US3892565A - Magnesium alloy for die casting - Google Patents

Magnesium alloy for die casting Download PDF

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Publication number
US3892565A
US3892565A US402019A US40201973A US3892565A US 3892565 A US3892565 A US 3892565A US 402019 A US402019 A US 402019A US 40201973 A US40201973 A US 40201973A US 3892565 A US3892565 A US 3892565A
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percent
magnesium
zinc
alloy
copper
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US402019A
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George S Foerster
Charles D Statham
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Farley Inc
NL Industries Inc
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NL Industries Inc
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Priority to US402019A priority Critical patent/US3892565A/en
Priority to DE19742445843 priority patent/DE2445843C3/en
Priority to NO743470A priority patent/NO132493C/no
Priority to JP49112244A priority patent/JPS5062112A/ja
Priority to AU73799/74A priority patent/AU480105B2/en
Priority to FR7432921A priority patent/FR2246647B1/fr
Priority to ES430531A priority patent/ES430531A1/en
Priority to BR8070/74A priority patent/BR7408070D0/en
Priority to GB4263274A priority patent/GB1423127A/en
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Assigned to FARLEY METALS, INC. reassignment FARLEY METALS, INC. ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: NL INDUSTRIES, INC. A NJ CORP.
Assigned to NATWEST USA CREDIT CORP. reassignment NATWEST USA CREDIT CORP. SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: FARLEY METALS, INC.,
Assigned to FARLEY, INC. reassignment FARLEY, INC. CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). EFFECTIVE DEC. 28, 1987 Assignors: FARLEY METALS, INC.
Assigned to BANK OF NEW YORK, THE reassignment BANK OF NEW YORK, THE SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: FARLEY INC.
Assigned to FARLEY, INC. reassignment FARLEY, INC. RELEASED BY SECURED PARTY (SEE DOCUMENT FOR DETAILS). RECORDED AT REEL 4739, FRAME 0041 Assignors: NATWEST USA CREDIT CORP.
Assigned to CONTINENTAL BANK N.A. reassignment CONTINENTAL BANK N.A. SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: DOEHLER-JARVIS LIMITED PARTNERSHIP, A DE. LIMITED PARTNERSHIP
Assigned to FARLEY INC. reassignment FARLEY INC. CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: FARLEY METALS, INC., A CORP. OF DE.
Assigned to FARLEY INC. reassignment FARLEY INC. RELEASED BY SECURED PARTY (SEE DOCUMENT FOR DETAILS). RELEASE OF SECURED PARTY OF INTEREST RECORDED AT REE 5221 FRAME 038-043 ON JUNE 21, 1989 Assignors: BANK OF NEW YORK, THE
Assigned to FARLEY INC. reassignment FARLEY INC. CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). EFFECTIVE ON 12/28/1987 Assignors: FARLEY METALS, INC., A CORP. OF DE
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • C22C23/04Alloys based on magnesium with zinc or cadmium as the next major constituent

Definitions

  • the pentagon is bounded by straight lines connecting the following points:
  • compositions of the various alloys are recorded in Table l.
  • alloys having compositions which contain less than 0.6 percent copper but which lie inside the pentagon ABCDE were prepared as controls and their results were compared with the above examples.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Prevention Of Electric Corrosion (AREA)
  • Treatment Of Steel In Its Molten State (AREA)
  • Continuous Casting (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Mold Materials And Core Materials (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Abstract

A die cast alloy of magnesium has been produced which contains the following ingredients:

ALL OF THE PERCENTAGES EXPRESSED ON A WEIGHT BASIS. This alloy has good castability properties coupled with reduced creep extension.

