GB2051129A - Oxidation Resistant Magnesium Alloys - Google Patents
Oxidation Resistant Magnesium Alloys Download PDFInfo
- Publication number
- GB2051129A GB2051129A GB8016671A GB8016671A GB2051129A GB 2051129 A GB2051129 A GB 2051129A GB 8016671 A GB8016671 A GB 8016671A GB 8016671 A GB8016671 A GB 8016671A GB 2051129 A GB2051129 A GB 2051129A
- Authority
- GB
- United Kingdom
- Prior art keywords
- beryllium
- alloy
- magnesium
- manganese
- molten
- 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.)
- Withdrawn
Links
- 229910000861 Mg alloy Inorganic materials 0.000 title claims abstract description 26
- 230000003647 oxidation Effects 0.000 title description 11
- 238000007254 oxidation reaction Methods 0.000 title description 11
- 229910052790 beryllium Inorganic materials 0.000 claims abstract description 69
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 claims abstract description 69
- 230000004907 flux Effects 0.000 claims abstract description 16
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 13
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 13
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims abstract description 11
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims abstract description 10
- 239000011701 zinc Substances 0.000 claims abstract description 10
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 10
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 7
- 239000010703 silicon Substances 0.000 claims abstract description 7
- 229910045601 alloy Inorganic materials 0.000 claims description 37
- 239000000956 alloy Substances 0.000 claims description 37
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 32
- 229910052749 magnesium Inorganic materials 0.000 claims description 31
- 239000011777 magnesium Substances 0.000 claims description 31
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 26
- 229910052748 manganese Inorganic materials 0.000 claims description 25
- 239000011572 manganese Substances 0.000 claims description 25
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 23
- 229910052757 nitrogen Inorganic materials 0.000 claims description 13
- 238000004512 die casting Methods 0.000 claims description 12
- 239000012298 atmosphere Substances 0.000 claims description 6
- 238000004519 manufacturing process Methods 0.000 claims description 2
- 238000000034 method Methods 0.000 claims 6
- 239000004411 aluminium Substances 0.000 claims 5
- 230000001681 protective effect Effects 0.000 abstract description 5
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 10
- 239000001301 oxygen Substances 0.000 description 10
- 229910052760 oxygen Inorganic materials 0.000 description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 7
- 238000007792 addition Methods 0.000 description 6
- 230000007797 corrosion Effects 0.000 description 6
- 238000005260 corrosion Methods 0.000 description 6
- 239000000155 melt Substances 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 4
- 238000005266 casting Methods 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000008030 elimination Effects 0.000 description 2
- 238000003379 elimination reaction Methods 0.000 description 2
- 239000011261 inert gas Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000012299 nitrogen atmosphere Substances 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- -1 0.12% Chemical compound 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000002845 discoloration Methods 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000012768 molten material Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000000063 preceeding effect Effects 0.000 description 1
- 230000009993 protective function Effects 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
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)
- Continuous Casting (AREA)
- Manufacture And Refinement Of Metals (AREA)
- Treatment Of Steel In Its Molten State (AREA)
Abstract
Magnesium alloys containing up to 12% aluminum, up to 1.5% zinc, up to 1.5% silicon, up to 0.18% manganese, 0.0025% to 0.015% beryllium are die cast without need for protective flux coverings. Die cast products that do not contain harmful flux inclusions are produced thereby.
Description
SPECIFICATION
Oxidation Resistant Magnesium Alloy
The invention generally relates to magnesium alloys that contain beryllium and are sufficiently resistant to oxidation in the molten condition to obviate the need for the use of protective flux covers to prevent excessive melt oxidation or burning when exposed to oxygen-containing atmospheres.
Beryllium functions to reduce the propensity of molten magnesium alloys to oxidize when exposed to oxygen-containing atmospheres such as air.
