US1906567A - Metal alloy - Google Patents

Metal alloy Download PDF

Info

Publication number
US1906567A
US1906567A US569539A US56953931A US1906567A US 1906567 A US1906567 A US 1906567A US 569539 A US569539 A US 569539A US 56953931 A US56953931 A US 56953931A US 1906567 A US1906567 A US 1906567A
Authority
US
United States
Prior art keywords
alloy
copper
less
nickel
ingots
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
US569539A
Inventor
Fritschle Arthur
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.)
OI Glass Inc
Original Assignee
Owens Illinois Glass 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 Owens Illinois Glass Co filed Critical Owens Illinois Glass Co
Priority to US569539A priority Critical patent/US1906567A/en
Application granted granted Critical
Publication of US1906567A publication Critical patent/US1906567A/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
    • C22C9/06Alloys based on copper with nickel or cobalt as the next major constituent

Definitions

  • a further im ortant aim of the invention is to provide a t oroughly homogeneous alloy rather than a raw mechanical mixture consisting of numerous elements held in suspens1on.
  • a further feature of the invention relates to. a novel method of manufacturing the alloy in a manner to reduce oxidation to a minimum, particularly as regards the more volatile. ingr the final alloy.
  • a pluralit of preliminary alloys are first produced in ependently of each other, permitting the more volatile elements to be melted. and united at comparatively .low temperatures, thus reducing oxidation.
  • the several reliminary alloys are then combined and melted. together to form the final alloy which is cast into ingots.
  • the ingots are designed for remelting and'making castings adapted to be' machined for producing variso. .ous objoek in their finaljorm, as,-or example,
  • the method of manufacturing the alloy comprises making three separate alloys, each containing certain of the elements entering into the final product, then melting the three alloys together to produce the complete alloy, and casting the latter into ingots.
  • the alloy thus produced may be rightfully termed a genuinely homogeneous alloy of the several elements in the proportions above indicated, and not a raw mechanical mixturesuch as would result if the various ingredients were combined in a conventional manner.
  • Third AZl0y.-A third alloy is prepared which contains copper, aluminum, zinc, an preferably a small amount of lead.
  • I alloy the raw or unamalgamated state, they are much more susceptible to volatilization and oxidation.
  • the final complete alloy is produced by amalgamating the three alloys above described.
  • the two primary alloys namely, the copper-nickel alloy and the copper-aluminum-zinc-lead alloyare remelted in the proper proportions and when the metal bath hus produced has become thoroughly liquid, the cuprous-man- Y ganese alloy is added for the purpose of deoxidation.
  • the manganese thus introduced also adds material strength and malleability to the finished product.
  • the fusing points of the more refractory metals are greatly reduced. This is highly desirable because it permits the introduction of the more volatile elements at a comparatively low temperature which results in greatly reduced'oxidation and also reduces the possible ill efiects resulting from the distribution of oxide par.- ticles thus produced.
  • a liquid slag covering for the bath consisting of substantially 50% silica sand and 50% lime, which fuses well in advance of any portion of the metal charge.
  • the ingots are chill cast and are dumped. into water immediately upon solidification of the metal. This insures rapid cooling which in itself prevents separation or segregation of the individual elements which otherwise might occur during the process of solidification of the alloyed metal after pouring'into the ingot or pig molds.
  • iron, lead and manganese comprise only small percentages of the alloy as given in the above formulae, they are not without importance.
  • the iron is obtained principally from the l nickel and aluminum, so that in one sense it is incidental, but I find it is beneficial to the particular type of alloy forming the subject of the present invention, so that in selecting the raw materials the iron content is considered the same as any of the other ingredients.
  • the lead is found to be of value particularly as it materially improves the machining qualities of the alloy without sacrificing tensile strength. It reduces to a moderate extent the hardness of the alloy which is a desirable feature.
  • the manganese serves as a deoxidizer in the manufacture of the alloy and also serves to toughen the mixture and render the alloy less brittle.
  • a metal alloy comprising the following elements in substantially the following proportions by weight, namely,
  • a metal alloy comprising the following elements in substantially the following proportions by weight, namely,
  • Nickel not less than 17.50% and not more than 21.50%.

