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Publication numberUS2210670 A
Publication typeGrant
Publication dateAug 6, 1940
Filing dateFeb 18, 1939
Priority dateFeb 18, 1939
Publication numberUS 2210670 A, US 2210670A, US-A-2210670, US2210670 A, US2210670A
InventorsKelly James M
Original AssigneeWestinghouse Electric & Mfg Co
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Copper alloy
US 2210670 A
Abstract  available in
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Claims  available in
Description  (OCR text may contain errors)

Patented Aug. 6 1940 UNITED STATES PATENT OFFICE COPPER ALLOY sylvania No Drawing. Application February 18, 1939, Serial No. 257,144

2 Claims.

This invention relates to alloys, and particularly to copper base alloys.

An object of this invention is the provision of a copper base alloy which is susceptible to precipitation hardening.

A more specific object of this invention is the provision of a copper base alloy of the bronze classification which has a high hardness and tensile strength in the as cast condition and which has precipitation hardening characteristics.

Other objects of this invention will become apparent from the following description when taken in conjunction with the appended claims.

In order to produce the copper base alloy having the desired hardness and physical characteristics, metals which can be precipitated from solutionin the copper are added to a copper melt.

It has been found that a copper base alloy con-' taining from a small but effective amount up to of cobalt, from a small but effective amount up to 5% of iron and from about .10% up to of tin has the desired characteristics. In a prior application Serial No. 149,146, filed June 19, 1937,

and issued as Patent 2,147,844 on February 21,

1939, I have disclosed and claimed the alloy of copper, cobalt and iron and have disclosed a particular relationship for the cobalt and'iron contents. In the alloy of this invention, it is desirable to maintain substantially the same relation of the cobalt and iron contents, since it has been found that in the ratio of between .5 and 1.25 to l, as disclosed in the aforesaid patent, the cobalt and iron contents cooperate with the alloying element tin in the copper base to give the desired characteristics.

As examples of the results obtained with the alloy of this invention, a direct comparison is made in the following table between the copper, cobalt and iron alloy of Patent 2,147,844 and alloys of similar cobalt and iron content but containing tin as an essential alloying element thereof. In-the table, the copper content is omitted, it being understood that the balance of the alloying r content comprises copper with possible incidental impurities occurring during the alloying process:

Table I Per cent of constituents Hardness Alloy No. Rocgwell mama These results were obtained from the alloys which were precipitation hardened by the preferred treatment consisting of quenching from a temperature of between 750 C. and the melting point of the alloys and ageing themat a temper- 15 atur of between 400 C. and 550 C. The particular treatment given the alloys in the foregoing table consisted of quenching them from 1000 C. in water and ageing them for 25 hours at 500 C. after which they'were swaged about 23% and tensile tests were conducted'on samples 12" long by .25" in diameter using a. constant strain rate on all specimens. 7

From the results given, it is apparent that the cobalt, iron and tin cooperate in the copper base to give an alloy having improved characteristics. Although tin because of its high solid solubility in copper is not generallyconsidered to be a precipitation hardening element when added to copper, it is thought that, in combination with the iron and cobalt in the alloy of this invention that it accelerates and intensifies the beneficial effect of these alloying elements.

In the alloys produced, it is found that the tin is very active in restricting columnar crystal growth in the alloy in the as cast condition. Thus, the inclusion of tin in this partioular alloy is conducive to a fine grain structure producing castings which are stronger mechanically and which are easily reproduced. In addition, it is found that tin in the alloy of this invention improves the elongation characteristics of the al- 10y giving an alloy in which tensile tests produces a neck down type of fracture instead of a shear type of fracture.

strength 5 n The beneficial effects of the alloying elements cobalt, iron and tin in copper are particularly found in the alloys containing tin in up to 20% as an essential alloying constituent thereof. Such alloys are found to be precipitation hardening as well as having the unusual characteristic of being extremely strong in the as cast condi tion. As representative of the alloys containing the higher tin content, reference may be had to the following table giving the alloying constituents of certain of the alloys examined both as to the results obtained for. the particular alloy of this invention and for comparison with the well known standard bronze alloy containing 90% copper and 10% tin,

Table II Percent Percent Percent Percent Alloy N Cu Sn Fe It is to be noted that alloy 3844 in Table H contains as essential elements thereof, tin, cobalt and iron, whereas alloy 3841 contains only tin, 3842 contains tin and iron and 3843 contains tin and cobalt. By making such a series of alloys and subjecting them to the same conditions of casting and. heat treatment, the effect ofeach of the alloying elements on the copper base is determined and the beneficial effects of the combined alloying constituents in the alloy of this invention are apparent.

Each of the alloys identified in Table II were Y subjected to the same casting procedure, after which hardness measurements were taken, and then subjected to a heat treatment consisting of quenching them from 800 C. in water, after which hardness measurements were again taken, and then ageing them 'for diiferent periods of time at 450 C. The results obtained on the alloys identified in Table II when subjected to the hereinbefore decribed heat treatment are given in the following table.

Table III Hardness-liockwell B As Quenched aged at 450 C.for Alloy No. cast from hrs. hrs. hrs. hrs.

46 a7 a9 41 44 44 4s 42 ea 61 c7 e4 3843 71 as as 56 62 e1 3844 ea 59 74 s0 s1 73 From the results given in Table m it is apparent that the combined efiect of the alloying eleas of themselves to impart desired characteristies to copper. Nor is the combined effect of'tin and iron, or tin and cobalt, in the copper base satisfactory for producing the desired characteristics. This is espectially noted in alloy 3843 which has the highest hardness inthe as cast condition but which upon precipitation hardenloses a le part of its hardness. Other aaraevc alloys containing tin in'quantities up to 20% in combination with cobalt and iron in up to. of each have similar characteristics of being extremely hard in the as cast condition and of being susceptible to precipitation hardening.

