US2231881A

US2231881A - Magnesium alloy

Info

Publication number: US2231881A
Application number: US198690A
Authority: US
Inventors: Burkhardt Arthur; Knabe Richard
Original assignee: GEORG VON GIESCHE S ERBEN BRES
Current assignee: GEORG VON GIESCHE S ERBEN BRES; GEORG VON GIESCHE'S ERBEN BRESLAU
Priority date: 1937-04-16
Filing date: 1938-03-29
Publication date: 1941-02-18
Anticipated expiration: 1958-02-18
Also published as: US2226549A; AT160729B; GB519304A; FR836328A; FR843312A; US2204568A; GB490712A; AT160440B; DE741507C; FR843311A; FR836327A; GB504602A; DE732188C; GB489320A; GB519302A; AT158393B; AT160903B; FR843310A; US2204567A; DE700517C

Description

Patented Feb. 18, 1941 PATENT ol=l=lcs 2,231,881 v M GNESIUM Armor Arthur Richard Knabe,

hurkhardt, Berlin Lichterfelde,

Berlin-Zehlendo Germany,

and

assignors' to Georg Von Giesches- Erben, W Breslau, Germany, a corporation of Germany No Drawing. Applicati on Maren-29, 193s, Serial No. 198,690. In Germany April 15, 1937 3 Claims.

Our invention relates to magnesium alloys and to a process of making same.

It is an object of our invention to provide a process by which higher resistance to corrosion,

and better machinability, are imparted to ma nesium alloys.

To this end, we make an addition of sodium plus potassium, or of sodium alone, or of potasslum alone, to a magnesium alloy of any suitable composition.

If sodium plus potassium are added, the total content of both constituents is 1 to 5%.

Sodium alone is added at the rate of 2 to 5%, and potassium alone at the rate of 1 to 5%.

By the term magnesium alloy used throughout the following specification is generally understood a magnesium base alloy containing at least 50% 'of magnesium; but we are not limited to this, or any other, percentage of magnesium.

The. other constituents of the alloys according to our invention-with the obvious exception of the additions of sodium plus potassium, or sodium or potassium-and their percentages may be as desired.

Our invention may be adapted, by way of example, to the magnesium alloys known by the registered trade name of Electron" metal which,

in addition to a magnesium base, contain zinc, an aluminium, or copper in varying proportions, ac-

cording to the purpose for which the alloy is intended. Such an alloy, with a baseof magnesium, may for example contain 0.2 to 0.5% of aluminium, and 0.1 to 0.3% of zinc; or 6 t0.6.5%

" of aluminium, and 1% zinc.

It has already been proposed to increase the resistance to corrosion of magnesium alloys of the Electron metal type, or of a similar kind, by adding small quantities of certain metals, such 10 for example as'manganese. In this way, the two Electron metal alloys recited above, are prepared'with an addition of 0.5 to 1% of manganese, and 0.2 to 0.5% of manganese, respectively.

. Although such addition of manganese produces an appreciable increase in the corrosion resistance of the alloys, the increase is not sufficient for many purposes and requirements, and so some; application remained closed to ma fields of nesium alloys for which they would be excelv lently adapted in respect of their properties.

Another drawback of the known magnesium alloys is that they produce curly chips when machined on automatic,'or other machine tools which coil about the tools and interfere with the further corrosion, the surface was to be observed. 45

machining ofthe alloys, particularly on automatic machine tools. 1 4

' Surprisingly, it' has been found that by adding F sodium plus potassium, or sodium or potassium, as described, a resistance to corrosion is imparted 5 to the magnesium alloys which is far superior to that attained heretofore. Besides, the novel alloys produce short, spurting chips when machined on automatic or other machine tools. The

additions do not in any way deteriorate the me- 10'- chanical properties of the alloys.

The percentages of the several additions have already been stated. It should be noted that an addition of the sodium at the rate of less than 2%, and potassium'at the rate of less than 1%, 15 has been found not to exhibit the desired eifect. Preferably,"the content of sodium plus potassium is 2%, and the percentages of the individual constituents in the addition may be equal, i. e., 1% of sodium and 1% of potassium, or they may 2- be different. The percentage, of sodium alone is preferably about 3, and that of potassium is preferably about 5.

It will thus be' understood that the alloys em- 25 bodying our invention include a magnesium base, any desired usual additions, see supra, and an addition of sodium plus potassium, at the total rate of '1 to 5%, preferably 2%, or 2 to 5%, preferably 3%, of sodium, or 1 to 5%, preferably 2%, 3 of potassium.

It has already been proposed to add up to 10% of lithium to magnesium alloys but this did not produce increased corrosion resistance.

When submitted to a short-time corrosion test 35 in the salt spray apparatus, magnesium alloys of the Electron metal type exhibit eillorescence on the surface already aftei -a short time, and after four hours extensive destruction takes place. Under similar conditions, and after four hours, 0 the same alloy, but with an addition of 3% of sodium, developed a thin protective film at the surface which apparently protects the alloyfrom but otherwise no alteration of A comparison of the corrosion in a-ma'gnesium alloy of the usual typ and one with an addition according tothe invention, was made as follows: Alloy I was the usual alloy, with 815% of aluminium, 0.2% of manganese, and 0.5% of zinc, 5 rest magnesium. Alloy II was prepared by adding 2% of sodium to alloy 1. The two alloys were tested in a solution of 3% of sodium chloride, 1% of hydrogen peroxide, and 0.01 cubic centimetres of hydrochloric acid in cubic centimetres of u The amounts of hydrogen, in cubic solution. centimetres, evolved were as follows:

After hours Alloy I Alloy II We have iound that our method produces an tested.

increase in the corrosion resistance and better machinability of all magnesium alloys we have The following examples of magnesium-base alloys embodying our invention are given:

Percentage of- "l'tfi 0; Zinc sodium $23.?

5. 5 0. 5 0 5 l. 5 11 0. 3 1 11 0. 3' 1 1 1 11 0.3 1 1. 5 11 0. 3 1 4 11 0. 3 l 2 0. 5 11 0. 3 l 0. 5 1. 5

The remainder of these alloys consists substantially all of magnesium, that is, magnesium having the usual impurities and/or containing minor amounts of the customary additions above mentioned.

We claim:

1. A magnesium base alloy containing 2 to 5% cl sodium, from traces up to about 11% or aluminum, the remainder substantially all of magn'esium besides small amounts of customary additions and impurities.

2. A magnesium base alloy containing 1 to 5% of potassium, from traces up to about 11% of aluminum, the remainder consisting of magnesium besides small amounts of customary auxiliaries and impurities. l

8. A magnesium base alloy containing from traces up to 11% aluminum andlan addition 01' metal selected from the group consisting of sodium and potassium, the individual amounts of sodium and potassiumLbeing 2 to 5% and 1 to 5% respectively and the total amount of said addition being up to 5%, the remainder being substantially all magnesium besides small amounts of customary auxiliaries and impurities, said alloy being characterized by increased corrosion resist-' ance due to said addition.

ARTHUR BURKHARD'I'. RICHARD KNABE.