Description

. p Io Drawing.
PM... May 2, 1933 UNITED STATES PATENT; OFFICE um iriirrscma i, or am. more, iussouar, assroxon 'ro owns-rumors cuss comm, a coi'aroaa'rrox or 01110 METAL ALLOY M invention relates to metal alloys and particularly to an alloy in which the major ingredients are copper, nickel, zinc, and aluminum, and WhlCh also contains minor quantities of other metals, as iron, lead, manvide a highly refined alloy of the character indicated in the form of ingots for delivery to brass foundries where, under approved 20 foundry practice, they can be remelted to produce castings of great density and the utmost freedom from porosity caused by air and gas holes. The present invention deals with the production of such alloy and not with the remelting and recasting of the ingots in the manufacture of the final products of such alloy.
A further im ortant aim of the invention is to provide a t oroughly homogeneous alloy rather than a raw mechanical mixture consisting of numerous elements held in suspens1on.
A further feature of the invention relates to. a novel method of manufacturing the alloy in a manner to reduce oxidation to a minimum, particularly as regards the more volatile. ingr the final alloy. In accordance with this method,"a pluralit of preliminary alloys are first produced in ependently of each other, permitting the more volatile elements to be melted. and united at comparatively .low temperatures, thus reducing oxidation. The several reliminary alloys are then combined and melted. together to form the final alloy which is cast into ingots. The ingots are designed for remelting and'making castings adapted to be' machined for producing variso. .ous objoek in their finaljorm, as,-or example,
' ments, has been found to edients which constitute a part of nmanned October 17,1931. mm Ila- 060339.
molds and plungers of glass forming machines and numerous other articles.
e Other objects of he invention will appear hereinafter.
The following formula of an, alloy made ll in accordance Wlth my invention, containing the following, or approximately the followmg, percentages by weight of the several elegive very satisfactory results, namely:
Percent Copper 60.25. Nickel 19.25 Zinc 10.00 Aluminum 8.65
Iron .75 1075 Manganese .25 Silicon .10
It is to be understood, however, that varia- 7.
tions in the percentages of the several ingredients is permissible within certain limits. I have found that variations are permissible between the following approximate maximum and minimum percentages by weight,
The above formulae do not represent the exact percentages of all the elements entering .mto the final products made from the alloy because allowance is made in the ingots to 90 cover the normal melting loss of aluminum and zinc due to volatilization in remelting the ingots under average good foundry manipulation and melting control. Certain amounts of zinc and aluminum are invariably 95 volatilized in the'operation of remeltingthe ingot in the brass foundry. Accordingly,
.the nickel and copper ingredients in the remelted metal which actually goes into the sand molds, are correspondingly .raised in about the proportion of their percentages given in the above formulae.
In accordance with the present invention, the method of manufacturing the alloy comprises making three separate alloys, each containing certain of the elements entering into the final product, then melting the three alloys together to produce the complete alloy, and casting the latter into ingots. The alloy thus produced may be rightfully termed a genuinely homogeneous alloy of the several elements in the proportions above indicated, and not a raw mechanical mixturesuch as Would result if the various ingredients were combined in a conventional manner.
First AZZOy.-As it requires considerably more heat to liquefy nickel than any other major element entering the alloy, I first melt together in a special furnace and alloy high grade refined nickel with an equivalentamount of pure electrolytic copper and a very small percentage of silicon for deoxidizof iron, but as only about 1% of the cuprousmanganese alloy is required in the final ingot alloy, it will be observed that the amount of iron obtained from the cuprous-manganese is practically negligible.
Third AZl0y.-A third alloy is prepared which contains copper, aluminum, zinc, an preferably a small amount of lead. The
- copper, aluminum, and zinc are melted together. The lead is added to the molten bath of this particular alloy after the bath is thorvoughly liquid, so that the lead will be more readily absorbed. Silicon is used for deoxidizing this alloy. The purpose of separately preparing this third alloy is to raise the melting point thereof as compared with the melting or fusingpoint of the individual ingredients, aluminum, zinc, and lead, and thus more nearly approach the melting point of the copper-nickel alloy (which latter obviously is to constitute the basic metallic bath for the final amalgamation of all the component parts of the alloy). Also, in the production of this third alloy, volatilization and the resulting I excessive oxidation of the volatile ingredients are greatly reduced because the individual volatile elements are not exposed separately in the raw state to the high temperatures. In
