US1932838A

US1932838A - Aluminum alloys

Info

Publication number: US1932838A
Application number: US634156A
Authority: US
Inventors: Walter A Dean; Louis W Kempf
Original assignee: Aluminum Company of America
Current assignee: Howmet Aerospace Inc
Priority date: 1932-09-21
Filing date: 1932-09-21
Publication date: 1933-10-31
Anticipated expiration: 1950-10-31

Description

Patented Get. 31, 1933 ATENT @FFICE ALLOYS Walter 13. been and Louis W. Kempi', Cleveland,

Ethic, assignors to Aluminum America, Eittsbnrgh, Pennsylvania Company of Pin, a corporation of No Drawing. Application September 21, 1932 Serial No. 634,158

The invention relates to aluminum base alioys containing magnesium and cobalt and to such alloys of this nature as have excellent properties at elevated temperatures.

We have discovered that aluminum base alloys, by which we mean alloys containing about 80 per cent by weight or more of aluminum, containing 1 to per cent by weight of magnesium, are greatly improved in their properties 10 at high temperatures if there is added to the alloys amounts of cobalt from about 0.2 to 3.5 per cent by weight. The alloys by reason of these additions of cobalt are considerably hardened, particularly as regards their properties at elevated temperatures, i. e., in the neighborhood of 400 to 700 Fahrenheit, and this increased hardness is effected without an appreciable decrease in elongation. Since increased hardness, without substantial decrease in elongation, is a property greatly desired at elevated temperatures, the addition of cobalt to the aluminum-magnesium alloys above mentioned increases their commercial usefulness, particularly their use as structural material in reciprocating parts operating at high temperatures. The addition of cobalt in the amounts named also increases the ease with which the aluminum base magnesium alloys are out in permanent molds. i

The aluminum base alloys containing about 1 to 8 per cent of magnesium and about 0.2 to 1 per cent of cobalt are readily placed in a wrought condition, and when alloys for working are desired, we have iound'it advantageous to maintain the cobalt content between 0.2 to l per cent since greater amounts of cobalt increase the difliculties of working without producing advantages which compensate therefor. The aluminum base alloys containing 2.0 to 15.0 per cent of magnesium are most advantageously used as casting alloys, and in such case amounts of cobalt from 0.2 to 3.5 per cent will produce the advantageous results above noted.

In these alloys-the addition of 0.05 to 0.4 per cent of antimony or bismuth, or both of these metals in total amount not exceeding that named, has a pronounced effect in maintaining a high elongation in the alloys when they are subjected to elevated temperatures. Either or both of these metals added to the alloys in total amount much greater than about 0.4 per cent by weight bring about a decrease in elongation which is very disadvantageous when the alloys are to be used at elevated temperatures.

' as an example of the alloys herein described temperature, it had a tensile strength of 15,700

pounds per square inch and an elongation of 8.2 per cent in 2 inches. containing cobalt but similarly treated and test- A similar alloy not 7 ed has a tensile strength of about 15,300 and an elongation of about 5.5 per cent in 2 inches.

The aluminum used in the manufacture of the alloys may be of the highest purity or it may contain amounts of usual impurities, and the term aluminum as used herein and in the claims designates the aluminum of commerce.

It is an incidental property of our alloys that the presence of iron in amounts as high as 2 per cent by weight is not harmful to the high temperature properties of the alloys and, therefore, a wide choice between the various grades of commercial aluminum is possible.

We claim:

1. A metallic alloy characterized by high tensile and physical properties at elevated temperatures and consisting of 1.0 to 15.0 per cent by weight of magnesium and 0.2 to 8.5 per cent by weight of cobalt, the balance being aluminuxn.

2. A workable metallic alloy characterized by high tensile and physical properties at elevated temperatures and consisting of 1.0 to 6.0 per cent by weight of magnesium and 0.2 to-1.0 per cent by weight of cobalt, the balance being 00 aluminum.

3. A metallic alloy characterized by high tensile and physical properties at elevated temperatures and consisting of 2.0 to 15.0 per cent by weight of magnesium and 0.2 to 3.5 per cent by 05 weight of cobalt, the balance being aluminum.

WALTER A. DEAN. LOUIS W. KEMPF.