Welding of Copper Alloys 
JABIN MATHEW BENJAMIN 
13MY04
Copper And Copper Alloys 
• Excellent electrical and thermal conductivities 
• Outstanding resistance to corrosion 
• Ease of fabrication 
• Good strength and fatigue resistance 
2 
Dept. of Metallurgical Enng 10/16/2014
Copper Alloys 
• COPPERS, WHICH CONTAIN A MINIMUM OF 99.3% CU 
• HIGH-COPPER ALLOYS, WHICH CONTAIN UP TO 5% ALLOYING ELEMENTS 
• COPPER-ZINC ALLOYS (BRASSES), WHICH CONTAIN UP TO 40% ZN 
• COPPER-TIN ALLOYS (PHOSPHOR BRONZES), WHICH CONTAIN UP TO 10% SN 
AND 0.2% P 
• COPPER-ALUMINUM ALLOYS (ALUMINUM BRONZES), WHICH CONTAIN UP TO 10% 
AL 
• COPPER-SILICON ALLOYS (SILICON BRONZES), WHICH CONTAIN UP TO 3% SI 
• COPPER-NICKEL ALLOYS, WHICH CONTAIN UP TO 30% NI 
• COPPER-ZINC-NICKEL ALLOYS (NICKEL SILVERS), WHICH CONTAIN UP TO 27% ZN 
AND 18% NI 
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Dept. of Metallurgical Enng 10/16/2014
Alloying Elements and weldability 
• Zinc 
• reduces the weldability of all brasses 
• Tin 
• increases the hot-crack susceptibility 
• Beryllium, aluminum, and nickel 
• Oxide entrapment, which may reduce the strength of the weldment. 
• Formation of these oxides prevented by shielding gas or by fluxing 
• Silicon 
• beneficial because of its deoxidizing and fluxing actions. 
• Low thermal conductivity makes silicon bronzes the most weldable of the 
4 
copper Dept. of Metallurgical Enng alloys for any arc process. 10/16/2014
• Phosphorus 
• does not adversely affect or hinder welding 
• Chromium 
• inert protective atmosphere to prevent formation of chromium oxides. 
• Cadmium 
• no serious effect on the weldability of copper 
• Oxygen 
• cause porosity and reduce the strength of welds 
• Deoxidizing elements--usually phosphorus, silicon, aluminum, iron, or 
manganese. 
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Dept. of Metallurgical Enng 10/16/2014
Factors Affecting Weldability 
 Effect of Thermal Conductivity. 
 Cu has high thermal conductivities 
 the type of current and shielding gas must be selected to provide maximum heat input to the joint 
 preheating may be decided based on thickness 
 Counteracts the rapid head dissipation 
 Cold worked Cu alloys tend to become weaker and softer at HAZ 
hot cracking may occur in heavily cold worked 
 Welding Position 
 highly fluid nature 
 flat position is used whenever possible 
 Vertical, overhead and the horizontal position- seldom used 
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Dept. of Metallurgical Enng 10/16/2014
 Precipitation-Hardenable Alloys 
 Beryllium, chromium, boron, nickel, silicon, and zirconium. 
 Care must be taken to avoid oxidation and incomplete fusion. 
 Reduction in mechanical properties due to overageing 
 Should be welded in the annealed condition, followed by precipitation hardening treatment 
 Hot Cracking 
 copper-tin and copper-nickel, are susceptible to hot cracking 
 wide liquidus-to-solidus temperature range 
 Severe shrinkage stresses produce interdendritic separation during metal solidification 
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Dept. of Metallurgical Enng 10/16/2014
 Porosity 
 zinc, cadmium, and phosphorus have low boiling points. 
 Vaporization of these elements during welding may result in porosity. 
