US3006758A - Zinc alloy - Google Patents

Zinc alloy Download PDF

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Publication number
US3006758A
US3006758A US514A US51460A US3006758A US 3006758 A US3006758 A US 3006758A US 514 A US514 A US 514A US 51460 A US51460 A US 51460A US 3006758 A US3006758 A US 3006758A
Authority
US
United States
Prior art keywords
zinc
alloy
alloys
copper
titanium
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
US514A
Other languages
English (en)
Inventor
Raymond E Giuliani
John D Scudder
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.)
Hydrometals Inc
Original Assignee
Hydrometals Inc
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 Hydrometals Inc filed Critical Hydrometals Inc
Priority to US514A priority Critical patent/US3006758A/en
Priority to ES0258144A priority patent/ES258144A1/es
Priority to BE591005A priority patent/BE591005A/fr
Priority to LU38726D priority patent/LU38726A1/xx
Priority to GB19381/60A priority patent/GB920282A/en
Application granted granted Critical
Publication of US3006758A publication Critical patent/US3006758A/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
    • C22C18/00Alloys based on zinc
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C18/00Alloys based on zinc
    • C22C18/02Alloys based on zinc with copper as the next major constituent

Definitions

  • a further object of the present invention is to provide an improved zinc base alloy of the foregoing character which, after forming into sheet or strip, can be readily bent and shaped for use in the formation of sheet metal products and which can be radically bent in a complete reverse cold bend without cracking or weakening and which can be severely formed and deep drawn Without stage annealing thereby making the alloy extremely useful for metal fabrication industries such as construction work, sheet metal work, automobile parts, and industrial sheet fabrication in general.
  • the alloy composition including amounts of copper, titanium, manganese and chromium is given first, followed by the physical properties measured.
  • T temperature in degrees Fahrenheit
  • G gauge thickness in inches
  • H Rockwell hardness on the 1ST scale
  • DD DD.
  • B cold bend value represented by the diameter of uncracked 180 bends and multiples of gauge (sheet thickness), and thus the lower values indicate better bending properties with a value of 2 being the maximum or best possible bend
  • the zinc base is preferably high grade or special high grade zinc.
  • Zinc analyzing at least 99.9% pure is preferred, and satisfactory alloys are obtained from zinc of the grade used in the production of commercial rolled zinc, for example, zinc metal containing as a maximum, .07% lead, .02% iron and .07% cadmium. It is preferred to use high grade zinc having no more than 0.002% iron, and lead and cadmium under 0.005%.
  • Alloys produced in accordance with the present invention do not tend to darken excessively upon exposure to the atmosphere or to various combinations of chemicals and lubricants during rolling. Further, an alloy of the composition advocated is capable of withstanding working temperatures as high as 500 F. for extended periods of time without danger of producing grain structure substantially coarser than originally existed and without adversely affecting ductility. The alloy is thus highly amenable to extrusion processes for the production of extruded shapes and to cold working and fabrication.
  • a high grade zinc base alloy rolled strip product comprising from about 0.08 to about 0.15% titanium, from about 0.15 to about 0.35% copper, from about 0.001 to about 0.05% chromium, up to about 0.05% manganese, and the balance zinc, said alloy having a dynamic ductility greater than 300 in thicknesses of 0.18" and greater and a cold bend value of 2, and having been subjected to a finishing treatment consisting of hot rolling at a temperature within the range of about 300 F. to about 450 F.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Conductive Materials (AREA)
  • Heat Treatment Of Sheet Steel (AREA)
  • Metal Rolling (AREA)
US514A 1960-01-05 1960-01-05 Zinc alloy Expired - Lifetime US3006758A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
US514A US3006758A (en) 1960-01-05 1960-01-05 Zinc alloy
ES0258144A ES258144A1 (es) 1960-01-05 1960-05-16 Un metodo de hacer una aleaciën de cinc
BE591005A BE591005A (fr) 1960-01-05 1960-05-19 Alliage de zinc
LU38726D LU38726A1 (es) 1960-01-05 1960-05-27
GB19381/60A GB920282A (en) 1960-01-05 1960-06-01 Zinc alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US514A US3006758A (en) 1960-01-05 1960-01-05 Zinc alloy

Publications (1)

Publication Number Publication Date
US3006758A true US3006758A (en) 1961-10-31

Family

ID=21691834

Family Applications (1)

Application Number Title Priority Date Filing Date
US514A Expired - Lifetime US3006758A (en) 1960-01-05 1960-01-05 Zinc alloy

Country Status (5)

Country Link
US (1) US3006758A (es)
BE (1) BE591005A (es)
ES (1) ES258144A1 (es)
GB (1) GB920282A (es)
LU (1) LU38726A1 (es)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3146098A (en) * 1962-04-16 1964-08-25 American Metal Climax Inc Zinc base alloys
US3254993A (en) * 1963-03-18 1966-06-07 Ball Brothers Co Inc Zinc alloy and method of making same
US3527601A (en) * 1967-06-14 1970-09-08 Dow Chemical Co Process of making creep-resistant zinc-base alloys
US3772007A (en) * 1970-02-24 1973-11-13 Metallgesellschaft Ag Wrought zinc alloy
CN101914704A (zh) * 2010-08-05 2010-12-15 中南大学 一种含Cr的抗蠕变挤压锌合金及其制备方法
CN104630560A (zh) * 2015-02-09 2015-05-20 宁波博威合金材料股份有限公司 一种具有高塑性的变形锌合金及其制备方法和应用

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107496993B (zh) * 2017-01-12 2022-10-11 乐普(北京)医疗器械股份有限公司 一种医用可降解植入性金属材料

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2054398A (en) * 1931-01-20 1936-09-15 Leland E Wemple Zinc alloys
US2472402A (en) * 1948-06-17 1949-06-07 New Jersey Zinc Co Zinc-copper-titanium alloys

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2054398A (en) * 1931-01-20 1936-09-15 Leland E Wemple Zinc alloys
US2472402A (en) * 1948-06-17 1949-06-07 New Jersey Zinc Co Zinc-copper-titanium alloys

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3146098A (en) * 1962-04-16 1964-08-25 American Metal Climax Inc Zinc base alloys
US3254993A (en) * 1963-03-18 1966-06-07 Ball Brothers Co Inc Zinc alloy and method of making same
US3527601A (en) * 1967-06-14 1970-09-08 Dow Chemical Co Process of making creep-resistant zinc-base alloys
US3772007A (en) * 1970-02-24 1973-11-13 Metallgesellschaft Ag Wrought zinc alloy
CN101914704A (zh) * 2010-08-05 2010-12-15 中南大学 一种含Cr的抗蠕变挤压锌合金及其制备方法
CN104630560A (zh) * 2015-02-09 2015-05-20 宁波博威合金材料股份有限公司 一种具有高塑性的变形锌合金及其制备方法和应用

Also Published As

Publication number Publication date
BE591005A (fr) 1960-09-16
GB920282A (en) 1963-03-06
LU38726A1 (es) 1960-07-27
ES258144A1 (es) 1960-11-16

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