US1946069A - Magnesium base die casting alloys - Google Patents

Magnesium base die casting alloys Download PDF

Info

Publication number
US1946069A
US1946069A US679713A US67971333A US1946069A US 1946069 A US1946069 A US 1946069A US 679713 A US679713 A US 679713A US 67971333 A US67971333 A US 67971333A US 1946069 A US1946069 A US 1946069A
Authority
US
United States
Prior art keywords
per cent
alloys
magnesium
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
US679713A
Inventor
Leo B Grant
Otis E Grant
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.)
Dow Chemical Co
Original Assignee
Dow Chemical 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 Dow Chemical Co filed Critical Dow Chemical Co
Priority to US679713A priority Critical patent/US1946069A/en
Application granted granted Critical
Publication of US1946069A publication Critical patent/US1946069A/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
    • C22C23/00Alloys based on magnesium
    • C22C23/02Alloys based on magnesium with aluminium as the next major constituent

Definitions

  • the present invention relates to improved magnesium base alloys containing aluminum and manganese.
  • One object of our invention is to produce magnesium base alloys which contains both aluminum and manganese that are capable of being die-cast readily.
  • the magnesium base alloys containing from 8 to 15 per cent of aluminum and manganese in amount usually from 0.1 to about 0.5per cent have a good degree of resistance to corrosion and are among the strongest of the known alloys possessing the characteristic lightness and other valuable properties of the magnesium alloys, but they are difiicult to cast successfully in permanent die molds under pressure, as in die-casting. For example, it is extremely difiicult, at times impossible, to fill a permanent die mold of usual design, and when the cast metal solidifies in the mold cracks develop which render the casting unfit for use.
  • the development of cooling cracks is particularly noticeable when the castings are ribbed on the outer edges and thereby are held rigidly in the mold.
  • the only known procedures employed at present to minimize this crack formation have been to design a die mold so as to provide for as thick sections as possible and to avoid ribs, core pins, and the like, which tend to prevent uniform or regular shrinkage on cooling.
  • magnesium-aluminum-manganese alloys which contain from 8 to 15 per cent of aluminum and from 0.1 to 0.5 per cent of manganese are improved as respects their die-casting properties by the addition of small amounts of silicon, usually from 0.35 to 1.0 per cent being sufficient for the purpose.
  • the alloys which form the subject matter of our invention contain the four metals consisting of magnesium, aluminum, manganese, and silicon.
  • the aluminum content coming within the scope of our invention is between 8 and 15 per cent, that of manganese between 0.1 and 0.5 per cent, silicon between 0.35 and 1.0 per cent, the balance being magnesium.
  • the ease of die-casting the alloy increases slightly as the aluminum content is increased from the lower to the upper limit of the proportions specified, but the tensile strength appears We have discovered that the to reach a maximum at about 10 per cent.
  • the aluminum content therefore, may be chosen in accordance with the maximum die-casting quality desired in relation to the tensile strength.- From about 9 to 12 per cent of aluminum is satisfactory for most uses.
  • Manganese has a limited solubility in the alloys of this invention. What appears to be the saturating quantity of manganese varies from about 0.1 to 0.3 per cent as the aluminum content varies from 15 to 8 per cent, respectively, since aluminum reduces the solubility of manganese in the alloy. We have found that from 0.1 per cent up to about 0.15 or 0.2 per cent of manganese is a sufficient amount to employ in most instances although up to 0.5 per cent may be introduced if desired.
  • alloys may be prepared in any convenient manner by employing any of the well known metallurgical methods of melting and alloying magnesium, and any combination of proportions 1
  • a magnesium base alloy consisting of aluminum in amount from 8 to 15 per cent, manganese from 0.5 to 0.1 per cent, silicon from 0.35 to 1.0 per cent, the balance being magnesium.
  • a magnesium base alloy consisting .of aluminum in amount from 8 to 12 per cent, manganese from 0.3 to 0.1 per cent, silicon from 0.35 to 1L0 per cent, the balance being magnesium.
  • a magnesium base alloy consisting of aluminum in amount from 9 to 12 per cent, manganese from. 0.2 to 0.1 per cent, silicon from 0.5 to

