US3551144A - Aluminium-bronze alloy - Google Patents
Aluminium-bronze alloy Download PDFInfo
- 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
Links
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title description 20
- 229910000906 Bronze Inorganic materials 0.000 title description 6
- 239000004411 aluminium Substances 0.000 description 13
- 229910052782 aluminium Inorganic materials 0.000 description 13
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 10
- 229910052796 boron Inorganic materials 0.000 description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 229910045601 alloy Inorganic materials 0.000 description 8
- 239000000956 alloy Substances 0.000 description 8
- 230000006911 nucleation Effects 0.000 description 5
- 238000010899 nucleation Methods 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 238000007792 addition Methods 0.000 description 3
- 230000005496 eutectics Effects 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 210000001787 dendrite Anatomy 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000005482 strain hardening Methods 0.000 description 2
- 238000000137 annealing Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
- C22C9/02—Alloys based on copper with tin as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys 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.
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) |
-
1966
- 1966-12-07 GB GB54760/66A patent/GB1213275A/en not_active Expired
-
1967
- 1967-12-06 DE DE1967A0057598 patent/DE1608101B2/en active Granted
- 1967-12-06 US US688304A patent/US3551144A/en not_active Expired - Lifetime
- 1967-12-07 FR FR49414A patent/FR1547992A/en not_active Expired
- 1967-12-07 CH CH1712667A patent/CH476847A/en not_active IP Right Cessation
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 |
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