 Higher travel speed and filler metals with less volatile element content 
 Surface Condition 
 Oxides formed are difficult to remove 
 Cleaning and shielding helps to avoid oxide formation 
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Dept. of Metallurgical Enng 10/16/2014
Welding of Cu 
 Difficulties: High oxygen content and impurities 
 Electrode: Ecu and filler: ERCu 
 Preheating : thickness, conductivity 
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Dept. of Metallurgical Enng 10/16/2014
Preheating 
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Dept. of Metallurgical Enng 10/16/2014
Effect of shielding gas 
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Dept. of Metallurgical Enng 10/16/2014
 GTAW 
 Upto 3.2mm thickness but more for flat position 
 Shielding: upto 1.6mm Ar and over 1.6mm He, deeper penetration 
 Pulsed current can be used 
 GMAW 
 Shielding: Ar or mixture of Ar and He 
 Filler: ERCu 
 Spray transfer and pulsed current 
 SMAW 
 ECuSi, ECuSn-A 
 DCEP 
 Flat position 
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Dept. of Metallurgical Enng 10/16/2014
Welding of Copper-Zinc Alloys (Brass) 
• C20500, C49080, C83300 
• Evolution of zinc fumes is a problem 
• Low-zinc brasses are shown to have good weldability using GTAW 
• High-zinc brasses, tin brasses, special brasses, and nickel silvers have only fair weldability 
• Preheating is not normally required 
• Leaded brasses are unweldable 
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Dept. of Metallurgical Enng 10/16/2014
• Shielding: He-for alloys having higher thermal conductivities. 
• Filler should not contain zinc 
• Low zinc- ERCuSn-A 
 GMAW 
14 
• Unleaded brasses can be welded using GMAW.- low-zinc alloys (red brasses) and the high zinc 
alloys 
• Filler should not contain copper-zinc- Silicon bronze (ERCuSi-A)- good fluidity 
• DCEP 
• Preheat: 95 to 315 °C- low zinc alloys 
• High zinc alloys- more porosities 
• Filler ERCuAl-A2 strength or ERCuSn-A colour match 
Dept. of Metallurgical Enng 10/16/2014
• SMAW 
• Covered electrodes- ECuSi, ECuSn-A, ECuSn-C, ECuAl-A2, ECuAl-B 
• Low zinc- ECu-Sn-A and ECuSn-C 
• Preheating of the base metal from 200 to 260 °C 
• High zinc copper alloys can be welded with aluminum bronze (ECuAl-A2) 
electrodes 
• Preheat and interpass temperatures are 260 to 370 °C 
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Dept. of Metallurgical Enng 10/16/2014
Welding of Copper-Tin alloys 
(Phosphor Bronzes) 
• C50100-C52400 
• GTAW 
• Up to approximately 13 mm 
• DCEN or a stabilized alternating current 
• Shot peening each layer of multi-pass welds reduces cracking and stresses 
• Shielding- Argon- restricts the size of the HAZ. 
• Thicker sections, helium shielding gas 
• Filler metal- ERCuSn-A 
• Preheating: not required for thin sections, Thick sections require preheating to 
175 or 200 °C 
• Interpass temperature should not exceed 200 °C 
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Dept. of Metallurgical Enng 10/16/2014
• GMAW 
• Thicknesses of 9.5 to 13 mm. 
• 90° single-V grooves are used 
• Filler Metal- ERCuSn-A 
17 
• Preheating of the phosphor bronzes helps in obtaining complete fusion, less porosity, but columnar 
grains and hot cracking 
• SMAW 
• Covered electrodes: ECuSn-A and ECu-Sn-C 
• Preheating is required in the range of 150 to 200 °C 
• Maximum ductility, the welded assembly should be postweld heat treated to 480 °C (900 °F) and 
Dept. of Metallcurogicoalle Endn grapidly. 10/16/2014
Welding of Copper-Nickel Alloys 
(C70000-C79900) 
• GTAW 
• Preferred for copper-nickel alloys with section thicknesses up to 1.6 mm 
• Electrode- EWTH-2 
• Ar shielding gas- provides better arc control and stability, 
• DCEN, Alternating current can be employed for automatic welding 
• Preheating is not necessary and backing strips or rings can be used 
18 
• Filler Metals: Deoxidized- ERCuNi- minimize porosity and the possibility of oxygen embrittlement 
• Autogenous welds can sometimes be made on sheet thicknesses up to 1.6 mm 
Dept. of Metallurgical Enng 10/16/2014
• GMAW 
19 
• Preferred welding process for non-leaded copper-nickel alloys thicker than approximately1.6 mm 
(0.06 in.). 