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

Patented Feb. 6, 1934 UNITED STATES MAGNESIUM BASE DIE CASTING ALLOYS Leo B. Grant and Otis E. Grant, Midland, Mich., assignors to The Dow Chemical Company, Mid land, Mich., a corporation of Michigan No Drawing. Application July 10, 1933 Serial No. 679,713
3 Claims.
The present invention relates to improved magnesium base alloys containing aluminum and manganese. One object of our invention is to produce magnesium base alloys which contains both aluminum and manganese that are capable of being die-cast readily.
The magnesium base alloys containing from 8 to 15 per cent of aluminum and manganese in amount usually from 0.1 to about 0.5per cent have a good degree of resistance to corrosion and are among the strongest of the known alloys possessing the characteristic lightness and other valuable properties of the magnesium alloys, but they are difiicult to cast successfully in permanent die molds under pressure, as in die-casting. For example, it is extremely difiicult, at times impossible, to fill a permanent die mold of usual design, and when the cast metal solidifies in the mold cracks develop which render the casting unfit for use. The development of cooling cracks is particularly noticeable when the castings are ribbed on the outer edges and thereby are held rigidly in the mold. The only known procedures employed at present to minimize this crack formation have been to design a die mold so as to provide for as thick sections as possible and to avoid ribs, core pins, and the like, which tend to prevent uniform or regular shrinkage on cooling.
Inasmuch as it is not possible in all instances to modify the shape of. the casting to suit the characteristics of the alloy, we have attempted to find other metals which, when added to the aforementioned magnesium-aluminum-manganese alloys, would provide an alloy which tends to fill the mold'readily and to solidify without developing cracks. magnesium-aluminum-manganese alloys which contain from 8 to 15 per cent of aluminum and from 0.1 to 0.5 per cent of manganese are improved as respects their die-casting properties by the addition of small amounts of silicon, usually from 0.35 to 1.0 per cent being sufficient for the purpose.
The alloys which form the subject matter of our invention, then, contain the four metals consisting of magnesium, aluminum, manganese, and silicon. The aluminum content coming within the scope of our invention is between 8 and 15 per cent, that of manganese between 0.1 and 0.5 per cent, silicon between 0.35 and 1.0 per cent, the balance being magnesium.
The ease of die-casting the alloy increases slightly as the aluminum content is increased from the lower to the upper limit of the proportions specified, but the tensile strength appears We have discovered that the to reach a maximum at about 10 per cent. The aluminum content, therefore, may be chosen in accordance with the maximum die-casting quality desired in relation to the tensile strength.- From about 9 to 12 per cent of aluminum is satisfactory for most uses.
Manganese has a limited solubility in the alloys of this invention. What appears to be the saturating quantity of manganese varies from about 0.1 to 0.3 per cent as the aluminum content varies from 15 to 8 per cent, respectively, since aluminum reduces the solubility of manganese in the alloy. We have found that from 0.1 per cent up to about 0.15 or 0.2 per cent of manganese is a sufficient amount to employ in most instances although up to 0.5 per cent may be introduced if desired.
In testing the casting quality of our new alloys, we prepared a die mold in which a die-casting could be made that was 18.5" long by 6" wide and 0.090" thick throughout except for the edges which were 0.25" thick. Into this mold we attempted to cast a number of magnesium-aluminum-manganese alloys containing from 8 to 15 per cent aluminum and from 0.1 to 0.5 per cent manganese, the balance being magnesium, that were substantially free from silicon. We have found that such alloys did not readily take the mold impression and flow lines on the surface of the casting spoiled their appearance and utility. In addition to these defects the castings usually were cracked near the edges. Commercial casting free from cracks and surface fiow lines were readily obtained from the same mold when the composition of the alloy was changed by adding thereto from 0.35 to 1.0 per cent of silicon. The maximum improving effect of silicon on the die-casting quality of these alloys is developed when the silicon content is from 0.5 to 1.0 per cent which amount preferably is employed. The addition of silicon also reduces the casting temperature approximately 25 F. over the temperature necessary for the alloys without silicon, thus reducing the tendency for flaws to be produced from excessive oxidation.
After casting our new alloys are capable of improvement in mechanical properties by the well known heat treatment procedures provided for magnesium alloys which are capable of undergoing solid solution changes or precipitation changes on prolonged heating.
These alloys may be prepared in any convenient manner by employing any of the well known metallurgical methods of melting and alloying magnesium, and any combination of proportions 1 A magnesium base alloy consisting of aluminum in amount from 8 to 15 per cent, manganese from 0.5 to 0.1 per cent, silicon from 0.35 to 1.0 per cent, the balance being magnesium.
2. A magnesium base alloy consisting .of aluminum in amount from 8 to 12 per cent, manganese from 0.3 to 0.1 per cent, silicon from 0.35 to 1L0 per cent, the balance being magnesium.
3. A magnesium base alloy consisting of aluminum in amount from 9 to 12 per cent, manganese from. 0.2 to 0.1 per cent, silicon from 0.5 to
1Z0 per cent, the balance being-magnesium.
. .LEO B. GRANT,
OTIS E. GRANT.
US679713A 1933-07-10 1933-07-10 Magnesium base die casting alloys Expired - Lifetime US1946069A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US679713A US1946069A (en) 1933-07-10 1933-07-10 Magnesium base die casting alloys

