US2224151A - Magnesium alloys - Google Patents

Magnesium alloys Download PDF

Info

Publication number
US2224151A
US2224151A US189645A US18964538A US2224151A US 2224151 A US2224151 A US 2224151A US 189645 A US189645 A US 189645A US 18964538 A US18964538 A US 18964538A US 2224151 A US2224151 A US 2224151A
Authority
US
United States
Prior art keywords
beryllium
alloys
zirconium
magnesium
alloy
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
Application number
US189645A
Inventor
Gauthier Gaston
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.)
Compagnie de Produits Chimiques et Electrometallurgiques Alais Froges et Camargue
Original Assignee
Compagnie de Produits Chimiques et Electrometallurgiques Alais Froges et Camargue
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Compagnie de Produits Chimiques et Electrometallurgiques Alais Froges et Camargue filed Critical Compagnie de Produits Chimiques et Electrometallurgiques Alais Froges et Camargue
Application granted granted Critical
Publication of US2224151A publication Critical patent/US2224151A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S122/00Liquid heaters and vaporizers
    • Y10S122/13Tubes - composition and protection

Definitions

  • magnesium base alloys It is a well known disadvantage of magnesium base alloys that they are liable to progressive oxidation when in the molten state and that they are also subject to superficial oxidation when in 5 the solid state, particularly at relatively high temperatures such as for instance higher than 300 C.
  • the alloys containing beryllium have low mechanical strength properties and particularly fatigue strength; moreover, when a thermal treatment of the metal or alloy is required, then the coarse-grain texture necessitates a much longer duration of such treatment than otherwise would be required.
  • zirconium in magnesium base alloys containing beryllium has the effect of imparting thereto, on solidification, a fine-grain structure without in any way impairing the resistance to oxidation due to the presence of the beryllium.
  • the joint presence of zirconium in the alloy avoids the undesirable reduction in mechanical properties imparted thereto by the presence of the beryllium, the mechanical strength properties being at least equal to those of the original metal or alloy containing neither beryllium nor. zirconium.
  • beryllium can be present in the metal or alloys in amounts lying between 0.005 and 0.5% while zirconium is present in amounts lying between 0.005 and 0.5%.
  • the present invention provides a magnesium base alloy containing both beryllium and zirconium, preferably each in an amount lying between 0.005 and 0.5%.
  • Theinvention also provides a process of grainrefining magnesium base alloys containing beryllium, which consists in adding zirconium to said alloys.
  • the zirconium can be added either in making 15 up the alloys or when remelting ingots or scrap.
  • the zirconium may be introduced in any desired manner, for example in the form pro-alloys, or in the form of salts of zirconium which are adapted to be reduced to metal in contact with the molten magnesium or magnesium base alloys.
  • the alloys of the present invention can even be melted without use .of a flux. Due to the decreased liability to oxidation of the molten alloy, losses by burning arereduced to a minimum and when no flux is used, salt inclusions in the metal, and therefore with their attendant risks of corrosion are impossible.
  • a further advantage arising out of the invention is that when subjecting the alloys to heat treatment, the duration of the latter is the same as that for the same alloy, containing neither beryllium nor zirconium. In addition the parts subjected to the heat treatment do not become oxidised and retain their original lustre.
  • a magnesium base alloy containing about 0.025% beryllium and about 0.05% zirconium characterized by a refined grain structure and by mechanical properties at least equal to those of the same alloy without beryllium.

