due to its high creep extension, AZ91 is unattractive in various applications such as components for automobile transmissions where fabricated parts must 20 fit together with high tolerances andL remain dimensionally stable during the operating life of the part.
A second magnesium based alloy which is available for use is designated AE42. This alloy comprises about 3.8% aluminum and about 2.4% rare earths together with trace amounts of other 25 elements. This product has a desirable creep extension (about 0.3% or less at 150 ~C). Accordingly, while this alloy may be used to fabricate parts having a high degree of dimensional stability. However, due to the use of rare earth elements in fabricating this al:Loy, the alloy is uneconomical.
CA 02213~0 1997-08-21 SUMMARY OF THE INVENTION
In accordance with the instant invention, there is r provided a magnesium based alloy comprising from about 2 to about 6 wt. % aluminum and from about 0.1 to about 0.8 wt. % calcium, the 5 alloy having a creep extension less than about 0.5 %.
Preferably, the amount of aluminum varies from about 2 to about 5 wt. % and, more t,re~ldbly from about 4 to about 5 wt. %. In addition, the amount of calcium present in the alloy preferably varies from about 0.4 to about 0.8 wt. % calcium and, more preferably, from 10 about 0.5 to about 0.7 wt. % calcium.
As is appreciated from the forgoing, the main constituent elements of the alloy are magnesium, aluminum and calcium. The alloy may also contain other elements (e.g. up to about 0.05 wt. %
silicon, up to about 0.2 wt. % zinc, up to about 0.25 wt. % manganese) 15 and impurities (e.g. less than about 0.004 wt. % iron, less than about 0.008 wt. % copper and less than about 0.002 wt. % nickel).
It has surprisingly been found that the addition of the specified amount of aluminum and calcium result in the formation of the intermetallic compound Al2Ca at the grain boundaries of the 20 magnesium. Without being limited by theory, it is believed that the intermetallic compound Al2Ca results in high metallurgical stability (due to its high melting point) and strengthens the boundaries of the magnesium grains in the alloy.
Preferably, the alloy comprises from about 1 to about 24 25 volume % of the intermetallic compound A12Ca, more preferably from about 12 to about 24 volume % and, most preferably from about 15 to about 20 volume %.
The alloys of this invention are particularly useful as die casting alloys due to their decreased tendencies of hot-cracking and die-CA 022l3~0 l997-08-2l WO 96(25529 PCT/CA96100091 sticking, their high creep extension and their relative low cost. The alloys may be produced by any standard process used in the industry.
BRIEF DESCRIPTION OF THE DRAWINGS
These and other advantages of the instant invention will 5 be more fully and particularly explaLined in association with the following discussion of the preferred embodiment a,f the invention and the following drawings in which:
Figure 1 is a enlargement of the a section of a die cast alloy according to the instant invention;
Figure 2 is a second section of a die cast alloy according to the instant invention;
Figure 3 is a third section of a die cast alloy according to the instant invention; and Figure 4 is a drawing of an industrial die casting part used 15 in Example 2;
DESCRIPTION OF THE PREFERRED EMBODIMENT
The alloy of this invention comprises magnesium, aluminum and calcium. Calcium and aluminum comprise the main constituent elements in the magnesiu.m based alloy. As discussed 20 below, the alloy may also include other elements as additives or impurities.
The magnesium based a]loy preferably contains from about 0.1 to about 0.8 wt. % calcium, more ~re~eLably, f:rom about 0.4 to about 0.8 wt. % calcium and, most preferably, from about 0.5 to about 25 0.7 wt. % calcium. The use of more than about 0.8 wt. % calcium adversely affects the die castability of the alloy due to extensive hot-cracking and die sticking. In addition, if the alloy contains more than CA 02213~0 1997-08-21 WO 96t25529 PCT/CA96/00091 about 0.8 wt. % calcium, the corrosion resistance of the alloy tends to decrease.
The alloy preferably contains from about 2 to about 6 wt.