In examining the alloys of this invention, it is noted that for all the contents of tin in combination with the cobalt and iron in the copper base, as hereinbefore described, the alloys have extremely fine grain size. In order to'illustrate a representative grain size occasioned by the cooperation of the tin, cobalt and iron in this alloy, reference may be had to the following table in which a direct comparison is made on the grain size of the alloys identified in Table II the results of which are given in Table III.

From this table it is quite apparent that the particular combination of the alloying elements in the alloy of this invention is a finer grain structure than is obtained with the .simpler ternary alloys.

In practice, it is found that the higher additions of tin of from about 15% up to with the cobalt and iron within the range and ratio given, lowers the melting point of the resulting alloy to around 975 C. producing an alloy suitable as a brazing alloy. The resulting alloy has exceptional strength and good ductility and is quite suitable for brazing joints where it is desired to later heat treat the brazed joint. In certain applications of the alloy of this invention as a brazing alloy, it has been found desirable to add from .05% up to 2% of phosphorus as an essential alloying element thereof thereby further improving the wetting action of the alloy and also lowering its melting point. This addition of phosphorus, however, is not always essential as for certain applications the copper, cobalt, iron and tin alloy described hereinbefore is entirely satisfactory for the making of brazed joints.

Where desired, other alloying elements such as titanium, vanadium, lead, zinc, silver, zirconium, beryllium, silicon, aluminum and cadmium may be added to the copper, cobalt, iron and tin alloy of this invention in an "amount up to of the iron plus cobalt content. These different alloying elements may be added to the copper,

cobalt, iron and tin alloy depending upon the characteristic which it is desired to improve. For example, small additions of beryllium, titanium, zirconium, vanadium, silicon, alluminum and cadmium all improve the hardness of the basic alloy while lead improves its machineability, rendering the alloy substantially free cutting, and the silver renders the alloy thermally stable while the cadmium improves the electrical characteristics of the alloy. With any of these additions in an amount up to 25% of the iron plus cobalt content of the alloy, the resulting alloy is susceptible to precipitation hardening rendering it quite suitable for casting purposes and for other applications.

In addition to the advantes ted out hereinbefore for the alloy containing tin, it has been found that the tin additions in combination with the cobalt and iron in the copper base, gives an alloy very resistant to wear having desirable machining characteristics. These alloys are'also resistant to corrosion particularly in applications that involve salt water stability. These alloys are quite satisfactory for other applications such as pipe fittings, gears, bolts, bushings and bearings and are particularly applicable for use in the industry since castings and forgings of the alloy can be hardened and softened at will.

Although this invention has been described with reference to particular embodiments thereof, it is, of course, not to be limited thereto except insofar as is necessitated by the prior art and the scope of the appended claims.

I claim as my invention:

1. An age-hardened alloy composed of from a small but effective amount up to 5% of cobalt, from a small but efiective amount up to 5% of iron, from .10% up to about 20% of tin, and the balance substantially all copper which has been quenched from a temperature of between 750 C. and the melting point of the alloy and aged at a temperature of between 400 C. and 550 C.

2. An alloy composed of from a small but effective amount up to 5% of cobalt, from a small but effective amount up to 5% of iron, from 10% up to about 20% oftin, and the balance substantially all copper, the ratio of the cobalt to the JAMES M. KELLY.

iron in the alloy being between .5 and L25 to 1. 15

Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3639119 *May 4, 1970Feb 1, 1972Olin CorpCopper base alloy
US3923558 *Feb 25, 1974Dec 2, 1975Olin CorpCopper base alloy
US3930894 *Nov 29, 1974Jan 6, 1976Olin CorporationMethod of preparing copper base alloys
US3940290 *Jul 11, 1974Feb 24, 1976Olin CorporationProcess for preparing copper base alloys
US3953249 *Jul 11, 1974Apr 27, 1976Olin CorporationCopper base alloy
US3979208 *Sep 11, 1974Sep 7, 1976N. C. Ashton LimitedDuctile aluminum bronze alloy and article
US4116686 *Aug 25, 1977Sep 26, 1978Olin CorporationCopper base alloys possessing improved processability
US4249941 *Nov 13, 1979Feb 10, 1981Tamagawa Kikai Kinzoku Kabushiki KaishaCopper base alloy for leads of integrated circuit
US4443274 *Dec 3, 1982Apr 17, 1984Olin CorporationProcess for forming a protective film on Cu-Sn alloys
US5853505 *Apr 18, 1997Dec 29, 1998Olin CorporationIron modified tin brass
US5882442 *Feb 9, 1996Mar 16, 1999Olin CorporationIron modified phosphor-bronze
US6132528 *Jun 23, 1998Oct 17, 2000Olin CorporationIron modified tin brass
US6346215Jun 15, 2000Feb 12, 2002Wieland-Werke AgCopper-tin alloys and uses thereof
DE19928330A1 *Jun 21, 1999Jan 4, 2001Wieland Werke AgVerwendung einer zinnreichen Kupfer-Zinn-Eisen-Legierung
DE19928330C2 *Jun 21, 1999Jan 16, 2003Wieland Werke AgVerwendung einer zinnreichen Kupfer-Zinn-Eisen-Knetlegierung
EP1061147A1 *Jun 3, 2000Dec 20, 2000Wieland-Werke AGUse of a copper-tin-iron alloy
U.S. Classification420/473
International ClassificationC22C9/06, B23K35/30
Cooperative ClassificationC22C9/06, B23K35/302
European ClassificationB23K35/30D, C22C9/06