Description

United States Patent Foerster et a1. July 1, 1975 MAGNESIUM ALLOY FOR DIE CASTING 393,837 6/1933 United Kingdom 75/168 D 51 ,4 4 K' d H 7' [75] Inventors: George S. Foerster, Monmouth 6 64 Ummd mg om 3/168 C Junction; Charles D. Statham, Trenton, both of NJ. Primary ExaminerC. Lovell [73] Assignee: N L Industries, Incorporated, New
57 ABSTRACT 22 F1 d: O t. 1 1973 1 c A die cast alloy of magnesium has been produced 1 1 pp 402,019 which contains the following ingredients:
[52] US. Cl .1 75/168 C; 75/168 B; 75/168 D;
148/32 5.0% to 200% zinc 0% 815% l 511 lm. Cl. C22c 23/00 ;3 60% g 'gg [58] Field of Search 75/168 B, 168 C, 168 D, 10(5):: :0 rnlenganesc O SI ICOn 75/168 M, 168 E, 168 F, 148/32, 164/284, 303 he remainder magnesium [56] References Cited UNITED STATES PATENTS all of the percentages expressed on a weight basis. 1,341,774 6/1920 Backer 75/168 C Thi h d Stability properties coupled with FOREIGN PATENTS OR APPLICATIONS reduced Creep exlension 382,420 10/1931 United Kingdom 75/168 C 2 Claims Drawing Figure E a .E E a I: a-
D 1 c O 5 l0 15 2O 7,, Zinc 1 MAGNESIUM ALLOY FOR DIE CASTING BACKGROUND OF THE INVENTION Various magnesium base alloys are described in the art which are useful for die casting. Most of these alloys contain relatively large amounts of aluminum and small amounts of zinc. The instant invention is particularly concerned with the alloys which contain relatively large amounts of zinc and small amounts of aluminum. Although the prior art has prepared alloys containing aluminum and zinc, the prior art has failed to teach the preparation of alloys which have the combination of good castability with a decrease in creep extension.
SUMMARY OF THE INVENTION A ductile die cast alloy of magnesium has been prepared comprising aluminum, zinc, copper and manganese with the optional addition of silicon, the balance being magnesium, said alloy having an aluminum and zinc composition by weight which falls within the composition range represented by the pentagon shaped area A, B, C, D and E and bounded by the straight lines AB, BC, CD DE and EA of the graph in the appended drawing, and containing in addition from 0.6 percent to 6.0 percent copper and from 0.05 percent to 3.0 percent manganese, the balance magnesium.
Compositions of aluminum and zonc represented by the area covered by the pentagon ABCDE correspond in general to the range of zinc in the alloy from 5.0 percent to 20.0 percent and aluminum from percent to 8.5 percent. The alloys also contain copper in amount from 0.6 percent to 6.0 percent, manganese in amount from 0.05 percent to 3.0 percent, the balance being magnesium all of the percentages expressed on a weight basis.
The pentagon is bounded by straight lines connecting the following points:
Zn Al A 5.0 8.5 B [0.0 8.5 C 20.0 0.0 D [0.0 0.0 E 5.0 4.0
DESCRIPTION OF THE DRAWING Magnesium based alloys containing zinc and aluminum which fall within the compositions contemplated by the instant invention are shown in the drawing. The drawing represents the diagram of the composition Zn Al defined by the pentagon ABCDE which is bound by the lines AB, BC, CD, DE and EA.
DESCRIPTION OF THE PREFERRED EMBODIMENTS 5 kilo pounds per square inch (k.s.i.) for l00 hours at 350F. The addition of silicon up to 2.0 percent also tends to improve the fluidity and strength.
Alloys which are prepared having zinc contents below the minimum amount specified above have poor castability while alloys prepared having zinc contents above the maximum amounts specified become brittle.
It has also been found that the maximum amount of copper employed preferrably should be no more than 0.5 times the zinc content.
In order to describe the instant invention in more detail, the following examples are presented:
EXAMPLES 1-7 Several magnesium base alloys containing various amounts of zinc, aluminum, manganese and copper were prepared. All of these alloys fell within the zinc and aluminum pentagon ABCDE.
The compositions of the various alloys are recorded in Table l.
The various alloys were produced by melting commercial grade magnesium at l300F under halide flux cover. Zinc, aluminum and copper chunks in the desired proportions as shown in the Table were added to the molten magnesium to dissolve the chunks. The manganese was added as manganese chloride. The soprepared melts were then each die cast into a heated die at 500F and 8,000 psi, having a cavity configuration of an ASTM E8-68, FIG. le, 2 inch gauge length test bar. These bars were then tested for yield strength ultimate tensile strength, and percent creep at a tensile loading of 5 k.s.i. for I00 hours at 350F. All data are recorded in the table.
For comparative purposes, alloys having compositions which contain less than 0.6 percent copper but which lie inside the pentagon ABCDE were prepared as controls and their results were compared with the above examples.
These compositions and their properties are also recorded in the table as Controls A-D.
It has also been discovered that the presence of manganese in amounts from 0.05 percent to 3.0 percent is effective in increasing the corrosion resistance and tends to improve the creep resistance.
The corrosion resistance of these alloys was deter mined as follows:
Standard die-cast tensile bars were cut in half to ob tain corrosion test specimens 4 /2 inches long with a major diameter of inch. After cleaning to remove surface contamination, the specimens were weighed and then partially submerged in aerated 3% NaCl solution saturated with MgO (pl-I 10.3) for three days at room temperature. The specimens were mounted vertically through holes in a plastic sheet which served as the cover of the test vessel. Approximately of the specimen length was submerged. At the end of the test period, the products were removed by immersing the specimens in a solution containing 20% CrO and l% AgNO The final weights were then determined and the average corrosion rates calculated from weight loss, submerged area, and test duration.
It should be noted that the creep extensions of Examples l-6 were all less than all of the corresponding controls which contained less than 0.6 percent copper. In addition to improved creep resistance, these alloys also possess satisfactory corrosion resistance. From the above examples, it has clearly been shown that alloys ing of zinc, aluminum, copper, manganese, silicon and magnesium, said zinc and aluminum present in amounts which fall within the pentagon ABCDE in the accompaning drawing defined by the lines AB, BC, CD, DE and EA, said alloy also containing copper in amount from 0.6 percent to 6.0 percent, manganese in amount from 0.05 percent to 3.0 percent, silicon in amount from 0.0 percent to 2.0 percent, the remainder magnesium, all of the percentages expressed on a weight basis.
2. A die cast alloy of magnesium according to claim TABLE COMPOSITION AS CAST (Room Temperature) Ultimate Yield Tensile Corrosion Strength Strength Creep Resistance %Al %An %Cu %Mn Ksi Control A 0.0 15.9 0.3 2.! 26.5 33.2 3.0 4.84 0.7 Example l 0.0 l5!) 1.] 2.l 27.9 37.4 4.5 3.l 69 Example 2 0.0 15.) 3.2 2.| 26.8 34.3 4.0 l.2l 096 Control B 4.2 12.2 0.35 0.3 28.1 37.5 3.9 .62 0.l7 Example 3 4.2 12.2 l.l 0.3 28.2 35.7 2.6 .36 026 Example 4 4.2 12.2 3.l 0.3 29.6 37.0 2.0 .32 0.36 Control C 7.1 6.6 0 .2] 25.2 34.2 2.6 2.47 Example 5 7.l 6.6 L0 .2l 27.8 37.) 42 L48 0.22 Example 6 7.l 6.6 3.2 .2] 29.2 37.4 2.1 0.50 0.52 %Si Control D 3.8 9.6 0 .l4 1.0 25.6 34.] 2.8 0.90 Example 7' 3.8 9.6 0.95 .14 l.0 27.3 36.6 3.8 0.24 0.20
We claim: 1 in which the copper content of said alloy should be no more than 0.5 times the zinc content.