% aluminum, more preferably from about 2 to about 5 wt. %
5 aluminum and, most preferably from about 4 to about 5 wt. %
aluminum. If the alloy contains less than about 2 wt. % aluminum, then all of the aluminum will tend to be dissolved in the magnesium.
If the alloy contains more than about 6 wt. % aluminum, then the aluminum tends to combine with the magnesium to form significant 10 amounts of the intermetallic compound Mgl7All2. This intermetallic compound has a low melting point and accordingly has a deleterious affect on the properties of the magnesium based alloy. The balance of the alloy comprises magnesium.
The magnesium alloy may also include lesser amounts of 15 other additives and impurities. For example, up to about 0.5 wt. %
manganese, more preferably from about 0.25 to about 0.5 wt. %
manganese may be included in the alloy to improve corrosion resistance. Silicon and zinc are typical impurities which are contained in the magnesium which is used to prepare magnesium alloys. The 20 alloy may contain up to about 0.05 wt. % silicon and up to about 0.2 wt.
% zinc. Other elements may be present in amounts up to about 0.01 %
each.
Iron, copper and nickel have deleterious affects on the corrosion resistance of magnesium alloys. Accordingly, the alloy 25 preferably contains less than about 0.004 wt. % iron, and more preferably less than about 0.003 wt. % iron, preferably less than 0.008 wt. % copper and preferably less than about 0.002 wt. % nickel and, more preferably, less than about 0.001 wt. % nickel.
It has surprisingly been found that the addition of 30 calcium and aluminum in the weight percents set out herein results in the production of the intermetallic compound Al2Ca. This intermetallic compound is generally positioned along the grain CA 02213~0 1997-08-21 W~ 96125529 PCTJCA96JI)DD9I
boundaries of the magnesium crystals in the alloy. Preferably, the intermetallic continuously surrounds the grains of magnesium.
Figures 1 - 3 show micrographs of t]aree different alloys prepared according to the instant invention. The alloy in Figure 1, designated 5 AC50.6 is an alloy according to the inc;tant invention containing 4.5%
aluminum and 0.6% calcium. The al!Loy of Figure 2 is designated AC50.8 and contains 4.5% aluminum and 0.8% calcium. The alloy of Figure 3 is designated AC51 and contains 4.5% alurminum and 1.0%
~ calcium. These micrographs demons,trate the positioning of the 10 intermetallic substantially along the grain bow~daries of the magnesium crystals.
The magnesium based alloy of the instant invention has good creep resistance at temperatures commonly lencountered by components for cars (e.g. temperatures up to about 150~C). The alloy 15 preferably has a creep extension less than about 2.5%, more preferably less than about 0.5% and, most preferably less than about 0.35%. It will be appreciated that the greater the amount of Al2Ca which is formed, the lower the creep extension of the alla,y. Preferably, the alloy contains from about 1 to about 24 volume % of intermetallic Al2Ca, more 20 preferably from about 12 to about 24 volume % and"most preferably, from about 15 to about 20 volume %.
The alloy is particularly well adapted for use as a die casting alloy and may be made by any standard die casting process. For example, the alloy may be prepared by charging the constituent 25 elements to a suitable furnace and elevating the constituent elements to a temperature above their melting point. The mixture may be mixed as is known in the art and then poured into a suitable die and cooled to produced the die cast elem~ent. Alternately, a magnesium aluminum alloy such as AM50 may be charged to a furnace.
30 Subsequently, after the magnesium aluminum alloy has been melted or substantially melted, calcium, such ilS in the form of 70/30 Mg-Ca master alloy, may be charged to the furnace. Once this charge has been CA 02213~i~i0 1997-08-21 melted and mixed, the charge may be poured into a suitable die and cooled to produce the die cast element.
The alloys according to the instant invention have good tensile strength at temperatures up to about 150~C, as measured by 5 ASTM Test No. E8M-9OA, and yield strength, as measured by ASTM
Test No. E8M-9OA. The alloys of the instant invention preferably have a tensile strength greater than about 21 ksi, more preferably greater than about 22 ksi and, most preferably, greater than about 23 ksi. The yield strength is preferably greater than about 12 ksi, more preferably 10 greater than about 13 ksi and, most preferably greater than about 15 ksi.
