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US2204568A - Magnesium alloy - Google Patents

Magnesium alloy Download PDF

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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
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US
United States
Prior art keywords
alloys
magnesium
resistance
magnesium alloy
strength
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Expired - Lifetime
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US228323A
Inventor
Burkhardt Arthur
Knabe Richard
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GEORG VON GIESCHE S ERBEN
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GEORG VON GIESCHE S ERBEN
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Publication of US2204568A publication Critical patent/US2204568A/en
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Expired - Lifetime legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • C22C23/02Alloys 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.
US228323A 1937-04-16 1938-09-03 Magnesium alloy Expired - Lifetime US2204568A (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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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