US1852442A - Zinc-base die-casting alloy - Google Patents

Zinc-base die-casting alloy Download PDF

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Publication number
US1852442A
US1852442A US476946A US47694630A US1852442A US 1852442 A US1852442 A US 1852442A US 476946 A US476946 A US 476946A US 47694630 A US47694630 A US 47694630A US 1852442 A US1852442 A US 1852442A
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United States
Prior art keywords
zinc
alloy
aluminum
copper
base die
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
US476946A
Inventor
Edmund A Anderson
George L Werley
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.)
New Jersey Zinc Co
Original Assignee
New Jersey Zinc 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 New Jersey Zinc Co filed Critical New Jersey Zinc Co
Priority to US476946A priority Critical patent/US1852442A/en
Priority claimed from US478796A external-priority patent/US1852434A/en
Priority to AT134254D priority patent/AT134254B/en
Priority to FR721782D priority patent/FR721782A/en
Priority to GB23415/31A priority patent/GB376988A/en
Priority to CH160810D priority patent/CH160810A/en
Priority to GB24092/31A priority patent/GB376534A/en
Priority to CH159455D priority patent/CH159455A/en
Priority to AT138002D priority patent/AT138002B/en
Publication of US1852442A publication Critical patent/US1852442A/en
Application granted granted Critical
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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 zinc base die-casting alloys and has for its object the provision of an improved alloy of this character.
  • Zinc-aluminum alloys containing less than about 80% of aluminum undergo a structural change subsequent to solidification which is during the cooling of the alloy after casting or may through certain influences be retarded or inhibited. In such cases it may take place gradually over a period of months in at ordinary temperatures.
  • a secondary stage of phase change which sometimes occurs is the growth or coalescence of the extremely small particles of the new bases as first formed into larger particles.
  • This stage may be accompanied by softening Application filed August 21, 1930. Serial 1W0. 476,946.
  • Zinc-aluminum alloys in this range of composition are also subject to a type of disintegration commonly known as intercrystal- 4, line oxidation.
  • intercrystal- 4 line oxidation.
  • intercrystalline oxidation may'completely penetrate specimens of these alloys and cause swelling, warping and even complete disintegration.
  • t Intercrystalline oxidation is in some way associated with and partly dependent upon the phase change.
  • Our present invention is based on the discovery that in an alloy made with zinc metal of high purity and containing aluminum, for example 4%, the presence of a small amount r of copper (without magnesium), for example 1%, is sufiicient to give substantially complete resistance to intercrystalline oxidation.
  • the alloy containing 4% aluminum and 1% copper (without magnesium) has the advantage of a higher initial impact strength with a somewhat higher impact strength after ten days exposure to air saturated with moisture at 95 C.
  • the new alloy also has an appreciably higher ance zinc metal of high purity containing 9999+ zinc.
  • the zinc metal of high purity should contain not more than about 0.01% lead plus cadmium. Very satisfactory results have been secured with zinc metal containing 99.99+% zinc, less than 0.003% lead, less than 0.003% cadmium and less than 0.001% tin. Tin should be substantially excluded from the alloy and in no case should the tin content exceed about 0.001%.
  • alloy No. 4 is of the composition embraced within the present invention.
  • the tensile strength is indicated in pounds per square inch forflat and round test specimens.
  • the impact strength is indicated in foot pounds per square inch. Linear expansion is indicated in inches in; test sections in. and V in. in width.
  • a zinc base alloy consisting of about 4% aluminum, about 1% copper and the balance zinc metal of high purity with at least 99.98% v 2.
  • a zinc base alloy consisting of 2 to 5% aluminum, 0.05 to 2% copper, and in which the zinc base is zinc metal of high purity containing at least 99.98% zinc.