The elimination of the need to employ a protective flux cover for molten magnesium alloys is advantageous from at least several respects. First of all, the elimination of flux covers results in a significant cost reduction. In addition, the absence of flux covers means that flux particles cannot become mixed into the molten magnesium metal and then become trapped in the resultant casting in the form of flux inclusions. The lack of flux covers also results in increased magnesium yields because of the lack of entrapment and subsequent loss of molten magnesium in the flux covering.
It is known in the art to add beryllium to magnesium base alloys for various purposes. United
States Patent Numbers 2,380,200; 2,380,201; 2,383,281; 2,461,229 and 3,947,268 as well as an article by F. L. Burkett entitled "Beryllium in Magnesium Die Casting Alloys" which appeared in AFS
Transactions, Volume 62, pages 2-4 (1954) disclose the addition of beryllium to magnesium base alloys. Of the above cited information, United States Patent Numbers 2,380,200 and 2,380,201, and the Burkett article teach that beryllium reduces the propensity for molten magnesium alloys to oxidize.
These prior efforts to reduce oxidation do not involve beryllium additives at the levels of the invention and do not appear to involve the imposition of a restriction of manganese content to permit increased beryllium solubility in the magnesium alloy. Moreover, the Burkett article suggests that higher beryllium levels must be avoided.
The magnesium alloys of the invention comprise up to about 12% aluminum, up to about 1.5% zinc, up to about 1.5% silicon, up to about 0.18% manganese, from about 0.0025% to 0.015% beryllium, balance essentially magnesium. All compositional percentages are stated in weight percent.
It is preferred to restrict the manganese content to a maximum of about 0.05% when the beryllium content ranges between about 0.012% and 0.01 5% to increase the solubility of beryllium in molten magnesium to an extent sufficient to enable the above mentioned amount of beryllium to be dissolved in the magnesium. For example, about 0.15% manganese will permit the dissolution of from about 0.007% beryllium in molten magnesium.
It is preferred to maintain manganese from about 0.04% to 0.15% and beryllium from about 0.005% to 0.0125% in the magnesium alloys of the invention to enhance corrosion resistance of the alloy. It is further preferred to restrict manganese from about 0.08% to 0.15% and beryllium from about 0.006% to 0.01% to further enhance corrosion resistance of the magnesium alloys.
The principles of the invention are readily adaptable for use in the production of magnesium alloy die casting. Magnesium die casting alloys typically contain from 1% to 12% aluminum, up to 1.5% zinc, up to 1.5% silicon, from 0.2% to 1.0% manganese, balance essentially magnesium.
The manganese content of the alloys of the invention is important because of its influence upon the solubility and ease of alloying of beryllium in molten magnesium. Because this influence was not heretofore recognized, AZ91 B, a widely used die casting alloy having a nominal composition of 9% aluminum, 0.7% zinc, 0.2% manganese, 0.5% silicon maximum, 0.3% copper maximum, 0.03% nickel maximum, balance essentially magnesium has contained less than 0.001% beryllium. It has been discovered that beryllium is soluble in AZ91 B magnesium alloys to an extent greater than previously believed. In any event, a beryllium level of on the order of 0.001% is considered to be inadequate for purposes of achiev;ng good protection of the molten magnesium.Rather it has been determined that about 0.0025% to about 0.01 5% beryllium should be dissolved in molten magnesium or its alloys to inhibit burning, with the amount of beryllium being increased with increasing oxygen content of the atmosphere. Accordingly, the manganese content should not exceed more than about 0.18%, preferably no more than about 0.1 5%. When nitrogen atmospheres and short exposure times are involved, additions of from about 0.0025% to 0.005% beryllium are sufficient to provide protection of molten magnesium. However, when longer exposure times or significant air leakage into the nitrogen atmosphere occurs, beryllium contents on the order of from about 0.005% to 0.01% are recommended.On the other hand, should it be desired to inhibit the burning of molten magnesium or magnesium alloys held in air, a beryllium content of about 0.012% to 0.015% is preferred. Such beryllium contents require manganese to be restricted to no more than about 0.05%.
