US2204568A - Magnesium alloy - Google Patents
Magnesium alloy Download PDFInfo
- Publication number
- US2204568A US2204568A US228323A US22832338A US2204568A US 2204568 A US2204568 A US 2204568A US 228323 A US228323 A US 228323A US 22832338 A US22832338 A US 22832338A US 2204568 A US2204568 A US 2204568A
- Authority
- US
- United States
- Prior art keywords
- alloys
- magnesium
- resistance
- magnesium alloy
- strength
- 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
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
-
- 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
- Our invention relates to magnesium alloys, and more particularly to alloys of the class containing aluminium and bismuth.
- Magnesium alloys as known heretofore and having satisfactory resistance to corrosion are not strong, their strength being not much in excess of 30 kilogrammes per square millimeter. It is true that the strength can be increased to about 38 kgnlsq. mm. by suitable heat treatment but this is at the expense of corrosion resistance; ,The corrosion resistance of magnesium alloys is poor per se, and by the segregations which occur during the heat treatment, it is deteriorated to such an extent that the range of usefulness of such comparatively strong alloys is very'limited. Nor does the addition of manganese-which generally increases the resistance to corrosion-exert any favorable influence in the case of the alloys in consideration.
- the remainder of the alloys may be substantially allmagne'sium.
- substantially all magnesium is intended to include magnesium and magnesium with the usual impurities in technical magnesium, and minor amounts of alloying elements, provided that the said constituents are present only in such percentages as not to overstep the limit of solid solubility in the mixed crystal. ents are 0.1 to 1%.
- the usual alloying elements are, for instance, calcium which is added for improving the castability of the alloys; manganese for increasing their resistance to corrosion; or'at least one metal of the iron group, or silicon, for improving the strength of the alloys under high temperature conditions, and for increasing their yield point.
- the alloys Nos. 2 and 3 are particularly good.
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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)
- Powder Metallurgy (AREA)
- Contacts (AREA)
- Prevention Of Electric Corrosion (AREA)
- Heat Treatment Of Steel (AREA)
- Materials For Medical Uses (AREA)
- Soft Magnetic Materials (AREA)
- Cell Electrode Carriers And Collectors (AREA)
- Preventing Corrosion Or Incrustation Of Metals (AREA)
- Cookers (AREA)
- Sampling And Sample Adjustment (AREA)
- Laminated Bodies (AREA)
- Nonmetallic Welding Materials (AREA)
- Non-Reversible Transmitting Devices (AREA)
- Processing Of Solid Wastes (AREA)
- Physical Vapour Deposition (AREA)
Description
Patented June 18, 1940 MAGNESIUM ALLOY Arthur Burkhardt, Berlin-Lichterfelde, and Richard Knabe, Berlin-Zehlendorf, Germany, assignors to Georg Von Giesches Erben,
Breslau, Germany, a No Drawing.
corporation of Germany Application September 3, 1938,
Serial No. 228,323. In Germany September 21,
3 Claims.
Our invention relates to magnesium alloys, and more particularly to alloys of the class containing aluminium and bismuth.
It is an object of our invention to improve a magnesium alloy of the class aforesaid, with a view to increasing its strength, without deteriorating its resistance to corrosion.
Magnesium alloys as known heretofore and having satisfactory resistance to corrosion, are not strong, their strength being not much in excess of 30 kilogrammes per square millimeter. It is true that the strength can be increased to about 38 kgnlsq. mm. by suitable heat treatment but this is at the expense of corrosion resistance; ,The corrosion resistance of magnesium alloys is poor per se, and by the segregations which occur during the heat treatment, it is deteriorated to such an extent that the range of usefulness of such comparatively strong alloys is very'limited. Nor does the addition of manganese-which generally increases the resistance to corrosion-exert any favorable influence in the case of the alloys in consideration.
However, it has been found that the resistance to corrosion is not deteriorated if strength-increasing alloying elements are added in such quantities that such elements prevent the formation of a second phase. In the single-phase alloys thus produced the heterogenous inclusions which act as local elements and are the cause of poor corrosion resistance insecond-phase alloys of high strength, are absent. When such a single-phase alloy is heat treated for increasing its strength, segregation does not occur at the grain boundaries but, in uniform distribution, within the crystals themselves, so that the corresion resistance is not deteriorated.
