[go: up one dir, main page]

US3551144A - Aluminium-bronze alloy - Google Patents

Aluminium-bronze alloy Download PDF

Info

Publication number
US3551144A
US3551144A US688304A US3551144DA US3551144A US 3551144 A US3551144 A US 3551144A US 688304 A US688304 A US 688304A US 3551144D A US3551144D A US 3551144DA US 3551144 A US3551144 A US 3551144A
Authority
US
United States
Prior art keywords
aluminium
alloy
beta
boron
bronze alloy
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
US688304A
Inventor
Norman Coupe Ashton
John P Dennison
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Application granted granted Critical
Publication of US3551144A publication Critical patent/US3551144A/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
    • C22C9/02Alloys based on copper with tin as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper

Definitions

  • An aluminium-bronze alloy contains 8% to 9% aluminium or aluminium equivalent and sufficient boron (preferably in the range 0.01% to 0.02%) to create nucleation of the beta phase during cooling of the alloy before the creation of the alpha base. This facilitates removal of the beta regions in subsequent heat treatment.
  • This invention relates to aluminium bronze alloy, and the object of the invention is to provide an aluminium bronze alloy of refined grain structure which, in consequence of its grain structure, is inherently strong and combines the advantages of responding well to hot working in the alpha-i-beta range whilst after a suitable heat treatment being capable of extensive cold working.
  • an aluminium-bronze alloy contains 8%-9% aluminium (or aluminium equivalent) and sufficient boron to create nucleation of the beta phase during the cooling of the alloy before the creation of the alpha base.
  • aluminium equivalent is used herein to describe aluminium or a mixture of aluminium and tin as it is the aluminium equivalent which will determine response to nucleation by boron.
  • the aluminium equivalent shall be present in the range 8.2% to 8.6%, since the addition of boron is most effective in the nucleation of the beta phase within this range. It is thought that by promoting beta nucleation, the boron prevents the presence of large regions of beta in the final cast structure. More particularly, it appears to be effective in preventing the formation of wide bands of the easily deformed beta phase when the alloy is subjected to an extrusion process.
  • the boron shall be present in the range 0.01% to 0.02%, although larger amounts could be used if desired.
  • the alloy is hypoeutectic, so that the alpha phase would form first and beta would deposit as a coarse eutectic constituent.
  • the beta phase is formed as a fine well dispersed pro-eutectic dendrites. This facilitates the removal of the beta regions in subsequent heat treatment and thus improves subsequent cold workability.
  • iron has been used previously in quantities from 1.5% to 3.5% in order to refine the cast grain structure.
  • the iron presents a serious disadvantage if the material has to be softened to a very low hardness for cold working, because if there is an appreciable iron content, the hardness remains high despite heat treatment and annealing.
  • a typical alloy in accordance with the invention has the following composition:
  • Aluminium equivalent 8.4% Boron: 0.02% Copper: Balance.
  • An aluminiumbronze consisting essentially of 8 to 9% aluminium, 0.01 to 0.02% boron and the balance copper, said alloy characterized by an alpha plus beta microstructure wherein the beta phase is formed as fine well dispersed pro-eutectic dendrites.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Valve Housings (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Sliding-Contact Bearings (AREA)
  • Extrusion Of Metal (AREA)