The beryllium level used depends upon the amount of oxygen in the atmosphere over the melt.
For example, if the molten magnesium is exposed to air without a cover, the oxygen content of the atmosphere will remain at about 20%, and, accordingly, high beryllium levels, on the order of 0.01% to 0.015%, will be needed to avoid excessive oxidation or burning. Should the molten magnesium be exposed for prolonged periods, it may be desirable to periodically add beryllium to compensate for beryllium that is oxidized or to add larger amounts of beryllium; e.g., 0.02% in order that the excess above the solubility limit will gradualiy dissolve to compensate for oxidation losses and thereby maintain the beryllium at or close to the saturation level in the molten magnesium.
To reduce the beryllium level required for good melt protection it is desirable to keep the oxygen level as low as is practical. Placement of a lid or hood over the molten magnesium is helpful in this regard. Reaction of the molten metal with oxygen in the enclosed air will lower the oxygen content of the atmosphere. If the system is very tight and the resultant oxygen content becomes very low, beryllium levels as low as 0.0025% will provide adequate protection. If the system is not tight or is periodically opened for brief periods for operations such as ladling, it may be desirable to introduce sufficient nitrogen or other inert gases to maintain the low oxygen contents. In such situations an intermediate beryliium level, e.g., 0.005% to 0.01%, may be used.Other protective gases such as SF2,
SO2, and various inert gases may also be used, although nitrogen is preferred due to its relative availability.
Impurities such as iron tend to form insoluble intermetallic compounds with beryllium and
accordingly should be minimized. Beoause manganese, when in the presence of aluminum contents on the order of 1% to 12%, forms a relatively insoluble phase with iron which then settles to the bottom of the melt, small quantities of manganese such as 0.1% may be included in die casting alloys for
purification purposes. However, the manganese level should not be high enough to precipitate
beryllium. Typically, manganese contents should be decreased from 0.18% to 0.05% as the beryllium
level increases from 0.0025% to 0.015% in magnesium alloys containing about 9% aluminum.
The following experimental results illustrate certain of the principles of the invention.
A magnesium test alloy containing about 9% aluminum, about 0.7% zinc, and about 0.0025%
beryllium was held under a hood for 8 hours without burning or excessive oxidation.
A 130 Ib. batch of an alloy containing 7.1% aluminum, 0.71% zinc, 0.05% manganese, balance
magnesium was melted, covered with a flux and held under a hood at 1 2500F. Following removal of
the flux by skimming, burning of the molten alloy occurred after 1 minute. The burning was then
extinguished with the establishment of a flux cover. The hood was closed and nitrogen was flooded
over the surface of the flux-covered molten bath at a rate of 30 cfh for about 5 minutes. The hood was
closed, the flux cover removed, and nitrogen flow was continued at a rate of 30 cfh. After 30 minutes,
blooms (localized areas of high oxidation) began to form and increase in size. After 51 minutes the
blooms began to burn slowly and emit a bright light. The hood door was then briefly opened
periodically to permit ladling and casting of test bars.Burning became more vigorous after 5 minutes of
casting and very intense after 1 5 minutes.
Additional tests were conducted by adding various amounts of beryllium to the molten
magnesium test alloy described in the preceeding paragraph. In general, the tests indicated that
beryllium additions decrease the tendency of the molten alloy to burn. When on the order of 0.008%
beryllium was incorporated, the alloy was held satisfactorily under a 30 cfh nitrogen flow and then die
cast into test bars. This alloy was also held in air without burning for approximately 1 5 minutes. As the
beryllium content was increased during the various tests, it was noted that the oxidation resistance of
the molten magnesium alloy increased and that lessened rates of nitrogen flow were required for
satisfactory operation.When about 0.01 1% to 0.013% beryllium was incorporated into the molten
alloy, the surface of the alloy became silvery in appearance and was satisfactorily held under exposure
to air and then die cast. When the silvery protective surface film was deliberately disrupted, a new film
formed instantly, indicating that the protective function of beryllium was still operative. Following
exposure to air for about 1 hour, however, oxide blooms began to form and grow slowly.
