US2715577A - Copper-base alloys - Google Patents
Copper-base alloys Download PDFInfo
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- US2715577A US2715577A US297976A US29797652A US2715577A US 2715577 A US2715577 A US 2715577A US 297976 A US297976 A US 297976A US 29797652 A US29797652 A US 29797652A US 2715577 A US2715577 A US 2715577A
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- copper
- alloy
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- manganese
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- 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
- C22C9/05—Alloys based on copper with manganese as the next major constituent
Definitions
- low melting point is associated with the presence of the manganese, whilst grain refinement and considerable improvement in mechanical properties appear to be imparted by the iron content.
- Corrosion resistance is associated with the nickel content and it is a matter for surprise that a useful improvement can be secured with a relatively small content, this moreover without sensibly increasing the melting points of the alloy.
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- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Forging (AREA)
Description
2,7 15,5 7 7 Patented Aug. 16, 1 955 COPPER-BASE ALLOYS Ronald James Malcolm Payne, New Maiden, and Alfred William Owen Webb, Brockley, London, England, assignors to J. Stone & Company (Charlton) Limited, London, England, a British company No Drawing. Application July 9, 1952, Serial No. 297,976
Claims priority, application Great Britain July 24, 1951 1 Claim. (Cl. 75-162) This invention concerns improvements relating to r high strength and ductility and good resistance to fatigue and corrosion, but are at a particular disadvantage in comparison with other copper-base alloys for casting purposes. The principal difiiculties arise from the high temperatures at which the alloy has to be melted and poured and there are strong tendencies for the alloy to take up gas when melted on the large scale (particularly in reverberatory furnaces) and for dross and oxide inclusions to be formed in the mould and entrapped in the casting. Thus, for example, such serious difiiculties are encountered if the high-strength aluminium bronze containing 10% Al, Ni and 5% Fe (D. T. D. 412) is used for very large or heavy castings. These dilficulties have largely held back the application of this class of alloy to heavy castings.
An object of the having the good properties of the alum nium bronzes containing nickel and iron, especially good resistance to fatigue and to corrosion, but without the disadvantages for casting purposes of a high melting point.
According to the invention, aluminium bronze, or a casting or forging of such bronze, comprises to (preferably 11 to 14%) of manganese, 6% to 9% of aluminium, 2 to 4% (preferably 2.5 to 3.5%) of iron and 1.5 to 6% (preferably 2 to 5%) of nickel, the rest being copper (at least of the order of 70%) apart from the impurities or small quantities of other elements usually found in ordinary aluminium bronzes. Conversely those elements which are known to be objectionable in such bronzes should generally be avoided. Thus materially more than about 0.2% silicon or 0.02% phosphorus is deleterious.
An example of a composition which has been found to have good casting qualities as well as good tensile properties, good resistance to fatigue and corrosion fatigue in sea water and good resistance to corrosion and cavitation erosion (a combination of properties suitable for marine propellers) is as follows:
Per cent Manganese 11.7 Aluminium 7.2 Iron 3.3 Nickel 2.2 Copper Remainder A tested sample of this composition had the following properties:
0.15% proof stress 18.0 tons per sq. in.
present invention is to provide an alloy Ultimate tensile stress Elongation 28% on 2 inches. Fatigue strength 17.7 tons per sq. in. Melting point 960 C.
42.5 tons per sq. in.
The alloy according to the invention casts well in both sand and metal moulds. It is clean-running and free from troubles associated with dross formation in the mould. Furthermore, its properties, including tensile strength and fatigue strength, are not seriously reduced when it is cast in heavy sections, being especially surprising.
The alloy has been found to cast Well in die moulds and gives gravity die castings which have the strength and toughness expected of standard aluminium bronzes and which can be employed for equally arduous duties. By reason of its lower melting point, however, the alloy according to the invention shows less tendency than the said bronzes to produce crazing of the dies.
Finally, the alloy also has further useful properties in the wrought condition. Although it may have the same strength as a standard high-strength aluminium bronze, it is more easily forgeable and can be worked at lower temperatures with the further advantage of lower wear of the forging dies. An example of a forgeable composition with high corrosion resistances is as follows:
this advantageous feature Per cent Manganese 12 Aluminium 7.25 Iron 3.0 Nickel 5.0 Copper Remainder The qualities and properties of the invention are thus such as designers in several fields.
Copper-aluminium alloys containing substantial proportions of manganese have been studied by various workers, but practical interest in these alloys appears to have been largely confined to the wrought form and to a few compositions having special electrical or magnetic properties. At any rate little or no practical use has been made of such alloys for castings. Indeed it is most surprising that the composition in accordance with the invention has proved to have good casting qualities, as alloys with a high manganese content have generally enjoyed a bad reputation with regard to these qualities. Furthermore, little or no information was available as to the practical properties, for example the fatigue properties, of such copper-aluminium alloys containing substantial proportions of manganese.
In the composition according to the invention, low melting point is associated with the presence of the manganese, whilst grain refinement and considerable improvement in mechanical properties appear to be imparted by the iron content. Corrosion resistance is associated with the nickel content and it is a matter for surprise that a useful improvement can be secured with a relatively small content, this moreover without sensibly increasing the melting points of the alloy.
For purposes requiring a moderate degree of corrosion resistance, an alloy containing 2% (or at least 1 /2%) of nickel will normally be employed. For example, an advantageous such alloy comprises approximately 12% of manganese, 7 /2% of aluminium, 3% of iron and 2% of nickel, the rest being substantially copper. Increase in the nickel content results in improvement in the corrosion resistance without appreciable variation of the mechanical properties of the alloy. With a nickel content of 5% (or between 4 and 6%), corrosion resistance equivalent to that of the best manganese-free aluminium bronzes can be obtained. Small additions of tin may also the alloy according to to make it useful to be made for the purpose of improving the corrosion resistance. 7 Werclaim:
An aluminum bronze containing not less than 6 /2 nor more than 9%, aluminum, and manganese in an amount corresponding approximately to a manganese to aluminum ratio-of 1.6 to 1, 1.5 to 6% nickel, 2 to 4% iron, the rest being essentially copper, the said bronze having an alpha-beta microstrncture with minor quantities of other microstructural constituents, and the said bronze having a melting'point of about 960 C.
