US1945288A - Zinc base alloy - Google Patents

Zinc base alloy Download PDF

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Publication number
US1945288A
US1945288A US549804A US54980431A US1945288A US 1945288 A US1945288 A US 1945288A US 549804 A US549804 A US 549804A US 54980431 A US54980431 A US 54980431A US 1945288 A US1945288 A US 1945288A
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alloy
zinc
aluminum
base alloy
alloys
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Expired - Lifetime
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US549804A
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Pascal J Morell
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American Brass Co
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American Brass Co
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Priority to US549804A priority Critical patent/US1945288A/en
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C18/00Alloys based on zinc
    • C22C18/04Alloys based on zinc with aluminium as the next major constituent

Definitions

  • This invention relates to a new zinc base alloy of superior strength and permanence developed more particularly for casting purposes and especially for die casting purposes.
  • the new alloy disclosed herein has the special advantage that it combines high strength with considerable permanence even when made with zinc of less special quality. It is to be distinctly understood, however, that the alloy described herein may be made with zinc of the highest purity obtainable and that the use of such zinc will add to those superior properties generally associated with the use of such pure zinc. It is intended that this patent shall cover the alloy disclosed when the zinc used therein is either of the special high purity grade (99.98+% zinc content) or the more widely used high grade or No. 1 as specified by the American Society for Testing Materials.
  • a zinc base alloy commonly in use at the pres-.- ent time contains about 4% aluminum, about 3% of copper and about 0.1% of magnesium.
  • a committee of the American Society for Testing Materials is recommending an alloy of this composition for adoption as a standard alloy by the society.
  • this alloy has the disadvantage that the physical properties of tensile strength, elongation and impact strength decrease with time even at normal atmospheric temperatures and more rapidly at elevated temperatures.
  • This change in physical properties is considered to be due to a phase change in the alloy.
  • Zinc-aluminum-copper alloys of the type represented by the composition 4% aluminum, 3 copper and remainder zinc form a rather complex ternary system which has been studied in detail by various investigators. It is considered that due to the rapid freezing and cooling of alloys in the die casting process that casting alloys of the above type are left in a phase of unstable equilibrium and that the alloy consequently tends to change with time to that form which is stable at normal temperatures.
  • This change involves the precipitation within the alloy of a relatively hard and brittle compound of copperand aluminum. It is the precipitation of this hard and brittle compound within the alloy that causes the decrease in physical properties known to occur in castings with time, that is upon aging.
  • a zinc base alloy containing from about 15% to about 35% aluminum and from-about 0.01% to about 0.2% magnesium has superior physical properties to other alloys at present used in die castings.
  • the alloy is improved in certain respects, particularly by increased tensil strength and hardness, by additions of small amounts of copper.
  • the aluminum is preferably from about 20% to about 24% and it is desirable to keep the magnesium as low as possible but sufiicient to prevent inter-crystalline corrosion. Where copper is added it is preferred from about 0.01% to about 5%.
  • a zinc base alloy containing around 20% aluminum and about 0.1% magnesium has very superior physical properties to other alloys at present used in die castings. The same was found to be true of a similar alloy containing about 20% aluminum, about 1% copper and about 0.05% magnesium.
  • maaese aluminum, about 0.1 percent magnesium, and the remainder zinc metal are maaese aluminum, about 0.1 percent magnesium, and the remainder zinc metal.
  • a zinc base alloy comprising from about to about 24% aluminum, about 0.01% to about 0.2% magnesium, and the balance zinc metal.