When 0.0025% beryllium was alloyed into the magnesium test alloy, the melt was satisfactorily held under a nitrogen flow of 30 cfh with door closed and then was cast into test bars. Following 1 5 minutes, the molten magnesium alloy was heavily bloomed and commencing to burn. When 0.007% to 0.01% beryllium was alloyed, the casting run was successfully completed without the occurrence of blooming with 60 cfh nitrogen. The door of the hood was then held open for 15 minutes without bloom formation. Nitrogen flow was then stopped and the molten alloy was held for an additional 1 5 minutes without bloom formation.After the alloy was saturated with about 120-130 ppm beryliium at 1 200C1 3000F, it was held in air with the door open for over 30 minutes without bloom formation and was then successfully cast without a nitrogen atmosphere. Extended holding, however, finally led to bloom formation.
To determine the compatibility of manganese and beryllium in magnesium alloys, two AZ91 B ingots containing about 0.256 manganese were added to the melt. This addition reduced the beryllium content to about 0.008% and increased the manganese content to 0.12%. The molten alloy was successfully die cast with a flow of 60 cfh nitrogen and the hood door opened only as required. A portion of the melt was poured in air into a large ingot mold. No discoloration was noted on the metal surface as it slowly solidified.
Another AZ9 1 B ingot was added to the molten alloy with a resultant lowering of the beryllium content to about 0.007 ,ó and an increase in the manganese level to about 0. 15%. Test bars were again cast under 60 cfh of nitrogen. Several blooms had formed at the end of the run.
The variations in manganese and beryllium level had no apparent effect upon the castability of the magnesium test alloy. Some improvement in fluidity and surface appearance appears to result from increasing beryllium content because of less oxidation of the molten material.
Five die cast bars of each alloy were tested in tension to determine the effect of beryllium and manganese. The results set forth in Table I indicate that lower manganese and higher beryllium function to increase both ductility and tensile strength of the magnesium test alloy.
Sanded test bars of each alloy were also immersed in salt water (3% NaCI) for 3 days to determine corrosion resistance. The bars were sanded to remove the cast surface. The results in Table
II indicate that beryllium additions reduce the salt water corrosion rate of the magnesium test alloy to the same low level obtained by manganese additions. Small amounts of manganese, e.g., 0.12%, reduce the amount of beryllium required for good corrosion resistance. The improvement effected by beryllium can be attributed to a reduction in iron content.
Table I
% Be %Mn %E Ty's* TS*
0 0.05 6 21,500 36,300
0.0025 0.05 7 22,900 38,900
0.0086 0.05 6 22,700 36,800
0.0113 0.04 7 21,000 38,200
0.0125 0.04 5 22,000 37,800
0.0081 0.12 6 22,700 39,000
0.0071 0.15 8 21,900 40,500
0.0006** 0.2 4 21,700 34,600 * Pounds per Square Inch.
** (AZ91 B).
Table II Corrosion
% Be % Mn % Fe Rate-lPY* - 0.05 > 0.15 1.30
0.0025 0.05 0.15 0:95
0.0086 0.05 0.008 0.17
0.0113 0.04 0.005 0.03
0.0125 0.04 0.005 0.03
0.0081 0.12 0.006 0.03
0.0071 0.15 0.007 0.03
0.0006** 0.2 0.003 0.03
*inches per year.
**(AZ91 B).
Claims (20)
1. A magnesium alloy consisting essentially of up to 12% aluminium, up to 1.5% zinc, up to 1.5% silicon, up to 0.18% manganese, from 0.0025% to 0.015% beryllium, balance essentially magnesium.
