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US1273762A - Alloy. - Google Patents

Alloy. Download PDF

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Publication number
US1273762A
US1273762A US17073317A US17073317A US1273762A US 1273762 A US1273762 A US 1273762A US 17073317 A US17073317 A US 17073317A US 17073317 A US17073317 A US 17073317A US 1273762 A US1273762 A US 1273762A
Authority
US
United States
Prior art keywords
iron
alloy
aluminum
zinc
magnesium
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
US17073317A
Inventor
Truman S Fuller
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Priority to US17073317A priority Critical patent/US1273762A/en
Application granted granted Critical
Publication of US1273762A publication Critical patent/US1273762A/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
    • C22C21/00Alloys based on aluminium
    • C22C21/10Alloys based on aluminium with zinc as the next major constituent

Definitions

  • An dlloy containing aluminum, at least several per cent. of zinc, at least about onehalf per cent. ofmagnesium and at least aboutone per cent. of iron. 1
  • An alloy containing aluminum at'least several per cent. of zinc, at least about onehalf per cent. of magnesium and/about one to three per cent. of iron.
  • An alloy consisting of about 6 to 12 per cent. of zinc, about a to 2% percent. of magnesium, about 1 to 3 per cent.'of iron and the balance of aluminum.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Diaphragms For Electromechanical Transducers (AREA)

Description

UNIT D STATES PATENT OFFICE.
TRUMAN s. FULLER,- 0F SGHENECTADY, NEW YORK, AssIeNoR T0 GENERAL ELECTRIC COMPANY, A CORPORATION OF NEW YORK.
y ALLOY.
Specification of Letters Patent.
Patented July 23, 1918.
Application filed May 24, 1917. Serial No. 170,733.
To all whom it may concern:
Be it known that I, TRUMAN S. FULLER,
a citizen of the United States, residing at Schenectady, county of Schenectady, State of New York, have invented certain new and .alloy containing 'aluminum magnesium', zinc and either iron, chromium, cobalt, nickel, titanium or manganese, or a mixture of the same.
The addition of iron or one of the abovedescribed equivalents increases the tensile strength, hardness and stifiness of alloys containing aluminum, magnesium and zinc. Preferably the metal of theiron group is present in amounts of about 1 to 3%.
When preparing an alloy embodying my invention, containlng iron for example, the
aluminum is melted and the iron is added either as substantially pure iron, or as an alloy of aluminum and iron, until a homogeneous alloy containing the desired amount of iron is produced by the solution of the iron in the aluminum. The desired propor tion of zinc is then added to the melted alloy. Finally the magnesium is added and the alloy is immediately cooled as by casting or in any suitable manner. Alloys containing chromium, cobalt, nickel, titanium or manganese may be made in a similar mannese, the balance totaling 100% consisting of aluminum, although these proportions maybe departed'from when special properties for special uses are desired.
The following specific examples illustrate the improvement in tensile strength effected by iron or equivalent metal. An alloy consisting of about 92.7 5% aluminum, 6% zinc, 1.25% magnesium has an ultimate tensile strength of about 46,100 pounds per sq. in. An alloy of 90.75% aluminum, 6% zinc, 1.25% magnesium and 2% iron has an ultimate tensile strength of 69,600 pounds. In other words, thesubstitution'of 2% aluminum by 2% iron effects an increase in tensile strength of over 50%. An alloy of 86.75% aluminum, 12% zincand 1.25% magnesium has an ultimate tensile strength of 53,600 pounds. By replacing 3% of the aluminum by 3% iron the ultimate tensile strengthis increased to 63,000 poundsor 1 about 18%.
I desire by the appended claims to cover not only an alloy of aluminum, magnesium, zinc and iron but also metals equivalent to iron for this purpose, such as chromium,
cobalt, nickel, titanium or manganese.
What I claim as new and desire to secure by Letters Patent of the United States,'is,-
1. An dlloy containing aluminum, at least several per cent. of zinc, at least about onehalf per cent. ofmagnesium and at least aboutone per cent. of iron. =1
2. An alloy containing aluminum) at'least several per cent. of zinc, at least about onehalf per cent. of magnesium and/about one to three per cent. of iron.
3. An alloy consisting of about 6 to 12 per cent. of zinc, about a to 2% percent. of magnesium, about 1 to 3 per cent.'of iron and the balance of aluminum.
..In witness whereof, I have hereunto set my hand this 23rd day of May, 1917.
TRUMAN S. FULLER.
US17073317A 1917-05-24 1917-05-24 Alloy. Expired - Lifetime US1273762A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US17073317A US1273762A (en) 1917-05-24 1917-05-24 Alloy.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US17073317A US1273762A (en) 1917-05-24 1917-05-24 Alloy.

Publications (1)

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US1273762A true US1273762A (en) 1918-07-23

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Family Applications (1)

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US17073317A Expired - Lifetime US1273762A (en) 1917-05-24 1917-05-24 Alloy.

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2808327A (en) * 1953-04-14 1957-10-01 Us Reduction Co Method of deoxidizing steel with aluminum base alloy
US6368427B1 (en) 1999-09-10 2002-04-09 Geoffrey K. Sigworth Method for grain refinement of high strength aluminum casting alloys
US6645321B2 (en) 1999-09-10 2003-11-11 Geoffrey K. Sigworth Method for grain refinement of high strength aluminum casting alloys

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2808327A (en) * 1953-04-14 1957-10-01 Us Reduction Co Method of deoxidizing steel with aluminum base alloy
US6368427B1 (en) 1999-09-10 2002-04-09 Geoffrey K. Sigworth Method for grain refinement of high strength aluminum casting alloys
US6645321B2 (en) 1999-09-10 2003-11-11 Geoffrey K. Sigworth Method for grain refinement of high strength aluminum casting alloys

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