Description

Patented Apr. 5, 1932 UNITED STATES PATENT OFFICE}.
EDIUND A. ANDERSON AND GEORGE L. W'ERLEY, F PALMEfiTON, PENNSYLVANIA,
ASBIGNORS TO THE NEW JERSEY ZINC COMPANY, OF NEW YORK, N. Y., A 003- ronarron on NEW JERSEY ZINC-BASE DIE-CASTING- ALLOY Ho Drawing.
This invention relates to zinc base die-casting alloys and has for its object the provision of an improved alloy of this character.
The mechanical requirements of the diecasting operation necessitate the construction of the melting pot and die from iron and steel. These metals are subject to attack by molten zinc and it has been found from exerience that at least 0.25% aluminum must e added to the zinc in order to minimize this attack sufficiently to secure reasonable life from the apparatus. Alloys for die-casting must possess a sutficient degree of fluidity to properly flow into and completely fill the it dies used, and 2% or more aluminum appears to be necessary to secure an adequate degree of fluidity. It has also long been known that aluminum increases the tensile strength of zinc and this, in itself, makes its presence in zinc base die-casting'alloys desirable in quantities of form 2% to as much as 10 to 15%.
Zinc-aluminum alloys containing less than about 80% of aluminum undergo a structural change subsequent to solidification which is during the cooling of the alloy after casting or may through certain influences be retarded or inhibited. In such cases it may take place gradually over a period of months in at ordinary temperatures.
A secondary stage of phase change which sometimes occurs is the growth or coalescence of the extremely small particles of the new bases as first formed into larger particles. This stage may be accompanied by softening Application filed August 21, 1930. Serial 1W0. 476,946.
aussuEn and lowering of tensile strength and by an increase in ductility and impact strength.
Zinc-aluminum alloys in this range of composition are also subject to a type of disintegration commonly known as intercrystal- 4, line oxidation. In extreme cases, under the influence of warmth and moisture, intercrystalline oxidation may'completely penetrate specimens of these alloys and cause swelling, warping and even complete disintegration. t Intercrystalline oxidation is in some way associated with and partly dependent upon the phase change.
It has heretofore been recognized that certain other metals when present in these zinc-aluminum alloys exercise important effects on either the phase change or the intercrystalline oxidation or both. For example, copper and magnesium are known to exert an influence on the phase change either 1 5 in respect to the rate at which it takes place .or the completeness of the reaction or in some other respect not fully understood. The particular efl'ect produced by copper and magnesiumon the phase change reacts favorably in increasing the resistance of the alloys to intercrystalline oxidation. Lead, while not exerting any marked influence on the phase change, very seriously diminishes the resistance of these zinc-aluminum alloys to intercrystalline oxidation. Cadmium, though having a certain effect on the phase change, in the presence of lead usually diminishes the resistance of these alloys to intercrystalline oxidation. so
In the course of an exhaustive investigation of zinc base die-casting alloys, we have found that the tendency of zinc-aluminum alloys to undergo intercrystalline oxidation is greatly diminished by the elimination of harmful im- 55 August 17th, 1926, by the use of high grade zinc metal (e. g. horsehead brand) as the zinc base of the alloy. High grade zinc metal, however, contains as much as 0.05% of lead and to produce an alloy sufliciently free from intercrystalline oxidation with this amount of lead present, additions of both copper and magnesium are necessary since these metals individually tend to retard or prevent intercrystalline oxidation and when present together have a more or less additive beneficia effect. 1
Continued experiments with zinc metal con taining materially less lead than present in high grade zinc metal indicated definitely that there were important possibilities in this direction. The first important discovery was that if-the percentage of lead and other impurities in the zinc metal (used in making up the zinc base alloy) was less than 0.02%, with tin substantially absent, the presence of 0.1% magnesium in an alloy containing 4% aluminum (and without copper) was suflicient to prevent intercrystalline oxidation, and that such an alloy had other desirable physical properties. The advantage gained by the elimination of copper from this alloy was primarily an increased impact strength with better retention of this impact strength upon ageing either at room temperature or elevated temperatures. This discovery constitutes the basis of a copending patent application, Serial No. 368,730, filed June 5, 1929 (which has since issued into United States Patent No. 1,779,525, of October 28, 1930). However, the elimination of copper from the 4% aluminum, 3% copper, 0.1% magnesium alloy resulted in a lower tensile strength which under some circumstances, might make the alloy less valuable.
We next discovered that it was-not necessary to entirely eliminate the copper in order to obtain the advantageous characteristics of the last-mentioned alloy. On thecontrary, we found that additions of copper up to 1% are accompanied by slightly improved tensile strength apparently without any corollary disadvantages. This discovery forms the basis of our copending patent application Serial No. 476,452; filed August 19, 1930.
Our present invention is based on the discovery that in an alloy made with zinc metal of high purity and containing aluminum, for example 4%, the presence of a small amount r of copper (without magnesium), for example 1%, is sufiicient to give substantially complete resistance to intercrystalline oxidation. As compared with the 4% aluminum, 0.1% magnesium zinc base alloy (without copper), made with the same grade of high purity zinc metal, the alloy containing 4% aluminum and 1% copper (without magnesium) has the advantage of a higher initial impact strength with a somewhat higher impact strength after ten days exposure to air saturated with moisture at 95 C.
The new alloy also has an appreciably higher ance zinc metal of high purity containing 9999+ zinc. The zinc metal of high purity should contain not more than about 0.01% lead plus cadmium. Very satisfactory results have been secured with zinc metal containing 99.99+% zinc, less than 0.003% lead, less than 0.003% cadmium and less than 0.001% tin. Tin should be substantially excluded from the alloy and in no case should the tin content exceed about 0.001%.
The following tables illustrate the important physical properties of die-castings made of an alloy of the invention. Alloy No. 1 is of the composition described in United States Patent No. 1,596,761; alloy No. 2 is of the composition disclosed in my copending patent application Serial No. 368,730, alloy No.
-3 is of the composition disclosed in my copending patent application Serial No. 476,452; filed August 19, 1930; and alloy No. 4 is of the composition embraced within the present invention.
Composition 1 Alloy No. 1 41loyNo.2 Alloy No.3 g a 4 Pat. .N. 368,730 s. N. 476,452 1,596,761
Aluminum 4. 0% 4.0% 4. 0% 4.0% Copper 3. 0% 1. 0% 1. 0% Magnesium 0.1% v 0.1% p 0.1% Quality of zinc H i g h High puri- High puri- High puribase. grade ty 99.99% ty 99.99% ty 99.99%
Zn. Zn. Zn.
Properties as cast Tensile strength 46, 200 39, 400 42, 700 40. 800 Tensile strength round 45, 600 37,300 43,100 41,800 Impact strength" 108 130 169 288 Properties after ten days in steam at 95 C.
Tensile strength i] 27,800 31,600 33,400 34, 500 Tensile strength round 32, 800 31, 900 34, 400 36, 000 Impact strength" 8 142 137 170 Expansion wide 0. 0076 0. 0012 0. 0008 0 0006 Expansion $6" wide 0. 0068 0. 0016 0. 0006 0. 0007 The tensile strength is indicated in pounds per square inch forflat and round test specimens. The impact strength is indicated in foot pounds per square inch. Linear expansion is indicated in inches in; test sections in. and V in. in width.
We claim: 7
1. A zinc base alloy consisting of about 4% aluminum, about 1% copper and the balance zinc metal of high purity with at least 99.98% v 2. A zinc base alloy consisting of 2 to 5% aluminum, 0.05 to 2% copper, and in which the zinc base is zinc metal of high purity containing at least 99.98% zinc.
In testimony whereof we afiix our signatures.
EDMUND A. ANDERSON. GEORGE L. WERLEY.
US476946A 1930-08-21 1930-08-21 Zinc-base die-casting alloy Expired - Lifetime US1852442A (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
US476946A US1852442A (en) 1930-08-21 1930-08-21 Zinc-base die-casting alloy
CH160810D CH160810A (en) 1930-08-21 1931-08-19 Zinc-based alloy.
FR721782D FR721782A (en) 1930-08-21 1931-08-19 Zinc-based alloy for die-casting
GB23415/31A GB376988A (en) 1930-08-21 1931-08-19 Zinc-base die-casting alloy
AT134254D AT134254B (en) 1930-08-21 1931-08-19 Zinc alloy, especially for injection molding.
GB24092/31A GB376534A (en) 1930-08-21 1931-08-27 Zinc-base die-casting alloy
CH159455D CH159455A (en) 1930-08-21 1931-08-27 Zinc-based alloy.
AT138002D AT138002B (en) 1930-08-21 1931-08-27 Zinc alloy, especially for injection molding.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US476946A US1852442A (en) 1930-08-21 1930-08-21 Zinc-base die-casting alloy
US478796A US1852434A (en) 1930-08-29 1930-08-29 Zinc base die-casting alloy

