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Nickel Alloy Alloy 684-ST (Solution annealed)

Heat-treated state

UNS N07500 · EN 2.4983

Softest supplied state — use when heavy machining, hot/cold forming or fabrication must precede final ageing.

High cost $$$$

Values for the ST condition

Other Alloy 684 tempers and conditions

Alloy 684 is listed in 5 conditions; see the grade overview at Alloy 684.

Compare all 5 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
STThis page
Solution annealed
Softest supplied state — use when heavy machining, hot/cold forming or fabrication must precede final ageing.5859653526 HRC—
As hot forged / hot rolled
Mill-supplied forged stock intended for further solution treatment and ageing by the part maker.7001,1002232 HRC1.5 % IACS
Investment cast + solution and aged
Equiaxed investment-cast blades/vanes and integral wheels where forging is impractical; lower ductility than wrought.7901,035636 HRC—
STADefault
Solution treated and aged
Standard commercial bar/forging condition for disks, rings and high-temperature fasteners; best balance of strength and ductility.8601,3101638 HRC—
Full triple heat treatment
Turbine-blade / long-life creep condition: extra stabilising step maximises rupture life above 750 °C at some loss of RT ductility.9001,3501340 HRC1.4 % IACS

What is Alloy 684-ST?

Alloy 684-ST is Alloy 684 heat treated to ST — softest supplied state — use when heavy machining, hot/cold forming or fabrication must precede final ageing. Alloy 684-ST has a yield strength of 585 MPa (84.8 ksi) and a tensile strength of 965 MPa (140 ksi) — stronger than 81% of nickel alloy grades. Elongation at break is 35% and the elastic modulus is 213 GPa (30.9 Msi). Alloy 684-ST has a density of 8.02 g/cm³ (0.29 lb/in³), lighter than 84% of nickel alloy grades. It melts at 1,300°C (2,372 °F). STA is the default condition FabDigit quotes; ST is available on request or by drawing note.

Advantages

  • High strength — 585 MPa (84.8 ksi), better than 81% of nickel alloy grades

Limitations

  • Difficult to weld — 32/100, worse than 77% of nickel alloy grades

Alloy 684-ST properties

Typical room-temperature values for Alloy 684-ST; 12 are specific to this condition. Other listed values are Alloy 684 reference data and may not represent this condition. Bars are the position among nickel alloy grades.

Physical3

Alloy 684-ST has a density of 8.02 g/cm³ (0.29 lb/in³), lighter than 84% of nickel alloy grades. It melts at 1,300°C (2,372 °F).

Density8.02 g/cm³0.29 lb/in³
Melting Point (Solidus)1,300°C2,372 °F
Liquidus Temperature1,395°C2,543 °F

Mechanical16

Alloy 684-ST has a yield strength of 585 MPa (84.8 ksi) and a tensile strength of 965 MPa (140 ksi) — stronger than 81% of nickel alloy grades. Elongation at break is 35% and the elastic modulus is 213 GPa (30.9 Msi).

Elastic (Young's) Modulus213 GPa30.9 Msi
Shear Modulus82 GPa11.9 Msi
Bulk Modulus178 GPa25.8 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)965 MPa140 ksi
Yield Strength (0.2% offset)585 MPa84.8 ksi
Elongation at Break35%
Reduction in Area40%
Compressive Strength900 MPa131 ksi
Shear Strength800 MPa116 ksi
Fatigue Strength (Endurance Limit)350 MPa50.8 ksi
Fracture Toughness (K_IC)90 MPa·√m81.9 ksi·√in
Charpy V-Notch Impact (RT)55 J40.6 ft·lbf
Hardness, Brinell255 HB
Hardness, Rockwell C26 HRC
Hardness, Vickers375 HV

Thermal6

Alloy 684-ST is rated for continuous service to 700°C (1,292 °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 12.1 µm/m·K (6.72 µin/in·°F).

Thermal Conductivity11 W/m·K6.4 BTU/hr·ft·°F
Specific Heat Capacity420 J/kg·K0.1 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)12.1 µm/m·K6.7 µin/in·°F
Latent Heat of Fusion290 J/g125 BTU/lb
Max Service Temperature (continuous)700°C1,292 °F
Min Service Temperature-196°C-321 °F

Electrical3

Alloy 684-ST 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 (paramagnetic austenitic γ matrix; µr ≈ 1.00–1.02)

Chemical & Environmental3

Corrosion resistance is very good (72/100), worse than 71% of nickel alloy grades.

Galvanic Potential (seawater, vs SCE)-0.15 V
Corrosion ResistanceVery good72/100
Chemical Resistance SummaryExcellent high-temperature oxidation and hot-gas corrosion resistance from Cr₂O₃/Al₂O₃ scales; good resistance to neutral salts and mildly oxidising acids, but attacked by hot reducing acids (HCl, H₂SO₄) and by sulfidising or molten-salt environments above ~800 °C.

