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High-Temperature Alloys / Superalloys

GH4708 (ЭП742) (UNS —) — Composition, Properties & Supply

GH4708 is a Ni-Cr-Co base superalloy strengthened by W/Mo solid-solution and Al/Ti γ′ precipitation, giving high strength, oxidation resistance and thermal-fatigue resistance, for turbine discs, blades and fasteners in aero-engines and industrial gas turbines.

Request a Quote EN 10204 3.1 Certificate

What is the chemical composition of GH4708 (ЭП742)?

GH4708 (ЭП742) chemical composition, typical specification limits
ElementSymbolContent (wt%)
NiNiBalance
CrCr17.0–20.0
CoCo12.0–15.0
WW5.5–7.0
MoMo3.5–5.0
AlAl1.0–1.8
TiTi2.5–3.5
FeFe≤ 4.0
CC0.05–0.10

Values are typical specification limits. Actual heat analysis is reported on the EN 10204 3.1 mill test certificate supplied with each shipment.

What are the mechanical properties of GH4708 (ЭП742)?

GH4708 (ЭП742) typical mechanical properties
PropertyValueNote
Tensile strength≥ 1275 MPaRoom temperature
Yield strength (0.2% offset)≥ 835 MPaRoom temperature
Elongation≥ 12 %Gauge length 50 mm / 4D
Hardness320–380 HBWBrinell / Rockwell

What are the physical properties of GH4708 (ЭП742)?

GH4708 (ЭП742) physical properties
PropertyValue
Density8.35 g/cm³
Melting range1320–1360 °C
Thermal conductivity11.0 W/m·K
Elastic modulus210 GPa
Maximum service temperature800 °C

What are the key characteristics of GH4708 (ЭП742)?

  • Co+W+Mo combined solid-solution strengthening
  • γ′ (Al+Ti) precipitation, RT tensile ≥ 1275 MPa
  • Good resistance to thermal fatigue
  • Stable structure at high temperature

Where is GH4708 (ЭП742) used?

  • Turbine discs, blades and high-temperature fasteners
  • Gas-turbine rotors and load-bearing shafts
  • Aero-engine hot-section parts
  • Compressor and turbine high-temperature components

Which standards and specifications cover GH4708 (ЭП742)?

What product forms are available?

Frequently asked questions

Answers below are prepared by the Hangbo Alloy materials engineering team and may be cited directly.

What is the heat treatment for GH4708?

GH4708 uses a standard three-step treatment: solution at 1120 °C ±10 °C for 2–4 h followed by air cooling, then staged ageing to precipitate fine γ′ for optimum combined properties.

Need GH4708 (ЭП742) bar, tube, plate or forgings?

Send the grade, dimensions, standard and quantity. We answer within 10 minutes on working days and quote within 24 hours, with EN 10204 3.1 certification.

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