AZZOy.--In like manner, I alloy the raw or unamalgamated state, they are much more susceptible to volatilization and oxidation.
Combining the three alloys. The final complete alloy is produced by amalgamating the three alloys above described. The two primary alloys, namely, the copper-nickel alloy and the copper-aluminum-zinc-lead alloyare remelted in the proper proportions and when the metal bath hus produced has become thoroughly liquid, the cuprous-man- Y ganese alloy is added for the purpose of deoxidation. The manganese thus introduced also adds material strength and malleability to the finished product.
Through the preliminary operations of first producing copper-nickel and coppermanganese alloys, the fusing points of the more refractory metals are greatly reduced. This is highly desirable because it permits the introduction of the more volatile elements at a comparatively low temperature which results in greatly reduced'oxidation and also reduces the possible ill efiects resulting from the distribution of oxide par.- ticles thus produced.
As a final stage of super-refinementin reducing the dissolved gases which may poss'ibly exist, and to reduce the oxides to the lowest possible degree, I introduce a quantity of boronic copper alloy.
As a means of protecting the molten bath from absorption of furnace gases andalso from oxidation during the entire process of fusing the alloys in the final melting operations, I use a liquid slag covering for the bath, consisting of substantially 50% silica sand and 50% lime, which fuses well in advance of any portion of the metal charge. Upon completion of the final alloy in the manner above described, the molten metal is drawn from the furnace and cast in molds, producing ingots of a convenient size for delivery to the foundry where they are recast in the manufacture of the final products. no
The ingots are chill cast and are dumped. into water immediately upon solidification of the metal. This insures rapid cooling which in itself prevents separation or segregation of the individual elements which otherwise might occur during the process of solidification of the alloyed metal after pouring'into the ingot or pig molds.
It will be seen that, the method above described is in reality a duplex smeltin method, b means of which an alloy is o tained which is converted into an improved finished product, namely, the finished castings made from the ingots of said alloy, as above pointed out. 125
Although the iron, lead and manganese comprise only small percentages of the alloy as given in the above formulae, they are not without importance.
The iron is obtained principally from the l nickel and aluminum, so that in one sense it is incidental, but I find it is beneficial to the particular type of alloy forming the subject of the present invention, so that in selecting the raw materials the iron content is considered the same as any of the other ingredients.
The lead is found to be of value particularly as it materially improves the machining qualities of the alloy without sacrificing tensile strength. It reduces to a moderate extent the hardness of the alloy which is a desirable feature.
'The manganese serves as a deoxidizer in the manufacture of the alloy and also serves to toughen the mixture and render the alloy less brittle.
The silicon is incorporated mainly as a deoxidizing-agency, but its presence in the ingot or alloy herein described is desirable because it prevents to some extent or reduces the amount of oxidation which takes place in the remelting of the ingot metal preparatory. to casting. It is not necessary to retain any of the silicon in the finished sand casting, but it is important to retain a small percentage of the silicon in the ingots which are supplied for conversion into castings.
What I claim is:
1. A metal alloy comprising the following elements in substantially the following proportions by weight, namely,
Copper 60.25 Nickel 19.25 Zinc 10.00 Aluminum 8.65 Iron .75 Lead .75 Manganese Silicon .10
2. A metal alloy comprising the following elements in substantially the following proportions by weight, namely,
Copper not less than 58.50% and not more than 63.50%.
Nickel not less than 17.50% and not more than 21.50%.
Zinc not less than 8.00% and not more than 11.00%. 95l(t)lumlnum not less than 7.00% and not more than Iron not less than 0.50% and not more than 0.75%. Lead not less than 0.50% and not more than 1.00%. 2Manganese not less than 0.15% and not more than Silicon not less than 0.05% and not more than 0.10%. 3. .A metal alloy comprising the following elements in substantially the following pro-' portions by weight, namely,
Copper not less than 58.50% and not more than 63.50%. Nickel not less than 17.50% and not more than 21.50%. Zinc not less than 8.00% and not more than 11.00%. %liminum not; less than 7.00% and not more than Lead not less than 0.50% and not more than 1.00%. d2lga7nganese not less than 0.15% and not more than Signed at St. Louis, Missouri, this 12th day of October, 1931.
. ARTHUR FRITSCHLE.
Per cent
US569539A 1931-10-17 1931-10-17 Metal alloy Expired - Lifetime US1906567A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US569539A US1906567A (en) 1931-10-17 1931-10-17 Metal alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US569539A US1906567A (en) 1931-10-17 1931-10-17 Metal alloy

