US3615374A - Alloyed copper - Google Patents

Alloyed copper Download PDF

Info

Publication number
US3615374A
US3615374A US877879A US3615374DA US3615374A US 3615374 A US3615374 A US 3615374A US 877879 A US877879 A US 877879A US 3615374D A US3615374D A US 3615374DA US 3615374 A US3615374 A US 3615374A
Authority
US
United States
Prior art keywords
zirconium
percent
approximately
aluminum
copper
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
US877879A
Other languages
English (en)
Inventor
Herbert Greenwald Jr
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.)
Berry Metal Co
Original Assignee
Berry Metal 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 Berry Metal Co filed Critical Berry Metal Co
Application granted granted Critical
Publication of US3615374A publication Critical patent/US3615374A/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
    • C22C9/00Alloys based on copper

Definitions

  • Copper such as deoxidized electrolytic copper or oxygenfree high-conductivity (OFHC) copper and having an iron content in a near-trace (approximately 50 parts per million by weight) amount, possibly a chromium content to as much as l parts per million by weight, and other elements in amounts considered to be impurities, is alloyed with zirconium in the approximate range from 0.005 percent by weight to 0.03 percent by weight in combination with aluminum in a like or even greater amount.
  • the resulting alloyed metal develops improved resistance to embrittlement at grain boundary regions, especially under conditions of approximately 900 F. to l,000 F. and 4,000 p.s.i. tensile stress to 5,000 psi. tensile stress.
  • the amount of zirconium added be in the range of 0.005 to 0.03 percent by weight of the total alloy. In many instances the amount of zirconium alloyed into the copper to obtain the advantages associated with this invention is in the narrower range of approximately 0.01 to 0.02 percent by weight of the total alloy.
  • the amount of aluminum to be alloyed into the same copper in the practice of this invention is essentially like the amount of zirconium although proportionally larger amounts of aluminum, within limits, do not appear to adversely affect the delay in onset of embrittlement that otherwise is obtained.
  • the invention also preferably involves the addition of a corresponding amount of aluminum in the range of approximately from 0.005 to 0.03 percent by weight to the copper and often an amount in the range from 0.01 to 0.02 percent is utilized. No clear upper limit for the aluminum content is known and in at least one instance a total of 0.3 percent aluminum has been employed with a 0.02 percent zirconium addition.
  • the alloying elements be combined with the copper in a controlled manner.
  • the copper is vacuum melted, deoxidized by hydrogen bubbling in a partial vacuum, combined with the alloying elements under a vacuum condition, thoroughly mixed by argon bubbling in a partial vacuum, and afterwards also cast and solidified under vacuum.
  • deoxidized copper is melted, alloyed, mixed, and cast and solidified entirely in a nonreactive gaseous environment such as in essentially pure argon. Exposure of the alloying elements to oxygen at metal-melting temperatures must be avoided.
  • alloying conditions should be such that the zirconium and aluminum additions not be in an oxide, nitride, or carbide form or their effectiveness will not be realized. Accordingly, it is preferred that the specified alloying ingredients be combined in their metallic form. Although not presently known, it is conjectured that homologues of the alloying elements, particularly hafnium, are operative to obtain the advantages of the instant invention.
  • Table 1 provides information regarding the improved alloys
  • table II relates to coppers alloyed in a conventional manner. In each case, however, the alloyed metal tested was prepared in a manner involving deoxidation and was subjected in tensile bar form, to a tensile stress of at least 4,000 psi. and a temperature of approximately 950 F. The time to embrittlement (rupture) under the specified test conditions is given for each of the representative melt alloy compositions indicated.
  • the method of alloying copper with the specified amounts of zirconium and aluminum is effective to significantly reduce the iron content of the copper.
  • a starting copper having approximately 50 parts per million of iron by weight exhibited an iron content of 10 parts per million by weight (approximately) after the alloying with zirconium and aluminum had been completed.
  • An improved copper alloy consisting on a weight basis of approximately from 0.005 to 0.03 percent zirconium, at least approximately from 0.005 to 0.03 percent aluminum, and the balance except for impurities deoxidized copper.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Conductive Materials (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
US877879A 1969-11-18 1969-11-18 Alloyed copper Expired - Lifetime US3615374A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US87787969A 1969-11-18 1969-11-18

