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Cobalt-Chrome Alloy L605 As Printed

Print state

UNS R30605 · EN 2.4964, CoCr20W15Ni · also Haynes 25, CoCrWNi

Baseline LPBF/SLM condition: fine cellular structure gives high yield strength but reduced ductility and high residual stress — usually heat treated before service.

CNC machiningSpecialty cost $$$$$

Values for the As Printed condition

Other L605 tempers and conditions

L605 is listed in 5 conditions; see the grade overview at L605.

Compare all 5 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
1175–1230 °C, rapid cool
Standard mill condition for sheet, plate, bar and tube — maximum ductility and formability, best corrosion and creep behaviour baseline.4601,01058240 HB—
Hot isostatic pressed
Choose for AM or cast parts needing closed porosity, homogenised structure and best ductility/fatigue for flight or implant hardware.48098050245 HB—
sub-solution anneal (approx. 900–1100 °C)
Use to relax residual stress in welded, cold-formed or additively built parts while keeping most of the strength.5701,0303228 HRC1.9 % IACS
As PrintedThis page
laser powder-bed fusion, no post heat treatment
Baseline LPBF/SLM condition: fine cellular structure gives high yield strength but reduced ductility and high residual stress — usually heat treated before service.7009802032 HRC—
Cold Worked / Cold Drawn (approx. 30–50 % reduction)
Pick for high-strength springs, wire, stents and thin-wall tube where strength matters more than ductility.1,2501,5201042 HRC—

What is L605 As Printed?

L605 As Printed is L605 in the As Printed condition — baseline LPBF/SLM condition: fine cellular structure gives high yield strength but reduced ductility and high residual stress — usually heat treated before service. L605 As Printed has a yield strength of 700 MPa (102 ksi) and a tensile strength of 980 MPa (142 ksi) — stronger than 81% of cobalt-chrome alloy grades. Elongation at break is 20% and the elastic modulus is 215 GPa (31.2 Msi). L605 As Printed has a density of 9.1 g/cm³ (0.329 lb/in³), heavier than 96% of cobalt-chrome alloy grades. It melts at 1,329°C (2,424 °F). Solution Annealed is the default condition FabDigit quotes; As Printed is available on request or by drawing note.

Advantages

  • Forms and bends easily — 60/100, better than 95% of cobalt-chrome alloy grades
  • Readily welded — 72/100, better than 93% of cobalt-chrome alloy grades
  • High strength — 700 MPa (102 ksi), better than 81% of cobalt-chrome alloy grades
  • Ductile — tolerates forming and impact — 20%, better than 78% of cobalt-chrome alloy grades

Limitations

  • Poor heat conductor — 9.4 W/m·K (5.43 BTU/hr·ft·°F), worse than 100% of cobalt-chrome alloy grades
  • High embodied carbon — 19 kg CO₂/kg, worse than 98% of cobalt-chrome alloy grades

L605 As Printed properties

Typical room-temperature values for L605 As Printed; 11 are specific to this condition. Other listed values are L605 reference data and may not represent this condition. Bars are the position among cobalt-chrome alloy grades.

Physical3

L605 As Printed has a density of 9.1 g/cm³ (0.329 lb/in³), heavier than 96% of cobalt-chrome alloy grades. It melts at 1,329°C (2,424 °F).

Density9.1 g/cm³0.33 lb/in³
Melting Point (Solidus)1,329°C2,424 °F
Liquidus Temperature1,410°C2,570 °F

Mechanical14

L605 As Printed has a yield strength of 700 MPa (102 ksi) and a tensile strength of 980 MPa (142 ksi) — stronger than 81% of cobalt-chrome alloy grades. Elongation at break is 20% and the elastic modulus is 215 GPa (31.2 Msi).

Elastic (Young's) Modulus215 GPa31.2 Msi
Shear Modulus87 GPa12.6 Msi
Bulk Modulus178 GPa25.8 Msi
Poisson's Ratio0.29
Tensile Strength (Ultimate)980 MPa142 ksi
Yield Strength (0.2% offset)700 MPa102 ksi
Elongation at Break20%
Reduction in Area55%
Shear Strength620 MPa89.9 ksi
Fatigue Strength (Endurance Limit)300 MPa43.5 ksi
Charpy V-Notch Impact (RT)90 J66.4 ft·lbf
Hardness, Brinell240 HB
Hardness, Rockwell B98 HRB
Hardness, Vickers320 HV

Thermal6

L605 As Printed is rated for continuous service to 700°C (1,292 °F). It conducts heat at 9.4 W/m·K (5.43 BTU/hr·ft·°F), worse than 100% of cobalt-chrome alloy grades. Thermal expansion is 12.3 µm/m·K (6.83 µin/in·°F).

Thermal Conductivity9.4 W/m·K5.4 BTU/hr·ft·°F
Specific Heat Capacity385 J/kg·K0.09 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)12.3 µm/m·K6.8 µin/in·°F
Latent Heat of Fusion270 J/g116 BTU/lb
Max Service Temperature (continuous)700°C1,292 °F
Min Service Temperature-196°C-321 °F

Electrical3

L605 As Printed conducts electricity at 1.9 % IACS, worse than 52% of cobalt-chrome alloy grades.

Electrical Conductivity1.9 % IACS
Electrical Resistivity8.9×10⁻⁷ Ω·m35 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is very good (74/100), worse than 54% of cobalt-chrome alloy grades.

