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Copper Alloy C62580-TQ50

Supply condition

UNS C62580 · ASTM B150

TQ50 = quench hardened and temper annealed

Pick for maximum hardness and galling/wear resistance (dies, wear plates, guide blocks); ductility drops to ~2%.

High cost $$$$

Values for the TQ50 condition

Other C62580 tempers and conditions

C62580 is listed in 4 conditions; see the grade overview at C62580.

Compare all 4 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Soft annealed
Softest supply condition for easier machining or before a subsequent hardening cycle; strength and wear resistance are reduced.3507008217 HB—
As forged and quenched
Closed-die or open-die forgings supplied without further heat treatment — used for high-strength fittings and fastener blanks.414758622 HRC7.5 % IACS
M30Default
As hot extruded
Standard stocked bar/rod condition: full hot-worked strength with the best elongation this alloy offers.427772522 HRC7.5 % IACS
TQ50This page
Quench hardened and temper annealed
Pick for maximum hardness and galling/wear resistance (dies, wear plates, guide blocks); ductility drops to ~2%.545827229 HRC—

What is C62580-TQ50?

C62580-TQ50 is C62580 supplied in the TQ50 condition — pick for maximum hardness and galling/wear resistance (dies, wear plates, guide blocks); ductility drops to ~2%. C62580-TQ50 has a yield strength of 545 MPa (79 ksi) and a tensile strength of 827 MPa (120 ksi) — stronger than 92% of copper alloy grades. Elongation at break is 2% and the elastic modulus is 110 GPa (16 Msi). C62580-TQ50 has a density of 7.25 g/cm³ (0.262 lb/in³), lighter than 100% of copper alloy grades. It melts at 1,027°C (1,881 °F). M30 is the default condition FabDigit quotes; TQ50 is available on request or by drawing note.

Advantages

  • Lightweight — 7.25 g/cm³ (0.262 lb/in³), better than 100% of copper alloy grades
  • High strength — 545 MPa (79 ksi), better than 92% of copper alloy grades
  • High service temperature — 300°C (572 °F), better than 85% of copper alloy grades
  • Good corrosion resistance — 72/100, better than 84% of copper alloy grades

Limitations

  • Difficult to machine — 18/100, worse than 100% of copper alloy grades
  • Limited ductility — 2%, worse than 98% of copper alloy grades
  • Limited formability — 5/100, worse than 98% of copper alloy grades
  • Difficult to weld — 20/100, worse than 88% of copper alloy grades
  • Low electrical conductivity — 7.5 % IACS, worse than 84% of copper alloy grades

C62580-TQ50 properties

Typical room-temperature values for C62580-TQ50; 16 are specific to this condition. Other listed values are C62580 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C62580-TQ50 has a density of 7.25 g/cm³ (0.262 lb/in³), lighter than 100% of copper alloy grades. It melts at 1,027°C (1,881 °F).

Density7.25 g/cm³0.26 lb/in³
Melting Point (Solidus)1,027°C1,881 °F
Liquidus Temperature1,046°C1,915 °F

Mechanical14

C62580-TQ50 has a yield strength of 545 MPa (79 ksi) and a tensile strength of 827 MPa (120 ksi) — stronger than 92% of copper alloy grades. Elongation at break is 2% and the elastic modulus is 110 GPa (16 Msi).

Elastic (Young's) Modulus110 GPa16 Msi
Shear Modulus42 GPa6.1 Msi
Bulk Modulus105 GPa15.2 Msi
Poisson's Ratio0.32
Tensile Strength (Ultimate)827 MPa120 ksi
Yield Strength (0.2% offset)545 MPa79 ksi
Elongation at Break2%
Reduction in Area3%
Shear Strength500 MPa72.5 ksi
Fatigue Strength (Endurance Limit)275 MPa39.9 ksi
Charpy V-Notch Impact (RT)5 J3.7 ft·lbf
Hardness, Brinell285 HB
Hardness, Rockwell C29 HRC
Hardness, Vickers300 HV

Thermal6

C62580-TQ50 is rated for continuous service to 300°C (572 °F). It conducts heat at 42 W/m·K (24.3 BTU/hr·ft·°F), worse than 80% of copper alloy grades. Thermal expansion is 16.2 µm/m·K (9 µin/in·°F).

Thermal Conductivity42 W/m·K24.3 BTU/hr·ft·°F
Specific Heat Capacity375 J/kg·K0.09 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)16.2 µm/m·K9 µin/in·°F
Latent Heat of Fusion220 J/g94.6 BTU/lb
Max Service Temperature (continuous)300°C572 °F
Min Service Temperature-200°C-328 °F

Electrical3

C62580-TQ50 conducts electricity at 7.5 % IACS, worse than 84% of copper alloy grades.

