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US1572489A - Aluminum alloy - Google Patents

Aluminum alloy Download PDF

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Publication number
US1572489A
US1572489A US426793A US42679320A US1572489A US 1572489 A US1572489 A US 1572489A US 426793 A US426793 A US 426793A US 42679320 A US42679320 A US 42679320A US 1572489 A US1572489 A US 1572489A
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US
United States
Prior art keywords
per cent
silicon
copper
alloy
aluminum
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
US426793A
Inventor
Roderick L Johnston
Robert S Archer
Jeffries Zay
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.)
Alcoa Corp
Original Assignee
Aluminum Company of America
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 Aluminum Company of America filed Critical Aluminum Company of America
Priority to US426793A priority Critical patent/US1572489A/en
Priority to FR543938D priority patent/FR543938A/en
Priority to US8517A priority patent/US1572490A/en
Application granted granted Critical
Publication of US1572489A publication Critical patent/US1572489A/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
    • C22C21/02Alloys based on aluminium with silicon as the next major constituent

Definitions

  • the metals capable of forming solid solutions in the aluminum we have found copper and zinc particularly advantageous.
  • the metals referred to may be used singly or in combination
  • the silicon content of the alloy should in general be not less than about 3 per cent nor more than about 10 per cent, and the copper should be preferably from about 2 per cent to. about 5 per cent; the proportions of copper and silicon being variable, however, according to the particular combination of properties desired.
  • the attainment of good casting qualities depends largely upon the relative proportions of the silicon and copper, the latter being preferably reduced as the former is increased, and vice versa.
  • Such a bar after heat treatment by the method described in the above mentioned application, showed an increase of tensile strength up to 30,000 pounds per square inch and an increase of elongation up to 2.5 per cent.
  • a similar bar, heat treated had a tensile strength of 40,000 pounds per square inch and 6 per cent elongation.
  • a chill-cast heat-treated bar of an alloy containing about 6 per cent silicon and about 4 per cent copper was found to have a tensile strength exceeding 42,000 pounds per square inch and an elongation exceeding 8 per cent in 2 inches.
  • alloys described herein are also well adapted to forging and like operations.
  • An-alloy composed chiefly of aluminum, containing a substantial amount of silicon and substantial amounts of copper and zinc.
  • An alloy composed chiefly of aluminum, containing between 3 and 10 per cent silicon, approximately, and substantial amounts of copper and zinc.
  • An alloy composed chiefly of aluminum, containing between 3 and 10 per cent silicon, approximately, copper between 2 and 5 per cent, approximately, and asubstantial amount of zinc.
  • An alloy composed chiefly of aluminum, containing between 3 andlO per cent silicon, approximately, a substantial amount of copper, and zinc between 5' and'15 per cent, approximately.
  • An alloy composed chiefly of aluminum and low in iron, containing copper between 2 and 5 per cent, and silicon between 3 and 10 per cent, approximately.
  • An alloy composed chiefly. of aluminum, containing copper between 2 and 5 per cent, and silicon between 3 and 10 per cent, approximately, with an iron content not exceeding about 0.6 per cent.

