US2385685A - Magnesium base alloy - Google Patents
Magnesium base alloy Download PDFInfo
- Publication number
- US2385685A US2385685A US438783A US43878342A US2385685A US 2385685 A US2385685 A US 2385685A US 438783 A US438783 A US 438783A US 43878342 A US43878342 A US 43878342A US 2385685 A US2385685 A US 2385685A
- Authority
- US
- United States
- Prior art keywords
- per cent
- magnesium
- alloy
- lithium
- burning
- 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.)
- Expired - Lifetime
Links
- 229910045601 alloy Inorganic materials 0.000 title description 28
- 239000000956 alloy Substances 0.000 title description 28
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 title description 16
- 229910052749 magnesium Inorganic materials 0.000 title description 16
- 239000011777 magnesium Substances 0.000 title description 16
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 17
- 229910052744 lithium Inorganic materials 0.000 description 17
- 229910052751 metal Inorganic materials 0.000 description 11
- 239000002184 metal Substances 0.000 description 11
- 229910052782 aluminium Inorganic materials 0.000 description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 8
- 238000005275 alloying Methods 0.000 description 7
- 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 description 7
- 229910000861 Mg alloy Inorganic materials 0.000 description 6
- 230000004907 flux Effects 0.000 description 5
- 230000003647 oxidation Effects 0.000 description 5
- 238000007254 oxidation reaction Methods 0.000 description 5
- 239000011701 zinc Substances 0.000 description 5
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 229910052725 zinc Inorganic materials 0.000 description 4
- 238000005266 casting Methods 0.000 description 3
- 229910052709 silver Inorganic materials 0.000 description 3
- 239000004332 silver Substances 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- TWRXJAOTZQYOKJ-UHFFFAOYSA-L Magnesium chloride Chemical compound [Mg+2].[Cl-].[Cl-] TWRXJAOTZQYOKJ-UHFFFAOYSA-L 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 230000001747 exhibiting effect Effects 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000002699 waste material Substances 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- SNAAJJQQZSMGQD-UHFFFAOYSA-N aluminum magnesium Chemical compound [Mg].[Al] SNAAJJQQZSMGQD-UHFFFAOYSA-N 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 229910001629 magnesium chloride Inorganic materials 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 239000000126 substance Substances 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
Definitions
- the invention relates to magnesium base alloys and in particular concerns alloys of this nature having reduced burning or oxidation characteristics in the molten state.
- Magnesium alloys are now widely used in the industrial and structural arts for forgings, castings, and extruded shapes where a light .weight metal having good strength properties is highly desirable. It is, of course, generally necessary to melt themagnesium as produced commercially and alloy it with other elements to give it the desired properties priorto use. Additionally, it may be necessary to remelt the so-formed alloy a number of times as when it is used for casting operations. It is well known that when magneslum and its alloys are handled in the molten state it is necessary to maintain the metal under a protective blanket of a suitable flux in order to control the oxidation and burning or the metal to the extent that it may be commercially used and, even then, an appreciable waste occurs due to burning. In case the materal is to be used in casting operations more waste occurs as the molten metal is ladled from the melting pot and poured into molds since this operation is carried out while the metal is in direct contact with air.
- Another object oi the invention is to provide magnesium base alloys which may be ladled in the molten state and poured into ingots without exhibiting marked burning tendencies.
- My invention is based on the discovery that the burning characteristics of some of the well known commercial magnesium alloys are greatly improved by alloying therewith a comparatively small amount of lithium.
- the quantity of lithium to be added -to produce the desired eiiect ranges between about 0.001 to 0.01 per cent.
- the effect oi the lithium is obtained in magnesium alloys in which aluminum, manganese, silver, and zinc are present either alone or in combination in the usual amounts for commercial alloys of magnesium containing these elements, such as from l-to 12 per cent of aluminum, 0.01 to 3 per cent of manganese, depending upon the amount of aluminum present, 1 to per cent of silver, and from 1 to 10 per cent of zinc, providing the magnesium content is maintained above about 80 per cent.