References Cited in the file of this patent UNITED STATES PATENTS 1,369,818 Kosugi Mar. I, 1921 4 1,491,782 Iytaka Jan. 22, 1924 1,651,970 Schenck Dec. 6, 1927 FOREIGN PATENTS 5 414,748 Great Britain Aug. 13, 1934 159,537 Great Britain 'Feb. 24, 1951 OTHER REFERENCES Nonferrous Foundry Practice, Laing and Rolfe, Van m Nostrand C0,, publishers (1943), pages 181-186 relied Metallurgia, Cast Bronze, H. I. Roast, (1953), pages 208-215.
vol. 41, issue 245, March 1950, page 242. American Society for Metals
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2715577X | 1951-07-24 |
Publications (1)
Publication Number | Publication Date |
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US2715577A true US2715577A (en) | 1955-08-16 |
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Application Number | Title | Priority Date | Filing Date |
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US297976A Expired - Lifetime US2715577A (en) | 1951-07-24 | 1952-07-09 | Copper-base alloys |
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Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2944889A (en) * | 1957-11-20 | 1960-07-12 | John F Klement | Aluminum bronze alloy containing chromium and having improved wear resistance |
US3007821A (en) * | 1958-02-12 | 1961-11-07 | Ampco Metal Inc | Method of heat treating a cast aluminum bronze article |
US3049424A (en) * | 1957-10-15 | 1962-08-14 | Stone & Company Charlton Ltd J | Copper-base alloys |
US3079252A (en) * | 1960-01-25 | 1963-02-26 | Stone & Company Propellers Ltd | Copper-base alloys |
US3901692A (en) * | 1969-08-29 | 1975-08-26 | Tsuneaki Mikawa | Corrosion resistant copper alloy and the method of forming the alloy |
US4113475A (en) * | 1976-04-09 | 1978-09-12 | Kennecott Copper Corporation | Tarnish resistant copper alloy |
WO1984001965A1 (en) * | 1982-11-16 | 1984-05-24 | Brockway Inc | Aluminum bronze glassmaking molds |
US20110229367A1 (en) * | 2010-03-17 | 2011-09-22 | Shau-Kuan Chiu | Copper nickel aluminum alloy |
EP3910086A1 (en) | 2020-05-14 | 2021-11-17 | Wieland-Werke AG | Copper manganese aluminium-iron wrought alloy |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB159537A (en) * | 1919-10-24 | 1921-02-24 | Armstrong Whitworth Co Eng | Improvements in copper alloys |
US1369818A (en) * | 1920-06-30 | 1921-03-01 | Kosugi Tatsuzo | Alloy |
US1491782A (en) * | 1922-10-06 | 1924-04-29 | Revere Rubber Co | Protective case for explosive containers |
US1651970A (en) * | 1925-08-11 | 1927-12-06 | Duriron Co | Corrosion-resisting alloy |
GB414748A (en) * | 1933-01-13 | 1934-08-13 | Henry Winder Brownsdon | Improvements in and relating to copper alloys and articles made therefrom |
-
1952
- 1952-07-09 US US297976A patent/US2715577A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB159537A (en) * | 1919-10-24 | 1921-02-24 | Armstrong Whitworth Co Eng | Improvements in copper alloys |
US1369818A (en) * | 1920-06-30 | 1921-03-01 | Kosugi Tatsuzo | Alloy |
US1491782A (en) * | 1922-10-06 | 1924-04-29 | Revere Rubber Co | Protective case for explosive containers |
US1651970A (en) * | 1925-08-11 | 1927-12-06 | Duriron Co | Corrosion-resisting alloy |
GB414748A (en) * | 1933-01-13 | 1934-08-13 | Henry Winder Brownsdon | Improvements in and relating to copper alloys and articles made therefrom |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3049424A (en) * | 1957-10-15 | 1962-08-14 | Stone & Company Charlton Ltd J | Copper-base alloys |
US2944889A (en) * | 1957-11-20 | 1960-07-12 | John F Klement | Aluminum bronze alloy containing chromium and having improved wear resistance |
US3007821A (en) * | 1958-02-12 | 1961-11-07 | Ampco Metal Inc | Method of heat treating a cast aluminum bronze article |
US3079252A (en) * | 1960-01-25 | 1963-02-26 | Stone & Company Propellers Ltd | Copper-base alloys |
US3901692A (en) * | 1969-08-29 | 1975-08-26 | Tsuneaki Mikawa | Corrosion resistant copper alloy and the method of forming the alloy |
US4113475A (en) * | 1976-04-09 | 1978-09-12 | Kennecott Copper Corporation | Tarnish resistant copper alloy |
WO1984001965A1 (en) * | 1982-11-16 | 1984-05-24 | Brockway Inc | Aluminum bronze glassmaking molds |
US20110229367A1 (en) * | 2010-03-17 | 2011-09-22 | Shau-Kuan Chiu | Copper nickel aluminum alloy |
EP3910086A1 (en) | 2020-05-14 | 2021-11-17 | Wieland-Werke AG | Copper manganese aluminium-iron wrought alloy |
DE102020002885A1 (en) | 2020-05-14 | 2021-11-18 | Wieland-Werke Aktiengesellschaft | Wrought copper-manganese-aluminum-iron alloy |
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