Sustainability4

Producing a kilogram of Alloy 684-ST takes about 165 MJ of energy and emits 14 kg of CO₂ — more than 54% of nickel alloy grades. Typical recycled content is 35%.

Embodied Energy (primary production)165 MJ/kg70,937 BTU/lb
Embodied Carbon (primary production)14 kg CO₂/kg
Embodied Water1,500 L/kg180 gal/lb
Typical Recycled Content35%

Manufacturability8

Alloy 684-ST's machinability is poor (18/100, worse than 61% of nickel alloy grades); weldability poor (32/100); formability fair (40/100).

MachinabilityPoor18/100
Machinability Rating (AISI 1212 = 100 %)8%
WeldabilityPoor32/100
Formability (cold)Fair40/100
CastabilityGood55/100
Brazeability / SolderabilityFair40/100
PolishabilityVery good70/100
Anodizing Responsen/a — nickel alloy; surface engineering is by grit blast + aluminide/MCrAlY coating, shot peening or electroplating rather than anodising.

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

Working with Alloy 684-ST

Is Alloy 684 easy to machine?

Machine solution-treated where possible; rigid setups, positive-rake carbide or ceramic tools, 8–20 m/min for carbide, heavy flood coolant, constant feed to avoid work-hardened glaze.

Can Alloy 684 be welded?

Weld only in the solution-treated state with matched or Waspaloy/Alloy 625 filler, low heat input and immediate post-weld solution + age; high Al+Ti makes strain-age cracking a real risk.

Can Alloy 684 be formed, bent or molded?

Hot work between about 1090 and 1150 °C with reheats; cold forming is limited to gentle bends in the solution-treated condition due to very high work-hardening rate.

What surface finishes work on Alloy 684?

Grind/belt with SiC or ceramic abrasives and shot peen loaded surfaces; protect hot-gas parts by aluminide or MCrAlY coating — no anodising applies.

Alloy 684 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
Croxidation resistance17 – 2018.5
Co15 – 2018
Mosolid-solution strengthening3.5 – 54
Tiγ′ former2.5 – 3.252.9
Alγ′ former2.5 – 3.252.9
C0.05 – 0.120.08
Bgrain-boundary ductility0 – 0.010.01
Zr≤ 0.10.05
Feresidual≤ 41
Mn≤ 0.750.1
Si≤ 0.750.15
S≤ 0.02—
Nibalance, typically 50–55 %balance—

Alloy 684-ST — frequently asked

What is Alloy 684-ST used for?

Alloy 684-ST is typically used for gas turbine fasteners and studs, high-temperature bolting, turbine disks and rotor hardware, hot-section blade retention parts, heat-treated cast turbine components and high-temperature spring and washer stacks. In short: turbine-disk strength class; 870 °C service limit; very difficult to weld.

What is the yield strength of Alloy 684-ST?

Alloy 684-ST has a typical yield strength of 585 MPa (84.8 ksi) and a tensile strength of 965 MPa (140 ksi) — stronger than 81% of nickel alloy grades. Strength varies by condition: see the 5 listed tempers.

Is Alloy 684-ST easy to machine?

Not especially — machinability is rated poor (18/100, worse than 61% of nickel alloy grades). Machine solution-treated where possible; rigid setups, positive-rake carbide or ceramic tools, 8–20 m/min for carbide, heavy flood coolant, constant feed to avoid work-hardened glaze.

Can Alloy 684-ST be welded?

Not readily — weldability is rated poor (32/100). Weld only in the solution-treated state with matched or Waspaloy/Alloy 625 filler, low heat input and immediate post-weld solution + age; high Al+Ti makes strain-age cracking a real risk.

What surface finishes work on Alloy 684-ST?

Grind/belt with SiC or ceramic abrasives and shot peen loaded surfaces; protect hot-gas parts by aluminide or MCrAlY coating — no anodising applies.

Can Alloy 684-ST be formed, bent or molded?

Hot work between about 1090 and 1150 °C with reheats; cold forming is limited to gentle bends in the solution-treated condition due to very high work-hardening rate.

What is the maximum service temperature of Alloy 684-ST?

Alloy 684-ST 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 Alloy 684-STA and Alloy 684-ST?

STA is the default condition — standard commercial bar/forging condition for disks, rings and high-temperature fasteners; best balance of strength and ductility. ST: softest supplied state — use when heavy machining, hot/cold forming or fabrication must precede final ageing. Yield strength is 860 MPa in STA versus 585 MPa in ST.

Sources

  1. ASM Handbook Vol.1 — Properties and Selection: Irons, Steels and High-Performance Alloys — ASM International (1990)
  2. ASM Superalloys: A Technical Guide, 2nd ed. — ASM International (2002)
  3. AMS 5751 / UNS N07500 nickel alloy bar and forging specifications — SAE International (2018)
  4. DIN EN 10302 / W.-Nr. 2.4983 creep-resisting alloys — DIN/CEN (2008)
  5. ASM Handbook Vol.13B — Corrosion: Materials — 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.