US1941039A - Magnesium alloy - Google Patents
Magnesium alloy Download PDFInfo
- Publication number
- US1941039A US1941039A US581050A US58105031A US1941039A US 1941039 A US1941039 A US 1941039A US 581050 A US581050 A US 581050A US 58105031 A US58105031 A US 58105031A US 1941039 A US1941039 A US 1941039A
- Authority
- US
- United States
- Prior art keywords
- alloys
- magnesium alloy
- alloy
- magnesium
- 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.)
- Expired - Lifetime
Links
- 229910000861 Mg alloy Inorganic materials 0.000 title description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 15
- 229910052742 iron Inorganic materials 0.000 description 14
- 229910052725 zinc Inorganic materials 0.000 description 14
- 239000011701 zinc Substances 0.000 description 14
- 229910045601 alloy Inorganic materials 0.000 description 10
- 239000000956 alloy Substances 0.000 description 10
- 229910052709 silver Inorganic materials 0.000 description 10
- 229910052790 beryllium Inorganic materials 0.000 description 8
- 239000011777 magnesium Substances 0.000 description 7
- 229910052748 manganese Inorganic materials 0.000 description 7
- 239000011572 manganese Substances 0.000 description 7
- 229910052749 magnesium Inorganic materials 0.000 description 4
- 239000010944 silver (metal) Substances 0.000 description 4
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 3
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 3
- 238000005266 casting Methods 0.000 description 3
- 229910001316 Ag alloy Inorganic materials 0.000 description 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 2
- 239000004332 silver Substances 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 229910017916 MgMn Inorganic materials 0.000 description 1
- 241000183024 Populus tremula Species 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 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
- C22C23/04—Alloys based on magnesium with zinc or cadmium as the next major constituent
Definitions
- Magnesium alloys with zinc or zinc and manganese are already in use for several technical purposes. However, their application is limited onaccount of their tensile strength, especially 5 with castings, being not very satisfactory. These known magnesium alloys also have no great resistance against chemical and corrosive attacks.
- the invention obviates these drawbacks by the addition of iron and. silver or beryllium to alloys of the aforesaid type; it therefore refers to magnesium alloys with at least 80% Mg and Zn or Zn and Mn and Fe, Ag or beryllium.
- the Mg, Zn, Fe, Ag alloys may contain up to 15% Zn, 2% Fe and 2% Ag, the rest being Mg.
- the uniform structure protects the alloys against corrosive attacks of the surface; the re- The Mg, Zn, Mn, Fe, Ag alloys may contain upv loys have far .better mechanical capacities espe cially higher tensile strength, ductility, elongation and hardness. They are less inflammable, they flow well and can be easily cast; they can be mechanically worked with no difiiculty, have a very low spec. weightof about 1,7 and a silvery, wonderful colour.
- the silver can be replaced, wholly or partly, by beryllium; this addition increases particularly the hardness of these alloys.
- the selection of the components used and their quantities depends mainly on the special application of the alloy, the maximum of spec. weight, which is allowable in the special case, and the varying working conditions.
- a preliminary alloy which contains the necessary amount of Zn, Fe, Ag or Zn, Fe, Be or Zn, Fe, Ag, Be is added to the molten Mg or MgMn alloy.
- manganese it has been found advisable to divide the quantity of this metal and to add one part to the same to the magnesium and the other part to the preliminary alloy of Zn, Fe, Ag or Zn, Fe, Be or zn, Fe, Ag, Be; in such way a better distribution of the manganese is obtained.
- Aluminium may be present up to 5%, silicon only as an impurity.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Adornments (AREA)
Description
Patented Dec. 26, 1933 UITED STATES PATENT QFFICE No Drawing. Application December 14, 1931, Serial No. 581,050, and in Germany December 1 Claim.
Magnesium alloys with zinc or zinc and manganese are already in use for several technical purposes. However, their application is limited onaccount of their tensile strength, especially 5 with castings, being not very satisfactory. These known magnesium alloys also have no great resistance against chemical and corrosive attacks.
Besides they are inflammable, which renders their casting diflicult and forms a great source of danger. Finally these alloys do not flow and especiallycan not be used for castings, which have thin walls.
The invention obviates these drawbacks by the addition of iron and. silver or beryllium to alloys of the aforesaid type; it therefore refers to magnesium alloys with at least 80% Mg and Zn or Zn and Mn and Fe, Ag or beryllium.
The Mg, Zn, Fe, Ag alloys may contain up to 15% Zn, 2% Fe and 2% Ag, the rest being Mg.
to 15% Zn, up to 3% Mn, up to 1% Fe and up to The simultaneous presence of Fe and Ag or Be produces a very satisfactory crystal-formation and the structure of these alloys shows a fine,
homogeneous and uniform grain.
The addition of Ag prevents an incomplete equilibrium of the mixed crystals or with other words it prevents the so-called? inter-crystalline liquation.
The uniform structure protects the alloys against corrosive attacks of the surface; the re- The Mg, Zn, Mn, Fe, Ag alloys may contain upv loys have far .better mechanical capacities espe cially higher tensile strength, ductility, elongation and hardness. They are less inflammable, they flow well and can be easily cast; they can be mechanically worked with no difiiculty, have a very low spec. weightof about 1,7 and a silvery, wonderful colour. I
The silver can be replaced, wholly or partly, by beryllium; this addition increases particularly the hardness of these alloys.
The selection of the components used and their quantities depends mainly on the special application of the alloy, the maximum of spec. weight, which is allowable in the special case, and the varying working conditions.
In order to manufacture the present alloys the following manner was found to give best results.
A preliminary alloy which contains the necessary amount of Zn, Fe, Ag or Zn, Fe, Be or Zn, Fe, Ag, Be is added to the molten Mg or MgMn alloy. In case manganese is used, it has been found advisable to divide the quantity of this metal and to add one part to the same to the magnesium and the other part to the preliminary alloy of Zn, Fe, Ag or Zn, Fe, Be or zn, Fe, Ag, Be; in such way a better distribution of the manganese is obtained.
Aluminium may be present up to 5%, silicon only as an impurity.
What I claim is:
Magnesium-alloy containing not more than 15% and not less than 0,5% Zn, not more than 3% and not less than 0,01% Mn, not more than 1,5% and not less than 0,01% Fe, not less than 0,005% and not more than 1,23% Ag, the balance being Mg;
ALEXANDER LUSCHENOWSKY.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE1941039X | 1930-12-17 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1941039A true US1941039A (en) | 1933-12-26 |
Family
ID=7750464
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US581050A Expired - Lifetime US1941039A (en) | 1930-12-17 | 1931-12-14 | Magnesium alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1941039A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2829973A (en) * | 1953-04-09 | 1958-04-08 | Magnesium Elektron Ltd | Magnesium base alloys |
| US2839394A (en) * | 1953-11-09 | 1958-06-17 | Invetions Aeronautiques Et Mec | Magnesium alloys |
| US2844463A (en) * | 1953-11-09 | 1958-07-22 | Siam | Magnesium-base alloys |
-
1931
- 1931-12-14 US US581050A patent/US1941039A/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2829973A (en) * | 1953-04-09 | 1958-04-08 | Magnesium Elektron Ltd | Magnesium base alloys |
| US2839394A (en) * | 1953-11-09 | 1958-06-17 | Invetions Aeronautiques Et Mec | Magnesium alloys |
| US2844463A (en) * | 1953-11-09 | 1958-07-22 | Siam | Magnesium-base alloys |
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