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Copper Alloy C62400-TQ50

Supply condition

UNS C62400 · ASTM B150

TQ50 = quench hardened and temper annealed

Quench from ~870 °C and temper (~600 °C): highest strength and hardness plus refined β structure that greatly improves resistance to dealuminification — preferred for seawater wear parts.

High cost $$$$

Values for the TQ50 condition

Other C62400 tempers and conditions

C62400 is listed in 7 conditions; see the grade overview at C62400.

Compare all 7 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Hot extruded and annealed
Softest supplied condition for extruded rod: lower strength but maximum ductility for subsequent bending, sizing or machining.27062020170 HB—
Hot rolled and annealed
Annealed flat product for parts that must be machined or lightly formed after rolling.27062020170 HB8.5 % IACS
Hot forged and annealed
For closed-die forgings (valve bodies, gear blanks, flanges) supplied annealed to relieve forging stresses.27562018175 HB8.5 % IACS
As hot rolled
Choose for hot-rolled plate and flat products where extruded sections are not available.30065514185 HB—
M30Default
As hot extruded
Standard stock condition for C62400 rod and bar per ASTM B150; best combination of strength, toughness and availability.31066014190 HB8 % IACS
TQ50This page
Quench hardened and temper annealed
Quench from ~870 °C and temper (~600 °C): highest strength and hardness plus refined β structure that greatly improves resistance to dealuminification — preferred for seawater wear parts.4157601022 HRC—
Drawn and stress relieved
Cold-drawn (light draft) then stress relieved: highest yield strength with straight, close-tolerance bar for shafts and pins.45072510205 HB—

What is C62400-TQ50?

C62400-TQ50 is C62400 supplied in the TQ50 condition — quench from ~870 °C and temper (~600 °C): highest strength and hardness plus refined β structure that greatly improves resistance to dealuminification — preferred for seawater wear parts. C62400-TQ50 has a yield strength of 415 MPa (60.2 ksi) and a tensile strength of 760 MPa (110 ksi) — stronger than 82% of copper alloy grades. Elongation at break is 10% and the elastic modulus is 110 GPa (16 Msi). C62400-TQ50 has a density of 7.45 g/cm³ (0.269 lb/in³), lighter than 99% of copper alloy grades. It melts at 1,015°C (1,859 °F). M30 is the default condition FabDigit quotes; TQ50 is available on request or by drawing note.

Advantages

  • Good corrosion resistance — 85/100, better than 100% of copper alloy grades
  • Lightweight — 7.45 g/cm³ (0.269 lb/in³), better than 99% of copper alloy grades
  • High service temperature — 300°C (572 °F), better than 85% of copper alloy grades
  • High strength — 415 MPa (60.2 ksi), better than 82% of copper alloy grades
  • Readily welded — 65/100, better than 80% of copper alloy grades

Limitations

  • Difficult to machine — 22/100, worse than 94% of copper alloy grades
  • Limited formability — 10/100, worse than 89% of copper alloy grades
  • Low electrical conductivity — 8 % IACS, worse than 81% of copper alloy grades
  • Limited ductility — 10%, worse than 76% of copper alloy grades

C62400-TQ50 properties

Typical room-temperature values for C62400-TQ50; 14 are specific to this condition. Other listed values are C62400 reference data and may not represent this condition. Bars are the position among copper alloy grades.

Physical3

C62400-TQ50 has a density of 7.45 g/cm³ (0.269 lb/in³), lighter than 99% of copper alloy grades. It melts at 1,015°C (1,859 °F).

Density7.45 g/cm³0.27 lb/in³
Melting Point (Solidus)1,015°C1,859 °F
Liquidus Temperature1,038°C1,900 °F

Mechanical13

C62400-TQ50 has a yield strength of 415 MPa (60.2 ksi) and a tensile strength of 760 MPa (110 ksi) — stronger than 82% of copper alloy grades. Elongation at break is 10% and the elastic modulus is 110 GPa (16 Msi).

Elastic (Young's) Modulus110 GPa16 Msi
Shear Modulus41 GPa5.9 Msi
Bulk Modulus118 GPa17.1 Msi
Poisson's Ratio0.32
Tensile Strength (Ultimate)760 MPa110 ksi
Yield Strength (0.2% offset)415 MPa60.2 ksi
Elongation at Break10%
Reduction in Area20%
Shear Strength450 MPa65.3 ksi
Fatigue Strength (Endurance Limit)270 MPa39.2 ksi
Charpy V-Notch Impact (RT)16 J11.8 ft·lbf
Hardness, Brinell217 HB
Hardness, Rockwell B97 HRB

Thermal6

C62400-TQ50 is rated for continuous service to 300°C (572 °F). It conducts heat at 46 W/m·K (26.6 BTU/hr·ft·°F), worse than 73% of copper alloy grades. Thermal expansion is 16.2 µm/m·K (9 µin/in·°F).

Thermal Conductivity46 W/m·K26.6 BTU/hr·ft·°F
Specific Heat Capacity419 J/kg·K0.1 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-196°C-321 °F

Electrical3

C62400-TQ50 conducts electricity at 8 % IACS, worse than 81% of copper alloy grades.