• Preferred welding position: Flat position 
• Preferred shielding gas: Ar 
• Argon-helium mixes give better penetration on thick sections. 
• Direct current electrode positive is recommended. 
• Spray or short-circuiting transfer 
• Filler Metals. ERCuNi- 0.15 to 1.00% Ti, which serves as a deoxidizer 
• No preheating or postheating 
• Interpass temperatures should be maintained below 65 °C 
Dept. of Metallurgical Enng 10/16/2014
• SMAW 
• Both wrought and cast forms 
• Copper-nickel electrode- ECuNi 
• DCEP 
• Special care is needed to ensure complete slag removal 
• Vertical and overhead positions 
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Dept. of Metallurgical Enng 10/16/2014
Other processes for welding of Cu 
 Laser beam welding 
 Difficulties: high reflection of laser beam and high thermal conductivity 
 Absorption increases with temperature 
 Shorter wavelength has better welding 
 Electron beam welding 
 Thin and thick sections 
 Resistance spot welding 
 Lower conductivity alloys readily spot welded 
 Not practical for unalloyed Cu 
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Dept. of Metallurgical Enng 10/16/2014
 Flash welding 
 Leaded Cu (upto 1% Pb) can be flash welded 
 Rapid upsetting at minimum pressure 
 Low melting point and narrow plastic range 
 Premature termination of current: lack of fusion 
 Delayed termination: over heating 
 Solid state welding 
 Annealed Cu can be welded at room temperature: good malleability 
 Diffusion welded or explosive welding 
22 
Dept. of Metallurgical Enng 10/16/2014
Reference 
 Welding of copper and copper alloys, AWS welding handbook, Volume 3, 
Ed. 8, 1997 
 ASM metal handbook, volume 6, 1993 
23 
Dept. of Metallurgical Enng 10/16/2014
THANK YOU 
24 
Dept. of Metallurgical Enng 10/16/2014

Welding of copper alloys

  • 1.
    Welding of CopperAlloys JABIN MATHEW BENJAMIN 13MY04
  • 2.
    Copper And CopperAlloys • Excellent electrical and thermal conductivities • Outstanding resistance to corrosion • Ease of fabrication • Good strength and fatigue resistance 2 Dept. of Metallurgical Enng 10/16/2014
  • 3.
    Copper Alloys •COPPERS, WHICH CONTAIN A MINIMUM OF 99.3% CU • HIGH-COPPER ALLOYS, WHICH CONTAIN UP TO 5% ALLOYING ELEMENTS • COPPER-ZINC ALLOYS (BRASSES), WHICH CONTAIN UP TO 40% ZN • COPPER-TIN ALLOYS (PHOSPHOR BRONZES), WHICH CONTAIN UP TO 10% SN AND 0.2% P • COPPER-ALUMINUM ALLOYS (ALUMINUM BRONZES), WHICH CONTAIN UP TO 10% AL • COPPER-SILICON ALLOYS (SILICON BRONZES), WHICH CONTAIN UP TO 3% SI • COPPER-NICKEL ALLOYS, WHICH CONTAIN UP TO 30% NI • COPPER-ZINC-NICKEL ALLOYS (NICKEL SILVERS), WHICH CONTAIN UP TO 27% ZN AND 18% NI 3 Dept. of Metallurgical Enng 10/16/2014
  • 4.
    Alloying Elements andweldability • Zinc • reduces the weldability of all brasses • Tin • increases the hot-crack susceptibility • Beryllium, aluminum, and nickel • Oxide entrapment, which may reduce the strength of the weldment. • Formation of these oxides prevented by shielding gas or by fluxing • Silicon • beneficial because of its deoxidizing and fluxing actions. • Low thermal conductivity makes silicon bronzes the most weldable of the 4 copper Dept. of Metallurgical Enng alloys for any arc process. 10/16/2014
  • 5.
