|Publication number||US2076569 A|
|Publication date||Apr 13, 1937|
|Filing date||Dec 28, 1935|
|Priority date||Dec 28, 1935|
|Publication number||US 2076569 A, US 2076569A, US-A-2076569, US2076569 A, US2076569A|
|Inventors||Dean Walter A, Kempf Louis W|
|Original Assignee||Aluminum Co Of America|
|Export Citation||BiBTeX, EndNote, RefMan|
|Referenced by (3), Classifications (5)|
|External Links: USPTO, USPTO Assignment, Espacenet|
Patented Apr. 13, 1937 AUNITED- STATES PATENT "OFFICE Ohio, assignors to America, Pittsburgh,
Pennsylvania Aluminum Company of Pa., a corporation'of No Drawing. Application December 28, 1935, Serial No. 56,543
The invention relates to aluminum base alloys and is particularly concerned with aluminum base alloys containing copper, magnesium and silicon.
, Aluminum base alloys containing between 3 5 per cent and 12 per cent of copper have beenwldely used heretofore. The copper imparts good casting characteristics and increases the tensile strength, yield strength, and hardness of the alloy. In the lower portion of the copper range the alloy may be mechanically deformed by the well known commercial processes such as rolling, forging, drawing, or extrusion. Alloys containing more than about 6 per cent copper are gen erally used in the cast' condition. Throughout 15 the entire range of 3 to 12 per cent copper, however, the alloys are susceptible to variations and improvements in their physical properties by thermal treatments.
Alloys of the foregoing type are greatly improved in casting characteristics and strength through the addition of from 0.5 to 2.5 per cent of silicon and 0.1 to 1 per cent of magnesium. The silicon serves chiefly to improve the casting and physical qualities of the alloy while the magnesium tends to make it more responsive to solution heat treatment and induces a more rapid aging after such heat treatment. Our invention, which is described hereinbelow, is directed to improving the machining quality of such aluminum-copper-magnesium-silicon alloys.
Since all commercial aluminum base alloys contain some silic'on as an impurity, usually less than, or not greatly in excess of, 0.5 per cent, it is to be understood that the amount of silicon discussed herein, and hereinafter claimed, represents the total quantity of silicon present, and that the silicon content of the aluminum used should be known in order to provide a basis for determining the eventual composition of the aluminumcopper-magnesium-silicon alloy.
There are, however, some applications wherein aluminum-copper-magnesium-silicon alloys as hereinabove disclosed might be conveniently and profitably used except for an inherent disadvantage which militates against their usein the production of certain articles requiring exact-.
ing machining operations. Mechanical cutting operations such as drilling, shaping, or lathe-cutting are successfully carried out only by using cer- 0 tain precautions which increase the cost of production and perhaps favor the choice of another metal or alloy which can be machined more readily but which is not so desirable in other respects, as for example, in physical properties. When alloys are difficult to machine this disadvantage becomes evident, in many cases, through rapid wear of the cutting tool edge, so that frequent tool re-sharpening is required. Despite continual lubrication the machined surface is rough and irregular, and the chip has a tendency to form a continuous curl or spiral which often fouls the tool or the moving parts of the machine. It is immediately apparent that there is need for an alloy of good working characteristics and satisfactory physical properties, yet possessing such favorable machining properties that the complete machining operations may be performed economically and successfully, and may be productive of a pleasing surface appearance.
Accordingly an object of our invention is the provision of an aluminum base alloy containing from about 3 per cent to about 12 per cent of copper, from about 0.1 to about 1 per cent of magnesium, and from about 0.5 per cent to about 2.5 per cent of silicon which may be readily and economically machined.
Our invention resides in the discovery that the foregoing object is effected by the addition of two or more of the elements lead, tin, thallium, cadmium or bismuth. The aluminum base alloys to which these elements are added in the proportions specified below, are known as free cutting or free machining alloys because they can be machined more rapidly than similar alloys without these elements and yet have as good orbetter finished surface. After an extended series of investigations we have discovered that these five metals when added to aluminum base alloys, form a class of alloying elements by reason of their 3 favorable effect upon the machining properties of these alloys. In recognition of this effect we term lead, tin, thallium, cadmium and bismuth free machining elements. We have further discovered that the simultaneous presence of two or more of these elements is productive of an improvement in free machining characteristics which is considerably greater than that caused by the presence of the same total amount of a single free machining element. For example, the additionof 0.5 per cent of lead and 0.5 per cent of bismuth to an aluminum base alloy containing about 5 per cent of copper, 0.5 per cent of magnesium, and 1.25 per cent of silicon effects a greater improvement in machining quality than does the addition of 1.0 per cent of either lead or bismuth singly.
These five elements, we believe, are unique with respect to their effect on the machining characteristics of aluminum-copper-magnesium-silicon alloys. It is a fortunate circumstance, therefore, that they are also of relatively low melting point, a fact which makes possible their addition to molten aluminum in the pure state, without the intervention of so-called "rich alloys". As a matter of fact, we have observed that of all the metals whose melting point is lower than about 327 C., the melting point of lead, the five elements we have selected are the only ones which are commercially suitable and that impart free cutting characteristics but do not have undesirable effeet on the fundamental physical properties of the base alloy.