Starting with these considerations, we have made the surprising discovery that magnesium alloys of the class referred to in which the content of aluminium is 8 to 14%, and the content of bismuth is 2 to 4%, possess very high strength in heat treated condition.
The remainder of the alloys may be substantially allmagne'sium. The phrase substantially all magnesium is intended to include magnesium and magnesium with the usual impurities in technical magnesium, and minor amounts of alloying elements, provided that the said constituents are present only in such percentages as not to overstep the limit of solid solubility in the mixed crystal. ents are 0.1 to 1%.
The usual rates of such constitu- The usual alloying elements are, for instance, calcium which is added for improving the castability of the alloys; manganese for increasing their resistance to corrosion; or'at least one metal of the iron group, or silicon, for improving the strength of the alloys under high temperature conditions, and for increasing their yield point.
Examples of suitable alloys-according to our invention will appear from the following table.
Alloy No. 132 1? gfi gg" he a t ii e t ed, Elfigga percent p c kg/sq. mm. percent It is understood that in all cases the remainder is substantially all magnesium.
The alloys Nos. 2 and 3 are particularly good.
We claim:
nesium.
3. A magnesium alloy containing from 8 to 14 per cent aluminium, 2.5 to 4 per cent bismuth, the remainder substantially all magnesium.
ARTHUR BURKHARDT. RICHARD KNABE.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1937B0178091 DE700517C (en) | 1937-04-16 | 1937-04-16 | Payable magnesium alloy |
DEG96291D DE741507C (en) | 1937-04-16 | 1937-09-22 | Magnesium alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
US2204568A true US2204568A (en) | 1940-06-18 |
Family
ID=34105315
Family Applications (4)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US198690A Expired - Lifetime US2231881A (en) | 1937-04-16 | 1938-03-29 | Magnesium alloy |
US228324A Expired - Lifetime US2226549A (en) | 1937-04-16 | 1938-09-03 | Magnesium alloy |
US228322A Expired - Lifetime US2204567A (en) | 1937-04-16 | 1938-09-03 | Magnesium alloy of high strength |
US228323A Expired - Lifetime US2204568A (en) | 1937-04-16 | 1938-09-03 | Magnesium alloy |
Family Applications Before (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US198690A Expired - Lifetime US2231881A (en) | 1937-04-16 | 1938-03-29 | Magnesium alloy |
US228324A Expired - Lifetime US2226549A (en) | 1937-04-16 | 1938-09-03 | Magnesium alloy |
US228322A Expired - Lifetime US2204567A (en) | 1937-04-16 | 1938-09-03 | Magnesium alloy of high strength |
Country Status (5)
Country | Link |
---|---|
US (4) | US2231881A (en) |
AT (4) | AT158393B (en) |
DE (4) | DE700517C (en) |
FR (5) | FR836327A (en) |
GB (5) | GB489320A (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2824515A (en) * | 1944-02-12 | 1958-02-25 | James C Loftin | Incendiary |
US2507713A (en) * | 1945-07-07 | 1950-05-16 | Olin Mathieson | Fluxing process for magnesium alloys |
US2546931A (en) * | 1949-03-18 | 1951-03-27 | Dow Chemical Co | Magnesium alloy |
US3166415A (en) * | 1960-12-28 | 1965-01-19 | Union Carbide Corp | Magnesium-based alloys |
US3278338A (en) * | 1963-07-23 | 1966-10-11 | Gen Electric | Water-activated battery |
CN1031416C (en) * | 1992-01-08 | 1996-03-27 | 南开大学 | Magnesium-base hydrogenous alloy electrode |
AUPP246998A0 (en) * | 1998-03-20 | 1998-04-09 | Australian Magnesium Corporation Pty Ltd | Magnesium alloying |
