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High-Temperature Alloys / Superalloys

GH4099 (ЭП693) (UNS —) — Composition, Properties & Supply

GH4099 is a Ni-Cr-Co-W-Mo precipitation-hardened nickel superalloy for long-term service at 900 °C and short-term at 1000 °C. Combining high-temperature strength with excellent oxidation resistance and weldability, it is the material of choice for aero-engine combustor and afterburner welded load-bearing sheet structures.

Request a Quote EN 10204 3.1 Certificate

What is the chemical composition of GH4099 (ЭП693)?

GH4099 (ЭП693) chemical composition, typical specification limits
ElementSymbolContent (wt%)
NiNiBalance
CrCr17.0–20.0
CoCo5.0–8.0
WW5.0–7.0
MoMo3.5–4.5
AlAl1.7–2.4
TiTi1.0–1.5
FeFe≤ 2.0
CC≤ 0.08

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 GH4099 (ЭП693)?

GH4099 (ЭП693) typical mechanical properties
PropertyValueNote
Tensile strength≥ 1100 MPaRoom temperature
Yield strength (0.2% offset)≥ 700 MPaRoom temperature
Elongation≥ 12 %Gauge length 50 mm / 4D
Hardness280–320 HBWBrinell / Rockwell

What are the physical properties of GH4099 (ЭП693)?

GH4099 (ЭП693) physical properties
PropertyValue
Density8.30 g/cm³
Melting range1330–1390 °C
Thermal conductivity21.8 W/m·K
Elastic modulus208 GPa
Maximum service temperature900 °C

What are the key characteristics of GH4099 (ЭП693)?

  • Oxidation resistant for long service at 900 °C
  • Large sheet structures usable directly after solution treatment without ageing
  • γ′ precipitation strengthening
  • Outstanding weldability

Where is GH4099 (ЭП693) used?

  • Aero-engine combustors and afterburners
  • High-temperature welded load-bearing sheet structures
  • Gas turbine hot components
  • Aero-engine heat-affected structures

Which standards and specifications cover GH4099 (ЭП693)?

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 GH4099?

Solution treatment at 1080–1140 °C (1140–1160 °C for sheet) followed by air cooling; to raise strength between 600–900 °C, age at 900 °C ±10 °C for 4 h and air cool. Large welded sheet assemblies can be used directly after solution treatment.

Need GH4099 (ЭП693) 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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