US1928641A - Aluminum manganese alloy - Google Patents
Aluminum manganese alloy Download PDFInfo
- Publication number
- US1928641A US1928641A US462419A US46241930A US1928641A US 1928641 A US1928641 A US 1928641A US 462419 A US462419 A US 462419A US 46241930 A US46241930 A US 46241930A US 1928641 A US1928641 A US 1928641A
- Authority
- US
- United States
- Prior art keywords
- aluminum
- manganese
- alloys
- per cent
- alloy
- 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
Links
- -1 Aluminum manganese Chemical compound 0.000 title description 15
- 229910000914 Mn alloy Inorganic materials 0.000 title description 14
- 229910045601 alloy Inorganic materials 0.000 description 21
- 239000000956 alloy Substances 0.000 description 21
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 10
- 229910052749 magnesium Inorganic materials 0.000 description 10
- 239000011777 magnesium Substances 0.000 description 10
- 229910052751 metal Inorganic materials 0.000 description 9
- 239000002184 metal Substances 0.000 description 9
- 229910052782 aluminium Inorganic materials 0.000 description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 7
- 238000004519 manufacturing process Methods 0.000 description 6
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 5
- 238000007792 addition Methods 0.000 description 5
- 229910052748 manganese Inorganic materials 0.000 description 5
- 239000011572 manganese Substances 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 239000000047 product Substances 0.000 description 3
- 238000005275 alloying Methods 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910000861 Mg alloy Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 230000009931 harmful effect Effects 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 230000005764 inhibitory process Effects 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 230000003746 surface roughness Effects 0.000 description 1
- 238000007669 thermal treatment Methods 0.000 description 1
- 230000003245 working effect Effects 0.000 description 1
Classifications
-
- 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
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
Definitions
- This invention relates to the control of grain characteristics in aluminum-base alloys containing aluminum in amounts of over about 50 per cent, and particularly to such of these alloys as 5 contain manganese.
- the aluminum-base alloys containing manganese have a distinct propensity to grain growth ,under certain conditions of working and thermal treatment which requires that the fabrication of suchalloys 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 semifabricated condition must undergo. 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.
- 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.
- One 01' the objects of this invention is the 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.
- the amount of magnesium which I have found it necessary to add to the aluminum-manganese alloys for the purpose of inhibiting grain growth is not large and in fact is surprisingly small. I have found that additions of 0.2 to 0.5 per cent are most efficient. 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 0.5 per cent do not increase the effect to an extent which would justify larger additions and the larger amounts of magnesium would change, in part, the useful and desired properties obtained in the aluminum-manganese alloys.
- the amount of magnesium added should not vary greatly from about 0.2 to 0.5 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 corrosionresistance of the original aluminum-manganese alloy.
- the magnesium can be added to the molten alloy at any convenient stage before cast.- ing the ingot or other article which is to be worked.
- the aluminum-manganese alloys to which the addition of magnesium is beneficial in reducing the grain size of the fabricated product are those containing from about 0.75 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.
- test pieces of the same form and having a diameter of about'l1.5 inches and a thickness of 0.08 inch were drawn to utensils having a diameter of about 8.5 inches and a depth of 2 to 2.5 inches.
- the finished drawn product was smooth in appearance and surface and exhibited none of the tendencies of aluminum-manganese alloys to develop the surface roughness and other well known defects incident to the working of metal of large grain size.
- 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.
- I claim- 1 An alloy consisting of aluminum, about 0.75 to 3 per cent of manganese, and about 0.2 to 0.5
- An alloy consisting of aluminum, about 1 to -l.5 per cent of manganese, and about 0.2 to 0.45
- An alloy consisting of aluminum, about 1 to 1.5 per cent of manganese, and about 0.25 per cent of magnesium.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Laminated Bodies (AREA)
Description
Patented Oct. 3, 1933 ALUMINUM MANGANESE ALLOY Theodore W. Bossert, New Kensington, Pa., as-
signor to Aluminum Company of America, Pittsburgh, Pa., a corporation of Pennsylvania No Drawing. Application June 19, 1930 Serial No. 462,419
3 Claims.
This invention relates to the control of grain characteristics in aluminum-base alloys containing aluminum in amounts of over about 50 per cent, and particularly to such of these alloys as 5 contain manganese.
The aluminum-base alloys containing manganese have a distinct propensity to grain growth ,under certain conditions of working and thermal treatment which requires that the fabrication of suchalloys 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 semifabricated condition must undergo. 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 the adjustment of the alloy composition', but although many experiments in this direction have been carried out, they have hitherto resulted in either failure or only partial success.
One 01' the objects of this invention is the 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 defeet in such alloy without simultaneously producing a harmful effect upon the desirable properties of the original alloy. The aluminum-manganese alloys, and particularly those containing 1 to 1.5 per cent of manganese, have certain work- 70 ing 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 7o. grain growth from which aluminum-manganese alloys are so prone to suffer can be effectively controlled, without appreciably affecting theadvantageous properties of the alloys, by adding to the alloy a. small amount of magnesium.
The amount of magnesium which I have found it necessary to add to the aluminum-manganese alloys for the purpose of inhibiting grain growth is not large and in fact is surprisingly small. I have found that additions of 0.2 to 0.5 per cent are most efficient. 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 0.5 per cent do not increase the effect to an extent which would justify larger additions and the larger amounts of magnesium would change, in part, the useful and desired properties obtained in the aluminum-manganese alloys. For these reasons, therefore, the amount of magnesium added should not vary greatly from about 0.2 to 0.5 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 corrosionresistance of the original aluminum-manganese alloy. The magnesium can be added to the molten alloy at any convenient stage before cast.- ing the ingot or other article which is to be worked.
The aluminum-manganese alloys to which the addition of magnesium is beneficial in reducing the grain size of the fabricated product are those containing from about 0.75 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, a number of drawing tests were made upon aluminum-manganese alloys containing .about 1.25 per cent of manganese and 0.25 per cent of magnesium. The tested pieces consisted of flat sheet circles having a thickness of 0.05 inch 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 inch 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'l1.5 inches and a thickness of 0.08 inch 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 aluminum-manganese 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-manganese-magnesium 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 aluminum-manganese alloys containing this added element are analogous to the other common aluminum alloys as respects grain growth in their reaction to such conditions.
It is to be understood that the term 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.
I claim- 1. An alloy consisting of aluminum, about 0.75 to 3 per cent of manganese, and about 0.2 to 0.5
per cent of magnesium.
2. An alloy consisting of aluminum, about 1 to -l.5 per cent of manganese, and about 0.2 to 0.45
per cent of magnesium.
3. An alloy consisting of aluminum, about 1 to 1.5 per cent of manganese, and about 0.25 per cent of magnesium.
THEODORE W. BOSSERT.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US462419A US1928641A (en) | 1930-06-19 | 1930-06-19 | Aluminum manganese alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US462419A US1928641A (en) | 1930-06-19 | 1930-06-19 | Aluminum manganese alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1928641A true US1928641A (en) | 1933-10-03 |
Family
ID=23836363
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US462419A Expired - Lifetime US1928641A (en) | 1930-06-19 | 1930-06-19 | Aluminum manganese alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1928641A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3930895A (en) * | 1974-04-24 | 1976-01-06 | Amax Aluminum Company, Inc. | Special magnesium-manganese aluminum alloy |
-
1930
- 1930-06-19 US US462419A patent/US1928641A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3930895A (en) * | 1974-04-24 | 1976-01-06 | Amax Aluminum Company, Inc. | Special magnesium-manganese aluminum alloy |
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