Electrical Conductivity7.5 % IACS
Electrical Resistivity2.3×10⁻⁷ Ω·m9.06 µΩ·in
Magnetic Responseweakly magnetic

Chemical & Environmental3

Corrosion resistance is very good (72/100), better than 84% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.27 V
Corrosion ResistanceVery good72/100
Chemical Resistance SummaryGood resistance to seawater, brines, non-oxidizing acids (dilute H2SO4, HCl at low concentration), organic acids and steam; poor in nitric/oxidizing acids, ammonia and amines (SCC risk); high Al with little Ni makes it susceptible to dealuminification in stagnant hot chlorides.

Sustainability4

Producing a kilogram of C62580-TQ50 takes about 58 MJ of energy and emits 3.8 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)3.8 kg CO₂/kg
Embodied Water320 L/kg38.3 gal/lb
Typical Recycled Content35%

Manufacturability8

C62580-TQ50's machinability is poor (18/100, worse than 100% of copper alloy grades); weldability poor (20/100); formability not recommended (5/100).

MachinabilityPoor18/100
Machinability Rating (AISI 1212 = 100 %)15%
WeldabilityPoor20/100
Formability (cold)Not recommended5/100
CastabilityGood55/100
Brazeability / SolderabilityPoor30/100
PolishabilityVery good70/100
Anodizing Responsen/a — copper-base alloy; use passivation, chemical blackening or electroless nickel instead

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

Working with C62580-TQ50

Is C62580 easy to machine?

Machine like a hard bronze: rigid setup, sharp carbide (K-grade) tools, 5–8° positive rake, 60–120 m/min, generous flood coolant; chips are short and abrasive — rating only about 20 % of free-cutting brass.

Can C62580 be welded?

GTAW/GMAW with matching Al-bronze filler (ERCuAl-A2/A3), preheat 150–250 °C, tight interpass control and slow cooling; high Al content makes it crack- and oxide-film sensitive, so post-weld temper anneal is recommended.

Can C62580 be formed, bent or molded?

Hot forge/extrude at roughly 750–870 °C; virtually no cold formability — bending or heading at room temperature will crack the eutectoid structure.

What surface finishes work on C62580?

Not anodizable; use vapour degrease plus mechanical polish, chemical blackening, passivation or electroless nickel; the alumina film gives good natural tarnish resistance.

C62580 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
Alhigh-aluminium (β-hardenable) range per ASTM B150; verify against mill certificate12 – 1312.5
Fegrain refiner / κ-phase former3 – 54
Nimax, improves dealuminification resistance≤ 20.5
Mn≤ 20.3
Si≤ 0.1—
Zn≤ 0.1—
Sn≤ 0.2—
Curemainder, approx. 81–84 %balance—

C62580-TQ50 — frequently asked

What is C62580-TQ50 used for?

C62580-TQ50 is typically used for aircraft fasteners, high-strength bolts and forged fittings. In short: high-strength forging bronze; aerospace fastener grade; low ductility, hot work only.

What is the yield strength of C62580-TQ50?

C62580-TQ50 has a typical yield strength of 545 MPa (79 ksi) and a tensile strength of 827 MPa (120 ksi) — stronger than 92% of copper alloy grades. Strength varies by condition: see the 4 listed tempers.

Is C62580-TQ50 easy to machine?

Not especially — machinability is rated poor (18/100, worse than 100% of copper alloy grades). Machine like a hard bronze: rigid setup, sharp carbide (K-grade) tools, 5–8° positive rake, 60–120 m/min, generous flood coolant; chips are short and abrasive — rating only about 20 % of free-cutting brass.

Can C62580-TQ50 be welded?

Not readily — weldability is rated poor (20/100). GTAW/GMAW with matching Al-bronze filler (ERCuAl-A2/A3), preheat 150–250 °C, tight interpass control and slow cooling; high Al content makes it crack- and oxide-film sensitive, so post-weld temper anneal is recommended.

What surface finishes work on C62580-TQ50?

Not anodizable; use vapour degrease plus mechanical polish, chemical blackening, passivation or electroless nickel; the alumina film gives good natural tarnish resistance.

Can C62580-TQ50 be formed, bent or molded?

Hot forge/extrude at roughly 750–870 °C; virtually no cold formability — bending or heading at room temperature will crack the eutectoid structure.

What is the maximum service temperature of C62580-TQ50?

C62580-TQ50 is rated for continuous use to about 300°C (572 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between C62580-M30 and C62580-TQ50?

M30 is the default condition — standard stocked bar/rod condition: full hot-worked strength with the best elongation this alloy offers. TQ50: pick for maximum hardness and galling/wear resistance (dies, wear plates, guide blocks); ductility drops to ~2%. Yield strength is 427 MPa in M30 versus 545 MPa in TQ50.

Sources

  1. ASTM B150/B150M — Aluminum Bronze Rod, Bar and Shapes — ASTM International (2019)
  2. CDA / copper.org alloy datasheets, wrought aluminium bronzes C62xxx — Copper Development Association (2023)
  3. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  4. High-aluminium wrought bronze wear-alloy datasheets (AMPCO-class bar/forgings) — AMPCO Metal (2022)

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.