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US679713A US1946069A (en) 1933-07-10 1933-07-10 Magnesium base die casting alloys

Publications (1)

Publication Number Publication Date
US1946069A true US1946069A (en) 1934-02-06

Family

ID=24728044

Family Applications (1)

Application Number Title Priority Date Filing Date
US679713A Expired - Lifetime US1946069A (en) 1933-07-10 1933-07-10 Magnesium base die casting alloys

Country Status (1)

Country Link
US (1) US1946069A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3162552A (en) * 1961-06-02 1964-12-22 Dow Chemical Co Magnesium-base extrusion alloy
US3630726A (en) * 1968-06-26 1971-12-28 Magnesium Elektron Ltd Magnesium base alloys
US3718460A (en) * 1970-06-05 1973-02-27 Dow Chemical Co Mg-Al-Si ALLOY
US5201352A (en) * 1989-05-30 1993-04-13 Fmg Timberjack Ab Rotatable blade for clearing units

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3162552A (en) * 1961-06-02 1964-12-22 Dow Chemical Co Magnesium-base extrusion alloy
US3630726A (en) * 1968-06-26 1971-12-28 Magnesium Elektron Ltd Magnesium base alloys
US3718460A (en) * 1970-06-05 1973-02-27 Dow Chemical Co Mg-Al-Si ALLOY
US5201352A (en) * 1989-05-30 1993-04-13 Fmg Timberjack Ab Rotatable blade for clearing units

Similar Documents

Publication Publication Date Title
US2336512A (en) Aluminum base alloy
US1946069A (en) Magnesium base die casting alloys
US2802733A (en) Process for manufacturing brass and bronze alloys containing lead
US2420293A (en) Magnesium base alloys
US2885286A (en) Anodizable aluminum die casting alloy
US1934281A (en) Aluminum-silicon alloy
US1932837A (en) Aluminum alloys
US2720459A (en) Highly wear-resistant zinc base alloy
US2123886A (en) Heat treated aluminum base alloy
US2098081A (en) Aluminum alloy
US1932838A (en) Aluminum alloys
US1718502A (en) Copper-aluminum alloy
US1852442A (en) Zinc-base die-casting alloy
US1572744A (en) Nickel alloy and method of making the same
US1932856A (en) Aluminum alloys
US1932872A (en) Aluminum alloys
US2583473A (en) Aluminum-magnesium alloys
US1932866A (en) Aluminum alloys
US1932844A (en) Aluminum alloys
US2254202A (en) Aluminum alloy
US1352272A (en) Alloy
US1932864A (en) Aluminum alloys
US1997494A (en) Aluminum-base alloy
US1932840A (en) Aluminum alloys
US3125443A (en) azzza