Claims (2)

1. A DIE CAST ALLOY OF MAGNESIUM HAVING GOOD CASTABILITY AND IMPROVED CREEP EXTENSION, SAID ALLOY CONSISTING OF ZINC, ALUMINUM, COPPER, MANGANESE, SILICON AND MAGNESIUM, SAID ZINC AND ALUMINUM PRESENT IN AMOUNTS WHICH FALL WITHIN THE PENTAGON ABCDE IN THE ACCOMPANING DRAWING DEFINED BY THE LINES AB, BC, CD, DE AND EA, SAID ALLOY ALSO CONTAINING COPPER IN AMOUNT FROM 0.6 PERCENT TO 6.0 PERCENT, MANGANESE IN AMOUNT FROM 0.05 PERCENT TO 3.0 PERCENT, SILICON IN AMOUNT FROM 0.0 PERCENT TO 2.0 PERCENT, THE REMAINDER MAGNESIUM, ALL OF THE PERCENTAGES EXPRESSED ON A WEIGHT BASIS.
2. A die cast alloy of magnesium according to claim 1 in which the copper content of said alloy should be no more than 0.5 times the zinc content.
US402019A 1973-10-01 1973-10-01 Magnesium alloy for die casting Expired - Lifetime US3892565A (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
US402019A US3892565A (en) 1973-10-01 1973-10-01 Magnesium alloy for die casting
DE19742445843 DE2445843C3 (en) 1973-10-01 1974-09-25 Magnesium die-cast alloy
NO743470A NO132493C (en) 1973-10-01 1974-09-26
JP49112244A JPS5062112A (en) 1973-10-01 1974-09-28
FR7432921A FR2246647B1 (en) 1973-10-01 1974-09-30
ES430531A ES430531A1 (en) 1973-10-01 1974-09-30 Magnesium alloy for die casting
BR8070/74A BR7408070D0 (en) 1973-10-01 1974-09-30 ALLOY FOR CASTING IN THE MOLD CONTAINING AT LEAST MAGNESIO ALUMINUM AND ZINC
AU73799/74A AU480105B2 (en) 1974-09-30 Magnesium alloy for dde casting
GB4263274A GB1423127A (en) 1973-10-01 1974-10-01 Magnesium alloy for die casting