- manganese In the case of manganese, it the amount of aluminum exceeds about Zr-per cent, more than about 0.5 per cent of manganese cannot be alloyed with the magnesium-aluminum alloy. It will be understood that these alloys may also contain the ordinary impurities that are found in the commercially known alloys, such as traces of iron, copper, nickel, and silicon.
- a preferred quantity of lithium is about 0.005 per cent.
- the following table compares a commercial al- 10y containing aluminum, manganese, and zinc having no lithium alloyed therewith with a siml6 ilar alloy containing 0.001 per cent of lithium.
- the flux should be substantially free from magnesium chloride if the highest alloying efllciency is to be obtained from the lithium.
- a magnesium base alloy containing from 0.001 to 0.01 per cent of lithium said alloy being additionally characterized by a reduced tendency to burn compared to a similar alloy not containing lithium in'the aforesaid proportions.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture And Refinement Of Metals (AREA)
Description
Patented Sept. 25, 1945 MAGNESIUM BASE ALLOY Robert s. Busk, Midland, Mich., asslgnorto The Dow Chemical Company, Mi
poration of Michigan dland, Mi'ch., acor- No Drawing. Application April 13, 1942, Serial No. 438,783
Claims.
The invention relates to magnesium base alloys and in particular concerns alloys of this nature having reduced burning or oxidation characteristics in the molten state.
Magnesium alloys are now widely used in the industrial and structural arts for forgings, castings, and extruded shapes where a light .weight metal having good strength properties is highly desirable. It is, of course, generally necessary to melt themagnesium as produced commercially and alloy it with other elements to give it the desired properties priorto use. Additionally, it may be necessary to remelt the so-formed alloy a number of times as when it is used for casting operations. It is well known that when magneslum and its alloys are handled in the molten state it is necessary to maintain the metal under a protective blanket of a suitable flux in order to control the oxidation and burning or the metal to the extent that it may be commercially used and, even then, an appreciable waste occurs due to burning. In case the materal is to be used in casting operations more waste occurs as the molten metal is ladled from the melting pot and poured into molds since this operation is carried out while the metal is in direct contact with air.
It is, therefore, the principal object of the invention to provide commercial alloys of magnesium exhibiting markedly decreased burning tendencies upon exposure to air.
Another object oi the invention is to provide magnesium base alloys which may be ladled in the molten state and poured into ingots without exhibiting marked burning tendencies.
Other objects and advantages of the invention I will be apparent as the description proceeds.
My invention is based on the discovery that the burning characteristics of some of the well known commercial magnesium alloys are greatly improved by alloying therewith a comparatively small amount of lithium. The quantity of lithium to be added -to produce the desired eiiect ranges between about 0.001 to 0.01 per cent. Specifically. it has been found that the effect oi the lithium is obtained in magnesium alloys in which aluminum, manganese, silver, and zinc are present either alone or in combination in the usual amounts for commercial alloys of magnesium containing these elements, such as from l-to 12 per cent of aluminum, 0.01 to 3 per cent of manganese, depending upon the amount of aluminum present, 1 to per cent of silver, and from 1 to 10 per cent of zinc, providing the magnesium content is maintained above about 80 per cent. In the case of manganese, it the amount of aluminum exceeds about Zr-per cent, more than about 0.5 per cent of manganese cannot be alloyed with the magnesium-aluminum alloy. It will be understood that these alloys may also contain the ordinary impurities that are found in the commercially known alloys, such as traces of iron, copper, nickel, and silicon.
Although the improved property of decreased burning of the new alloy is manifest over the entire range of composition indicated, a preferred quantity of lithium is about 0.005 per cent.
The following table compares a commercial al- 10y containing aluminum, manganese, and zinc having no lithium alloyed therewith with a siml6 ilar alloy containing 0.001 per cent of lithium.
Table. I
Per cent composition ma esium-rema det Crucible burning Ingot burning Al Zn Mn Li 1 o 2 0.2 Markedbuming.- Markedburning. 2 9 2 0.2 .001 Greatly improved lm rovod over over Example 1. xsmple 1.
