[go: up one dir, main page]

US1928641A - Aluminum manganese alloy - Google Patents

Aluminum manganese alloy Download PDF

Info

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
Application number
US462419A
Inventor
Theodore W Bossert
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Alcoa Corp
Original Assignee
Aluminum Company of America
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Aluminum Company of America filed Critical Aluminum Company of America
Priority to US462419A priority Critical patent/US1928641A/en
Application granted granted Critical
Publication of US1928641A publication Critical patent/US1928641A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys 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.

Landscapes

  • 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.
US462419A 1930-06-19 1930-06-19 Aluminum manganese alloy Expired - Lifetime US1928641A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (1)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
US2234552A (en) Hardened nonferrous alloy
US2245167A (en) Wrought aluminum base alloy and method of producing it
US2802733A (en) Process for manufacturing brass and bronze alloys containing lead
US1869996A (en) Controlling grain growth in aluminum-manganese alloys
US1928641A (en) Aluminum manganese alloy
US1845781A (en) Controlling grain growth in aluminum-manganese alloys
US3006758A (en) Zinc alloy
US2076575A (en) Free cutting alloys
US1785774A (en) Plastic heat-treated aluminum alloy
US1974970A (en) Alloy
US2295180A (en) Copper alloy
US1956251A (en) Copper alloys
US2280176A (en) Aluminum alloy
US2031316A (en) Copper base alloy
US2053346A (en) Roll for fabricating hot metal
US2047873A (en) Free cutting alloys
US2270716A (en) Copper alloy
US2076569A (en) Free cutting alloys
US2226594A (en) Aluminum alloy
US2314010A (en) Rolling magnesium-base alloys
JPH0346541B2 (en)
US2372546A (en) Zinc base alloy
US2026548A (en) Free cutting alloys
US1815071A (en) Nonferrous alloy
US1911080A (en) Aluminum alloy