US1764034A - Alloy - Google Patents

Alloy Download PDF

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Publication number
US1764034A
US1764034A US139020A US13902026A US1764034A US 1764034 A US1764034 A US 1764034A US 139020 A US139020 A US 139020A US 13902026 A US13902026 A US 13902026A US 1764034 A US1764034 A US 1764034A
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United States
Prior art keywords
alloy
zinc
aluminum
per cent
iron
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Expired - Lifetime
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US139020A
Inventor
John V O Palm
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.)
Cleveland Graphite Bronze Co
Original Assignee
Cleveland Graphite Bronze 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 Cleveland Graphite Bronze Co filed Critical Cleveland Graphite Bronze Co
Priority to US139020A priority Critical patent/US1764034A/en
Application granted granted Critical
Publication of US1764034A publication Critical patent/US1764034A/en
Anticipated expiration legal-status Critical
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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper
    • C22C9/04Alloys based on copper with zinc as the next major constituent

Definitions

  • the present invention relating, as indicated, to alloys is particularly directed to a new and improved copper alloy intended for various uses, such for example as in the cupffif like pistons which are employed in air brake and other fluid brake cylinders and for various other uses.
  • One of the principal objects of the invention is the provision of a relatively inexpensive alloy having good physical properties for the purposes desired, and particularly high ductility, permitting it to be readily worked into the shapes required for the final articles.
  • said invention consists of the means hereinafter fully described and particularly pointed out in the claim.
  • My improved alloy consists of copper as the predominant element, together with smaller quantities of aluminum, zinc and iron.
  • an alloy can be produced which has much greater ductility and 30 greater tensile strength than the usual aluminum bronze alloys by combining from 85 to 90 per cent. of copper with 5 to 8 per cent. of zinc, about 4 per cent. of aluminum and a smaller amount of iron, preferably from one to two per cent., and that such an alloy has a tensile strength of approximately 100,000 pounds in rolled form and can be given a Brinnell hardness of as high as 175 While stillretaining a very great amount of ductilit
  • I first melt copper, to which are added aluminum and iron in the amounts named, and finally zinc,
  • the resulting alloy may be poured to produce flat sheets or other articles, it being desirable, however, to pour the material into the molds with as little turbulence as possible in order to maintain the aluminum in the" composition without'the above described in tent at 5 aluminum, 5 to 8 Application filed October 1, 1926. Serial No. 139,020.
  • Zinc should be present in my improved alloy in an amount equal to 2 per cent. of the composition, or in even greater amount.
  • the quantities of the other ingredients may be varied somewhat, depending upon the particular use to which the material is to be put, I have found that compositions consisting of 90 parts of copper, 5 parts of zinc, 4 parts of aluminum and 1 part of iron are satisfactory, and also a composition consisting of 86 parts of copper, 8 parts of zinc, 4 parts of aluminum and 2 derstood that these proportions may be still further varied within the general limits making the alloy.
  • the iron and also, to some extent, the zinc act to prevent self-annealing and accordingly either rials may be somewhat reduced, provided the other is retained and the percentage thereof correspondingly increased, although it is highly desirable to maintain the zinc conper cent. or more if any considerable ductility is required in the alloy.

