US1868898A - Alloy - Google Patents

Alloy Download PDF

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Publication number
US1868898A
US1868898A US612639A US61263932A US1868898A US 1868898 A US1868898 A US 1868898A US 612639 A US612639 A US 612639A US 61263932 A US61263932 A US 61263932A US 1868898 A US1868898 A US 1868898A
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US
United States
Prior art keywords
alloy
manufacture
silicon
copper
manganese
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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
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US612639A
Inventor
Charles F Hammond
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Winchester Repeating Arms Co
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Winchester Repeating Arms Co
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Filing date
Publication date
Application filed by Winchester Repeating Arms Co filed Critical Winchester Repeating Arms Co
Priority to US612639A priority Critical patent/US1868898A/en
Application granted granted Critical
Publication of US1868898A publication Critical patent/US1868898A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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

  • This invention relates to an alloy and more particularly to an alloy adapted for use in the manufacture of cartridge cases for small arms ammunition.
  • a suitable substitute must not only possess the necessary strength to withstand the increased load but must-be workable to permit the formation of the cartridge cases in the usual manner and must be incapable of amalgamatin with free mercury. It has been propose to form the cases of brass and eliminate mercury fulmi'nate from the priming mixture. While priming mixtures' containing no mercury fulminate are known and have been used to some extent, such nonmercuric primingmixtures have not proved suitable for all purposes and accordingly the proposal referred to above has not solved the question.
  • the metals may be alloyed in any suitable way by melting the proper proportions together and casting into ingots.
  • the cast. ingots are mechanically worked and cold rolled into thin sheet or strip metal to further increase the stren th and d d f difliculties in ammumtlon manufacture due to g ma 8 Tea y or Sub sequent operations of cartridge manufacture.
  • the resulting alloy is readily workable permitting it to be used in the manufacture of cartridge cases and also possesses high tenslle strength permitting its use with modern ammunition.
  • the alloy may not only be used in the manufacture of cartridge cases but also in the manufacture of other products in which the properties referred to above are desired.

Description

v pressures and velocities of rim Patented July 26, 1932 CEABLES I. HAMMOND, OF NEW BEPEATING ARMS COMPANY,
HAVEN, CONNECTICUT, ASSIGNOR TO WINCHESTER OF NEW HAVEN, CONNECTICUT, A CORPORATION OF ALLOY MARYLAND In Drawing. Application filed May 20, This invention relates to an alloy and more particularly to an alloy adapted for use in the manufacture of cartridge cases for small arms ammunition.
Heretofore cart-ridge cases have been made of copper or gilding metal. Recently the fire ammunition have been increased to make the ammunition more suitable for rim fire target shooting. To obtain the increase in pressures and veloci; ties, it is necessary to employ a more powerful charge of propellant powder. This has led to the fact that the copper and gilding metal heretofore employed in the construction of cartridge cases do not have the inherent strength necessary to permit them to be used with the more powerful loads.
A suitable substitute must not only possess the necessary strength to withstand the increased load but must-be workable to permit the formation of the cartridge cases in the usual manner and must be incapable of amalgamatin with free mercury. It has been propose to form the cases of brass and eliminate mercury fulmi'nate from the priming mixture. While priming mixtures' containing no mercury fulminate are known and have been used to some extent, such nonmercuric primingmixtures have not proved suitable for all purposes and accordingly the proposal referred to above has not solved the question.
I have found that a copper alloy containing silicon, manganese and zinc has the additional strength necessary to withstand the increased pressure to which cartridge cases are submitted in modern ammunition, can be easily worked to permit the manufacture of cartridge cases by and will not amalgamate with any free mercury that maybe present in the mercury fulminate of the priming mixture.
I am aware of the prior use of manganese and silicon in a copper alloy to produce an acid resistant material. ever, that by adding zinc to the alloy heretofore used and reducing the amount of silicon and managanese the tensile strength and workability of the alloy is increased to a I have found, howthe methods now employed 1932. Serial no. 612,639.
marked extent. I therefore propose to use the ingredients in substantially the following proportions:
Silicon 0.15 7 to 1.007.preferably 0.697
Manganese 0.17 to 1.00'7:-preferably 0.24%
Zinc 143.01% to 6.00%.preferably 5.00%
The metals may be alloyed in any suitable way by melting the proper proportions together and casting into ingots. The cast. ingots are mechanically worked and cold rolled into thin sheet or strip metal to further increase the stren th and d d f difliculties in ammumtlon manufacture due to g ma 8 Tea y or Sub sequent operations of cartridge manufacture. The resulting alloy is readily workable permitting it to be used in the manufacture of cartridge cases and also possesses high tenslle strength permitting its use with modern ammunition.
The alloy may not only be used in the manufacture of cartridge cases but also in the manufacture of other products in which the properties referred to above are desired.
I claim:
1. An alloy comprising the following ingredients in substantially the following proportions: 1
Silicon 0. 15% to 1. 00%
Manganese 0. 17% to 1. 00% inc 4. 0% to 6. 00%
Copper alance.
2. An alloy comprising the following ingredients in substantially the following proportions:
Silicon 0. 69% Manganese 0. 24% Zinc 5. 00% Copper Balance.
In testimony whereof I aflix my CHARLES F. HAMMOND signature.
US612639A 1932-05-20 1932-05-20 Alloy Expired - Lifetime US1868898A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US612639A US1868898A (en) 1932-05-20 1932-05-20 Alloy

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US612639A US1868898A (en) 1932-05-20 1932-05-20 Alloy

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US1868898A true US1868898A (en) 1932-07-26

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