US2526227A - Aluminum base alloy - Google Patents

Aluminum base alloy Download PDF

Info

Publication number
US2526227A
US2526227A US40013A US4001348A US2526227A US 2526227 A US2526227 A US 2526227A US 40013 A US40013 A US 40013A US 4001348 A US4001348 A US 4001348A US 2526227 A US2526227 A US 2526227A
Authority
US
United States
Prior art keywords
per cent
aluminum base
base alloy
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
US40013A
Inventor
Erik G Grundstrom
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US40013A priority Critical patent/US2526227A/en
Application granted granted Critical
Publication of US2526227A publication Critical patent/US2526227A/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
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent
    • C22C21/08Alloys based on aluminium with magnesium as the next major constituent with silicon

Definitions

  • This invention relates to aluminum base alloys, and particularly to alloys of this type containing magnesium, silicon, zinc, titanium, and chromium.
  • An object of the invention is to provide an aluminum base alloy of greatly improved fluidity, so as to be especially suitable for the making of castings jg, sand, or in semi-permanent or permanent molds.
  • a further object of the invention is to provide an alloy as specified in the last preceding paragraph exceptionally free from surface pitting.
  • a further object of the invention is to provide an alloy as above defined and characterized and of greatly improved corrosion resistance.
  • a further object of the invention is to provide an aluminum base alloy suitable forthe making of cast cooking utensils.
  • alloys which come within the limits herein disclosed, and defined by the appended claims, may be used for many adaptationswhere good casting properties, including high fluidity, are-desired, and more particularly where good corrosion resistance and freedom from surface pitting are regarded as important. 7
  • An aluminum base alloy characterized by excellent casting characteristics,corrosion resistance, and freedom from. shrinkage cracks and pitting in the cast condition, and containing from 1.75 per cent to 2.25 per cent of silicon, from 0.3 per cent to 0.75 per cent of zinc, from 2.75 per cent to 3.25 per cent of magnesium, from 0.08
  • An aluminum base alloy characterized by excellent casting characteristics, corrosion resistance, and freedom from shrinkage cracks and,
  • the alloy comprises a major portion of any conventional, commercially available grade of about 3.0 per cent of magnesium, about 0.1 per cent of titanium, and about 0.15 per cent of chromium, the'balance being aluminum.

Description

Patented Oct. 17, 1950 UNITED STATES PATENTO'FFICE No Drawing. Application July 21, 1948,
' Serial No. 40,013
3 Claims. (Cl. 75-146) 1 V This invention relates to aluminum base alloys, and particularly to alloys of this type containing magnesium, silicon, zinc, titanium, and chromium.
An object of the invention is to provide an aluminum base alloy of greatly improved fluidity, so as to be especially suitable for the making of castings jg, sand, or in semi-permanent or permanent molds.
A further object of the invention is to provide an alloy as specified in the last preceding paragraph exceptionally free from surface pitting.
A further object of the invention is to provide an alloy as above defined and characterized and of greatly improved corrosion resistance.
A further object of the invention is to provide an aluminum base alloy suitable forthe making of cast cooking utensils.
Before the present invention is described in detail, it should be understood that the invention is not limited to the details herein disclosed, which are exemplary in character, and not tobe regarded as in any way limiting. It also should be understood that the phraseology or terminology herein employed is for the purpose of desoription andnot of limitation.
Thealloys which come within the limits herein disclosed, and defined by the appended claims, may be used for many adaptationswhere good casting properties, including high fluidity, are-desired, and more particularly where good corrosion resistance and freedom from surface pitting are regarded as important. 7
As a good example of one such adaptation we may consider a cast cooking utensil. Housewives who use aluminum cooking utensils become quite dissatisfied when the surface of a utensil such as a sauce pan becomes discolored, and polishing with steel wool or similar abrasive agent or cleaning powder merely reveals the presence of innumerable pits, either in local areas orgenerally distributed over the surface, which no amount of scrubbing can remove. Such pits become centers for the spread of corrosive attack and discoloration. As a result the housewife may decide, next time she needs a cooking utensil, that she will choose one made from a ferrous or cuprous alloy.
As a result of considerable study and experi- -mentation I have developed an alloy which avoids aluminum with the following alloying ingredients from 1.75 per cent to 2.25 per cent of silicon; from 0.3 per cent to 0.75 per cent of zinc; from 2.75 per cent to 3.25 per cent of magnesium; from 0.08 per cent to 0.2 per cent of titanium; from 0.1
I per cent to 0.2 per cent of chromium.
The combination of the magnesium, silicon and zinc, within the ranges above noted, greatly improves the castability while maintaining a desirable degree of corrosion resistance. An aluminum base alloy with these three constituents, in the amounts stated, is a desirable casting alloy without further alloying addition. As a matter of fact when the zinc ingredient is increased be yond the range limits disclosed, the pitting effect increases progressively.
The addition of the chromium within the disclosed range to the aluminum-silicon-zinc-magnesium alloy reduces even further any residual pitting tendency.
, The addition of the titanium Within the disclosed range aids in preventing any shrinkage cracking tendency.
One specific alloy which I have used with considerable success, as far as casting characteristics and freedom from shrinkage cracking and pitting are concerned, contained 2.0 per cent of silicon, 0.5 per cent of zinc, 3.0 per cent of magnesium, 0.1 per cent of titanium, .and 0.15 per cent of chromium. Cooking utensils cast from this alloy exhibit an exceptionally smooth surface appearance, andare entire y free from objectionable discoloration and corrosion.
What I claim is:
1. An aluminum base alloy characterized by excellent casting characteristics,corrosion resistance, and freedom from. shrinkage cracks and pitting in the cast condition, and containing from 1.75 per cent to 2.25 per cent of silicon, from 0.3 per cent to 0.75 per cent of zinc, from 2.75 per cent to 3.25 per cent of magnesium, from 0.08
er cent to 0.2 per centv of titanium, and from 0.1 per cent to 0.2 per cent of chromium, the balance being aluminum.
2. An aluminum base alloy characterized by excellent casting characteristics, corrosion resistance, and freedom from shrinkage cracks and,
'pitting in the cast condition, containing about 2.0 per cent of silicon, about 0.5 per cent of zinc,
tically completely free from surface pitting and resulting progressive discoloration and corrosion. The alloy comprises a major portion of any conventional, commercially available grade of about 3.0 per cent of magnesium, about 0.1 per cent of titanium, and about 0.15 per cent of chromium, the'balance being aluminum.
3. As a novel article of manufacture a cast cooking utensil exhibiting marked resistance to cast from an alloy containing from 1.75 per cent to 2.25 per cent of silicon, from 0.3 per cent to 0.75 per cent of zinc, from 2.75 per cent to 3.25 per cent of magnesium, from 0.08 per cent to 0.2 per cent of titanium, and from 0.1 per cent to 0.2 per cent of chromium, the balance being aluminum.
ERIK G. GRUNDSTROM.
REFERENCES CITED The following references are of record in the file of this patent:
Number 4 UNITED STATES PATENTS Name Date Grundstrom Mar. 14, 1939 Bonsack Mar. 3, 1942 Stroup Apr. 21, 1.942