Landscapes

  • 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 Dec. 10, 1940 UNITED STATES PATENT OFFICE I 2,224,151 MAGNESIUM ALLOYS No Drawing. Application February 9, 1938, Se-
rial No. 189,645. In France February 16, 1937 4 Claims.
It is a well known disadvantage of magnesium base alloys that they are liable to progressive oxidation when in the molten state and that they are also subject to superficial oxidation when in 5 the solid state, particularly at relatively high temperatures such as for instance higher than 300 C.
In order to reduce the liability of magnesium base alloys to oxidation it has been proposed to incorporate small quantities of calcium in the alloys. It has also been suggested that the addition of small quantities of beryllium to'such alloys reduces their liability to oxidation, and it is true that the effect of an addition of beryllium in respect of this liability to oxidation is far more pronounced than that of corresponding amounts of calcium. On the other hand it'has been observed that the incorporation of beryllium in magnesium. or magnesium base alloys imparts to the metal on solidification an extremely coarsegrain texture as compared with the corresponding metals in which beryllium is absent. Owing tothis coarse-grain texture, the alloys containing beryllium have low mechanical strength properties and particularly fatigue strength; moreover, when a thermal treatment of the metal or alloy is required, then the coarse-grain texture necessitates a much longer duration of such treatment than otherwise would be required.
It is an object of the present invention to provide magnesium base alloys containing beryllium in which the favourable known effects of beryllium as an inhibitor of oxidation are preserved, while at the same time avoiding the tendency to coarse-grain crystallisation otherwise observable in magnesium alloys containing beryllium.
I have found that the presence of zirconium in magnesium base alloys containing beryllium has the effect of imparting thereto, on solidification, a fine-grain structure without in any way impairing the resistance to oxidation due to the presence of the beryllium. At the same time, the joint presence of zirconium in the alloy avoids the undesirable reduction in mechanical properties imparted thereto by the presence of the beryllium, the mechanical strength properties being at least equal to those of the original metal or alloy containing neither beryllium nor. zirconium.
By way of example, beryllium can be present in the metal or alloys in amounts lying between 0.005 and 0.5% while zirconium is present in amounts lying between 0.005 and 0.5%.
It has been found that a content of 0.025% of beryllium imparts to the alloy 8. sufllcient resistance to oxidation for all practical purposes, while a zirconium content of 0.05% is sumcient to counteract the disadvantages caused by the presence of that amount of beryllium in the alloy.
Based on the foregoing observations, the present invention provides a magnesium base alloy containing both beryllium and zirconium, preferably each in an amount lying between 0.005 and 0.5%.
Theinvention also provides a process of grainrefining magnesium base alloys containing beryllium, which consists in adding zirconium to said alloys.
The zirconium can be added either in making 15 up the alloys or when remelting ingots or scrap.
The zirconium may be introduced in any desired manner, for example in the form pro-alloys, or in the form of salts of zirconium which are adapted to be reduced to metal in contact with the molten magnesium or magnesium base alloys.
The alloys of the present invention can even be melted without use .of a flux. Due to the decreased liability to oxidation of the molten alloy, losses by burning arereduced to a minimum and when no flux is used, salt inclusions in the metal, and therefore with their attendant risks of corrosion are impossible.
A further advantage arising out of the invention is that when subjecting the alloys to heat treatment, the duration of the latter is the same as that for the same alloy, containing neither beryllium nor zirconium. In addition the parts subjected to the heat treatment do not become oxidised and retain their original lustre.
What I claim is: l
1. A magnesium base alloy containing between about 0.005% and 0.5% beryllium and between about 0.005% and 0.5% zirconium characterized by a refined grain structure and by mechanical properties at least equal to those of the same alloy without beryllium.
2. A magnesium base alloy containing about 0.025% beryllium and about 0.05% zirconium characterized by a refined grain structure and by mechanical properties at least equal to those of the same alloy without beryllium.
3. A magnesium base alloy containing between about 0.005% and 0.5% beryllium and. between about 0.005% and 0.5% zirconium, the balance I being substantially all magnesium.
4. A magnesium base alloy containing about 0.025% beryllium and about 0.05 zirconium, the balance being substantially all magnesium. Y
GASTON GAUTHIER.
US189645A 1937-02-16 1938-02-09 Magnesium alloys Expired - Lifetime US2224151A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR2224151X 1937-02-16

Publications (1)

Publication Number Publication Date
US2224151A true US2224151A (en) 1940-12-10

Family

ID=9684596

Family Applications (1)

Application Number Title Priority Date Filing Date
US189645A Expired - Lifetime US2224151A (en) 1937-02-16 1938-02-09 Magnesium alloys

Country Status (1)

Country Link
US (1) US2224151A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2461229A (en) * 1944-07-11 1949-02-08 Magnesium Elektron Ltd Method of producing magnesium base alloys
US2497551A (en) * 1946-05-17 1950-02-14 Magnesium Elektron Ltd Composition for introducing zirconium and beryllium solubly into magnesium
US2609309A (en) * 1948-10-07 1952-09-02 Jerzy W Meier Magnesium alloy and method of treatment
US2849311A (en) * 1952-01-22 1958-08-26 Aluminum Co Of America Method of making magnesium-zirconium master alloy
US2882145A (en) * 1954-12-28 1959-04-14 Lucien Rene Magnesium alloys
US3094413A (en) * 1960-09-14 1963-06-18 Magnesium Elektron Ltd Magnesium base alloys

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2461229A (en) * 1944-07-11 1949-02-08 Magnesium Elektron Ltd Method of producing magnesium base alloys
US2497551A (en) * 1946-05-17 1950-02-14 Magnesium Elektron Ltd Composition for introducing zirconium and beryllium solubly into magnesium
US2609309A (en) * 1948-10-07 1952-09-02 Jerzy W Meier Magnesium alloy and method of treatment
US2849311A (en) * 1952-01-22 1958-08-26 Aluminum Co Of America Method of making magnesium-zirconium master alloy
US2882145A (en) * 1954-12-28 1959-04-14 Lucien Rene Magnesium alloys
US3094413A (en) * 1960-09-14 1963-06-18 Magnesium Elektron Ltd Magnesium base alloys

Similar Documents

Publication Publication Date Title
US2336512A (en) Aluminum base alloy
US2224151A (en) Magnesium alloys
US1558066A (en) Method of making light metal alloys
US2253502A (en) Malleable iron
US2204568A (en) Magnesium alloy
US2304353A (en) Heat resistant alloy
US2683662A (en) Manufacture of iron and steel and products obtained
US2317980A (en) Magnesium-base alloy
US2280170A (en) Aluminum alloy
US1745721A (en) Bearing metal
US2280174A (en) Aluminum alloy
US3369893A (en) Copper-zinc alloys
US2357451A (en) Aluminum alloy
US1718502A (en) Copper-aluminum alloy
US2948608A (en) Heat treatable alloys of titanium or zirconium
US2046380A (en) Copper base alloys
US2293864A (en) Aluminum base alloy
US2231940A (en) Alloy
US1869378A (en) Britannia metal or pewter alloy
EP0088114B1 (en) Improved addition agent for cast iron
US1567066A (en) Nickel-copper alloy
US2280173A (en) Aluminum alloy
US2763546A (en) Aluminum base bearing
US3634076A (en) Die-casting alloy compositions
US1731212A (en) Gold alloy