2.4633 (NiCr25FeAlY)
Classification
Country |
Section |
Category |
Germany |
Alloy DIN 17007−4 |
Ni Alloys with Co, Cr and Mo Co Alloys with Cr, Ni and Mo |
Chemical composition
Standard |
Fe, % |
Si, % |
Mn, % |
Cr, % |
Ti, % |
Cu, % |
Ni, % |
Zr, % |
Al, % |
P, % |
C, % |
S, % |
Y, % |
EN 10302 |
8–11 |
< 0.5 |
< 0.5 |
24–26 |
0.1–0.2 |
< 0.1 |
58.8–65.89 |
0.01–0.1 |
1.8–2.4 |
< 0.02 |
0.15–0.25 |
< 0.01 |
0.05–0.12 |
Information on suppliers
Mechanical properties at 20 °C
Rolling |
Standard |
Size, mm |
Tension |
Classifiers |
$$\sigma _{U}$$, $$MPa$$ |
$$\sigma_{0.2}$$, $$MPa$$ |
$$\epsilon_L$$, % |
Treatment |
|
|
|
|
solution annealing |
680 |
270 |
30 |
|
Analogues
USA |
CIS, Russia, Ukraine |
N06025 |
NiCr25Fe10AlY |
Standards
Description of chemical elements
Element |
Units of measurement |
Description |
Fe |
% |
Iron |
Si |
% |
Silicon |
Mn |
% |
Manganese |
Cr |
% |
Chrome |
Ti |
% |
Titan |
Cu |
% |
Copper |
Ni |
% |
Nickel |
Zr |
% |
Zirconium |
Al |
% |
Aluminium |
P |
% |
Phosphorus |
C |
% |
Carbon |
S |
% |
Sulfur |
Y |
% |
Yttrium |
Description of mechanical properties
Parameter |
Units of measurement |
Description |
$$\sigma_{0.2}$$ |
$$MPa$$ |
Tensile stress required to produce a total elongation of 0.2% |
$$\sigma _{U}$$ |
$$MPa$$ |
Ultimate tensile strength |
$$\epsilon_L$$ |
% |
Elongation at break (longitudinal) |