2. An alloy as claimed in claim 1, containing from 0.0025% to 0.005% beryllium.
3. An alloy as claimed in claim 1, containing from 0.005% to 0.01% beryllium.
4. An alloy as claimed in claim 1, containing from 0.04% to 0.15% manganese and from 0.005% to 0.0125% beryllium.
5. An alloy as claimed in claim 4, containing from 0.08% to 0.15% manganese and from 0.006% to 0.01% beryllium.
6. An alloy as claimed in claim 5, containing about 9% aluminium, about 0.7% zinc, about 0.12% manganese, and about 0.008% beryllium.
7. An alloy as claimed in claim 1, containing not more than 0.05% manganese and from 0.012% to 0.015% beryllium.
8. An alloy as claimed in any one of claims 1 to 7 containing from 1 to 12% aluminium.
9. An alloy as claimed in claim 8 in the form of a die casting.
10. An alloy as claimed in any one of claims 1 to 9 and substantially as hereinbefore described.
11. A die casting characterized by being essentially free of flux inclusions and consisting essentially of from about 1% to 12% aluminium, up to 1.5% zinc, up to 1.5% silicon, up to 0.18% manganese, from 0.0025% to 0.015% beryllium, balance essentially magnesium.
1 2. A die casting as claimed in claim 11 and substantially as hereinbefore described.
13. A method of making a magnesium alloy die casting, comprising:
a. providing a molten pool of a magnesium alloy consisting essentially of 1% to 12% aluminium, up to 1.5% zinc, up to 1.5% silicon, up to 0.18% manganese, from 0.0025% to 0.015% beryllium, balance essentially magnesium,
b. die casting said molten magnesium alloy.
14. A method as claimed in claim 13, wherein the molten pool is exposed to an oxygencontaining atmosphere.
15. A method as claimed in claim 14, wherein the magnesium alloy contains from 0.0025% to 0.005% beryllium and the molten pool is exposed to an atmosphere containing a greater amount of nitrogen than that contained in air.
1 6. A method as claimed either in claim 13 or claim 14, wherein the magnesium alloy contains from about 0.005% to 0.01% beryllium.
17. A method as claimed in claim 14, wherein the magnesium alloy contains from 0.01% to 0.015% beryllium and up to 0.05% manganese and the molten pool is exposed to air.
1 8. A method as claimed in any one of claims 1 3 to 1 7 and substantially as hereinbefore described.
19. Magnesium alloy die-castings whenever made by the method claimed in any one of claims 13 to 18.
20. A die-casting as claimed in claim 1 9 which is substantially free from flux inclusions.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US4180279A | 1979-05-23 | 1979-05-23 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB2051129A true GB2051129A (en) | 1981-01-14 |
Family
ID=21918397
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB8016671A Withdrawn GB2051129A (en) | 1979-05-23 | 1980-05-20 | Oxidation Resistant Magnesium Alloys |
Country Status (9)
| Country | Link |
|---|---|
| JP (1) | JPS55158248A (en) |
| AU (1) | AU5622780A (en) |
| BR (1) | BR8003132A (en) |
| CA (1) | CA1151908A (en) |
| DE (1) | DE3018531A1 (en) |
| FR (1) | FR2457329A1 (en) |
| GB (1) | GB2051129A (en) |
| IT (1) | IT1149295B (en) |
| NO (1) | NO801121L (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6793877B1 (en) * | 1999-07-02 | 2004-09-21 | Norsk Hydro Asa | Corrosion resistant Mg based alloy containing Al, Si, Mn and RE metals |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AU3463293A (en) * | 1992-02-04 | 1993-09-01 | Japan As Represented By Director General Of Agency Of Industrial Science And Technology | Method of flameproofing molten magnesium material, and alloy thereof |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH257160A (en) * | 1944-06-23 | 1948-09-30 | Stone & Company Limited J | Process for obtaining molten magnesium-based alloys intended to be die-cast. |
