US1845781A - Controlling grain growth in aluminum-manganese alloys - Google Patents
Controlling grain growth in aluminum-manganese alloys Download PDFInfo
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- US1845781A US1845781A US462418A US46241830A US1845781A US 1845781 A US1845781 A US 1845781A US 462418 A US462418 A US 462418A US 46241830 A US46241830 A US 46241830A US 1845781 A US1845781 A US 1845781A
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- aluminum
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- grain growth
- manganese
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
Definitions
- Patented Feb. 1 1932 CONTROLLING GRAIN GROWTH IN ALUMINUM-MANGANESE ALLOYS No Drawing.
- This invention relates to the control of grain characteristics in aluminum-base al-- loys containing aluminum in amountsof over about 50 per cent, and particularly to such of these alloys as contain manganese.
- the aluminum-base alloys containing manganese have a distinct propensity to grain growth under certain conditions of working I and thermal treatment which requires that 10 the fabrication of such alloys into the desired forms be carefully controlled lest the final product, because of its large grain size, be of little use.
- This tendency to grain growth is an undesirable characteristic of these alloys with reference to any fabricating or forming operations which the alloy in a scmi- It is particularly undesirable, however, in drawing operations as, for instance, the drawing operation by which a utensil is formed by a single or double draw from a flat sheet metal blank. In such instances, the working of the metal produces selective strain effects on adjacent grains or crystals in the sheet, and
- a further object of the invention is the provision of certain aluminum-manganese alloys having such controlled compositions that the propensity to large grain in the fabricated condition is substantially eliminated.
- the amount of uranium which I have found it necessary to add to the aluminum manganese alloys for the purposes of inhib- 1ting grain growth is not large and in fact is surprisingly small. I have found that additions of 0.2 to 0.7 per cent are most eflicient. Smaller amounts, while having some effect, do not entirely accomplish the desired purpose, and amounts of about 0.2 per cent are necessarily added before a satisfactory inhibition to grain growth is effected. On the other hand, amounts much greater than 0.7 per cent do not increase the efiect to an extent which would justify larger additions and the addition of larger amounts of uranium would change, in part, the useful and desired properties obtained in the aluminummanganese alloys.
- the amount of uranium added should not vary greatly from about 0.2 to 0.7 per cent, and for usual purposes an addition of about 0.25 to 0.45 per cent of that metal is preferred as producing a maximum desired effect on grain size with a minimum change in the physical properties, the working properties, and the corrosion-resistance of the original aluminum-manganese alloy.
- lhe uranium can be added to the molten alloy at i any convenient'stage before casting the ingot or other'article which is to be worked.
- the aluminum-manganese alloys to which the addition of uranium is beneficial in reducing the grain size of the'fabricated product are those containing from about 0.7 5 to 3 per cent of manganese.
- the invention is particularly advantageous, however, with alloys containing about 1.0 to 1.5 per cent of manganese.
- the tested pieces consisted of flat sheet circles having a thickness of 0.05 inches and a diameter of about 20 inches. These circles or disks were shaped by means of the usual drawing dies into utensils of a diameter of about 9.5 inches and a depth of 7 to 7.5 inches. Other test pieces of the same form and having a diameter of about 13 inches and a thickness of 0.04 inches were drawn to utensils having a diameter of about 6.5 inches and a depth of about 4.5 to 5 inches.
- v aluminum as used throughout the description and claims, is intended to include aluminum of very high purity as well as metal of the usual commercial grades which con-
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Description
Patented Feb. 1 1932 CONTROLLING GRAIN GROWTH IN ALUMINUM-MANGANESE ALLOYS No Drawing.
This invention relates to the control of grain characteristics in aluminum-base al-- loys containing aluminum in amountsof over about 50 per cent, and particularly to such of these alloys as contain manganese.
The aluminum-base alloys containing manganese have a distinct propensity to grain growth under certain conditions of working I and thermal treatment which requires that 10 the fabrication of such alloys into the desired forms be carefully controlled lest the final product, because of its large grain size, be of little use. This tendency to grain growth (or to a large apparent crystalline structure) is an undesirable characteristic of these alloys with reference to any fabricating or forming operations which the alloy in a scmi- It is particularly undesirable, however, in drawing operations as, for instance, the drawing operation by which a utensil is formed by a single or double draw from a flat sheet metal blank. In such instances, the working of the metal produces selective strain effects on adjacent grains or crystals in the sheet, and
when the original blank is of large grain, induced by the aforesaid grain growth, the surface of the resulting drawn product is rough,
uneven and generally unsatisfactory. Such phenomena as these have long been known to exist in connection with aluminummanganese alloys, and in order to avoid their cause, viz. excessive grain growth, it has been thought necessary to exercise in the fabrication of the metal a most rigorous control of fabrication and thermal processes. This control has naturally resulted in increased cost of manufacture but has not been so eflicient in action but what large quantities of fabricated metal made from such alloys are still rejected because of large grain size. The only other possible method of eliminating this propensity to grain growth in aluminum manganese alloys has been recognized to be fabricated condition must undergo.
although many experiments in this direction have been carried out, they have hitherto resulted in either failure or only partial success.
the adjustment of the alloy composition, but
One of the objects of this invention is the Application filed June 19, 1930. Serial No. 462,418.
provision of a method of treatment by which the propensity of aluminum-manganese alloys to excessive grain size may be overcome. A further object of the invention is the provision of certain aluminum-manganese alloys having such controlled compositions that the propensity to large grain in the fabricated condition is substantially eliminated.