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

Description

Patented Jan. 30,1934
ZINC BASE ALLOY Pascal J. Morell, Waterbury, Conn., assignor to The American Brass Company,
Waterbury,
Conn., a corporation of Connecticut No Drawing. Application July 9, 1931 Serial No. 549,804
3 Claims.
This invention relates to a new zinc base alloy of superior strength and permanence developed more particularly for casting purposes and especially for die casting purposes.
5 Die casting alloys have been developed within recent years which show considerable improvement in physical properties and more particularly superior'permanence of size and shape as compared to alloys widely used in the die casting industry but a few years ago. These newer alloys,
however, require the use of a special zinc of a very high degree of purity and consequently extreme care must be used in the preparation and handling of the alloys in the manufacture of castings therefrom to avoid contamination.
The new alloy disclosed herein has the special advantage that it combines high strength with considerable permanence even when made with zinc of less special quality. It is to be distinctly understood, however, that the alloy described herein may be made with zinc of the highest purity obtainable and that the use of such zinc will add to those superior properties generally associated with the use of such pure zinc. It is intended that this patent shall cover the alloy disclosed when the zinc used therein is either of the special high purity grade (99.98+% zinc content) or the more widely used high grade or No. 1 as specified by the American Society for Testing Materials.
A zinc base alloy commonly in use at the pres-.- ent time contains about 4% aluminum, about 3% of copper and about 0.1% of magnesium. In fact a committee of the American Society for Testing Materials is recommending an alloy of this composition for adoption as a standard alloy by the society.
It is well known that this alloy has the disadvantage that the physical properties of tensile strength, elongation and impact strength decrease with time even at normal atmospheric temperatures and more rapidly at elevated temperatures. This change in physical properties is considered to be due to a phase change in the alloy. Zinc-aluminum-copper alloys of the type represented by the composition 4% aluminum, 3 copper and remainder zinc form a rather complex ternary system which has been studied in detail by various investigators. It is considered that due to the rapid freezing and cooling of alloys in the die casting process that casting alloys of the above type are left in a phase of unstable equilibrium and that the alloy consequently tends to change with time to that form which is stable at normal temperatures. This change involves the precipitation within the alloy of a relatively hard and brittle compound of copperand aluminum. It is the precipitation of this hard and brittle compound within the alloy that causes the decrease in physical properties known to occur in castings with time, that is upon aging.
Study of the ternary equilibrium diagram of zinc-copper-aluminum shows that the presence of the copper-aluminum compound under equilibrium conditions at normal temperatures is dependent on the ratio of copper and aluminum in the alloy.
Based on these facts and laboratory investigation I have discovered that a zinc base alloy containing from about 15% to about 35% aluminum and from-about 0.01% to about 0.2% magnesium has superior physical properties to other alloys at present used in die castings. The alloy is improved in certain respects, particularly by increased tensil strength and hardness, by additions of small amounts of copper. The aluminum is preferably from about 20% to about 24% and it is desirable to keep the magnesium as low as possible but sufiicient to prevent inter-crystalline corrosion. Where copper is added it is preferred from about 0.01% to about 5%. I have discovered that a zinc base alloy containing around 20% aluminum and about 0.1% magnesium has very superior physical properties to other alloys at present used in die castings. The same was found to be true of a similar alloy containing about 20% aluminum, about 1% copper and about 0.05% magnesium.
I have discovered further that the physical properties especially the ductility and impact strength increase with time. I have discovered still further that this increase in physical properties may be obtained and hastened by suitable heat treatment. It is intended that this beneficiation of physical properties by heat treatment shall form a part of this patent. I have found that with these alloys by heating for various lengths of time depending on the temperature certain improvement in their properties can be secured particularly the ductility and impact resistance, and the higher the temperature the more rapid the efiect up to temperatures slightly below the transformation temperature of the alloy. The maximum temperatures to which the alloy can be heated to secure this improvement depend in a large measure upon the casting conditions, the design of casting and the composition of the alloy. The beneficiation by heat treatment, that is improvement in physical properties by heat treatment is very important.
maaese aluminum, about 0.1 percent magnesium, and the remainder zinc metal.
3. A zinc base alloy comprising from about to about 24% aluminum, about 0.01% to about 0.2% magnesium, and the balance zinc metal. i
PASCAL J. MORELL.
US549804A 1931-07-09 1931-07-09 Zinc base alloy Expired - Lifetime US1945288A (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE759258C (en) * 1939-07-01 1952-10-27 Metallgesellschaft Ag Use of zinc alloys for objects that must have good toughness at low temperatures
DE974460C (en) * 1942-07-18 1960-12-29 Fr Nielsen & Co G M B H The use of zinc alloys with a high aluminum content
DE975916C (en) * 1943-06-09 1962-12-06 Fr Nielsen & Co G M B H Use of aluminum-zinc alloys
US3753791A (en) * 1970-01-01 1973-08-21 Imp Smelting Corp Ltd Heat-treatment of zinc/aluminium alloys
US3798028A (en) * 1971-07-21 1974-03-19 Noranda Mines Ltd Zinc-aluminum alloys with good machinability
US3847556A (en) * 1971-12-07 1974-11-12 Noranda Mines Ltd Screw machining material
US3850622A (en) * 1973-05-08 1974-11-26 St Joe Minerals Corp High strength zinc alloys
US3880679A (en) * 1971-07-21 1975-04-29 Noranda Mines Ltd Method of forming zinc-aluminum alloys with good machinability
JPS51105809U (en) * 1975-02-21 1976-08-24
USRE29038E (en) * 1973-05-08 1976-11-16 St. Joe Minerals Corporation High strength zinc alloys
DE3633338A1 (en) * 1986-10-01 1988-04-07 Teves Gmbh Alfred METAL INSERT, IN PARTICULAR MONOMETAL INSERT FOR STEERING WHEELS

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE759258C (en) * 1939-07-01 1952-10-27 Metallgesellschaft Ag Use of zinc alloys for objects that must have good toughness at low temperatures
DE974460C (en) * 1942-07-18 1960-12-29 Fr Nielsen & Co G M B H The use of zinc alloys with a high aluminum content
DE975916C (en) * 1943-06-09 1962-12-06 Fr Nielsen & Co G M B H Use of aluminum-zinc alloys
US3753791A (en) * 1970-01-01 1973-08-21 Imp Smelting Corp Ltd Heat-treatment of zinc/aluminium alloys
US3798028A (en) * 1971-07-21 1974-03-19 Noranda Mines Ltd Zinc-aluminum alloys with good machinability
US3880679A (en) * 1971-07-21 1975-04-29 Noranda Mines Ltd Method of forming zinc-aluminum alloys with good machinability
US3847556A (en) * 1971-12-07 1974-11-12 Noranda Mines Ltd Screw machining material
US3850622A (en) * 1973-05-08 1974-11-26 St Joe Minerals Corp High strength zinc alloys
USRE29038E (en) * 1973-05-08 1976-11-16 St. Joe Minerals Corporation High strength zinc alloys
JPS51105809U (en) * 1975-02-21 1976-08-24
DE3633338A1 (en) * 1986-10-01 1988-04-07 Teves Gmbh Alfred METAL INSERT, IN PARTICULAR MONOMETAL INSERT FOR STEERING WHEELS

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