    • Phosphorus •does not adversely affect or hinder welding • Chromium • inert protective atmosphere to prevent formation of chromium oxides. • Cadmium • no serious effect on the weldability of copper • Oxygen • cause porosity and reduce the strength of welds • Deoxidizing elements--usually phosphorus, silicon, aluminum, iron, or manganese. 5 Dept. of Metallurgical Enng 10/16/2014
  • 6.
    Factors Affecting Weldability  Effect of Thermal Conductivity.  Cu has high thermal conductivities  the type of current and shielding gas must be selected to provide maximum heat input to the joint  preheating may be decided based on thickness  Counteracts the rapid head dissipation  Cold worked Cu alloys tend to become weaker and softer at HAZ hot cracking may occur in heavily cold worked  Welding Position  highly fluid nature  flat position is used whenever possible  Vertical, overhead and the horizontal position- seldom used 6 Dept. of Metallurgical Enng 10/16/2014
  • 7.
     Precipitation-Hardenable Alloys  Beryllium, chromium, boron, nickel, silicon, and zirconium.  Care must be taken to avoid oxidation and incomplete fusion.  Reduction in mechanical properties due to overageing  Should be welded in the annealed condition, followed by precipitation hardening treatment  Hot Cracking  copper-tin and copper-nickel, are susceptible to hot cracking  wide liquidus-to-solidus temperature range  Severe shrinkage stresses produce interdendritic separation during metal solidification 7 Dept. of Metallurgical Enng 10/16/2014
  • 8.
     Porosity zinc, cadmium, and phosphorus have low boiling points.  Vaporization of these elements during welding may result in porosity.  Higher travel speed and filler metals with less volatile element content  Surface Condition  Oxides formed are difficult to remove  Cleaning and shielding helps to avoid oxide formation 8 Dept. of Metallurgical Enng 10/16/2014
  • 9.
    Welding of Cu  Difficulties: High oxygen content and impurities  Electrode: Ecu and filler: ERCu  Preheating : thickness, conductivity 9 Dept. of Metallurgical Enng 10/16/2014
  • 10.
    Preheating 10 Dept.of Metallurgical Enng 10/16/2014
  • 11.
    Effect of shieldinggas 11 Dept. of Metallurgical Enng 10/16/2014
  • 12.
     GTAW Upto 3.2mm thickness but more for flat position  Shielding: upto 1.6mm Ar and over 1.6mm He, deeper penetration  Pulsed current can be used  GMAW  Shielding: Ar or mixture of Ar and He  Filler: ERCu  Spray transfer and pulsed current  SMAW  ECuSi, ECuSn-A  DCEP  Flat position 12 Dept. of Metallurgical Enng 10/16/2014
  • 13.
    Welding of Copper-ZincAlloys (Brass) • C20500, C49080, C83300 • Evolution of zinc fumes is a problem • Low-zinc brasses are shown to have good weldability using GTAW • High-zinc brasses, tin brasses, special brasses, and nickel silvers have only fair weldability • Preheating is not normally required • Leaded brasses are unweldable 13 Dept. of Metallurgical Enng 10/16/2014
  • 14.
    • Shielding: He-foralloys having higher thermal conductivities. • Filler should not contain zinc • Low zinc- ERCuSn-A  GMAW 14 • Unleaded brasses can be welded using GMAW.- low-zinc alloys (red brasses) and the high zinc alloys • Filler should not contain copper-zinc- Silicon bronze (ERCuSi-A)- good fluidity • DCEP • Preheat: 95 to 315 °C- low zinc alloys • High zinc alloys- more porosities • Filler ERCuAl-A2 strength or ERCuSn-A colour match Dept. of Metallurgical Enng 10/16/2014
  • 15.
