US1992655A - Alloy - Google Patents

Alloy Download PDF

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Publication number
US1992655A
US1992655A US709970A US70997034A US1992655A US 1992655 A US1992655 A US 1992655A US 709970 A US709970 A US 709970A US 70997034 A US70997034 A US 70997034A US 1992655 A US1992655 A US 1992655A
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US
United States
Prior art keywords
magnesium
antimony
alloy
per cent
metal
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
US709970A
Inventor
Edward F Fischer
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.)
MAGNESIUM DEV CORP
MAGNESIUM DEVELOPMENT Corp
Original Assignee
MAGNESIUM DEV CORP
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 MAGNESIUM DEV CORP filed Critical MAGNESIUM DEV CORP
Priority to US709970A priority Critical patent/US1992655A/en
Application granted granted Critical
Publication of US1992655A publication Critical patent/US1992655A/en
Anticipated expiration legal-status Critical
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

Definitions

  • a particular object is to improve the strength of the metal without substantially diminishing its ductility.
  • the weight of the alloy does not differ substantially from that of the unalloyed metal.
  • magnesium-antimony alloys herein described may be readily extruded under the same conditions employed in handling the 35 pure metal while at the same time a material is obtained which has appreciably higher strength values than the pure magnesium.
  • a magnesium-antimony alloy, for example, containing about 1 per cent of antimony had a tensile strength of about 33,600 pounds per square inch and an elongation of about 3.5 per cent in two inches in the as-extruded condition.
  • An increase in the antimony content of 4 per cent served further increase the strength, a value of abo 36,400 pounds per square inch being obtained.
  • the elongation inthis case was 5 per cent, somewhat more than in the alloy of lower antimony content.
  • the alloy may be prepared in any manner knownto those skilled in the art but preferably I use a rich alloy? for the purpose of adding the antimony because of the vigorous action between molten magnesium and metallic antimony.
  • a rich alloy obviates this dificulty to a great extent.
  • magnesium refers to the commercially available metal.
  • a magnesium base alloy composed of magnesium and from about 0.5 to 5 per cent of antimony.
  • a magnesium base alloy composed of magnesium and from about 1 to 4 per cent of antimony.
  • a magnesium base alloy consisting of magnesium and about 1 per cent antimony.
  • a magnesium base alloy consisting of magnesium and about 4 per cent antimony.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Extrusion Of Metal (AREA)

Description

Patente Fe. Z6, 13
a m as a...
armon Edward F. Fischer, Cleveland, (Dhio, assignor, by
mesne assignments, to Magnesium Development Corporation, a corporation of Delaware No Drawing. Application February 6, 1934,
Serial No. 709,970
4 Claims. (ill. 35-1) of the metal, the tensile strength in the as cast con-' dition being about 13,000 pounds per square inch while the rolled metal only has a tensile strength of about 25,000 pounds per square inch. Such 1 limitations in strength have restricted the wider use of the metal.
It is an object of my invention to utilize the inherently advantageous properties of the pure metal and at the same time to overcome some 20 of the handicaps. A particular object is to improve the strength of the metal without substantially diminishing its ductility.
I have found that from about 0.5 to per cent of antimony can be added to magnesium thereby 25 causing a surprisingly large increase in strength;
The weight of the alloy does not differ substantially from that of the unalloyed metal.
For many purposes an extruded product is desirable either by reason of low production cost 30 or because the intricate shape of the article renders difficult other methods of working. I have found that the magnesium-antimony alloys herein described may be readily extruded under the same conditions employed in handling the 35 pure metal while at the same time a material is obtained which has appreciably higher strength values than the pure magnesium. A magnesium-antimony alloy, for example, containing about 1 per cent of antimony had a tensile strength of about 33,600 pounds per square inch and an elongation of about 3.5 per cent in two inches in the as-extruded condition. An increase in the antimony content of 4 per cent served further increase the strength, a value of abo 36,400 pounds per square inch being obtained. The elongation inthis case was 5 per cent, somewhat more than in the alloy of lower antimony content. For most purposes I prefer to use between about 1 and 4 percent of antimony.
The alloy may be prepared in any manner knownto those skilled in the art but preferably I use a rich alloy? for the purpose of adding the antimony because of the vigorous action between molten magnesium and metallic antimony. The use of a rich alloy obviates this dificulty to a great extent.
The term magnesium as used herein and in the appended claims refers to the commercially available metal.
I claim:
. 1. A magnesium base alloy composed of magnesium and from about 0.5 to 5 per cent of antimony.
2. A magnesium base alloy composed of magnesium and from about 1 to 4 per cent of antimony.
3. A magnesium base alloy consisting of magnesium and about 1 per cent antimony.
4. A magnesium base alloy consisting of magnesium and about 4 per cent antimony.
- EDWARD F. FISCHER.
US709970A 1934-02-06 1934-02-06 Alloy Expired - Lifetime US1992655A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US709970A US1992655A (en) 1934-02-06 1934-02-06 Alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US709970A US1992655A (en) 1934-02-06 1934-02-06 Alloy

Publications (1)

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US1992655A true US1992655A (en) 1935-02-26

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Family Applications (1)

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US709970A Expired - Lifetime US1992655A (en) 1934-02-06 1934-02-06 Alloy

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2753723A1 (en) * 1996-09-21 1998-03-27 Daimler Benz Ag USE OF A MAGNESIUM-BASED MATERIAL

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2753723A1 (en) * 1996-09-21 1998-03-27 Daimler Benz Ag USE OF A MAGNESIUM-BASED MATERIAL
US6264762B1 (en) 1996-09-21 2001-07-24 Daimlerchrysler Ag Corrosion resistant magnesium compositions and applications thereof

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