DE714821C - Copper alloy - Google Patents

Copper alloy

Info

Publication number
DE714821C
DE714821C DES137364D DES0137364D DE714821C DE 714821 C DE714821 C DE 714821C DE S137364 D DES137364 D DE S137364D DE S0137364 D DES0137364 D DE S0137364D DE 714821 C DE714821 C DE 714821C
Authority
DE
Germany
Prior art keywords
copper
tin
copper alloy
alloy
niobium
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
Application number
DES137364D
Other languages
German (de)
Inventor
Dipl-Ing Lothar Sempell
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.)
Dipl-Ing Lothar Sempell
Original Assignee
Dipl-Ing Lothar Sempell
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 Dipl-Ing Lothar Sempell filed Critical Dipl-Ing Lothar Sempell
Priority to DES137364D priority Critical patent/DE714821C/en
Application granted granted Critical
Publication of DE714821C publication Critical patent/DE714821C/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02—Parts of sliding-contact bearings
    • F16C33/04—Brasses; Bushes; Linings
    • F16C33/06—Sliding surface mainly made of metal
    • F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
    • F16C33/121—Use of special materials
    • 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
    • C22C9/02—Alloys based on copper with tin as the next major constituent
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2204/00—Metallic materials; Alloys
    • F16C2204/10—Alloys based on copper
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2204/00—Metallic materials; Alloys
    • F16C2204/10—Alloys based on copper
    • F16C2204/12—Alloys based on copper with tin as the next major constituent

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Sliding-Contact Bearings (AREA)

Description

Kupferlegierung Die bekannten Metallegierungen auf Basis Kupfer, beispielsweise solche mit bis zu i z a/o Zinn, bis zu 50116 Nickel, bis zu 2 0'o Eis-en und im Rest Kupfer und die üblichen Verunreinigungen erstarren meist verhältnismäßig grobkörnig, so daß sie gegen hohe Schlag-und Druckbeanspruchung nicht genügend widerstandsfähig sind. Es zeigte sich nun, daß sich die Festigkeitseigenschaften dieser Legierungen ganz erheblich verbessern lassen, wenn man ihnen Birnen Zuschlag von bis zu 30'o Tantal und/oder Niob gibt. Dadurch erhalten die Legierungen ein sehr dichtes, feinkörniges und sehniges Gefüge, so daß sie sich nicht nur für die Herstellung von Lagern mit hohen Druckbeanspruchungen und überhaupt für Teile, die einem Verschleif') durch Reibung ,ausgesetzt sind, eignen, sondern auch für die Herstellung von Gegenständen mit .einer- besonders guten Korrosionsbeständigkeit, insbesondere mit hoher Säurebeständigkeit. Dabei kann man das Zinn in den Legierungen auch ganz durch Mangan :ersetzen oder unter Beibehalt der sonstigen Legierungsbestandteile durch bis zu 40/0 Silicium und bis zu 400110 Zink. Da Tantal in der Natur immer mit Niob zusammen vorkommt, der Einfluß der Stoffe auf die Metallegierungen auf Basis Kupfer aber bei Gehalben bis zu ; % in gleicher Richtung wirkt, ist @es aus wirtschaftlichen Gründen zweckmäßig, keine Trennung der Metalle Tantal und Niob vorzunehmen. Es hat sich auch gezeigt, daß .es von Vorteil ist, eine Ferrolegierung mit möglichst hohen Gehalten an den Metallen Tantal und Niob zu verwenden.Copper alloy The known metal alloys based on copper, for example those with up to i z a / o tin, up to 50116 nickel, up to 20'o iron and im The remainder of copper and the usual impurities usually solidify in a relatively coarse-grained manner, so that they are not sufficiently resistant to high impact and compressive stress are. It has now been shown that the strength properties of these alloys Can be improved quite considerably if you give them pear surcharge of up to 30'o Tantalum and / or niobium. This gives the alloys a very dense, fine-grained appearance and sinewy structure, so they are not just suitable for making bearings with high pressure loads and generally for parts that are subject to wear and tear Friction, exposed, are suitable, but also for the manufacture of objects with .einer- particularly good corrosion resistance, especially with high acid resistance. The tin in the alloys can also be completely replaced by manganese: or while retaining the other alloy components with up to 40/0 silicon and up to 400110 zinc. Since tantalum always occurs together with niobium in nature, the influence of the substances on the metal alloys based on copper but at salaries up to ; % acts in the same direction, @it is advisable for economic reasons, to not separate the metals tantalum and niobium. It has also been shown that it is advantageous to use a ferro-alloy with the highest possible levels of Use metals tantalum and niobium.

Claims (1)

PATENTANSPRÜCHE: i. Metallegierung auf. Basis Kupfer, bestehend aus: bis 12 % Zinn, bis 5 % Nickel, bis z 0,ö Eisen, bis 3 % Tantal und/oder Niob, Rest Kupfer mit den üblichen Verunreinigungen. a. Metallegierung auf Basis Kupfer nach Anspruch i, dadurch gekennzeichnet, daß das Zinn in der Legierung ganz durch Mangan ersetzt ist. 3. Metallegierung auf Basis Kupfer nach Anspruch i, dadurch gekennzeichnet, daß das Zinn in der Legierung ganz durch bis zu 40()/o Zink und bis zu 40/0 Silicium ersetzt ist. PATENT CLAIMS: i. Metal alloy. Base copper, consisting of: up to 12% tin, up to 5% nickel, up to z 0. ö iron, up to 3% tantalum and / or niobium, the remainder copper with the usual impurities. a. Metal alloy based on copper according to Claim i, characterized in that the tin in the alloy is completely replaced by manganese. 3. Metal alloy based on copper according to claim i, characterized in that the tin in the alloy is completely replaced by up to 40/0 zinc and up to 40/0 silicon.
DES137364D 1939-06-09 1939-06-09 Copper alloy Expired DE714821C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DES137364D DE714821C (en) 1939-06-09 1939-06-09 Copper alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DES137364D DE714821C (en) 1939-06-09 1939-06-09 Copper alloy

Publications (1)

Publication Number Publication Date
DE714821C true DE714821C (en) 1941-12-08

Family

ID=7540569

Family Applications (1)

Application Number Title Priority Date Filing Date
DES137364D Expired DE714821C (en) 1939-06-09 1939-06-09 Copper alloy

Country Status (1)

Country Link
DE (1) DE714821C (en)

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