Claims (1)

1. AN ALUMINUM BASE ALLOY CHARACTERIZED BY EXCELLENT CASTING CHARACTERISTICS, CORROSION RESISTANCE, AND FREEDOM FROM SHRINKAGE CRACKS AND PITTING IN THE CAST CONDITIONS, AND CONTAINING FROM 1.75 PER CENT TO 2.25 PER CENT OF SILICON, FROM 0.3 PER CENT TO 0.75 PER CENT OF ZINC, FROM 2.75 PER CENT TO 3.25 PER CENT OF MAGNESIUM, FROM 0.08 PER CENT TO 0.2 PER CENT OF TITANIUM, AND FROM 0.1 PER CENT TO 0.2 PER CENT OF CHROMIUM, THE BALANCE BEING ALUMINUM.
US40013A 1948-07-21 1948-07-21 Aluminum base alloy Expired - Lifetime US2526227A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US40013A US2526227A (en) 1948-07-21 1948-07-21 Aluminum base alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US40013A US2526227A (en) 1948-07-21 1948-07-21 Aluminum base alloy

Publications (1)

Publication Number Publication Date
US2526227A true US2526227A (en) 1950-10-17

Family

ID=21908595

Family Applications (1)

Application Number Title Priority Date Filing Date
US40013A Expired - Lifetime US2526227A (en) 1948-07-21 1948-07-21 Aluminum base alloy

Country Status (1)

Country Link
US (1) US2526227A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2782493A (en) * 1952-01-02 1957-02-26 Kaiser Aluminium Chem Corp Aluminum coated ferrous article
US3010190A (en) * 1957-02-25 1961-11-28 Kaiser Aluminium Chem Corp A composite metal body of a ferrous base and aluminum base alloy coat
US6035767A (en) * 1997-06-12 2000-03-14 Gibson; Ronald E. Camping skillet and biscuit maker

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2150219A (en) * 1939-01-16 1939-03-14 Advance Aluminum Castings Corp Aluminum alloys
US2274657A (en) * 1941-04-17 1942-03-03 Nat Smelting Co Aluminum alloy
US2280176A (en) * 1939-10-27 1942-04-21 Aluminum Co Of America Aluminum alloy

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2150219A (en) * 1939-01-16 1939-03-14 Advance Aluminum Castings Corp Aluminum alloys
US2280176A (en) * 1939-10-27 1942-04-21 Aluminum Co Of America Aluminum alloy
US2274657A (en) * 1941-04-17 1942-03-03 Nat Smelting Co Aluminum alloy

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2782493A (en) * 1952-01-02 1957-02-26 Kaiser Aluminium Chem Corp Aluminum coated ferrous article
US3010190A (en) * 1957-02-25 1961-11-28 Kaiser Aluminium Chem Corp A composite metal body of a ferrous base and aluminum base alloy coat
US6035767A (en) * 1997-06-12 2000-03-14 Gibson; Ronald E. Camping skillet and biscuit maker

Similar Documents

Publication Publication Date Title
US2526227A (en) Aluminum base alloy
US4063936A (en) Aluminum alloy having high mechanical strength and elongation and resistant to stress corrosion crack
JP4703033B2 (en) Aluminum alloy material for die casting
US2079786A (en) Container having a high resistance to corrosion by alkaline and soda ash solutions
JPS60255996A (en) Aluminum alloy product
US1946069A (en) Magnesium base die casting alloys
US2444271A (en) Composition for use in casting
US1934281A (en) Aluminum-silicon alloy
US2093380A (en) Aluminum bronze alloys
US2008862A (en) Alloy
US2075005A (en) Copper-silicon-zinc-lead alloy
US2150219A (en) Aluminum alloys
US2116923A (en) Process of heat-treating alloys
US2075004A (en) Copper-silicon-zinc-tin-lead alloy
US1163813A (en) Proces for the hardening of compositions of nickel and copper.
JP3152760B2 (en) Cooking container material having good heat efficiency without seizure and method for producing the same
US2041042A (en) Aluminum alloy
US1899465A (en) Aluminium alloy
US2583473A (en) Aluminum-magnesium alloys
US1932840A (en) Aluminum alloys
US1932844A (en) Aluminum alloys
US2041866A (en) Multiple alloys
US2231940A (en) Alloy
US1793023A (en) Magnesium alloy for pistons
US1932846A (en) Aluminum alloys