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US402019A US3892565A (en) 1973-10-01 1973-10-01 Magnesium alloy for die casting

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US3892565A true US3892565A (en) 1975-07-01

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JP (1) JPS5062112A (en)
BR (1) BR7408070D0 (en)
ES (1) ES430531A1 (en)
FR (1) FR2246647B1 (en)
GB (1) GB1423127A (en)
NO (1) NO132493C (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4239535A (en) * 1978-05-31 1980-12-16 King John F Magnesium alloys
US20090269236A1 (en) * 2008-04-23 2009-10-29 Gkss-Forschungzentrum Geesthacht Gmbh Ductile magnesium alloy
CN107447151A (en) * 2017-06-09 2017-12-08 福建坤孚股份有限公司 A kind of magnesium alloy materials of high surface hardness
CN115537620A (en) * 2021-06-30 2022-12-30 比亚迪股份有限公司 Die-casting magnesium alloy and preparation method and application thereof

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2196986B (en) * 1986-11-04 1990-12-12 Geoffrey Allan Chadwick Magnesium alloy
GB8626276D0 (en) * 1986-11-04 1986-12-31 Chadwick G A Magnesium alloy
JP2762115B2 (en) * 1989-05-25 1998-06-04 本田技研工業株式会社 Magnesium alloy with high temperature creep strength
JP2725112B2 (en) * 1992-03-25 1998-03-09 三井金属鉱業株式会社 High strength magnesium alloy
KR20070049114A (en) * 2004-06-24 2007-05-10 캐스트 센터 피티와이. 엘티디. Die cast magnesium alloy
US7704366B2 (en) * 2005-08-17 2010-04-27 Trevor Pearson Pretreatment of magnesium substrates for electroplating
JP5703881B2 (en) * 2011-03-22 2015-04-22 株式会社豊田自動織機 High strength magnesium alloy and method for producing the same

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1341774A (en) * 1918-12-30 1920-06-01 Backer Christian Bergh Metal alloy

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1341774A (en) * 1918-12-30 1920-06-01 Backer Christian Bergh Metal alloy

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4239535A (en) * 1978-05-31 1980-12-16 King John F Magnesium alloys
US20090269236A1 (en) * 2008-04-23 2009-10-29 Gkss-Forschungzentrum Geesthacht Gmbh Ductile magnesium alloy
CN107447151A (en) * 2017-06-09 2017-12-08 福建坤孚股份有限公司 A kind of magnesium alloy materials of high surface hardness
CN115537620A (en) * 2021-06-30 2022-12-30 比亚迪股份有限公司 Die-casting magnesium alloy and preparation method and application thereof
CN115537620B (en) * 2021-06-30 2024-02-27 比亚迪股份有限公司 Die-casting magnesium alloy and preparation method and application thereof

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Publication number Publication date
NO743470L (en) 1975-04-28
FR2246647B1 (en) 1977-07-08
FR2246647A1 (en) 1975-05-02
BR7408070D0 (en) 1975-07-22
DE2445843A1 (en) 1975-04-17
NO132493B (en) 1975-08-11
ES430531A1 (en) 1976-10-01
AU7379974A (en) 1976-04-01
NO132493C (en) 1975-11-19
GB1423127A (en) 1976-01-28
JPS5062112A (en) 1975-05-28
DE2445843B2 (en) 1976-02-26

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