Electrical Conductivity8 % IACS
Electrical Resistivity2.15×10⁻⁷ Ω·m8.46 µΩ·in
Magnetic Responseweakly magnetic

Chemical & Environmental3

Corrosion resistance is excellent (85/100), better than 100% of copper alloy grades.

Galvanic Potential (seawater, vs SCE)-0.31 V
Corrosion ResistanceExcellent85/100
Chemical Resistance SummaryVery good in seawater, brines, neutral and mildly acidic waters, dilute sulfuric/organic acids and non-oxidizing media; self-healing alumina film gives good erosion–cavitation resistance. Attacked by oxidizing acids, ammonia and ammoniacal solutions, moist chlorine and sulfides; the high-Al β phase is prone to dealuminification unless quench-hardened and temper-annealed.

Sustainability4

Producing a kilogram of C62400-TQ50 takes about 62 MJ of energy and emits 3.9 kg of CO₂ — more than 76% of copper alloy grades. Typical recycled content is 40%.

Embodied Energy (primary production)62 MJ/kg26,655 BTU/lb
Embodied Carbon (primary production)3.9 kg CO₂/kg
Embodied Water300 L/kg35.9 gal/lb
Typical Recycled Content40%

Manufacturability8

C62400-TQ50's machinability is poor (22/100, worse than 94% of copper alloy grades); weldability good (65/100); formability not recommended (10/100).

MachinabilityPoor22/100
Machinability Rating (AISI 1212 = 100 %)18%
WeldabilityGood65/100
Formability (cold)Not recommended10/100
CastabilityGood55/100
Brazeability / SolderabilityPoor30/100
PolishabilityVery good70/100
Anodizing Responsen/a — copper-base alloy; not anodized. Decorative finishing is by mechanical polish plus lacquer or chemical patination.

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

Working with C62400-TQ50

Is C62400 easy to machine?

Tough, gummy chips — use rigid setups, positive-rake carbide, moderate speed (~60–120 m/min) with heavy soluble-oil flood; rating only ~20 % of free-cutting brass.

Can C62400 be welded?

GTAW/GMAW with matching aluminium-bronze filler (ERCuAl-A2) works well; preheat 150–200 °C on heavy sections, keep interpass low, remove the tenacious alumina film, and re-heat-treat if dealuminification resistance is critical.

Can C62400 be formed, bent or molded?

Hot work at 700–900 °C (forging/extrusion is the normal route); cold formability is poor, so limit cold bending and stress relieve at ~350–400 °C afterwards.

What surface finishes work on C62400?

Polishes to a golden lustre and can be chemically patinated or lacquered; not anodizable, and electroplating requires careful oxide removal/strike layers.

C62400 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
Al10 – 11.510.8
Fe2 – 4.53.2
Mn≤ 0.30.1
Si≤ 0.25—
Ninot specified separately; counted with Co where applicable——
Pbresidual, typical mill limit≤ 0.05—
Curemainder, 86.0 % min per ASTM B150≥ 86 (balance)—

C62400-TQ50 — frequently asked

What is C62400-TQ50 used for?

C62400-TQ50 is typically used for high-strength fasteners, aerospace fittings, gears and structural components. In short: higher-strength aluminum bronze; hot-forged near net shape; low machinability and formability.

What is the yield strength of C62400-TQ50?

C62400-TQ50 has a typical yield strength of 415 MPa (60.2 ksi) and a tensile strength of 760 MPa (110 ksi) — stronger than 82% of copper alloy grades. Strength varies by condition: see the 7 listed tempers.

Is C62400-TQ50 easy to machine?

Not especially — machinability is rated poor (22/100, worse than 94% of copper alloy grades). Tough, gummy chips — use rigid setups, positive-rake carbide, moderate speed (~60–120 m/min) with heavy soluble-oil flood; rating only ~20 % of free-cutting brass.

Can C62400-TQ50 be welded?

Yes — weldability is rated good (65/100). GTAW/GMAW with matching aluminium-bronze filler (ERCuAl-A2) works well; preheat 150–200 °C on heavy sections, keep interpass low, remove the tenacious alumina film, and re-heat-treat if dealuminification resistance is critical.

What surface finishes work on C62400-TQ50?

Polishes to a golden lustre and can be chemically patinated or lacquered; not anodizable, and electroplating requires careful oxide removal/strike layers.

Can C62400-TQ50 be formed, bent or molded?

Hot work at 700–900 °C (forging/extrusion is the normal route); cold formability is poor, so limit cold bending and stress relieve at ~350–400 °C afterwards.

What is the maximum service temperature of C62400-TQ50?

C62400-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 C62400-M30 and C62400-HR50?

M30 is the default condition — standard stock condition for C62400 rod and bar per ASTM B150; best combination of strength, toughness and availability. HR50: cold-drawn (light draft) then stress relieved: highest yield strength with straight, close-tolerance bar for shafts and pins. Yield strength is 310 MPa in M30 versus 450 MPa in HR50.

Sources

  1. ASTM B150/B150M — Aluminum Bronze Rod, Bar and Shapes — ASTM International (2019)
  2. CDA Alloy Datasheet C62400 — Copper Development Association (copper.org) (2023)
  3. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  4. 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.