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Copper Alloy C61400-HR50

Supply condition

UNS C61400 · EN CW303G

HR50 = drawn and stress relieved

Preferred condition for condenser/heat-exchanger tube: cold-drawn strength with residual stresses removed to resist stress-corrosion cracking.

High cost $$$$

Values for the HR50 condition

Other C61400 tempers and conditions

C61400 is listed in 7 conditions; see the grade overview at C61400.

Compare all 7 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Soft annealed
Fully softened tube/sheet for expanding, bending, flaring and tube-to-tubesheet rolling.20550550128 HB14 % IACS
Hot rolled and annealed
Choose when maximum uniformity and formability of plate/sheet is needed after hot rolling.22051545133 HB14 % IACS
M20Default
As hot rolled
Standard stocked condition for plate, sheet and tubesheet; best all-round strength/ductility balance.23052545140 HB14 % IACS
As hot extruded
Rod, bar and hollow sections supplied straight from the press; slightly higher strength than hot-rolled plate.25055038145 HB14 % IACS
Light drawn
Lightly cold-drawn tube where straightness and moderate strength gain are wanted with usable ductility.34556532155 HB14 % IACS
HR50This page
Drawn and stress relieved
Preferred condition for condenser/heat-exchanger tube: cold-drawn strength with residual stresses removed to resist stress-corrosion cracking.40058528168 HB14 % IACS
Hard drawn
Maximum-strength cold-drawn rod/tube for wear parts and shafting where ductility is secondary.45062020185 HB14 % IACS

What is C61400-HR50?

C61400-HR50 is C61400 supplied in the HR50 condition — preferred condition for condenser/heat-exchanger tube: cold-drawn strength with residual stresses removed to resist stress-corrosion cracking. C61400-HR50 has a yield strength of 400 MPa (58 ksi) and a tensile strength of 585 MPa (84.8 ksi) — stronger than 80% of copper alloy grades. Elongation at break is 28% and the elastic modulus is 117 GPa (17 Msi). C61400-HR50 has a density of 7.89 g/cm³ (0.285 lb/in³), lighter than 89% of copper alloy grades. It melts at 1,040°C (1,904 °F). M20 is the default condition FabDigit quotes; HR50 is available on request or by drawing note.

Advantages

  • Good corrosion resistance — 78/100, better than 94% of copper alloy grades
  • Readily welded — 70/100, better than 85% of copper alloy grades
  • High strength — 400 MPa (58 ksi), better than 80% of copper alloy grades
  • High service temperature — 260°C (500 °F), better than 75% of copper alloy grades

C61400-HR50 properties

Typical room-temperature values for C61400-HR50; 15 are specific to this condition. Other listed values are C61400 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C61400-HR50 has a density of 7.89 g/cm³ (0.285 lb/in³), lighter than 89% of copper alloy grades. It melts at 1,040°C (1,904 °F).

Density7.89 g/cm³0.29 lb/in³
Melting Point (Solidus)1,040°C1,904 °F
Liquidus Temperature1,045°C1,913 °F

Mechanical14

C61400-HR50 has a yield strength of 400 MPa (58 ksi) and a tensile strength of 585 MPa (84.8 ksi) — stronger than 80% of copper alloy grades. Elongation at break is 28% and the elastic modulus is 117 GPa (17 Msi).

Elastic (Young's) Modulus117 GPa17 Msi
Shear Modulus44 GPa6.4 Msi
Bulk Modulus110 GPa16 Msi
Poisson's Ratio0.32
Tensile Strength (Ultimate)585 MPa84.8 ksi
Yield Strength (0.2% offset)400 MPa58 ksi
Elongation at Break28%
Reduction in Area40%
Shear Strength370 MPa53.7 ksi
Fatigue Strength (Endurance Limit)210 MPa30.5 ksi
Charpy V-Notch Impact (RT)45 J33.2 ft·lbf
Hardness, Brinell168 HB
Hardness, Rockwell B88 HRB
Hardness, Vickers180 HV

Thermal6

C61400-HR50 is rated for continuous service to 260°C (500 °F). It conducts heat at 66.6 W/m·K (38.5 BTU/hr·ft·°F), worse than 57% of copper alloy grades. Thermal expansion is 16.2 µm/m·K (9 µin/in·°F).

Thermal Conductivity66.6 W/m·K38.5 BTU/hr·ft·°F
Specific Heat Capacity376 J/kg·K0.09 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)16.2 µm/m·K9 µin/in·°F
Latent Heat of Fusion210 J/g90.3 BTU/lb
Max Service Temperature (continuous)260°C500 °F
Min Service Temperature-196°C-321 °F

Electrical3

C61400-HR50 conducts electricity at 14 % IACS, worse than 56% of copper alloy grades.