The invention will be further understood by the following examples which are not to be construed as a limitation of the invention. Those skilled in the art will appreciate that other and further embodiments are obvious and within the spirit and scope of 15 this invention from the teachings of the present examples taken with the accompanying specifications.
Example 1 Several alloys were produced from a magnesium aluminum alloy (AM50) and a calcium magnesium alloy (Mg-Ca 20 master alloy). The composition of these alloys are set out in Table 1:
MA'lkl~lAL Al Ca Cu l~e Mn Ni Si Zn Wt. % Wt. % ppm PDm Wt. % DDm DDm DDm AM50 (1) 5.0 0.0002 10 20 0.32 10 70 200 30/70 Mg-Ca (1) ---- 30.2 0.08% 0.01% 0.01% 0.001% 0.015% 0 . 0 0 6 %
MASTER ALLOY
(1) balance is magnesium These alloys were charged to a 250 tonne frech hot-chamber die casting machine. The feed alloys were raised to a temperature in the range 620~C to about 635~C and mixed. This liquid 30 mixture was then charged into a die to form a test specimen. When CA 022l3~i~i0 l997-08-2l WO 96125529 ~ PCT~CA96~0~1~91 cooled, the die was removed and the test specimens were subjected to tests. The amounts of alloy AM50 and Mg-Ca Master Alloy used in each run, and the composition of the resulting alloys are set out in Table No. 2.
ALLOY AM50 Ca-Mg Al CaCu Fe Mn Ni Si Zn kg. Master Wt. % Wt. % ppm ppm Wt. % ppm ppm ppm Alloy AC50.6 180 . 4.53 0.61 2 10 0.24 l 16 31 AC50.8 180 . 4.53 0.85 2 13 0.25 l 20 29 AC51 180 ., 4.56 1.02 2 20 0.24 :Z 18 30 Various properties of the alloys where then tested and compared against other magnesium based alloys, namely AZ91 and AE42. The creep resistance of the alloys, was measured according to ASTM Test No. E139-83. The results of the 150~C creep performance tests are set out in Table No. 3.
TABLE 3 - CREEP PERl~ORMANCE
AZ91AE42 AC50.6AC50.8 ~C51 S--~ SS (MPa) ' 5 5 T ,' PERATURE (~C) ~ -~ 5~ 5 I .TION (HOURS) ' ~ 0~ ~ 0 % '~/0 ' ' C/o ~%
~ " % % - % ~ %
~ -- ' ~ % % . o ~0 . ,%
,~ ,' . AGE _. ~~ . /o .. h .~6 6 .. ~O
The results demonstrate that the alloys prepared according to the instant invention, namely AC50.6 AC50.8 and AC51 25 have a creep extension comparable to t]:Lose of AE42 at 150~C. With a creep extension of only about 0.3%, only slight cleformation of structural elements prepared using the~,e alloys will occur over time.
The creep extension was one order of magnitude less than the creep extension of standard magnesium based alloy AZ91.
CA 022l35~0 l997-08-2l The tensile properties of each of these alloys were also evaluated at 150~C according to ASTM Test No. E8M-90. The results are set out in Table No. 4.
PROPERTYi AC50.6 AC50.8 AC51 AE42 AZ91 YIELD STRENGTh 13,754 14,844 16,266 15,513 15,965 psi(MPa) (95) (102) (112) (107) (110) TENSILE STRENGTH 22,686 23,369 23,973 23,234 23,197 psi(MPa) (156) (161) (165) (160) (159) 10 ELONGAT'lON % 8.4 7.4 8.4 3~ 6.7 ~average of three specimens Table 4 shows that the 150~C tensile strength and yield strength of the alloys prepared according to the instant invention are equal to or better than those of magnesium based alloy AE42.
However, the elongation is substantially lower than the elongation of magnesium based alloy AE42.
The salt spray corrosion performance of each of these alloys was then measured pursuant to ASTM Test No. B117. The results are set out in Table No. 5.
