US2296866A - Aluminum alloy - Google Patents

Aluminum alloy Download PDF

Info

Publication number
US2296866A
US2296866A US281219A US28121939A US2296866A US 2296866 A US2296866 A US 2296866A US 281219 A US281219 A US 281219A US 28121939 A US28121939 A US 28121939A US 2296866 A US2296866 A US 2296866A
Authority
US
United States
Prior art keywords
manganese
alloy
alloys
aluminum
tensile strength
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
US281219A
Inventor
Cresap M Moss
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.)
CHICAGO DEV CO
CHICAGO DEVELOPMENT Co
Original Assignee
CHICAGO DEV CO
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 CHICAGO DEV CO filed Critical CHICAGO DEV CO
Priority to US281219A priority Critical patent/US2296866A/en
Application granted granted Critical
Publication of US2296866A publication Critical patent/US2296866A/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

Definitions

  • This invention relates to alloys of aluminum and manganese with or without the addition of other metals. It relates more in particular to methods of preparing aluminum alloys containing manganese by which enhanced properties are obtained.
  • My invention comprises preparing an alloy of aluminum and manganese wherein the iron is less than 0.5% of the manganese content and the silicon preferably is less than 0.1% of the manganese content, and wherein the non-metallic impurities introduced by the use of manganese of aluminothermic or silicothermic origin are obviated, and casting this allay in a chill mold from a temperature well above the liquidus.
  • Alloys prepared in accordance with my invention are entirely different in properties and appearance from those made from aluminothermic or silicothermic manganese. The latter particularly begin to show the needle-like crystals of the manganese aluminum compound to the naked eye at about 3% manganese and at more than 5% manganese the alloys become coarsely crystalline and mechanically worthness. Alloys made in accordance with my invention remain finely crystalline and ductile even when containing more than 10% manganese.
  • alloys containing 1.25-10% manganese prepared in accordance with my invention are such as make the alloys useful for purposes that could not be fulfilled by the heretofore known alloys of the same nominal composition.
  • Earample 1.I have found that. an alloy containing 2% electrolytic manganese, balance aluminum, made in accordance with my invention, is highly ductile and can be rolled intosheet or shapes. Its tensile strength in the annealed state is 18,000 pounds per square inch and its elongation in 2 in. 20%. In the hard rolled state it shows a tensile strength of 35,000 pounds per square inch. This alloy can also be cast as.
  • Example 2.-I have found that an alloy of 3% electrolytic manganese, balance aluminum, has very valuable properties. In the cast and annealed state, it has a tensile strength of 20,000 pounds per square inch. It can be readily rolled without preliminary or intermediate heating to fine gauge sheet. At 50% reduction in thickness from the ingot it shows a tensile strength of 27,000 pounds per square inch and an elongation of 7%. With reduction, it shows a tensile strength of 50,000 pounds per square inch and an elongation of 3%. This alloy is useful as both a die cast and a wrought alloy.
  • Example 3 An alloy of 5% electrolytic manganese, balance aluminum, has a tensile strength as cast of 24,000 pounds per square inch and can be rolled to fine gauge sheet with a tensile strength of 60,000 pounds per square inch and 2% elongation.
  • Example 5 An alloy of 10% electrolytic manganese, balance aluminum, has a tensile strength as cast of 37,000 pounds and an elongation of 5%. This alloy is quite ductile but will find its greatest value in castings rather than as a wrought alloy.
  • Alloys containing somewhat more than 10% electrolytic manganese are generally similar to the 10% alloy but suffer a gradual decrease in ductility with increased manganese and are more difficult to make because of the increased melting point. However, my invention may be applied successfully up to about 20% electrolytic manganese.