It is well recognized in the art of alloying metals that the addition of one or more alloying metals to a given alloy having certain advantageous characteristics usually modifies these characteristics in a marked degree, often to such an extent that the properties of the original alloy are seriously impaired or even no longer available. It is a problem of major importance, therefore, to modify the composition of a, given alloy to the extent necessary to overcome a latent defect in such alloy without simultaneously producing a harmful effect upon the desirable properties of the original alloy. The aluminum-mam gan'ese alloys, and particularly those containing 1 to 1.5 per cent of manganese, have certain working properties and properties of strength and corrosion resistance which in combination have made such alloys especially useful for the fabrication of certain types of articles. In the present case, however, I have found that the disadvantageous grain growth from which aluminum-manganese alloys are so prone to suffer can be effectually controlled, without appreciably affecting their advantageous properties, by adding to the alloy a small amount of uranium.
The amount of uranium which I have found it necessary to add to the aluminum manganese alloys for the purposes of inhib- 1ting grain growth is not large and in fact is surprisingly small. I have found that additions of 0.2 to 0.7 per cent are most eflicient. Smaller amounts, while having some effect, do not entirely accomplish the desired purpose, and amounts of about 0.2 per cent are necessarily added before a satisfactory inhibition to grain growth is effected. On the other hand, amounts much greater than 0.7 per cent do not increase the efiect to an extent which would justify larger additions and the addition of larger amounts of uranium would change, in part, the useful and desired properties obtained in the aluminummanganese alloys. For these reasons, therefore, the amount of uranium added should not vary greatly from about 0.2 to 0.7 per cent, and for usual purposes an addition of about 0.25 to 0.45 per cent of that metal is preferred as producing a maximum desired effect on grain size with a minimum change in the physical properties, the working properties, and the corrosion-resistance of the original aluminum-manganese alloy. lhe uranium can be added to the molten alloy at i any convenient'stage before casting the ingot or other'article which is to be worked.
The aluminum-manganese alloys to which the addition of uranium is beneficial in reducing the grain size of the'fabricated product are those containing from about 0.7 5 to 3 per cent of manganese. The invention is particularly advantageous, however, with alloys containing about 1.0 to 1.5 per cent of manganese.
As illustrative of the benefits of the invention, drawing tests were made upon aluminum-manganese alloys containing about 1.25
'per cent of manganese and 0.25 per cent of uranium. The tested pieces consisted of flat sheet circles having a thickness of 0.05 inches and a diameter of about 20 inches. These circles or disks were shaped by means of the usual drawing dies into utensils of a diameter of about 9.5 inches and a depth of 7 to 7.5 inches. Other test pieces of the same form and having a diameter of about 13 inches and a thickness of 0.04 inches were drawn to utensils having a diameter of about 6.5 inches and a depth of about 4.5 to 5 inches. Still other test pieces of the same form and having a diameter of about 11.5 inches and a thickness of 0.08 inches were drawn to utensils having a diameter of about 8.5 inches and a depth of 2 to 2.5 inches. In every case the finished drawn product was smooth in appearance and surface and exhibited none of the tendencies of aluminummanganese alloys to develop the surface roughness and other well known defects incident to the working of metal of large grain size. I have also found that in the fabrication of these new aluminum-manganeseuranium alloys from ingot to sheet or in other working operations the necessity for nicety of control of working and thermal conditions is eliminated and the aluminummanganese alloys containing this added element are analogous to the other common aluminum alloys as respects grain growth in their reactlon to such conditions.
It is to be understood that the term v aluminum, as used throughout the description and claims, is intended to include aluminum of very high purity as well as metal of the usual commercial grades which con-
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US462418A US1845781A (en) | 1930-06-19 | 1930-06-19 | Controlling grain growth in aluminum-manganese alloys |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US462418A US1845781A (en) | 1930-06-19 | 1930-06-19 | Controlling grain growth in aluminum-manganese alloys |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1845781A true US1845781A (en) | 1932-02-16 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US462418A Expired - Lifetime US1845781A (en) | 1930-06-19 | 1930-06-19 | Controlling grain growth in aluminum-manganese alloys |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3098742A (en) * | 1962-08-09 | 1963-07-23 | Gilbert S Layne | Uranium-molybdenum-aluminum ternary alloy |
| US3183079A (en) * | 1963-06-26 | 1965-05-11 | Dow Chemical Co | Uranium-niobium-aluminum ternary alloy |
-
1930
- 1930-06-19 US US462418A patent/US1845781A/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3098742A (en) * | 1962-08-09 | 1963-07-23 | Gilbert S Layne | Uranium-molybdenum-aluminum ternary alloy |
| US3183079A (en) * | 1963-06-26 | 1965-05-11 | Dow Chemical Co | Uranium-niobium-aluminum ternary alloy |
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