RUN NO. AE42 AZ91 AC50.6 AC50.8 AC51 n~'cn2/dav n~/cm2/dav ~ ~n2/dav ~Is~/cn2/dav ~/cm2/dav : .un ~ o. ~ z~- 7 .un ~ o. :.' O :. :.: ' ~ .:: .' 1 un\o. :.-- :. ( ~. :.: :.
25 :.un ~ o. ~ ' ~ :.U ~
:.un~o. :.' :.~ :.1, :. :.. __ : .un \ o. . , ~ 0, ~ , _ ,~vera~e . :.l :.1 ;.:. :
As can be seen from the forgoing table, the alloys of the instant invention have similar corrosion resistance to magnesium based alloy AZ91 and AE42. In fact, alloy AC50.6, which contains only about 0.6% calcium, has a corrosion resistance which is twice that of alloy AE42. Accordingly, by selecting an alloy according to the instant invention having a lower level of calcium, the corrosion resistance of the resulting alloy may be substantially improved.
CA 022l3~0 l997-08-2l WO 96l25529 PCT/CA9GJDOD9I
Example 2 Two alloys with different c alcium levels ~ere prepared by the procedure of Example 1 and cast into an industrial die for die castability study.
The alloys were charged to a 600 tonne Prince cold-chamber die casting machine. The feed alloys were raised to a temperature of 660~C and mixed. This liquid mixture was then charged into an industrial die having five zones numbered 1 - 5 through a siphon tube to form an industrial die casting as shown in Figure 4. When cooled, the casting was removed from the die. One hundred (100) castings of each alloy were produced andL subjected to die castability evaluation and mechanical testing. Both visual and real-time X-ray inspections were used to detect the castin~; defects such as cracks and incomplete filling. Test specimens for tensile and creep testing were then machined from zone 3 of the die castings as shown in Figure 4.
The amounts of alloy A~50 and Mg-C a Master Alloy used in each run, and the composition of the resulting alloys are set out in Table No. 6.
TABLE 6 - COMPOSITION O:F DIE CAST ALLOYS
Alloy AM50 Mg-Ca Al Ca Cu Fe Mn Ni Si Zn kg. Master Wt. % Wt. % ppm ppm Wt. % ppm ppm ppm Alloy kg AC50.7 780 18.6 4.40 0.68 4 16 0.26 ,! 10 200 AC51 780 29.0 4.40 0.99 4 18 0.25 2 10 200 The die castability evaluation results obtained from the visual real-time X-ray inspections demonstrate that the alloy AC50.7 is readily die castable with very few casting defects. However, in the production of die castings using alloy AC51, substantial die-sticking 25 problems occurred, and significantly more casting defects such as cold shots, cracks and sink marks were observed in the castings.
CA 022l3~0 l997-08-2l The results show that the use of more than about 0.8 wt.
% calcium adversely affects the die castability due to the increased tendencies of hot-cracking and die-sticking during die casting productions. The magnesium based alloys of this invention preferably 5 contain up to 0.7 wt. % of calcium.
The creep and tensile properties of the alloys were tested and compared against other magnesium based alloys, namely AZ91 and AM50. The results of the 150~C creep performance tests are set out in Table No. 7.
TABLE NO. 7 - CREEP PERFORMANCE
AZ91 AM50 AC50.7 AC51 Stress (MPa) 35 35 35 35 T~ (~C) 150 150 150 150 Duration (Hours) 200 200 200 200 RUN 1 2.34% 1.58% 0.159% 0.145%
RI~N 2 1.88% 1.67% 0.146% 0.145%
RUN 3 2.34% 3.21% 0.218% 0.217%
AVERAGE 2.19% 2.15% 0.17% 0.17%
The results show that the creep extension of the alloys prepared according to the instant invention is about one order of magnitude less than those of standard magnesium based alloys AZ91 and AM50. The results also demonstrate that the creep resistance of 15 the alloys of this invention can be obtained with a calcium content as low as 0.6 to 0.7 wt. %.
The tensile properties of these alloys were also tested at 150~C, and the results are set out in Table No. 8.