  • All manganese-aluminum alloys made in accordance with my invention containing more than 2% pure or electrolytic manganese, may be hardened by suitable heat treatment. .
  • the preferred heat treatment is to quench from 600 degrees 0., cold work and then reheat to 180 degrees C. In this way, the strength is increased by about 10,000 pounds per square inch. Lesser increasesare obtained by reheating the quenched but unworked alloys.
  • my invention in making the binary aluminummanganese alloys is also obtained when ternary and quaternary alloys are made by adding other elements to the aluminum manganese alloys. This is especially true of alloys containing magnesium.
  • alloys containing magnesium I have found that the manganese content of many alloys, especially those of the hardening type, may be advantageously increased by the practice of my invention. These alloys usually contain 0.5 to 0.8% manganese. I have found that this may be increased to as much as 2% with a definite improvement in mechanical properties and corrosion resistance.
  • Example 6.--I produce an alloy containing .5% magnesium, 3.5% copper, .5% silicon, .5% to 2% electrolytic manganese, and balance aluminum.
  • This alloy through the range of manganese given, has substantially the same properties of the same alloy without the manganese, but with improved mechanical properties, and even some improvement in corrosion resistance.
  • Example 7.-I produce an alloy consisting of 4.5% copper, .5% to 2% electrolytic manganese
  • the resulting alloy has desirable working properties, is ductile, and possesses substantially higher tensile strength and reater resistance to corrosion than a binary a1- loy of aluminum and electrolytic manganese.
  • Example 8-High purity aluminum is alloyed with copper, magnesium and electrolytic manganese in accordance with the following proporions:
  • This alloy has desirable mechanical properties and the resistance to corrosion is improved over a similar alloy without the manganese.
  • the manganese may be increased to about 1%, with a corresponding reduction in aluminum, and a useful alloy obtained. Cast into a chill mold, it produces a casting of good machining properties and desirable tensile strength.
  • Example 9 Alloys were produced containing in the range 1% to 2% electrolytic manganese, and containing in addition about 7% silicon, .3% magnesium, and balance aluminum. In the range of manganese given, corrosion resistance was high, and mechanical properties good.
  • the alloy is particularly adapted for casting in a chill mold.
  • pure manganese and high purity manganese as employed in the claims are used to identify electrolytic manganese, or manganese having substantially the same percentage and character of impurities as electrolytic manganese.
  • the method of preparing an al oy consisting substantially entirely of aluminum and man ganese which comprises producing a liquid solution of electrolytic manganese, having a. purity of at least 99.9%, in high purity aluminum, the manganese comprising from'l.25% to 20% of the whole, and the product having less than .5% iron bed upon the manganese content, chill casting tl alloy from a temperature well above the liqui s, quenching the alloy from a relatively high temperature in the solid range, and reheating the alloy to a temperature of approximately degrees C., the resultant alloy being relatively free from the large needle-like crystals characteristic of ordinary alloys of aluminum with upwards of 2% manganese.
  • the method of preparing an alloy consisting substantially entirely of aluminum and manganese which comprises producing a liquid solution of electrolytic manganese, having a purity of at least 99.9%, in high purity aluminum, the manganese comprising from 1.25% to 20% of the whole, and the product having less than .5% iron .based upon the manganese content, chill casting CRESAP M. MOSS.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Continuous Casting (AREA)

Description

Patented Sept. 29, 1942 ALUMINUM ALLOY Cresap M. Moss, Washington, D. 0., assignor to Chicago Development Company, Chicago, Ill.
No Drawing. Application June 26, 1939, Serial No. 281,219
2 Claims.
This invention relates to alloys of aluminum and manganese with or without the addition of other metals. It relates more in particular to methods of preparing aluminum alloys containing manganese by which enhanced properties are obtained.
In the known art, alloys of aluminum and manganese have been made and it has been established that, from the standpoint of corrosion resistance, manganese is far superior to any other metal as an addition to pure aluminum to increase its strength and hardness. It has been found impossible, however, to use more than about 1.25 percent manganese in wrought alloys without too great a decrease in ductility; in commercial cast alloys 2 percent has been the limit. Corson, an authority in this field, states that 3% is undoubtedly the maximum which can be alloyed with aluminum without badly affecting its ductility. It is recognized that other elements such as copper, nickel, silicon and magnesium, which are added to aluminum to give increased strength, do so at the sacrifice of corrosion resistance. My invention permits the obtaining of high strength by the addition of manganese alone and without the sacrifice in corrosion resistance which marks the addition of other elements.
I have found that the large needle-like crystals which develop in alloys of manganese and aluminum containing more than 2% manganese when made by the prior art are responsible for the lack of ductility in these alloys. My investigations lead me to believe that these crystals are the compound MnAls. I have further found that the formation of the structure containing these crys tals is favored by the presence of iron and silicon and by slow cooling. With alloys made in the heretofore known way from silicothermic manganese or aluminother-mic manganese, I have found that no practical rate of cooling is great enough to suppress entirely .the formation of the brittle structure. However, with alloys made from materials containing only very small amounts of iron, chill casting produces alloys of entirely different properties than have heretofore been obtained. My invention comprises preparing an alloy of aluminum and manganese wherein the iron is less than 0.5% of the manganese content and the silicon preferably is less than 0.1% of the manganese content, and wherein the non-metallic impurities introduced by the use of manganese of aluminothermic or silicothermic origin are obviated, and casting this allay in a chill mold from a temperature well above the liquidus.
In a preferred form of my invention, I take a pure manganese containing not over .01% of any other metal and reduce it to a coarse powder. The best results are obtained with electrolytic manganese of high purity. The flakes stripped from the cathodes are easily broken up to pro-1 duce the coarse powder. I place the pure manganese powder in an alumina crucible with the desired amount of high purity aluminum. I have found that Hoopes process aluminum is very satisfactory. I then heat the mixture at 850-900 degrees C. with stirring until a homogeneous alloy is obtained. The alloy is then cast directly in a steel mold.
Alloys prepared in accordance with my invention are entirely different in properties and appearance from those made from aluminothermic or silicothermic manganese. The latter particularly begin to show the needle-like crystals of the manganese aluminum compound to the naked eye at about 3% manganese and at more than 5% manganese the alloys become coarsely crystalline and mechanically worthness. Alloys made in accordance with my invention remain finely crystalline and ductile even when containing more than 10% manganese. My conception of the theory which accounts for this difference in behavior is that the needle-like compound which causes brittleness is formed by the decomposition on cooling of another compound MnALi which forms first; and that the decomposition of this compound is so greatly accelerated by the impurities introduced by the ordinary methods of preparing the alloys that it is impossible to suppress its formation by a practicable rate of cooling.
The properties of alloys containing 1.25-10% manganese prepared in accordance with my invention are such as make the alloys useful for purposes that could not be fulfilled by the heretofore known alloys of the same nominal composition.
Earample 1.I have found that. an alloy containing 2% electrolytic manganese, balance aluminum, made in accordance with my invention, is highly ductile and can be rolled intosheet or shapes. Its tensile strength in the annealed state is 18,000 pounds per square inch and its elongation in 2 in. 20%. In the hard rolled state it shows a tensile strength of 35,000 pounds per square inch. This alloy can also be cast as.
is the practice with heretofore known alloys of this nominal composition and a much more duetile casting obtained.
Example 2.-I have found that an alloy of 3% electrolytic manganese, balance aluminum, has very valuable properties. In the cast and annealed state, it has a tensile strength of 20,000 pounds per square inch. It can be readily rolled without preliminary or intermediate heating to fine gauge sheet. At 50% reduction in thickness from the ingot it shows a tensile strength of 27,000 pounds per square inch and an elongation of 7%. With reduction, it shows a tensile strength of 50,000 pounds per square inch and an elongation of 3%. This alloy is useful as both a die cast and a wrought alloy.
Example 3.An alloy of 5% electrolytic manganese, balance aluminum, has a tensile strength as cast of 24,000 pounds per square inch and can be rolled to fine gauge sheet with a tensile strength of 60,000 pounds per square inch and 2% elongation.
Example 4.-An alloy of 7.5% electrolytic manganese, balance aluminum, has a tensile strength as cast of 30,000 pounds per square inch. This alloy is still sufiiciently ductile to roll with light passes and intermediate anneals. Full hard, it has a tensile strength of 63,000 pounds and an elongation of 1%. The intermediate anneals should be for a short time at about 500 degrees C.
Example 5.An alloy of 10% electrolytic manganese, balance aluminum, has a tensile strength as cast of 37,000 pounds and an elongation of 5%. This alloy is quite ductile but will find its greatest value in castings rather than as a wrought alloy.
Alloys containing somewhat more than 10% electrolytic manganese are generally similar to the 10% alloy but suffer a gradual decrease in ductility with increased manganese and are more difficult to make because of the increased melting point. However, my invention may be applied successfully up to about 20% electrolytic manganese.
All manganese-aluminum alloys, made in accordance with my invention containing more than 2% pure or electrolytic manganese, may be hardened by suitable heat treatment. .The preferred heat treatment is to quench from 600 degrees 0., cold work and then reheat to 180 degrees C. In this way, the strength is increased by about 10,000 pounds per square inch. Lesser increasesare obtained by reheating the quenched but unworked alloys.
The properties of all alloys of aluminum and pure or electrolytic manganese alone up to about 20% manganese will be clear from the above examples. I have found that the great enhancement of properties obtained by the practice of.
my invention in making the binary aluminummanganese alloys is also obtained when ternary and quaternary alloys are made by adding other elements to the aluminum manganese alloys. This is especially true of alloys containing magnesium. I have found that the manganese content of many alloys, especially those of the hardening type, may be advantageously increased by the practice of my invention. These alloys usually contain 0.5 to 0.8% manganese. I have found that this may be increased to as much as 2% with a definite improvement in mechanical properties and corrosion resistance. Some of the alloy compositions in which I have found it advantageous to practice my invention are as follows:
Example 6.--I produce an alloy containing .5% magnesium, 3.5% copper, .5% silicon, .5% to 2% electrolytic manganese, and balance aluminum. This alloy, through the range of manganese given, has substantially the same properties of the same alloy without the manganese, but with improved mechanical properties, and even some improvement in corrosion resistance.
Example 7.-I produce an alloy consisting of 4.5% copper, .5% to 2% electrolytic manganese,
and balance aluminum. The resulting alloy has desirable working properties, is ductile, and possesses substantially higher tensile strength and reater resistance to corrosion than a binary a1- loy of aluminum and electrolytic manganese.
Example 8.-High purity aluminum is alloyed with copper, magnesium and electrolytic manganese in accordance with the following proporions:
' Per cent Copper 4 Magnesium 2 Manganese .5 Aluminum 93.5
This alloy has desirable mechanical properties and the resistance to corrosion is improved over a similar alloy without the manganese. The manganese may be increased to about 1%, with a corresponding reduction in aluminum, and a useful alloy obtained. Cast into a chill mold, it produces a casting of good machining properties and desirable tensile strength.
Example 9.Alloys were produced containing in the range 1% to 2% electrolytic manganese, and containing in addition about 7% silicon, .3% magnesium, and balance aluminum. In the range of manganese given, corrosion resistance was high, and mechanical properties good. The alloy is particularly adapted for casting in a chill mold.
The terms pure manganese and high purity manganese as employed in the claims are used to identify electrolytic manganese, or manganese having substantially the same percentage and character of impurities as electrolytic manganese.
What I claim as new and desire to protect by Letters Patent of the United States is:
l. The method of preparing an al oy consisting substantially entirely of aluminum and man ganese, which comprises producing a liquid solution of electrolytic manganese, having a. purity of at least 99.9%, in high purity aluminum, the manganese comprising from'l.25% to 20% of the whole, and the product having less than .5% iron bed upon the manganese content, chill casting tl alloy from a temperature well above the liqui s, quenching the alloy from a relatively high temperature in the solid range, and reheating the alloy to a temperature of approximately degrees C., the resultant alloy being relatively free from the large needle-like crystals characteristic of ordinary alloys of aluminum with upwards of 2% manganese.
2. The method of preparing an alloy consisting substantially entirely of aluminum and manganese, which comprises producing a liquid solution of electrolytic manganese, having a purity of at least 99.9%, in high purity aluminum, the manganese comprising from 1.25% to 20% of the whole, and the product having less than .5% iron .based upon the manganese content, chill casting CRESAP M. MOSS.
US281219A 1939-06-26 1939-06-26 Aluminum alloy Expired - Lifetime US2296866A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US281219A US2296866A (en) 1939-06-26 1939-06-26 Aluminum alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US281219A US2296866A (en) 1939-06-26 1939-06-26 Aluminum alloy

Publications (1)

Publication Number Publication Date
US2296866A true US2296866A (en) 1942-09-29

Family

ID=23076427

Family Applications (1)

Application Number Title Priority Date Filing Date
US281219A Expired - Lifetime US2296866A (en) 1939-06-26 1939-06-26 Aluminum alloy

Country Status (1)

Country Link
US (1) US2296866A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3301711A (en) * 1964-09-25 1967-01-31 Jr Burnham W King Al-si-mn-li anode for high temperature galvanic cell
US3891433A (en) * 1973-02-16 1975-06-24 Alusuisse Induction-type reaction rails for high speed trains
US3899723A (en) * 1971-01-21 1975-08-12 Alusuisse Cathode foil for electrolytic condensers
EP0731185A1 (en) * 1995-03-10 1996-09-11 Pechiney Rhenalu Alumium-copper-magnesium alloy sheets with low residual stresses
US6077363A (en) * 1996-06-17 2000-06-20 Pechiney Rhenalu Al-Cu-Mg sheet metals with low levels of residual stress

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3301711A (en) * 1964-09-25 1967-01-31 Jr Burnham W King Al-si-mn-li anode for high temperature galvanic cell
US3899723A (en) * 1971-01-21 1975-08-12 Alusuisse Cathode foil for electrolytic condensers
US3891433A (en) * 1973-02-16 1975-06-24 Alusuisse Induction-type reaction rails for high speed trains
EP0731185A1 (en) * 1995-03-10 1996-09-11 Pechiney Rhenalu Alumium-copper-magnesium alloy sheets with low residual stresses
FR2731440A1 (en) * 1995-03-10 1996-09-13 Pechiney Rhenalu AL-CU-MG ALLOY SHEETS WITH LOW LEVEL OF RESIDUAL CONSTRAINTS
US6077363A (en) * 1996-06-17 2000-06-20 Pechiney Rhenalu Al-Cu-Mg sheet metals with low levels of residual stress

Similar Documents

Publication Publication Date Title
DE69801133T2 (en) Magnesium alloy with high high temperature properties and with good castability
US4239535A (en) Magnesium alloys
JPH0118979B2 (en)
US2210670A (en) Copper alloy
US3522039A (en) Copper base alloy
US3759758A (en) High strength aluminum casting alloy
US2296866A (en) Aluminum alloy
US2188203A (en) Aluminum base alloy
US2445868A (en) Copper base alloys
US2185348A (en) Aluminum base alloy
US2157934A (en) Copper-magnesium alloys of improved properties
US4072513A (en) Copper base alloys with high strength and high electrical conductivity
US3419385A (en) Magnesium-base alloy
US3764306A (en) Copper base alloy
US2280170A (en) Aluminum alloy
US3082082A (en) High strength, corrosionresistant alloy
US2098081A (en) Aluminum alloy
US1261987A (en) Method of making aluminum-alloy articles.
US3297435A (en) Production of heat-treatable aluminum casting alloy
US1912382A (en) Method of making and casting aluminum alloys
US2249740A (en) Aluminum alloys
US2720459A (en) Highly wear-resistant zinc base alloy
US3512961A (en) Fine grained white gold alloy
US2564044A (en) Aluminum-magnesium casting alloys
US4808243A (en) High damping zinc alloy with good intergranular corrosion resistance and high strength at both room and elevated temperatures