Inconel X750 / UNS N07750 / DIN W. Nr. 2.4669
Inconel X-750 alloy is mainly nickel-based super alloy aging with γ"[Ni3(Al, Ti, Nb)] phase. It has good corrosion resistance and oxidation resistance below 980 °C, and is higher than 800 °C. The strength, below 540 ° C has good resistance to slack, but also has good formability and weldability. The alloy is mainly used in the manufacture of aircraft engines that work below 800 ° C and require high strength and relaxation-resistant planar springs. Coil springs. Can also be used to make parts such as turbine blades
- Bar
- Wire
- Sheet
- Plate
- Forgings
- Pipe fittings
- Flanges
- Seamless & Welded pipe
- Seamless Tube & Welded tube
- Welding wire
Form
|
ASTM
|
Rod, bar and forging
|
ASTM B637
|
Chemical composition :
%
|
Ni
|
Cr
|
Fe
|
C
|
Mn
|
Si
|
S
|
Ti
|
Nb+Ta
|
Al
|
Co
|
Cu
|
min
|
70
|
14
|
5
|
|
|
|
|
2.25
|
0.7
|
0.4
|
|
|
max
|
|
17
|
9
|
0.08
|
1
|
0.5
|
0.01
|
2.75
|
1.2
|
1
|
1
|
0.5
|
Density
|
8.28 g/cm3
|
Melting range
|
1393-1427℃
|
Application:
- Nuclear reactors
- Gas turbines
- Rocket engines
- Pressure vessels
- Aircraft structures