CA 022l3550 l997-08-2l TABLE 8 - TENSILE I'ROPERll~:S
PROPERTY~ AC50.7 AC51 AZ91 AM50 YIELD STRENGTH 15,100 (104.1) 16,700 (115.4) 15,100 (104.3) 11,700 (80.4) psi (MPa) TENSILE 25,900 (178.8) 26,000 (179.3) 27,800 (191.9) 23,200 (159.9)STRENGTH
psi(MPa) ELONGATION % 16.7 18.3 13.3 24.0 ~ average of three specimens Table 8 shows that the 150~C tensile strength and yield strength of the alloys prepared accordi:ng to the instant invention are 5 equal to or better than those of magnesium based alloy AZ91 or AE42.
The elongation is higher than that of AZ91, but substantially lower than that of AM50.
Claims (20)
1. A magnesium based alloy comprising magnesium, from about 2 to about 6 wt. % aluminum and from about 0.1 to about 0.8 wt.
% calcium, said magnesium forming magnesium crystals in said alloy, at least a portion of said aluminum and calcium forming the intermetallic compound Al2Ca, said Al2Ca being located at the grain boundaries of said magnesium crystals.
% calcium, said magnesium forming magnesium crystals in said alloy, at least a portion of said aluminum and calcium forming the intermetallic compound Al2Ca, said Al2Ca being located at the grain boundaries of said magnesium crystals.
2. The alloy as claimed in claim 1 wherein said intermetallic compound comprises from about 1 to about 24 volume % of said alloy.
3. The alloy as claimed in claim 1 wherein said intermetallic compound comprises from about 12 to about 24 volume % of said alloy.
4. The alloy as claimed in claim 1 wherein the main constituent elements are magnesium, aluminum and calcium.
5. The alloy as claimed in claim 2 wherein said alloy has a creep extension less than about 0.5% at about 150°C.
6. A magnesium based alloy comprising from about 2 to about 6 wt. % aluminum and from about 0.1 to about 0.8 wt. %
calcium, said alloy having a creep extension less than about 0.5 % at about 150°C.
calcium, said alloy having a creep extension less than about 0.5 % at about 150°C.
7. The alloy as claimed in claim 6 wherein said alloy comprises from about 2 to about 5 wt. % aluminum and from about 0.4 to about 0.8 wt. % calcium.
8. The alloy as claimed in claim 6 wherein said alloy comprises from about 4 to about 5 wt. % aluminum and from about 0.5 to about 0.7 wt. % calcium.
9. The alloy as claimed in claim 6 wherein said alloy further comprises less than about 0.05 wt % silicon, less than about 0.2 wt. %
zinc, less than about 0.5 wt. % manganese, less than about 0.0004 wt %
iron, less than about 0.008 wt. % copper and less than about 0.002 wt. %
nickel.
zinc, less than about 0.5 wt. % manganese, less than about 0.0004 wt %
iron, less than about 0.008 wt. % copper and less than about 0.002 wt. %
nickel.
10. The alloy as claimed in claim 6 wherein said alloy is a die casting alloy.
11. A process for producing cast magnesium based alloy articles having decreased elongation comprising the steps of:
a. forming a molten alloy comprising from about 2 to about 6 wt. % aluminum and from about 0.1 to about 0.8 wt. % calcium, the remainder essentially being magnesium; and, b. molding said molten alloy and solidifying to form the cast alloy article, said magnesium forming magnesium crystals in said alloy, at least a portion of said aluminum and calcium forming the intermetallic compound Al2Ca, said Al2Ca being located at the grain boundaries of said magnesium crystals..
a. forming a molten alloy comprising from about 2 to about 6 wt. % aluminum and from about 0.1 to about 0.8 wt. % calcium, the remainder essentially being magnesium; and, b. molding said molten alloy and solidifying to form the cast alloy article, said magnesium forming magnesium crystals in said alloy, at least a portion of said aluminum and calcium forming the intermetallic compound Al2Ca, said Al2Ca being located at the grain boundaries of said magnesium crystals..