Publications (1)

Publication Number Publication Date
US1906567A true US1906567A (en) 1933-05-02

Family

ID=24275853

Family Applications (1)

Application Number Title Priority Date Filing Date
US569539A Expired - Lifetime US1906567A (en) 1931-10-17 1931-10-17 Metal alloy

Country Status (1)

Country Link
US (1) US1906567A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2768102A (en) * 1952-01-31 1956-10-23 Olin Mathieson Wrought nickel bronze
US2834098A (en) * 1953-11-06 1958-05-13 Int Nickel Co Metal arc welding of 90-10 type copper-nickel material
US4434016A (en) 1983-02-18 1984-02-28 Olin Corporation Precipitation hardenable copper alloy and process
US4555272A (en) * 1984-04-11 1985-11-26 Olin Corporation Beta copper base alloy adapted to be formed as a semi-solid metal slurry and a process for making same
US4585494A (en) * 1984-04-11 1986-04-29 Olin Corporation Beta copper base alloy adapted to be formed as a semi-solid metal slurry and a process for making same
US4642146A (en) * 1984-04-11 1987-02-10 Olin Corporation Alpha copper base alloy adapted to be formed as a semi-solid metal slurry
US4661178A (en) * 1984-04-11 1987-04-28 Olin Corporation Beta copper base alloy adapted to be formed as a semi-solid metal slurry and a process for making same
EP0383998A1 (en) * 1989-02-24 1990-08-29 O-I Brockway Glass, Inc. Corrosion resistant bronze alloys
US11123825B2 (en) * 2016-08-31 2021-09-21 Faurecia Emissions Control Technologies, Germany Gmbh Copper-based brazing material and use of the brazing material

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2768102A (en) * 1952-01-31 1956-10-23 Olin Mathieson Wrought nickel bronze
US2834098A (en) * 1953-11-06 1958-05-13 Int Nickel Co Metal arc welding of 90-10 type copper-nickel material
US4434016A (en) 1983-02-18 1984-02-28 Olin Corporation Precipitation hardenable copper alloy and process
US4555272A (en) * 1984-04-11 1985-11-26 Olin Corporation Beta copper base alloy adapted to be formed as a semi-solid metal slurry and a process for making same
US4585494A (en) * 1984-04-11 1986-04-29 Olin Corporation Beta copper base alloy adapted to be formed as a semi-solid metal slurry and a process for making same
US4642146A (en) * 1984-04-11 1987-02-10 Olin Corporation Alpha copper base alloy adapted to be formed as a semi-solid metal slurry
US4661178A (en) * 1984-04-11 1987-04-28 Olin Corporation Beta copper base alloy adapted to be formed as a semi-solid metal slurry and a process for making same
EP0383998A1 (en) * 1989-02-24 1990-08-29 O-I Brockway Glass, Inc. Corrosion resistant bronze alloys
US11123825B2 (en) * 2016-08-31 2021-09-21 Faurecia Emissions Control Technologies, Germany Gmbh Copper-based brazing material and use of the brazing material

Similar Documents

Publication Publication Date Title
EP1266974B1 (en) Gold alloys and master alloys for obtaining them
US1906567A (en) Metal alloy
US4451430A (en) Method of producing copper alloy by melting technique
US2304353A (en) Heat resistant alloy
US2578098A (en) Aluminum base alloy
US3598170A (en) Fluid-mold casting process
US2676097A (en) Composition for addition to cast iron or steel
CN110484765B (en) Aluminum bronze alloy and preparation method thereof
US2173254A (en) Copper alloy
US2850381A (en) Process and alloy for adding rare earth elements and boron to molten metal baths
US2059557A (en) Copper-base alloys
US3993474A (en) Fluid mold casting slag
US2059555A (en) Alloys
US2720459A (en) Highly wear-resistant zinc base alloy
US3676114A (en) Improvement in the process relating to alloys containing platinum group metals
US2693414A (en) Methods of casting titanium stabilized steel
US2408342A (en) Alloy
US2752242A (en) Copper-nickel-titanium alloy and process for making same
US3375104A (en) Method of producing magnesium ferrosilicon
US2060919A (en) Nonferrous metal
US2048824A (en) Alloys and method of manufacture
US2059558A (en) Copper-base alloys containing chromium and iron
US1731212A (en) Gold alloy
US2684900A (en) Intermediate alloy and process for forming wear-resistant cast iron
US2046380A (en) Copper base alloys