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

Description

Patented Feb. 9, 1926.
UNITED STATES PATENT OFFICE.
RODERICK L. JOHNSTON, NEW YORK, N. 'Y., RCBERT S. ARCHER, OF EAST CLEVE- LAND, AND ZAY JEFFRIES, F CLEVELAND HEIGHTS, OHIO, ASSIGNORS TO ALUMINUM COMPANY OF AMERICA, OF PITTSBURGH, PENNSYLVANIA A. COR- PORATION OF PENNSYLVANIA.
ALUMINUM ALLOY.
No Drawing.
T 0 all whom it may concern: 7
Be it known that we, RODERICK L. J OHN- STON, ROBERT S. ARCHER, and ZAY Jnrrnms, all citizens of the United States, the said Johnston residing at New York, Kings County, State of New York, and the remaining two at East Cleveland and Cleveland Heights, respectively, in the county of Cuyahoga and State of Ohio, have invented 10 certain new and useful Improvements in Aluminum Alloys, of which the following is a full, clear, and exact description.
The presence of small amounts of silicon in aluminum and in aluminum alloys is usually considered objectionable. In the course of an investigation upon the effects of silicon we have discovered that by using a substantial amount of silicon, materially greater than the quantity usually found as 'an impurity, with the addition of a metal or metals, for example one or more of those hereinafter named, it'is possible to produce an alloy having excellent casting qualities combined with good physical properties.
Among the metals capable of forming solid solutions in the aluminum we have found copper and zinc particularly advantageous. The metals referred to may be used singly or in combination In the use of copper alone, the silicon content of the alloy should in general be not less than about 3 per cent nor more than about 10 per cent, and the copper should be preferably from about 2 per cent to. about 5 per cent; the proportions of copper and silicon being variable, however, according to the particular combination of properties desired. In general, the attainment of good casting qualities depends largely upon the relative proportions of the silicon and copper, the latter being preferably reduced as the former is increased, and vice versa. Increasing the copper, at least up to the limit of its capacity for entering into solid solution in the aluminum, tends in general to increase the tensile strength, especially if subjected to a suitable heat treatment, say that described in the copending application r of Zay J eifries and Robert S. Archer, Serial No. 435,024. A test bar cast in sand in the ordinary way, of an-aluminum alloy con- Applieation filed November 27, 1920. Serial No. 426,793.
taining 10 per cent silicon and 3 per cent copper, showed a tensile strength of about 23,000 pounds per square inch and an elongation of about 1.5 per cent in two inches.
Such a bar, after heat treatment by the method described in the above mentioned application, showed an increase of tensile strength up to 30,000 pounds per square inch and an increase of elongation up to 2.5 per cent. A bar of the same alloy but cast in a chill mold, in order to cause rapid solidification of the molten metal, was found to have a tensile strength of about 30,000 pounds per square inch and an elongation of about 2.7 per cent, even without heat treatment. A similar bar, heat treated, had a tensile strength of 40,000 pounds per square inch and 6 per cent elongation. On the other hand, a chill-cast heat-treated bar of an alloy containing about 6 per cent silicon and about 4 per cent copper was found to have a tensile strength exceeding 42,000 pounds per square inch and an elongation exceeding 8 per cent in 2 inches.
The addition of zinc up to about 5 per cent has a slight effect on the tensile strength of the alloy. Above that amount a greater increase of tensile strength is observed. The presence of the zinc is often an advantage by reason of the whiter color of the polished alloy. We have found that with the addition of an alkali metal or metals to the alloy, as described in the copending application of Junius D. Edwards, Francis (J. Frary and Harry V. Churchill, Serial No. 426,796, now Patent No. 1,410,461, issued March 21, 1922, very satisfactory physical properties can be obtained alongwith the other advantages incident to the presence of the zinc, particularly if the alloy to which alkali metal has been added is cast in such a manner, as for example by the use of a chill mold, that the molten metal is caused to solidify rapidly. For instance, an alloy containing about 10 per cent zinc and about 8 per cent silicon, to which alkali metal had been added and which was cast in a chill mold, has been found to have a tensile strength exceeding 42,000 pounds per square inch, with an elongation up to 7 per cent in two inches. A similar casting, after being subjected to In the case of aluminum-silicon alloys containing both copper and zinc, a sand cast test bar of an alloy containing 8 per cent silicon,*10 per cent zinc and 2.5 per cent copper, was found to have a tensile strength of 27,000 pounds per square inch and an elongation of 1.5 per cent. This alloy is also susceptible to improvement by addition of alkali metal before casting; sand cast specimens-of the alloy so treated having a tensile strength of 30,000 pounds per square inch with an elongation of 2 per cent, while chill'cast specimens have a tensile strength of 38,000 pounds per square inch and an elongation of 3.5 percent. Heat treatment by the method described in the application of Archer and Jeflries before-referred to has been found to increase the tensile strength of the chill cast alloy up to 45,000 pounds per square inch and at the same time increase the elongation to 7.5 per cent.
In the alloys referred to above we have observed that the elongation is better if the iron content is low, and for that reason there are many cases where the iron should not exceed about 0.6 per cent. In other cases much higher iron can be used, especially in chill castings, as for example pressure die castings.
The alloys described herein are also well adapted to forging and like operations.
We claim:
1. An-alloy composed chiefly of aluminum, containing a substantial amount of silicon and substantial amounts of copper and zinc.
2. An alloy composed chiefly of aluminum,
containing a substantial amount of silicon,
copper not exceeding about 5 per cent, and a substantial amount of zinc.
3. An alloy composed chiefly of aluminum, containing a substantial amount of silicon,
containing silicon in substantial amount but not exceeding about 10 per cent, and substantial amounts of copper and zinc.
6. An alloy composed chiefly of aluminum, containing between 3 and 10 per cent silicon, approximately, and substantial amounts of copper and zinc.
7 An alloy composed chiefly of aluminum, containing between 3 and 10 per cent silicon, approximately, copper between 2 and 5 per cent, approximately, and asubstantial amount of zinc.
8. An alloy composed chiefly of aluminum, containing between 3 andlO per cent silicon, approximately, a substantial amount of copper, and zinc between 5' and'15 per cent, approximately.
9. An alloy composed chiefly of aluminum and low in iron, containing copper between 2 and 5 per cent, and silicon between 3 and 10 per cent, approximately.
10. An alloy composed chiefly of aluminum. and low in iron, containing 4 percent copper and 6 per cent silicon, approximately.
11. An alloy composed chiefly of aluminum, containing a substantial amount of silicon and substantial amounts of copper and zinc, with an iron content not exceeding about 0.6 per cent.
12. An alloy composed chiefly. of aluminum, containing copper between 2 and 5 per cent, and silicon between 3 and 10 per cent, approximately, with an iron content not exceeding about 0.6 per cent.
-In testimony whereof we hereto afiix our signatures.
RODERICK L. JOHNSTON. ROBERT S. ARCHER. ZAY .JEFFRIES.
US426793A 1920-11-27 1920-11-27 Aluminum alloy Expired - Lifetime US1572489A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US426793A US1572489A (en) 1920-11-27 1920-11-27 Aluminum alloy
FR543938D FR543938A (en) 1920-11-27 1921-11-26 Improvements to metal alloys
US8517A US1572490A (en) 1920-11-27 1925-02-11 Aluminum alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US426793A US1572489A (en) 1920-11-27 1920-11-27 Aluminum alloy

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US1572489A true US1572489A (en) 1926-02-09

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US8517A Expired - Lifetime US1572490A (en) 1920-11-27 1925-02-11 Aluminum alloy

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2568179A (en) * 1949-04-12 1951-09-18 William F Jobbins Inc Aluminum base alloys
US2568180A (en) * 1949-04-12 1951-09-18 William F Jobbins Inc Aluminum base alloys
US2584772A (en) * 1949-05-10 1952-02-05 William F Jobbins Inc Aluminum base alloys

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2568179A (en) * 1949-04-12 1951-09-18 William F Jobbins Inc Aluminum base alloys
US2568180A (en) * 1949-04-12 1951-09-18 William F Jobbins Inc Aluminum base alloys
US2584772A (en) * 1949-05-10 1952-02-05 William F Jobbins Inc Aluminum base alloys

Also Published As

Publication number Publication date
FR543938A (en) 1922-09-12
US1572490A (en) 1926-02-09

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