Publications (1)

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US1852442A true US1852442A (en) 1932-04-05

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US476946A Expired - Lifetime US1852442A (en) 1930-08-21 1930-08-21 Zinc-base die-casting alloy

Country Status (5)

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US (1) US1852442A (en)
AT (2) AT134254B (en)
CH (2) CH160810A (en)
FR (1) FR721782A (en)
GB (2) GB376988A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0007695A1 (en) * 1978-06-09 1980-02-06 FORD AEROSPACE & COMMUNICATIONS CORPORATION Frangible projectile body

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE865978C (en) * 1941-03-04 1953-02-09 Metallgesellschaft Ag Use of zinc cast alloys
US2927856A (en) * 1952-03-31 1960-03-08 Chemalloy Electronics Corp Multi-purpose alloys of controlled homogeneity
US2907105A (en) * 1956-06-21 1959-10-06 Ohmi Rihei Method of soldering aluminum

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0007695A1 (en) * 1978-06-09 1980-02-06 FORD AEROSPACE & COMMUNICATIONS CORPORATION Frangible projectile body

Also Published As

Publication number Publication date
FR721782A (en) 1932-03-08
AT134254B (en) 1933-07-25
AT138002B (en) 1934-06-25
GB376534A (en) 1932-07-14
CH160810A (en) 1933-03-31
CH159455A (en) 1933-01-15
GB376988A (en) 1932-07-21

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