12. The process as claimed in claim 11 wherein said intermetallic compound comprises from about 1 to about 24 volume % of said alloy.
13. The process as claimed in claim 11 wherein said intermetallic compound comprises from about 12 to about 24 volume % of said alloy.
14. The process as claimed in claim 12 wherein said alloy comprises from about 2 to about 5 wt. % aluminum and from about 0.4 to about 0.8 wt. % calcium.
15. The process as claimed in claim 12 wherein said alloy comprises from about 4 to about 5 wt. % aluminum and from about 0.5 to about 0.7 wt. % calcium.
16. The process as claimed in claim 12 wherein said alloy has a creep extension less than about 0.5%.
17. A process for producing cast magnesium based alloy articles having a creep extension less than about 0.5 % at about 150°C
comprising the steps of:
a. forming a molten alloy comprising from about 2 to about 6 wt. % aluminum and from about 0.1 to about 0.8 wt. % calcium, the remainder essentially being magnesium; and, b. molding said molten alloy and solidifying to form the cast alloy article.
comprising the steps of:
a. forming a molten alloy comprising from about 2 to about 6 wt. % aluminum and from about 0.1 to about 0.8 wt. % calcium, the remainder essentially being magnesium; and, b. molding said molten alloy and solidifying to form the cast alloy article.
18. The process as claimed in claim 17 wherein said alloy comprises from about 2 to about 5 wt. % aluminum from about 0.4 to about 0.8 wt. % calcium.
19. The process as claimed in claim 17 wherein said alloy comprises from about 4 to about 5 wt. % aluminum from about 0.5 to about 0.7 wt. % calcium.
20. The process as claimed in claim 17 wherein said alloy further comprises less than about 0.05 wt % silicon, less than about 0.2 wt. % zinc, less than about 0.5 wt. % manganese, less than about 0.0004 wt % iron, less than about 0.008 wt. % copper and less than about 0.002 wt. % nickel.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US38999695A | 1995-02-17 | 1995-02-17 | |
| US08/389,996 | 1995-02-17 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2213550A1 true CA2213550A1 (en) | 1996-08-22 |
Family
ID=23540610
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA 2213550 Abandoned CA2213550A1 (en) | 1995-02-17 | 1996-02-14 | Creep resistant magnesium alloys for die casting |
Country Status (3)
| Country | Link |
|---|---|
| AU (1) | AU4617796A (en) |
| CA (1) | CA2213550A1 (en) |
| WO (1) | WO1996025529A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109321793A (en) * | 2018-10-31 | 2019-02-12 | 江苏理工学院 | Al2Y particle and carbon nano tube hybrid enhance ultralight Mg Li composites and preparation method |
Families Citing this family (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3415987B2 (en) * | 1996-04-04 | 2003-06-09 | マツダ株式会社 | Molding method of heat-resistant magnesium alloy molded member |
| JP2000104137A (en) * | 1998-09-30 | 2000-04-11 | Mazda Motor Corp | Magnesium alloy forging stock, forged member and production of the forged member |
| DE19915277A1 (en) * | 1999-04-03 | 2000-10-05 | Volkswagen Ag | Magnesium alloy used e.g. in the manufacture of a wheel rim contains traces of cadmium, copper, iron, nickel and lanthanum and yttrium |
| US6264763B1 (en) | 1999-04-30 | 2001-07-24 | General Motors Corporation | Creep-resistant magnesium alloy die castings |
| TW407079B (en) * | 1999-06-03 | 2000-10-01 | Mitsui Mining & Smelting Co | Method for die casting a magnesium alloy and die casting articles |
| DE60013695T2 (en) * | 1999-06-04 | 2005-09-29 | Mitsui Mining & Smelting Co., Ltd. | Die casting of magnesium alloys |
| US6342180B1 (en) | 2000-06-05 | 2002-01-29 | Noranda, Inc. | Magnesium-based casting alloys having improved elevated temperature properties |