    • SMAW •Covered electrodes- ECuSi, ECuSn-A, ECuSn-C, ECuAl-A2, ECuAl-B • Low zinc- ECu-Sn-A and ECuSn-C • Preheating of the base metal from 200 to 260 °C • High zinc copper alloys can be welded with aluminum bronze (ECuAl-A2) electrodes • Preheat and interpass temperatures are 260 to 370 °C 15 Dept. of Metallurgical Enng 10/16/2014
  • 16.
    Welding of Copper-Tinalloys (Phosphor Bronzes) • C50100-C52400 • GTAW • Up to approximately 13 mm • DCEN or a stabilized alternating current • Shot peening each layer of multi-pass welds reduces cracking and stresses • Shielding- Argon- restricts the size of the HAZ. • Thicker sections, helium shielding gas • Filler metal- ERCuSn-A • Preheating: not required for thin sections, Thick sections require preheating to 175 or 200 °C • Interpass temperature should not exceed 200 °C 16 Dept. of Metallurgical Enng 10/16/2014
  • 17.
    • GMAW •Thicknesses of 9.5 to 13 mm. • 90° single-V grooves are used • Filler Metal- ERCuSn-A 17 • Preheating of the phosphor bronzes helps in obtaining complete fusion, less porosity, but columnar grains and hot cracking • SMAW • Covered electrodes: ECuSn-A and ECu-Sn-C • Preheating is required in the range of 150 to 200 °C • Maximum ductility, the welded assembly should be postweld heat treated to 480 °C (900 °F) and Dept. of Metallcurogicoalle Endn grapidly. 10/16/2014
  • 18.
    Welding of Copper-NickelAlloys (C70000-C79900) • GTAW • Preferred for copper-nickel alloys with section thicknesses up to 1.6 mm • Electrode- EWTH-2 • Ar shielding gas- provides better arc control and stability, • DCEN, Alternating current can be employed for automatic welding • Preheating is not necessary and backing strips or rings can be used 18 • Filler Metals: Deoxidized- ERCuNi- minimize porosity and the possibility of oxygen embrittlement • Autogenous welds can sometimes be made on sheet thicknesses up to 1.6 mm Dept. of Metallurgical Enng 10/16/2014
  • 19.
    • GMAW 19 • Preferred welding process for non-leaded copper-nickel alloys thicker than approximately1.6 mm (0.06 in.). • Preferred welding position: Flat position • Preferred shielding gas: Ar • Argon-helium mixes give better penetration on thick sections. • Direct current electrode positive is recommended. • Spray or short-circuiting transfer • Filler Metals. ERCuNi- 0.15 to 1.00% Ti, which serves as a deoxidizer • No preheating or postheating • Interpass temperatures should be maintained below 65 °C Dept. of Metallurgical Enng 10/16/2014
  • 20.
    • SMAW •Both wrought and cast forms • Copper-nickel electrode- ECuNi • DCEP • Special care is needed to ensure complete slag removal • Vertical and overhead positions 20 Dept. of Metallurgical Enng 10/16/2014
  • 21.
    Other processes forwelding of Cu  Laser beam welding  Difficulties: high reflection of laser beam and high thermal conductivity  Absorption increases with temperature  Shorter wavelength has better welding  Electron beam welding  Thin and thick sections  Resistance spot welding  Lower conductivity alloys readily spot welded  Not practical for unalloyed Cu 21 Dept. of Metallurgical Enng 10/16/2014
  • 22.
     Flash welding  Leaded Cu (upto 1% Pb) can be flash welded  Rapid upsetting at minimum pressure  Low melting point and narrow plastic range  Premature termination of current: lack of fusion  Delayed termination: over heating  Solid state welding  Annealed Cu can be welded at room temperature: good malleability  Diffusion welded or explosive welding 22 Dept. of Metallurgical Enng 10/16/2014
  • 23.
    Reference  Weldingof copper and copper alloys, AWS welding handbook, Volume 3, Ed. 8, 1997  ASM metal handbook, volume 6, 1993 23 Dept. of Metallurgical Enng 10/16/2014
  • 24.
    THANK YOU 24 Dept. of Metallurgical Enng 10/16/2014