Description

United States Patent 3,551,144 ALUMINIUM-BRONZE ALLOY Norman Coupe Ashton, Corby, Birkby Road, Huddersfield, Yorkshire, England, and John P. Dennison, 1 Channel View Sketty, Swansea, Glamorgan, Wales No Drawing. Filed Dec. 6, 1967, Ser. No. 688,304 Claims priority, application Great Britain, Dec. 7, 1966, 54,760/ 66 Int. Cl. C22c 9/00 U.S. Cl. 75-162 1 Claim ABSTRACT OF THE DISCLOSURE An aluminium-bronze alloy contains 8% to 9% aluminium or aluminium equivalent and sufficient boron (preferably in the range 0.01% to 0.02%) to create nucleation of the beta phase during cooling of the alloy before the creation of the alpha base. This facilitates removal of the beta regions in subsequent heat treatment.
This invention relates to aluminium bronze alloy, and the object of the invention is to provide an aluminium bronze alloy of refined grain structure which, in consequence of its grain structure, is inherently strong and combines the advantages of responding well to hot working in the alpha-i-beta range whilst after a suitable heat treatment being capable of extensive cold working.
According to this invention an aluminium-bronze alloy contains 8%-9% aluminium (or aluminium equivalent) and sufficient boron to create nucleation of the beta phase during the cooling of the alloy before the creation of the alpha base.
Since in certain aluminium bronzes it is desirable to include small additions of tin it is to be understood that the term aluminium equivalent is used herein to describe aluminium or a mixture of aluminium and tin as it is the aluminium equivalent which will determine response to nucleation by boron.
It is preferred that the aluminium equivalent shall be present in the range 8.2% to 8.6%, since the addition of boron is most effective in the nucleation of the beta phase within this range. It is thought that by promoting beta nucleation, the boron prevents the presence of large regions of beta in the final cast structure. More particularly, it appears to be effective in preventing the formation of wide bands of the easily deformed beta phase when the alloy is subjected to an extrusion process.
Patented Dec. 29, 1970 It is also preferred that the boron shall be present in the range 0.01% to 0.02%, although larger amounts could be used if desired.
Without boron, the alloy is hypoeutectic, so that the alpha phase would form first and beta would deposit as a coarse eutectic constituent. With the addition of boron (in the specified range of aluminium equivalent) the beta phase is formed as a fine well dispersed pro-eutectic dendrites. This facilitates the removal of the beta regions in subsequent heat treatment and thus improves subsequent cold workability.
Apart from the creation of an inherently stronger alloy than known aluminium-bronzes, it is possibly by use of the invention to avoid use of appreciable amounts of iron in the alloy. Iron has been used previously in quantities from 1.5% to 3.5% in order to refine the cast grain structure. However, the iron presents a serious disadvantage if the material has to be softened to a very low hardness for cold working, because if there is an appreciable iron content, the hardness remains high despite heat treatment and annealing.
A typical alloy in accordance with the invention has the following composition:
Aluminium equivalent: 8.4% Boron: 0.02% Copper: Balance.
We claim:
1. An aluminiumbronze consisting essentially of 8 to 9% aluminium, 0.01 to 0.02% boron and the balance copper, said alloy characterized by an alpha plus beta microstructure wherein the beta phase is formed as fine well dispersed pro-eutectic dendrites.
References Cited UNITED STATES PATENTS 1,076,973 10/1913 Gleason -162 3,416,915 12/1968 Mikawa 75162 FOREIGN PATENTS 537,225 6/ 1941 Great Britain 75154 CHARLES N. LOVELL, Primary Examiner U.S. Cl. X.R.
US688304A 1966-12-07 1967-12-06 Aluminium-bronze alloy Expired - Lifetime US3551144A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB54760/66A GB1213275A (en) 1966-12-07 1966-12-07 Improvements in aluminium-bronze alloy

Publications (1)

Publication Number Publication Date
US3551144A true US3551144A (en) 1970-12-29

Family

ID=10471996

Family Applications (1)

Application Number Title Priority Date Filing Date
US688304A Expired - Lifetime US3551144A (en) 1966-12-07 1967-12-06 Aluminium-bronze alloy

Country Status (5)

Country Link
US (1) US3551144A (en)
CH (1) CH476847A (en)
DE (1) DE1608101B2 (en)
FR (1) FR1547992A (en)
GB (1) GB1213275A (en)

Also Published As

Publication number Publication date
GB1213275A (en) 1970-11-25
FR1547992A (en) 1968-11-29
DE1608101B2 (en) 1977-06-30
DE1608101A1 (en) 1970-11-05
CH476847A (en) 1969-08-15

Similar Documents

Publication Publication Date Title
US4636357A (en) Aluminum alloys
US4049426A (en) Copper-base alloys containing chromium, niobium and zirconium
US3827917A (en) Aluminum electrical conductor and process for making the same
US3031299A (en) Aluminum base alloy
ES375477A2 (en) Aluminum base alloy
US3703367A (en) Copper-zinc alloys
US4569702A (en) Copper base alloy adapted to be formed as a semi-solid metal slurry
US4238249A (en) Process for the preparation of a copper-zinc material
US4072513A (en) Copper base alloys with high strength and high electrical conductivity
US2204568A (en) Magnesium alloy
US3551144A (en) Aluminium-bronze alloy
US2253502A (en) Malleable iron
US3734785A (en) Zinc forging alloy
US3039868A (en) Magnesium base alloys
US4148671A (en) High ductility, high strength aluminum conductor
US3337335A (en) Leaded silicon manganese bearing brass
US3574001A (en) High conductivity copper alloys
US3573110A (en) Process for obtaining high conductivity copper alloys
US1848816A (en) Robert s
US2076575A (en) Free cutting alloys
US2022686A (en) Aluminum alloy casting and method of making the same
US2070833A (en) Method of treating aluminium alloy and product
US2280171A (en) Aluminum alloy
US1991162A (en) Process for improving coppertitanium alloys
US2564044A (en) Aluminum-magnesium casting alloys