Alloy X750
2.4669 – N07750

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Material description

The material 2.4669 is a precipitation-hardenable nickel-chromium alloy. The material has excellent corrosion and oxidation resistance up to temperatures of approx. 980 °C. In addition, 2.4669 (Alloy X750) has a high strength up to approx. 700 °C.

After ageing, the material also exhibits high creep rupture strength and a low creep rate up to approx. 815 °C. The good ductility (even at low temperatures) rounds off the positive material properties.

AN OVERVIEW OF THE PROPERTIES OF 2.4669:

  • Excellent corrosion and oxidation resistance
  • High strength
  • High creep strength
  • Low creep rate
  • Good ductility

Applications

  • Aircraft engines
  • Heat treatment devices
  • Extrusion and moulding tools

Material data

Material no.: 2.4669
Name: Alloy X750
UNS no.: N07750
ASTM: B637
VdTÜV:
Other:
Material type: Superalloy

Chemical composition in %

ASTM B637
C, max.0,08
Mn, max.1,00
Si, max.0,50
S, max.0,01
Cr14,00 – 17,00
Co, max.1,00
Nb + Ta0,70 – 1,20
Ti2,25 – 2,75
Al0,40 – 1,00
Fe5,00 – 9,00
Cu, max.0,50
Ni, min.70,00

Mechanical properties

solution annealed
at 1149°C, stabilised
+ precipitation hardened
Bar | forging
Type 1
Rm (MPa)≥ 965
Rp 0,2 (MPa)≥ 620
A (%)≥ 8
Hardness (HB)≥ 262

Mechanical properties

solution annealed
at 982°C
+ precipitation hardened
Bar | forging
Type 2 / D < 63,5 mm
Bar | forging
Type 2 / 63,5 mm ≤ D ≤ 101,6 mm
Rm (MPa)≥ 1170≥ 1170
Rp 0,2 (MPa)≥ 790≥ 790
A (%)≥ 18≥ 15
Z (%)≥ 18≥ 15
Hardness (HB)302 – 363302 – 363

Mechanical properties

solution annealed
at 1100°C
+ precipitation hardened
Bar | forging
Type 3
Rm (MPa)1103 – 1276
Rp 0,2 (MPa)689 – 896
A (%)≥ 20
Z (%)≥ 20
Hardness (HB)267 – 363

The specified values are non-binding guide values.

Data sheet