| IL146336A0 (en) | 2001-11-05 | 2002-07-25 | Dead Sea Magnesium Ltd | High strength creep resistant magnesium alloy |
| IL146335A0 (en) | 2001-11-05 | 2002-07-25 | Dead Sea Magnesium Ltd | Creep resistant magnesium alloys with improved castability |
| US8506733B2 (en) * | 2008-03-11 | 2013-08-13 | Topy Kogyo Kabusikikaisya | Al2Ca-containing magnesium-based composite material |
| CN102000808B (en) * | 2010-12-15 | 2013-01-30 | 重庆盛镁镁业有限公司 | Magnesium alloy grain refiner and grain refined magnesium alloy and preparation method of thereof |
| JP2018193592A (en) * | 2017-05-19 | 2018-12-06 | 株式会社豊田中央研究所 | Magnesium alloy, magnesium alloy cast, and manufacturing method therefor |
| CN109321794B (en) * | 2018-10-31 | 2021-01-19 | 江苏理工学院 | Al2Ca particle and carbon nano tube hybrid reinforced ultralight magnesium lithium-based composite material and preparation method thereof |
| CN109182809B (en) * | 2018-11-19 | 2020-07-28 | 河北工业大学 | Low-cost high-toughness wrought magnesium alloy and preparation method thereof |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2642439B2 (en) * | 1988-02-26 | 1993-04-16 | Pechiney Electrometallurgie |
-
1996
- 1996-02-14 AU AU46177/96A patent/AU4617796A/en not_active Abandoned
- 1996-02-14 CA CA 2213550 patent/CA2213550A1/en not_active Abandoned
- 1996-02-14 WO PCT/CA1996/000091 patent/WO1996025529A1/en active Application Filing
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109321793A (en) * | 2018-10-31 | 2019-02-12 | 江苏理工学院 | Al2Y particle and carbon nano tube hybrid enhance ultralight Mg Li composites and preparation method |
| CN109321793B (en) * | 2018-10-31 | 2021-01-19 | 江苏理工学院 | Al2Y particle and carbon nano tube hybrid reinforced ultra-light magnesium lithium-based composite material and preparation method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| AU4617796A (en) | 1996-09-04 |
| WO1996025529A1 (en) | 1996-08-22 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP3354098B2 (en) | Magnesium alloy with excellent high temperature properties and die castability | |
| US6767506B2 (en) | High temperature resistant magnesium alloys | |
| CA2213550A1 (en) | Creep resistant magnesium alloys for die casting | |
| EP0799901B1 (en) | Heat-resistant magnesium alloy member | |
| JP3929489B2 (en) | Magnesium alloy | |
| EP1127950B1 (en) | Die casting magnesium alloy | |
| KR100199362B1 (en) | Aluminum alloy for die casting and ball joint using the same | |
| KR20170138916A (en) | Aluminum alloy for die casting, and die-cast aluminum alloy using same | |
| US6846451B2 (en) | Magnesium alloy and magnesium alloy member superior in corrosion resistance | |
| EP1308531B1 (en) | High strength and creep resistant magnesium alloys | |
| KR20160011136A (en) | Magnesium alloy having improved corrosion resistance and method for manufacturing magnesium alloy member using the same | |
| US7547411B2 (en) | Creep-resistant magnesium alloy for casting | |
| Berkmortel et al. | Die castability assessment of magnesium alloys for high temperature applications: part 1 of 2 | |
| US7169240B2 (en) | Creep resistant magnesium alloys with improved castability | |
| JP2004238676A (en) | Magnesium alloy | |
| JP2001316752A (en) | Magnesium alloy for diecasting | |
| JP4526769B2 (en) | Magnesium alloy | |
| CN100366775C (en) | High strength creep-resisting magnetium base alloy | |
| CA2087217A1 (en) | Magnesium alloy | |
| CN102051510B (en) | Creep-resistance magnesium alloy with improved casting property | |
| US4919736A (en) | Aluminum alloy for abrasion resistant die castings | |
| KR100421102B1 (en) | Die casting magnesium alloy | |
| KR102197773B1 (en) | Magnesium alloy having high strength and high elongation for high pressure die casting and preparing method for the same |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FZDE | Dead |