. The tests labeled "Crucible burning" were made using alloys compounded .by adding the alloying 80' ingredients with stirring to a quantity of molten magnesium maintained under a suitable flux blanket. The test consisted in skimming the flux blanket from the surface of the melt and observing the comparative burning in the presence 5 and absence of lithium. In the case 01' the tests labeled Ingot burning" the molten metal, compounded in the foregoing manner, was poured into a suitable ingot mold and the. swim of the metal examined from time to time to determine 40 the degree of oxidation in the presence and absence of lithium.
It is clear from an examination of the table that the new alloy provides a distinct improvement as regards burning and oxidation over the well known commercial magnesium alloys. This improvement is observed in both the open crucible and when the metal is poured in ingot molds. Although the addition of the stated amounts o1 lithium greatly decreases the burning tendency of the noted alloys, it has been discovered that if the lithium content of the alloy exceeds 0.0l
per cent by any great amount, the burning characteristics of the known commercial alloy are not improved, but instead are deleteriously at- 56 iected to a very marked desree. Thus it is necesmelting and alloying metals with magnesium,
such as by adding the alloying ingredients as desired to-a bath of molten magnesium which is preferably protected from oxidation by providing a surface blanket of a suitable flux. It is be- 1 lieved that the flux should be substantially free from magnesium chloride if the highest alloying efllciency is to be obtained from the lithium.
I claim: 1. In a method of reducing the tendency to burn of a magnesium base alloy in the molten state. the step which comprises incorporating in the alloy while molten lithium in an amount from about 0.001 to 0.01 per cent of the weight of the alloy.
2. A magnesium base alloy containing from 0.001 to 0.01 per cent of lithium, said alloy being additionally characterized by a reduced tendency to burn compared to a similar alloy not containing lithium in'the aforesaid proportions.
3. The method of reducing the burning characteristics in the molten state of a magnesium base alloy' containing from 1 to 10 per cent of aluminum, from 1 to 10 per cent of zinc, and from 0.1 to 3 per cent of manganese, the total of the alloying metal not exceeding 20 per cent and the balance being magnesium, which comprises incorporating in the alloy in the molten state from 0.001 to 0.01 per cent of lithium.
4. The method of reducing the burning characteristics in the molten state of a magnesium base alloy containing from 1 to 10 per cent of aluminum and from 0.1 to 3 per cent of manganese, the balance being magnesium, which comprises incorporating in the alloy in the molten state from 0.001 to 0.01 per cent of lithium.
5. The method of reducing the burning characteristics in the molten state of a magnesium base alloy containing from 1 to 10 per cent of ;aluminum, from 0.1 to 3 per cent of manganese, and from 1 to 10 per cent of silver, the total of -the alloying metal not exceeding 20 per cent and the balance being magnesium, which comprises incorporating in the alloy in the molten state from 0.001 to 0.01 per cent of lithium.
ROBERT S. BUSK.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US438783A US2385685A (en) | 1942-04-13 | 1942-04-13 | Magnesium base alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US438783A US2385685A (en) | 1942-04-13 | 1942-04-13 | Magnesium base alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2385685A true US2385685A (en) | 1945-09-25 |
Family
ID=23741995
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US438783A Expired - Lifetime US2385685A (en) | 1942-04-13 | 1942-04-13 | Magnesium base alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2385685A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2507714A (en) * | 1945-09-14 | 1950-05-16 | Olin Mathieson | Magnesium-base alloys |
| US5059390A (en) * | 1989-06-14 | 1991-10-22 | Aluminum Company Of America | Dual-phase, magnesium-based alloy having improved properties |
-
1942
- 1942-04-13 US US438783A patent/US2385685A/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2507714A (en) * | 1945-09-14 | 1950-05-16 | Olin Mathieson | Magnesium-base alloys |
| US5059390A (en) * | 1989-06-14 | 1991-10-22 | Aluminum Company Of America | Dual-phase, magnesium-based alloy having improved properties |
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