WO2010056130A1 (en) * | 2008-11-14 | 2010-05-20 | Auckland Uniservices Limited | Magnesium based alloys and processes for preparation thereof |
CN105132772B (en) * | 2015-10-18 | 2017-05-17 | 河北工业大学 | Low-cost non-rare-earth type high-strength magnesium alloy and preparing method thereof |
CN109182810B (en) * | 2018-11-19 | 2021-03-02 | 河北工业大学 | Low-cost high-room-temperature plastic deformation magnesium alloy and preparation method thereof |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1558066A (en) * | 1921-11-26 | 1925-10-20 | Dow Chemical Co | Method of making light metal alloys |
US1998171A (en) * | 1933-10-04 | 1935-04-16 | Magnesium Dev Corp | Alloy |
US2026589A (en) * | 1933-10-04 | 1936-01-07 | Magnesium Dev Corp | Alloy |
US2026592A (en) * | 1933-10-04 | 1936-01-07 | Magnesium Dev Corp | Alloy |
US2045236A (en) * | 1933-10-04 | 1936-06-23 | Magnesium Dev Corp | Alloy |
US1998168A (en) * | 1933-10-04 | 1935-04-16 | Magnesium Dev Corp | Alloy |
US2045247A (en) * | 1933-10-04 | 1936-06-23 | Magnesium Dev Corp | Alloy |
US2029728A (en) * | 1934-02-12 | 1936-02-04 | Dow Chemical Co | Rolling magnesium alloys |
US2011613A (en) * | 1934-10-06 | 1935-08-20 | Magnesium Dev Corp | Magnesium duplex metal |
-
1937
- 1937-04-16 DE DE1937B0178091 patent/DE700517C/en not_active Expired
- 1937-07-09 AT AT158393D patent/AT158393B/en active
- 1937-08-05 GB GB21646/37A patent/GB489320A/en not_active Expired
- 1937-08-05 GB GB21647/37A patent/GB490712A/en not_active Expired
- 1937-09-22 DE DEG96290D patent/DE732188C/en not_active Expired
- 1937-09-22 DE DEG96289D patent/DE712922C/en not_active Expired
- 1937-09-22 DE DEG96291D patent/DE741507C/en not_active Expired
- 1937-12-07 AT AT160440D patent/AT160440B/en active
- 1937-12-12 AT AT160729D patent/AT160729B/en active
-
1938
- 1938-03-29 US US198690A patent/US2231881A/en not_active Expired - Lifetime
- 1938-04-07 FR FR836327D patent/FR836327A/en not_active Expired
- 1938-04-07 FR FR836328D patent/FR836328A/en not_active Expired
- 1938-09-03 US US228324A patent/US2226549A/en not_active Expired - Lifetime
- 1938-09-03 US US228322A patent/US2204567A/en not_active Expired - Lifetime
- 1938-09-03 US US228323A patent/US2204568A/en not_active Expired - Lifetime
- 1938-09-12 FR FR843310D patent/FR843310A/en not_active Expired
- 1938-09-12 FR FR843312D patent/FR843312A/en not_active Expired
- 1938-09-12 FR FR843311D patent/FR843311A/en not_active Expired
- 1938-09-13 GB GB26702/38A patent/GB519302A/en not_active Expired
- 1938-09-14 GB GB26823/38A patent/GB504602A/en not_active Expired
- 1938-09-14 GB GB26822/38A patent/GB519304A/en not_active Expired
-
1943
- 1943-02-25 AT AT160903D patent/AT160903B/en active
Also Published As
Publication number | Publication date |
---|---|
GB490712A (en) | 1938-08-19 |
FR843311A (en) | 1939-06-30 |
AT160729B (en) | 1941-12-10 |
US2226549A (en) | 1940-12-31 |
US2231881A (en) | 1941-02-18 |
AT160440B (en) | 1941-05-26 |
DE732188C (en) | 1943-03-02 |
GB504602A (en) | 1939-04-27 |
AT158393B (en) | 1940-04-10 |
FR843312A (en) | 1939-06-30 |
GB519304A (en) | 1940-03-21 |
FR836328A (en) | 1939-01-16 |
GB489320A (en) | 1938-07-25 |
DE700517C (en) | 1940-12-21 |
GB519302A (en) | 1940-03-21 |
FR843310A (en) | 1939-06-30 |
DE741507C (en) | 1943-11-12 |
DE712922C (en) | 1941-10-28 |
US2204567A (en) | 1940-06-18 |
FR836327A (en) | 1939-01-16 |
AT160903B (en) | 1943-08-24 |
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