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Nickel Alloy 2.4878 CD+P

Supply condition

EN 2.4878

CD+P = cold drawn / cold worked then precipitation hardened bar & wire

Small-diameter fastener and spring stock where cold work plus ageing lifts proof strength above the standard +P conditions.

High cost $$$$

Values for the CD+P condition

Other 2.4878 tempers and conditions

2.4878 is listed in 5 conditions; see the grade overview at 2.4878.

Compare all 5 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Solution annealed
Choose for forming, deep machining or as raw stock before the customer's own precipitation ageing.45090040220 HB—
As forged / hot rolled, unheat-treated stock
Semi-finished forging or billet stock intended for further hot work and a full solution + ageing cycle at the part maker.5601,0003025 HRC1.4 % IACS
Precipitation hardened
Choose where long-term creep and stress-relaxation resistance above ~650 °C matter more than peak room-temperature strength; the higher solution temperature coarsens the grain.7601,1902034 HRC—
+P1080Default
Precipitation hardened
Standard high-strength bolting condition: finer grain from the lower solution temperature gives the highest room-temperature proof strength.8201,2501837 HRC—
CD+PThis page
Cold drawn / cold worked then precipitation hardened bar & wire
Small-diameter fastener and spring stock where cold work plus ageing lifts proof strength above the standard +P conditions.9801,3801241 HRC—

What is 2.4878 CD+P?

2.4878 CD+P is 2.4878 supplied in the CD+P condition — small-diameter fastener and spring stock where cold work plus ageing lifts proof strength above the standard +P conditions. 2.4878 CD+P has a yield strength of 980 MPa (142 ksi) and a tensile strength of 1,380 MPa (200 ksi) — stronger than 95% of nickel alloy grades. Elongation at break is 12% and the elastic modulus is 213 GPa (30.9 Msi). 2.4878 CD+P has a density of 8.2 g/cm³ (0.296 lb/in³), lighter than 63% of nickel alloy grades. It melts at 1,310°C (2,390 °F). +P1080 is the default condition FabDigit quotes; CD+P is available on request or by drawing note.

Advantages

  • High strength — 980 MPa (142 ksi), better than 95% of nickel alloy grades

Limitations

  • Limited ductility — 12%, worse than 83% of nickel alloy grades
  • Limited formability — 12/100, worse than 83% of nickel alloy grades
  • Difficult to weld — 25/100, worse than 82% of nickel alloy grades

2.4878 CD+P properties

Typical room-temperature values for 2.4878 CD+P; 11 are specific to this condition. Other listed values are 2.4878 reference data and may not represent this condition. Bars are the position among nickel alloy grades.

Physical3

2.4878 CD+P has a density of 8.2 g/cm³ (0.296 lb/in³), lighter than 63% of nickel alloy grades. It melts at 1,310°C (2,390 °F).

Density8.2 g/cm³0.3 lb/in³
Melting Point (Solidus)1,310°C2,390 °F
Liquidus Temperature1,370°C2,498 °F

Mechanical16

2.4878 CD+P has a yield strength of 980 MPa (142 ksi) and a tensile strength of 1,380 MPa (200 ksi) — stronger than 95% of nickel alloy grades. Elongation at break is 12% and the elastic modulus is 213 GPa (30.9 Msi).

Elastic (Young's) Modulus213 GPa30.9 Msi
Shear Modulus82 GPa11.9 Msi
Bulk Modulus175 GPa25.4 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)1,380 MPa200 ksi
Yield Strength (0.2% offset)980 MPa142 ksi
Elongation at Break12%
Reduction in Area18%
Compressive Strength830 MPa120 ksi
Shear Strength755 MPa110 ksi
Fatigue Strength (Endurance Limit)500 MPa72.5 ksi
Fracture Toughness (K_IC)88 MPa·√m80.1 ksi·√in
Charpy V-Notch Impact (RT)25 J18.4 ft·lbf
Hardness, Brinell345 HB
Hardness, Rockwell C41 HRC
Hardness, Vickers405 HV

Thermal6

2.4878 CD+P is rated for continuous service to 650°C (1,202 °F). It conducts heat at 11 W/m·K (6.36 BTU/hr·ft·°F), worse than 60% of nickel alloy grades. Thermal expansion is 12.3 µm/m·K (6.83 µin/in·°F).

Thermal Conductivity11 W/m·K6.4 BTU/hr·ft·°F
Specific Heat Capacity435 J/kg·K0.1 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)12.3 µm/m·K6.8 µin/in·°F
Latent Heat of Fusion295 J/g127 BTU/lb
Max Service Temperature (continuous)650°C1,202 °F
Min Service Temperature-196°C-321 °F

Electrical3

2.4878 CD+P conducts electricity at 1.4 % IACS, worse than 65% of nickel alloy grades.

Electrical Conductivity1.4 % IACS
Electrical Resistivity1.24×10⁻⁶ Ω·m48.8 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is very good (78/100), better than 51% of nickel alloy grades.