Publications (1)

Publication Number Publication Date
US3615374A true US3615374A (en) 1971-10-26

Family

ID=25370906

Family Applications (1)

Application Number Title Priority Date Filing Date
US877879A Expired - Lifetime US3615374A (en) 1969-11-18 1969-11-18 Alloyed copper

Country Status (6)

Country Link
US (1) US3615374A (ja)
JP (1) JPS5015210B1 (ja)
CA (1) CA924933A (ja)
DE (1) DE2051493B2 (ja)
FR (1) FR2069490A5 (ja)
GB (1) GB1332315A (ja)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4224066A (en) * 1979-06-26 1980-09-23 Olin Corporation Copper base alloy and process
US20070246869A1 (en) * 2006-04-21 2007-10-25 Berry Metal Company Metal making lance tip assembly

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE899443A (nl) * 1984-04-17 1984-08-16 Achter Pieter Paul Van Werkwijze voor het behandelen van koper en voor het toepassen van het aldus behandeld koper.
WO2008041777A1 (fr) * 2006-10-04 2008-04-10 Sumitomo Light Metal Industries, Ltd. Alliage de cuivre pour tuyaux sans soudure
KR20170088418A (ko) * 2015-05-21 2017-08-01 제이엑스금속주식회사 구리 합금 스퍼터링 타겟 및 그 제조 방법

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4224066A (en) * 1979-06-26 1980-09-23 Olin Corporation Copper base alloy and process
FR2459838A1 (fr) * 1979-06-26 1981-01-16 Olin Corp Alliages a base de cuivre et leur procede de production
US20070246869A1 (en) * 2006-04-21 2007-10-25 Berry Metal Company Metal making lance tip assembly

Also Published As

Publication number Publication date
DE2051493B2 (de) 1977-11-10
JPS5015210B1 (ja) 1975-06-03
DE2051493A1 (de) 1971-05-27
FR2069490A5 (ja) 1971-09-03
CA924933A (en) 1973-04-24
GB1332315A (en) 1973-10-03

Similar Documents

Publication Publication Date Title
JPH059502B2 (ja)
JP2501275B2 (ja) 導電性および強度を兼備した銅合金
US3030206A (en) High temperature chromiummolybdenum alloy
CN110029252B (zh) 一种5g手机中板用高强高韧抗氧化铝镁合金材料及其制备方法
US3615374A (en) Alloyed copper
US3668758A (en) Bonding of metallic members with alkali metals and alkali metal containing alloys
US3726673A (en) Method of making alloyed copper
US2157934A (en) Copper-magnesium alloys of improved properties
JPH03226538A (ja) TiAl基耐熱合金及びその製造方法
US3156560A (en) Ductile niobium and tantalum alloys
US3403997A (en) Treatment of age-hardenable coppernickel-zinc alloys and product resulting therefrom
US3116145A (en) Tungsten-hafnium alloy casting
EP0964069B1 (en) Strontium master alloy composition having a reduced solidus temperature and method of manufacturing the same
JPS6158541B2 (ja)
US2964399A (en) Tantalum-titanium corrosion resistant alloy
US20060088437A1 (en) Copper based precipitation hardening alloy
US3684496A (en) Solder having improved strength at high temperatures
US3089769A (en) Nickel-chromium-palladium brazing alloy
US3046109A (en) High temperature niobium base alloy
US3323913A (en) Copper base alloys containing manganese, aluminum and zinc
US2383026A (en) Aluminum alloys
US2432149A (en) Heat resistant nickel alloys
US3063834A (en) Magnesium alloys
WO2012111674A1 (ja) 高強度銅合金鍛造材
JPH01165733A (ja) 高強度高導電性銅合金