Galvanic Potential (seawater, vs SCE)-0.25 V
Corrosion ResistanceVery good74/100
Chemical Resistance SummaryExcellent high-temperature oxidation and hot-gas/sulfidation resistance to ~1000 °C; very good resistance to body fluids and chloride pitting; good in oxidizing acids and molten salts, but attacked by hot concentrated reducing acids (HCl, H₂SO₄) and by strongly carburizing atmospheres over long exposures.

Sustainability4

Producing a kilogram of L605 As Printed takes about 250 MJ of energy and emits 19 kg of CO₂ — more than 95% of cobalt-chrome alloy grades. Typical recycled content is 30%.

Embodied Energy (primary production)250 MJ/kg107,481 BTU/lb
Embodied Carbon (primary production)19 kg CO₂/kg
Embodied Water500 L/kg59.9 gal/lb
Typical Recycled Content30%

Manufacturability8

L605 As Printed's machinability is poor (15/100, better than 79% of cobalt-chrome alloy grades); weldability very good (72/100); formability good (60/100).

MachinabilityPoor15/100
Machinability Rating (AISI 1212 = 100 %)12%
WeldabilityVery good72/100
Formability (cold)Good60/100
CastabilityGood55/100
Brazeability / SolderabilityVery good70/100
PolishabilityVery good80/100
Anodizing Responsen/a — cobalt-base alloy is not anodized; use passivation, electropolishing or thermal oxide/coatings

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

Working with L605 As Printed

Is L605 easy to machine?

Machine like a work-hardening superalloy: rigid setups, positive-rake carbide or ceramic tooling, low speed / heavy feed, flood coolant and no dwelling to avoid glazing and rapid tool wear.

Can L605 be welded?

Readily GTAW/PAW/EB/laser welded with matching L605 filler (AMS 5796); keep heat input low, use clean argon shielding and re-solution anneal heavily restrained or cold-worked joints.

Can L605 be formed, bent or molded?

Cold forms well when annealed but hardens fast — allow generous bend radii, interstage anneals at 1175–1230 °C; hot work at 1150–1230 °C and finish above ~1050 °C.

What surface finishes work on L605?

Not anodizable; use pickling/passivation, electropolishing or fine mechanical polishing (excellent mirror finish for implants), plus aluminide or thermal-barrier coatings for hot-gas parts.

L605 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
Cr19 – 2120
W14 – 1615
Ni9 – 1110
Fe≤ 31.5
Mn1 – 21.5
C0.05 – 0.150.1
Si≤ 0.40.2
P≤ 0.04
S≤ 0.03
Cobalance, nominally ~51 %balance

L605 As Printed — frequently asked

What is L605 As Printed used for?

L605 As Printed is typically used for combustion liners and transition ducts, turbine and exhaust valves, hot-gas ducting and seals, high-temperature springs, afterburner and nozzle components and surgical implants and stents. In short: aerospace high-temp cobalt.

What is the yield strength of L605 As Printed?

L605 As Printed has a typical yield strength of 700 MPa (102 ksi) and a tensile strength of 980 MPa (142 ksi) — stronger than 81% of cobalt-chrome alloy grades. Strength varies by condition: see the 5 listed tempers.

Is L605 As Printed easy to machine?

Not especially — machinability is rated poor (15/100, better than 79% of cobalt-chrome alloy grades). Machine like a work-hardening superalloy: rigid setups, positive-rake carbide or ceramic tooling, low speed / heavy feed, flood coolant and no dwelling to avoid glazing and rapid tool wear.

Can L605 As Printed be welded?

Yes — weldability is rated very good (72/100). Readily GTAW/PAW/EB/laser welded with matching L605 filler (AMS 5796); keep heat input low, use clean argon shielding and re-solution anneal heavily restrained or cold-worked joints.

What surface finishes work on L605 As Printed?

Not anodizable; use pickling/passivation, electropolishing or fine mechanical polishing (excellent mirror finish for implants), plus aluminide or thermal-barrier coatings for hot-gas parts.

Can L605 As Printed be formed, bent or molded?

Cold forms well when annealed but hardens fast — allow generous bend radii, interstage anneals at 1175–1230 °C; hot work at 1150–1230 °C and finish above ~1050 °C.

What is the maximum service temperature of L605 As Printed?

L605 As Printed is rated for continuous use to about 700°C (1,292 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between L605 Solution Annealed and L605-HIP?

Solution Annealed is the default condition — standard mill condition for sheet, plate, bar and tube — maximum ductility and formability, best corrosion and creep behaviour baseline. HIP: choose for AM or cast parts needing closed porosity, homogenised structure and best ductility/fatigue for flight or implant hardware. Yield strength is 460 MPa in Solution Annealed versus 480 MPa in HIP.

Can FabDigit make parts in L605 As Printed?

Yes — L605 As Printed is available for CNC machining with instant online pricing. Upload a STEP file to get a price and a DFM check.

Sources

  1. AMS 5537 — Cobalt Alloy Sheet, Strip and Plate (UNS R30605) — SAE International (2020)
  2. AMS 5759 — Cobalt Alloy Bars, Forgings and Rings (UNS R30605) — SAE International (2019)
  3. ASTM F90 — Wrought Co-20Cr-15W-10Ni Alloy for Surgical Implant Applications — ASTM International (2021)
  4. HAYNES 25 alloy technical data — Haynes International (2020)
  5. ASM Handbook Vol.1 & Vol.2 — Superalloys / Cobalt-base alloys — ASM International (1990)
  6. Additive manufacturing (LPBF) L605 mechanical property compilations — peer-reviewed AM literature / powder producer datasheets (2023)

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.