Electrical Conductivity14 % IACS
Electrical Resistivity1.23×10⁻⁷ Ω·m4.84 µΩ·in
Magnetic Responseweakly magnetic

Chemical & Environmental3

Corrosion resistance is very good (78/100), better than 94% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.28 V
Corrosion ResistanceVery good78/100
Chemical Resistance SummaryExcellent in seawater, brackish water and non-oxidising dilute acids (sulphuric, phosphoric, acetic); good against caustics and steam. Attacked by nitric acid, ferric/oxidising chloride salts and moist ammonia; risk of dealuminification in stagnant hot chlorides.

Sustainability4

Producing a kilogram of C61400-HR50 takes about 58 MJ of energy and emits 3.6 kg of CO₂ — more than 61% of copper alloy grades. Typical recycled content is 35%.

Embodied Energy (primary production)58 MJ/kg24,936 BTU/lb
Embodied Carbon (primary production)3.6 kg CO₂/kg
Embodied Water250 L/kg30 gal/lb
Typical Recycled Content35%

Manufacturability8

C61400-HR50's machinability is poor (32/100, worse than 57% of copper alloy grades); weldability very good (70/100); formability fair (38/100).

MachinabilityPoor32/100
Machinability Rating (AISI 1212 = 100 %)50%
WeldabilityVery good70/100
Formability (cold)Fair38/100
CastabilityGood55/100
Brazeability / SolderabilityPoor30/100
PolishabilityVery good70/100
Anodizing Responsen/a — copper alloy; use chemical passivation or clear lacquer instead

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with C61400-HR50

Is C61400 easy to machine?

Tough, gummy chips: use rigid setups, positive-rake carbide, 60–120 m/min surface speed and generous coolant; roughly 20 % of free-cutting brass throughput.

Can C61400 be welded?

GTAW/GMAW with ERCuAl-A2 filler works well; remove alumina film mechanically or with AC/He, preheat 150–200 °C on heavy sections and avoid excessive heat input to prevent aluminium oxide entrapment.

Can C61400 be formed, bent or molded?

Hot work at 750–900 °C; cold form only in O25/O60 tempers, with interstage anneal at 600–650 °C for severe drawing or tube expanding.

What surface finishes work on C61400?

Not anodizable; polishes to a golden lustre, can be pickled in sulphuric/HF-free acid to remove oxide, and takes electroless nickel or clear lacquer for atmospheric appearance retention.

C61400 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
Al6 – 87
Fegrain refiner, raises strength/wear resistance1.5 – 3.52.5
Mn≤ 10.3
Zn≤ 0.2—
Pb≤ 0.01—
P≤ 0.02—
CuCu + named elements 99.5 % minbalance—

C61400-HR50 — frequently asked

What is C61400-HR50 used for?

C61400-HR50 is typically used for ship propeller shafts, valve stems, pump shafts and condenser plates. In short: stronger iron-bearing aluminum bronze; weldable seawater shafting alloy; 300 °C service capability.

What is the yield strength of C61400-HR50?

C61400-HR50 has a typical yield strength of 400 MPa (58 ksi) and a tensile strength of 585 MPa (84.8 ksi) — stronger than 80% of copper alloy grades. Strength varies by condition: see the 7 listed tempers.

Is C61400-HR50 easy to machine?

Not especially — machinability is rated poor (32/100, worse than 57% of copper alloy grades). Tough, gummy chips: use rigid setups, positive-rake carbide, 60–120 m/min surface speed and generous coolant; roughly 20 % of free-cutting brass throughput.

Can C61400-HR50 be welded?

Yes — weldability is rated very good (70/100). GTAW/GMAW with ERCuAl-A2 filler works well; remove alumina film mechanically or with AC/He, preheat 150–200 °C on heavy sections and avoid excessive heat input to prevent aluminium oxide entrapment.

What surface finishes work on C61400-HR50?

Not anodizable; polishes to a golden lustre, can be pickled in sulphuric/HF-free acid to remove oxide, and takes electroless nickel or clear lacquer for atmospheric appearance retention.

Can C61400-HR50 be formed, bent or molded?

Hot work at 750–900 °C; cold form only in O25/O60 tempers, with interstage anneal at 600–650 °C for severe drawing or tube expanding.

What is the maximum service temperature of C61400-HR50?

C61400-HR50 is rated for continuous use to about 260°C (500 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between C61400-M20 and C61400-H80?

M20 is the default condition — standard stocked condition for plate, sheet and tubesheet; best all-round strength/ductility balance. H80: maximum-strength cold-drawn rod/tube for wear parts and shafting where ductility is secondary. Yield strength is 230 MPa in M20 versus 450 MPa in H80.

Sources

  1. ASTM B171/B171M — Copper-Alloy Plate and Sheet for Pressure Vessels, Condensers and Heat Exchangers — ASTM International (2018)
  2. ASTM B111/B111M — Copper and Copper-Alloy Seamless Condenser Tubes — ASTM International (2021)
  3. CDA Alloy Database — C61400 aluminium bronze, D — Copper Development Association (2023)
  4. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  5. ASM Handbook Vol. 13B — Corrosion: Materials (copper alloys in seawater) — ASM International (2005)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.