Description

Patented June 17, 1930 UNITED STATES.
JOHN V. O. PALM, F CLEVELAND HEIGHTS,
GRAPHITE BRONZE COMPANY,
ALLOY No Drawing.
The present invention, relating, as indicated, to alloys is particularly directed to a new and improved copper alloy intended for various uses, such for example as in the cupffif like pistons which are employed in air brake and other fluid brake cylinders and for various other uses. One of the principal objects of the invention is the provision of a relatively inexpensive alloy having good physical properties for the purposes desired, and particularly high ductility, permitting it to be readily worked into the shapes required for the final articles. To the accomplishment of the foregoing and related ends, said invention, then, consists of the means hereinafter fully described and particularly pointed out in the claim.
The following description sets forth in detail ope approved combination of ingredients 20 and method of making same embodying my invention, such disclosed ingredients and procedure constituting, however, but one of various forms in which the principle of the invention may be used.
My improved alloy consists of copper as the predominant element, together with smaller quantities of aluminum, zinc and iron. I have found that an alloy can be produced which has much greater ductility and 30 greater tensile strength than the usual aluminum bronze alloys by combining from 85 to 90 per cent. of copper with 5 to 8 per cent. of zinc, about 4 per cent. of aluminum and a smaller amount of iron, preferably from one to two per cent., and that such an alloy has a tensile strength of approximately 100,000 pounds in rolled form and can be given a Brinnell hardness of as high as 175 While stillretaining a very great amount of ductilit In making the present alloy I first melt copper, to which are added aluminum and iron in the amounts named, and finally zinc,
and after the various ingredients have become well mixed the resulting alloy may be poured to produce flat sheets or other articles, it being desirable, however, to pour the material into the molds with as little turbulence as possible in order to maintain the aluminum in the" composition without'the above described in tent at 5 aluminum, 5 to 8 Application filed October 1, 1926. Serial No. 139,020.
formation of flaws in the resulting castings.
In order to secure the desirable ductility Zinc should be present in my improved alloy in an amount equal to 2 per cent. of the composition, or in even greater amount. \Vhile the quantities of the other ingredients may be varied somewhat, depending upon the particular use to which the material is to be put, I have found that compositions consisting of 90 parts of copper, 5 parts of zinc, 4 parts of aluminum and 1 part of iron are satisfactory, and also a composition consisting of 86 parts of copper, 8 parts of zinc, 4 parts of aluminum and 2 derstood that these proportions may be still further varied within the general limits making the alloy. The iron andalso, to some extent, the zinc act to prevent self-annealing and accordingly either rials may be somewhat reduced, provided the other is retained and the percentage thereof correspondingly increased, although it is highly desirable to maintain the zinc conper cent. or more if any considerable ductility is required in the alloy.
Other modes of applying the principle of my invention may be employed instead of the one explained, change being made as regards the process herein disclosed or the materials employed in carrying out the process, provided the ingredient or ingredients stated by the following claim or the equivalent of such stated ingredient or ingredients be employed. I
I therefore tiuctly claim as my invention An aluminum bronze alloy comprising 85 to 90 per cent. of copper, about 4 per cent. of per cent. of zinc, and 1 to 2 per cent. of iron.
Signed by me, 1926.
JOHN V. O. PALM OHIO, ASSIGNOR TO THE CLEVELAND. OF CLEVELAND, OHIO, A CORPORATION OF OHIO parts of iron, and it will be unparticularly point out and disthis 29th day of September,
of the composition, of these two mate-v
US139020A 1926-10-01 1926-10-01 Alloy Expired - Lifetime US1764034A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2494736A (en) * 1945-10-20 1950-01-17 Olin Ind Inc Copper base alloy
US2935400A (en) * 1959-01-12 1960-05-03 Dorsilium Corp Of America Simulated gold alloy
US3214269A (en) * 1963-09-12 1965-10-26 Nordiske Kabel Traad Seawater-resistant alloy of brass or aluminum brass
US4786470A (en) * 1987-06-19 1988-11-22 Aalba Dent, Inc. Aluminum-bronze dental alloy

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2494736A (en) * 1945-10-20 1950-01-17 Olin Ind Inc Copper base alloy
US2935400A (en) * 1959-01-12 1960-05-03 Dorsilium Corp Of America Simulated gold alloy
US3214269A (en) * 1963-09-12 1965-10-26 Nordiske Kabel Traad Seawater-resistant alloy of brass or aluminum brass
US4786470A (en) * 1987-06-19 1988-11-22 Aalba Dent, Inc. Aluminum-bronze dental alloy

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