| DE1019093B (en) * | 1953-07-31 | 1957-11-07 | Fuchs Fa Otto | Use of cast magnesium alloys with low beryllium additions |
| FR1108980A (en) * | 1954-10-06 | 1956-01-19 | Magnesium Elektron Ltd | Magnesium alloys |
| DE1027410B (en) * | 1955-03-08 | 1958-04-03 | Fuchs Fa Otto | Use of cast magnesium alloys with low beryllium additions |
| GB963073A (en) * | 1962-04-12 | 1964-07-08 | Magnesium Elektron Ltd | Improvements in or relating to magnesium base alloys |
| SU393343A1 (en) * | 1971-06-01 | 1973-08-10 | MAGNESIUM ALLOY |
-
1980
- 1980-03-06 AU AU56227/80A patent/AU5622780A/en not_active Abandoned
- 1980-03-21 IT IT20859/80A patent/IT1149295B/en active
- 1980-03-27 CA CA000348593A patent/CA1151908A/en not_active Expired
- 1980-04-18 NO NO801121A patent/NO801121L/en unknown
- 1980-04-21 FR FR8008932A patent/FR2457329A1/en not_active Withdrawn
- 1980-05-14 DE DE19803018531 patent/DE3018531A1/en not_active Withdrawn
- 1980-05-19 JP JP6546980A patent/JPS55158248A/en active Pending
- 1980-05-20 BR BR8003132A patent/BR8003132A/en unknown
- 1980-05-20 GB GB8016671A patent/GB2051129A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6793877B1 (en) * | 1999-07-02 | 2004-09-21 | Norsk Hydro Asa | Corrosion resistant Mg based alloy containing Al, Si, Mn and RE metals |
Also Published As
| Publication number | Publication date |
|---|---|
| CA1151908A (en) | 1983-08-16 |
| IT8020859A0 (en) | 1980-03-21 |
| JPS55158248A (en) | 1980-12-09 |
| NO801121L (en) | 1980-11-24 |
| FR2457329A1 (en) | 1980-12-19 |
| AU5622780A (en) | 1980-11-27 |
| DE3018531A1 (en) | 1980-12-04 |
| IT1149295B (en) | 1986-12-03 |
| BR8003132A (en) | 1980-12-23 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US5039479A (en) | Silver alloy compositions, and master alloy compositions therefor | |
| EP1266974B1 (en) | Gold alloys and master alloys for obtaining them | |
| Foerster | HiLoN: A new approach to magnesium die casting | |
| US4659377A (en) | Method for producing an oxidation resistant magnesium alloy melt | |
| GB2085471A (en) | Oxidation resistant magnesium alloy | |
| CA1319280C (en) | Creep resistant zinc-aluminum based casting alloy | |
| US4543234A (en) | Oxidation resistant magnesium alloy | |
| JPS5918457B2 (en) | Magnesium-based alloy with high mechanical strength and low corrosion tendency | |
| US6139654A (en) | Strontium master alloy composition having a reduced solidus temperature and method of manufacturing the same | |
| US20070212250A1 (en) | Die cast magnesium alloy | |
| JP4287594B2 (en) | Treatment of aluminum alloy melt | |
| GB2051129A (en) | Oxidation Resistant Magnesium Alloys | |
| DE3109066C2 (en) | ||
| JPH11323456A (en) | Production of aluminum alloy ingot | |
| JP3242493B2 (en) | Heat resistant magnesium alloy | |
| US2385685A (en) | Magnesium base alloy | |
| US4439397A (en) | Process for adjusting the composition of a zinc alloy used in the galvanization of steel | |
| US2385686A (en) | Magnesium base allot | |
| JP2640405B2 (en) | Corrosion resistant magnesium alloy | |
| US3416978A (en) | Magnesium base alloys | |
| RU2026395C1 (en) | Master alloy | |
| SU478886A1 (en) | Alloy for alloying | |
| US9708691B2 (en) | Process for investment casting and casting grain for use in the process | |
| Bodene | What are the potentialities of beryllium-light-metal alloys? | |
| SU514035A1 (en) | Modifier |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |