US2671039A - Magnesium die casting alloy and process - Google Patents

Magnesium die casting alloy and process Download PDF

Info

Publication number
US2671039A
US2671039A US666759A US66675946A US2671039A US 2671039 A US2671039 A US 2671039A US 666759 A US666759 A US 666759A US 66675946 A US66675946 A US 66675946A US 2671039 A US2671039 A US 2671039A
Authority
US
United States
Prior art keywords
magnesium
alloy
die casting
manganese
aluminum
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
US666759A
Inventor
Richard F Hauser
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Priority to US666759A priority Critical patent/US2671039A/en
Application granted granted Critical
Publication of US2671039A publication Critical patent/US2671039A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • C22C23/02Alloys based on magnesium with aluminium as the next major constituent

Definitions

  • the present invention relates to a novel magnesium die casting alloy and process for producing such an alloy, and is a continuation in part as to all common subject matter of my copending application Serial No. 575,568 filed January 31, 1945, for Magnesium Die Casting Alloy and Process, now abandoned.
  • An object of the invention is to provide a magnesium alloy having excellent die casting characteristics, whereby both light and heavy sections may be die cast with slight tendency to- .wards hot cracking during the die casting process and only moderate tendency towards internal porosity in the heavy sections.
  • Another object of the invention is to provide a magnesium alloy having superior corrosion resistance due in part to its manganese content and also to its low impurity content caused by the settling out in large part of such impurities through the nove1 method employed in preparing the alloy.
  • Another object of the invention is to provide a novel process for preparing a magnesium al-
  • Another object of the invention is'to provide a novel method of preparing a magnesium alloy in which there is added to a magnesium-manganese alloy an amount of aluminum to decrease the solubility of the manganese in the alloy so as to precipitate a portion of the manganese out of solution tending to cleanse the melt of suspended iron particles while the temperature-of the melt is maintained sufiiciently high so as to prevent reduction of the manganese below a predetermined desired value.
  • Another object of the invention is to provide 7 a process for causing an equi-axed grain structure to occur with resultant improved ductility and stability to the material.
  • equiaxed is meant the approximate equal dimensions of the grain with relation to their own axes and in relation to each other.
  • the alloy is prepared by melting a binary magnesium-manganese alloy containing approximately 1.5% manganese by weight, and to the molten metal adding'l.00% to 1.5% aluminum byweight at approximately 1250-1350 degrees Fahrenheit.
  • the temperature of the alloy should never be allowed to drop below 1250 degrees Fahrenheit before being cast or frozen, as such a decrease in temperature below 1250 degrees Fahrenheit during the settling process might cause an adverse reduction of the manganese below the specified desired minimum of .5%. It is important to retain at least this amount of manganese in order to still further increase the "corrosion resistance of the alloy.
  • the magnesium-alloy thus obtained will have an aluminum content by weight of between 1.0% to 1.5 a manganese content by weight of not less than a .5% minimum and impurities or other ingredients by weight not in excess of a .3% maximum.
  • v r Upon completion of the settling process-the thus-cleansed magnesium-manganese-aluminum alloy is removed and may be directly die cast or may be cast into pigs for convenience in handling. In the latter event, the pigs, as desired, are reheated to atemperature of between 1250 degrees and 1350 degrees Fahrenheit for pouring into a die casting mechanism of conventional type.
  • This alloy has the following composition:
  • Yield strength is defineclasthestressat which thev-stressestrain curve-deviates: 2%? from the modulus line.
  • a die cast magnesium-alloy consisting of between about 1.0%and about 1.5% by weight of aluminum; total elements other than-magnesiumand aluminum not in excess of about 1.3% by weight, and the balance of magnesium, said alloy having a substantially homogeneous equi-axed grain stucture.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Description

MAGNESIUM DIE CASTING ALLOY AND PROCESS Filed May 2, 1946 I NVENTOR R/L'HHHU E HflL/SEH ATTORNEY {y for use in die casting.
Patented Mar. 2, 1954 UNITED STATES PATENT- OFFICE MAGNESIUM DIE CASTING'ALLOY AND PROCESS Richard F. Hauser, Bergenfield, N. J assignor to Bendix Aviation Corporation, Teterboro, N. J a corporation of Delaware Application May 2, 1946, Serial No. 666,759
4 Claims.
The present invention relates to a novel magnesium die casting alloy and process for producingsuch an alloy, and is a continuation in part as to all common subject matter of my copending application Serial No. 575,568 filed January 31, 1945, for Magnesium Die Casting Alloy and Process, now abandoned.
An object of the invention is to provide a magnesium alloy having excellent die casting characteristics, whereby both light and heavy sections may be die cast with slight tendency to- .wards hot cracking during the die casting process and only moderate tendency towards internal porosity in the heavy sections.
Another object of the invention is to provide a magnesium alloy having superior corrosion resistance due in part to its manganese content and also to its low impurity content caused by the settling out in large part of such impurities through the nove1 method employed in preparing the alloy.
Another object of the invention is to provide a novel process for preparing a magnesium al- Another object of the invention is'to provide a novel method of preparing a magnesium alloy in which there is added to a magnesium-manganese alloy an amount of aluminum to decrease the solubility of the manganese in the alloy so as to precipitate a portion of the manganese out of solution tending to cleanse the melt of suspended iron particles while the temperature-of the melt is maintained sufiiciently high so as to prevent reduction of the manganese below a predetermined desired value.
Another object of the invention is to provide 7 a process for causing an equi-axed grain structure to occur with resultant improved ductility and stability to the material. By the term equiaxed is meant the approximate equal dimensions of the grain with relation to their own axes and in relation to each other.
Other objects and advantages of this invention 4 are set forth in the following description and the novel features thereof are pointed out in the appended claims. The disclosure, however, is il lustrative only and changes may be made therein within the principle of the invention to the full extent indicated by the broad and general meanings of the terms in which the appended claims are expressed.
In Figure 1, there is illustrated a photo-micrograph of a typical grain structure obtained in this alloy in the as cast condition and before aging. In Figure 2, there is illustrated a photo-micrograph of a typical grain structure obtained in this alloy after the heat treatment or artificial aging process explained hereinafter and forming the subject matter of the present application. 1 I v Specifically, as an example of my invention, the alloy is prepared by melting a binary magnesium-manganese alloy containing approximately 1.5% manganese by weight, and to the molten metal adding'l.00% to 1.5% aluminum byweight at approximately 1250-1350 degrees Fahrenheit.
The addition of this amount of aluminum will decrease the solubility of the manganese in the magnesium to between .5% and 1.0% by Weight. The melt is held at this temperature for an appreciable period depending upon size of melt, for example, a minimum of fifteen minutes for a thousand pound melt; so that the manganese which is precipitated out of solution tends to cleansethe melt of suspended iron and other particles by causing them to sink to the bottom of the melt due to agglomeration of these particles to the precipitated primary manganese. This action is not to be confused with the heretofore known settling process in which the precipitation of manganese depends primarily upon holding the melt for long periods of time at relatively low temperatures. In the instant process the temperature of the alloy should never be allowed to drop below 1250 degrees Fahrenheit before being cast or frozen, as such a decrease in temperature below 1250 degrees Fahrenheit during the settling process might cause an adverse reduction of the manganese below the specified desired minimum of .5%. It is important to retain at least this amount of manganese in order to still further increase the "corrosion resistance of the alloy. v
The magnesium-alloy thus obtained will have an aluminum content by weight of between 1.0% to 1.5 a manganese content by weight of not less than a .5% minimum and impurities or other ingredients by weight not in excess of a .3% maximum. v r Upon completion of the settling process-the thus-cleansed magnesium-manganese-aluminum alloy is removed and may be directly die cast or may be cast into pigs for convenience in handling. In the latter event, the pigs, as desired, are reheated to atemperature of between 1250 degrees and 1350 degrees Fahrenheit for pouring into a die casting mechanism of conventional type.
- Due to the short time for diffusion during solidification, sufficient deviation from equilibrium conditions are attained to permit a small amount .of theharclening materia1-or eutectic to be retained atithe grainiboundarie's ofv the solidified metal. Precipitation of the eutectic, an aluminum magnesium compound, is later ac= centuated 'by a novel artifical aging process explained hereinafter. However, the: amount of this material in the grain boundaries is not suni cient to cause excessive hot shortness or embrittlement of the die castings atielevated terns peratures, since the aluminum content is prefer.- ably maintained at a value not in excess of 1.5% by weight. It has been found.- that' with an aluminum content in excess of 1.5%, hot-shortness or embrittlement at elevated temperatures becomes so pronounced-that it would be very 'dimcult to make" certain die castings without hot-cracking occurring as the casting is ejected from :thedie.
vvItjis important, however, that the" aluminum 'content'of the alloy'b'e maintainedat a mini-- mum'of 1.0% or good mechanical properties will 'notbeobtained' in'the subsequent die castings after the heat treatment or aging processand internal'porosity will be increased to such an extent as'to cause'the castings to be unsound;
This alloy has the following composition:
Aluminum 1.0-1.5% -Manganese-- 0.5-1.0% Nickel 0.005%max. Iron 0.005% max. Copper 0.05%max. Silicon 1 0.03% max. Total elements other. than .Mg, Al,
and Mn 0.3 max. Magnesium Balance I Theab'ove alloy is-then die cast andit has been found' that'by subjecting the die casting to a higher annealing temperature than customarily used'for annealing or aging, and reducing the time at suchtemperature, a maximum amountof precipitation of the intermetallicchemical'compound of aluminum-magnesium could be obtained; This-resulted in increased yield strength and-hardness of castings of this alloy so treated,
equi axedzstructure as?shown for'example. in the drawingof Figure 2 which materially improves the mechanical properties of the. material.
The comparative mechanical properties of the sameiare: as. follows:
Heat AS Cast Treated Condition 4 hrs. at
Tensile Strength, p. s. i 30, 000 32, 000 Yield Strength.-. 8, 000 21,000 Elongation, pcrcen l6 9 Impact, loot lbs l4 l0 Hardness RE; -l 35, 65
Yield strength is defineclasthestressat which thev-stressestrain curve-deviates: 2%? from the modulus line.
From the foregoing it will be readily seen that there has been provided a novel improved magnesiunr. alloy? and novel heat treating or aging process for producing the same.
Whileonly one.form of the invention is illustrated'herein, it isto be clearly understood that the inventionisnot to be limited thereto, but the same is to be considered merely as illustra tive of'theipraetice thereof, since the invention is nottobe limited except by the appended claims.
What is claimed is:
1; A die cast magnesium alloyconsistingof between 113% and 1.5% by weight of aluminum; between 0.5% and'1.0% by weightof manganese; total elements other than magnesium, manganese and aluminum not in excessof .3%-by weight, and the-balance of magnesium, said alloy having a substantially homogeneous equi axed grain structure.
2. A die cast magnesium-alloy consisting of between about 1.0%and about 1.5% by weight of aluminum; total elements other than-magnesiumand aluminum not in excess of about 1.3% by weight, and the balance of magnesium, said alloy having a substantially homogeneous equi-axed grain stucture.
3. A process for heat treating a die casting of a magnesium base alloyto improve the grain structurethereoi, in which said magnesium alloy contains between 1.0% to 15% by weight' of aluminum and the balance substantially of magnesium; comprising subjecting thescasting' to-a temperature of approximately 475-' F. for approximately four hours.
4. A process for heat treating a die casting-of a magnesium base alloy' to improve the grain structure thereof, inwhich said'magnesium alloy contains between 1.0% to 1.5% by weight of aluminum and the balance substantially of magnesium; comprising'subiecting the casting to heat treatment at'a temperature'of from about 450'to about 500 F. for approximately three tofi-'ve hours.
RICHARD F. HAUSERi References Cited in .thesfil'efof this: patent."
, UNITED STATES PATENTS Number.
(Provisional and amended) OTHER REFERENCES Die'Casting, by-Herb, page 51, 1936.
Metals Handbook, page 1583, Am. Soc. for Metals, 1939.
Die Casting; for Engineers, pub. by New Jersey Zinc, pages 28-31, 1942.
Magnesium, pages 67 and 68. Am. Soc. for Metals; 1946.

Claims (1)

  1. 3. A PROCESS FOR HEAT TREATING A DIE CASTING OF A MAGNESIUM BASE ALLOY TO IMPROVE THE GRAIN STRUCTURE THEREOF, IN WHICH SAID MAGNESIUM ALLOY CONTAINS BETWEEN 1.0% TO 1.5% BY WEIGHT OF ALUMINUM AND THE BALANCE SUBSTANTIALLY OF MAGNESIUM; COMPRISING SUBJECTING THE CASTING TO A TEMPERATURE OF APPROXIMATELY 475* F. FOR APPROXIMATELY FOUR HOURS.
US666759A 1946-05-02 1946-05-02 Magnesium die casting alloy and process Expired - Lifetime US2671039A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US666759A US2671039A (en) 1946-05-02 1946-05-02 Magnesium die casting alloy and process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US666759A US2671039A (en) 1946-05-02 1946-05-02 Magnesium die casting alloy and process

Publications (1)

Publication Number Publication Date
US2671039A true US2671039A (en) 1954-03-02

Family

ID=24675342

Family Applications (1)

Application Number Title Priority Date Filing Date
US666759A Expired - Lifetime US2671039A (en) 1946-05-02 1946-05-02 Magnesium die casting alloy and process

Country Status (1)

Country Link
US (1) US2671039A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3370945A (en) * 1965-06-28 1968-02-27 Dow Chemical Co Magnesium-base alloy
US5679381A (en) * 1992-08-11 1997-10-21 E. Khashoggi Industries Systems for manufacturing sheets from hydraulically settable compositions

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1959913A (en) * 1932-01-29 1934-05-22 Dow Chemical Co Magnesium base forging alloy
US2029898A (en) * 1929-01-02 1936-02-04 Magnesium Dev Corp Method of purifying magnesium
US2029728A (en) * 1934-02-12 1936-02-04 Dow Chemical Co Rolling magnesium alloys
US2205851A (en) * 1938-04-01 1940-06-25 Rca Corp Temperature cycling
US2267862A (en) * 1940-09-21 1941-12-30 Dow Chemical Co Removal of iron from magnesiumbase alloys
US2280103A (en) * 1939-12-09 1942-04-21 Cleveland Graphite Bronse Comp Rolled copper alloy article
GB560104A (en) * 1940-05-01 1944-03-21 Tennyson Fraser Bradbury Magnesium alloy

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2029898A (en) * 1929-01-02 1936-02-04 Magnesium Dev Corp Method of purifying magnesium
US1959913A (en) * 1932-01-29 1934-05-22 Dow Chemical Co Magnesium base forging alloy
US2029728A (en) * 1934-02-12 1936-02-04 Dow Chemical Co Rolling magnesium alloys
US2205851A (en) * 1938-04-01 1940-06-25 Rca Corp Temperature cycling
US2280103A (en) * 1939-12-09 1942-04-21 Cleveland Graphite Bronse Comp Rolled copper alloy article
GB560104A (en) * 1940-05-01 1944-03-21 Tennyson Fraser Bradbury Magnesium alloy
US2267862A (en) * 1940-09-21 1941-12-30 Dow Chemical Co Removal of iron from magnesiumbase alloys

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3370945A (en) * 1965-06-28 1968-02-27 Dow Chemical Co Magnesium-base alloy
US5679381A (en) * 1992-08-11 1997-10-21 E. Khashoggi Industries Systems for manufacturing sheets from hydraulically settable compositions

Similar Documents

Publication Publication Date Title
US3794531A (en) Method of using a highly stable aluminum alloy in the production of recrystallization hardened products
US4636357A (en) Aluminum alloys
JP2011208253A (en) Aluminum die-cast alloy for vehicle material
US2915390A (en) Aluminum base alloy
US2671039A (en) Magnesium die casting alloy and process
US1508556A (en) Making castings of aluminum alloys
JPH09296245A (en) Aluminum alloy for casting
US2795501A (en) Copper base alloys
US2185452A (en) Method of heat treating magnesium base alloys
US2280170A (en) Aluminum alloy
US2575273A (en) Process for producing a magnesium die-casting alloy
US2022686A (en) Aluminum alloy casting and method of making the same
US1960916A (en) Aluminium alloy
US1936550A (en) Heat treating magnesium base alloys
US2214432A (en) Aluminum alloy containing copper, iron, and columbium
JPH01108339A (en) Aluminum alloy for piston combining heat resistance with high strength
US2123886A (en) Heat treated aluminum base alloy
US2280174A (en) Aluminum alloy
GB638733A (en) Improvements in and relating to zinc casting alloys
US2781263A (en) Aluminium base alloy
US2280176A (en) Aluminum alloy
US2226594A (en) Aluminum alloy
JPS633020B2 (en)
US2263823A (en) Method of producing and treating aluminum alloy castings
US1572489A (en) Aluminum alloy