The total amount of free machining elements should not be less than about 0.05 per cent since below this amount there is scarcely any advantageous effect. We have determined that a maximum limit of about 6 per cent total of two or 2 more of the free machining elements is suiiicient for satisfactory commercial results, since although the free machining effect persists beyond this amount, certain of the other physical properties may be unfavorably affected.
Aluminum-copper-magnesium-silicon allo ys containing two or more of the free machining elements lead, tin, thallium, cadmium and bismuth may be machined more rapidly, with less tool wear, less tool sharpening, better quality of chip and better machined surface than the same base alloys without the free machining additions, and in fact better than the same base alloys containing an equivalent total amount of a single free machining element.
Since aluminum base alloys containing from 3 to 12 per cent of copper have a wide variety of applications we list several alloys each of which may be said to be preferred for a particular purpose. As an alloy for mechanical deformation 4 we suggest an aluminum base alloy containing 5 per cent of copper, 0.5 per cent of magnesium, 1.25 per cent of silicon, and a total of 1 per cent of free cutting constituents, for example, 0.5 per cent of bismuth and 0.5 per cent of cadmium, the
balance being aluminum. For an alloy with excellent casting characteristics to be used in the unworked condition we suggest an alloy containing 10 per cent of copper, 0.5 per cent of magnesium, 2 per cent of silicon and a total of 3 per cent of free machining elements, the balance being aluminum.
For certain purposes, notably the improvement of tensile strength, hardness and grain structure, the alloys as hereinabove disclosed may be improved by the addition of one or more of the group of elements composed of molybdenum, vanadium, titanium, tungsten, zirconium, and chromium. From 0.05 to 1 per cent of any one of these elements may be used alone, but if more 00 than one is employed the total amount should not exceed about 2 per cent.
It is characteristic of the five elements lead, tin, thallium, cadmium, and bismuth that they form with aluminum a series of alloys of limited 05 liquid solubility. We have reason to believe that the free machining elements are the only elements which exhibit this characteristic, with the possible exception of several metals which are not regarded as having any commercial promise as 70 additions to aluminum base alloys. Within the range disclosed and claimed however the free machining elements may be added without unusual diillculty. We suspect that this characteristic feature of the disclosed elements may be one of the significant factors which contribute to their free machining eflect. We'believe that this effect is further strengthened by distributing the free machining constituent relatively homogeneously throughout the solid matrix, since these free machining constituents are also practically insoluble in the solid aluminum base.
The free machining alloys which have been described hereinabove may be subjected to the thermal treatments well known in the art to improve their strength and hardness. We have found that a solution heat treatment and subsequent aging do not impair the free machining quality of the alloys and in many instances the treatment even tends to improve this property. For many purposes a relatively high strength and hardness are necessary to the successful performance of the machined article and hence the alloy must be heat treated. This treatment is generally applied prior to the machining operation.
As hereinabove indicated the free machining elements, by reason of their low melting point, may be added to the molten aluminum alloy in pure metallic form. However, since some dimculty may be encountered in introducing them in the higher percentages of our disclosed range we prefer to use the method which is more fully described in U. S. Patent No. 1,959,029, issued March 15, 1934; Briefly it involves heating the melt to a somewhat higher temperature than is customary, and vigorously stirring it in excess of a critical period of time.
The term aluminum as used herein and in the appended claims embraces the usual impurities found in aluminum ingot of commercial grade or picked up in the course of the ordinary handling operations incident to melting practice.
1. An aluminum base alloy consisting of about 5 per cent copper, 0.5 per cent magnesium, 1.25 per cent silicon, 0.5 per cent lead and 0.5 per cent bismuth, the balance being aluminum.
2. An aluminum base alloy consisting of about 5 per cent copper, 0.5 per cent magnesium, 1.25 per cent silicon, 0.5 per cent bismuth and 0.5 per cent cadmium, the balance being aluminum.
3. A free cutting alloy containing from 3 to 12 per cent of copper, from 0.1 to 1 per cent of magnesium, from 0.5 to 2.5 per cent of silicon and a total of from 0.05 to 6 per cent of at least two of the elements from the following metals, lead, tin, thallium, cadmium, and bismuth, to improve its machining properties, the balance being substantially aluminum.
4. A free cutting alloy containing from 3 to 12 per cent of copper, from 0.1 to 1 per cent of magnesium, from 0.5 to 2.5 per cent of silicon, from 0.05 to 2 per cent of hardening metal from the group composed of molybdenum, vanadium, titanium, tungsten, zirconium and chromium, and a total of from 0.05 to 6 per cent of at least two of the elements from the following metals lead, tin, thallium, cadmium, and bismuth, to improve its machining properties, the balance being substantially aluminum.
5. An aluminum base alloy consisting of about 5 per cent copper, 0.5 per cent magnesium, 1.25 per cent silicon, 0.5 per cent cadmium, and 0.5 per cent lead, the balance being aluminum.
-LOUIS W. KEMPF. WALTER A. DEAN.
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US4062704 *||Jul 9, 1976||Dec 13, 1977||Swiss Aluminium Ltd.||Aluminum alloys possessing improved resistance weldability|
|US5863359 *||Jun 9, 1995||Jan 26, 1999||Aluminum Company Of America||Aluminum alloy products suited for commercial jet aircraft wing members|
|US6113850 *||Aug 9, 1994||Sep 5, 2000||Aluminum Company Of America||2XXX series aluminum alloy|
|U.S. Classification||420/535, 420/536|