Galvanic Potential (seawater, vs SCE)-0.1 V
Corrosion ResistanceVery good78/100
Chemical Resistance SummaryExcellent oxidation and sulphidation resistance to ~900 °C thanks to ~25 % Cr; good in steam, hot gases and many neutral/alkaline media; attacked by hot concentrated halide acids and molten salts containing lead/sulphur.

Sustainability4

Producing a kilogram of 2.4878 CD+P takes about 150 MJ of energy and emits 13 kg of CO₂ — less than 68% of nickel alloy grades. Typical recycled content is 30%.

Embodied Energy (primary production)150 MJ/kg64,488 BTU/lb
Embodied Carbon (primary production)13 kg CO₂/kg
Embodied Water400 L/kg47.9 gal/lb
Typical Recycled Content30%

Manufacturability7

2.4878 CD+P's machinability is not recommended (12/100, worse than 86% of nickel alloy grades); weldability poor (25/100); formability not recommended (12/100).

MachinabilityNot recommended12/100
Machinability Rating (AISI 1212 = 100 %)11%
WeldabilityPoor25/100
Formability (cold)Not recommended12/100
Brazeability / SolderabilityFair45/100
PolishabilityVery good70/100
Anodizing Responsen/a — nickel alloy, not anodizable; use passivation, electropolish or protective coatings

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

Working with 2.4878 CD+P

Is 2.4878 easy to machine?

Machine preferably in the solution-annealed state with rigid setups, positive-rake carbide or ceramic tooling, low surface speed, heavy constant feed and flood coolant to avoid work hardening and glazing.

Can 2.4878 be welded?

GTAW with matched or Ni-Cr-Mo filler in the solution-annealed condition; the alloy is strain-age crack sensitive, so weld cold, minimise restraint and re-solution/age after welding.

Can 2.4878 be formed, bent or molded?

Hot work between about 1100 and 950 °C; cold forming is only practical in the +AT condition and requires high press loads plus intermediate annealing.

What surface finishes work on 2.4878?

Not anodizable — use pickling/passivation, electropolishing, shot peening of thread roots for fatigue life, or aluminide/thermal-barrier coatings for hot-gas service.

2.4878 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
Ccarbide former for grain-boundary strength0.03 – 0.10.06
Croxidation/hot corrosion resistance23 – 2625
Co18 – 2220
Mosolid-solution strengthening3 – 54
Tiγ′ former1.8 – 2.72.3
Alγ′ former0.8 – 1.61.2
Feresidual≤ 20.8
Mn≤ 10.3
Si≤ 10.3
Bcreep-ductility micro-addition0 – 0.010.01
Zr≤ 0.10.03
Cu≤ 0.2—
S≤ 0.02—
P≤ 0.02—
Nibalance, typically 43–50 %balance—

2.4878 CD+P — frequently asked

What is 2.4878 CD+P used for?

2.4878 CD+P is typically used for gas turbine fasteners, high-temperature bolting and turbine hot-section hardware. In short: waspaloy-class bolting alloy; 1250 MPa at 730 °C service; hardest to machine of family.

What is the yield strength of 2.4878 CD+P?

2.4878 CD+P has a typical yield strength of 980 MPa (142 ksi) and a tensile strength of 1,380 MPa (200 ksi) — stronger than 95% of nickel alloy grades. Strength varies by condition: see the 5 listed tempers.

Is 2.4878 CD+P easy to machine?

Not especially — machinability is rated not recommended (12/100, worse than 86% of nickel alloy grades). Machine preferably in the solution-annealed state with rigid setups, positive-rake carbide or ceramic tooling, low surface speed, heavy constant feed and flood coolant to avoid work hardening and glazing.

Can 2.4878 CD+P be welded?

Not readily — weldability is rated poor (25/100). GTAW with matched or Ni-Cr-Mo filler in the solution-annealed condition; the alloy is strain-age crack sensitive, so weld cold, minimise restraint and re-solution/age after welding.

What surface finishes work on 2.4878 CD+P?

Not anodizable — use pickling/passivation, electropolishing, shot peening of thread roots for fatigue life, or aluminide/thermal-barrier coatings for hot-gas service.

Can 2.4878 CD+P be formed, bent or molded?

Hot work between about 1100 and 950 °C; cold forming is only practical in the +AT condition and requires high press loads plus intermediate annealing.

What is the maximum service temperature of 2.4878 CD+P?

2.4878 CD+P is rated for continuous use to about 650°C (1,202 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Sources

  1. EN 10269 — Steels and nickel alloys for fasteners with specified elevated and/or low temperature properties — CEN (2013)
  2. EN 10302 — Creep resisting steels, nickel and cobalt alloys — CEN (2008)
  3. ASM Handbook Vol. 1 — Properties and Selection: Irons, Steels and High-Performance Alloys (Ni-base superalloys) — ASM International (1990)
  4. Superalloys: A Technical Guide, 2nd ed. — ASM International (2002)
  5. Nickel-base precipitation-hardening bolting alloy datasheets (Waspaloy / Nimonic 90 class) — Special Metals / Böhler (2020)

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.