High Temperature Components Forging Alloy 718 Round Bar
High Temperature Components Forging Alloy 718 Round Bar
Inconel 718 Round Bar Feature
1. According to the preparation process can be divided into deformation superalloys, casting superalloys and powder metallurgy superalloys.
2. According to the strengthening mode, there are solid solution strengthening type, precipitation strengthening type, oxide dispersion strengthening type and fiber strengthening type, etc.
Inconel 718 Round Bar Application:
High temperature components, such as turbine blades, guide vanes, turbine disks, high pressure
compressor disks,machine manufacturing and combustion chambers used in the manufacture of aviation, naval and industrial gas turbines.
Inconel 718 Round Bar Parameters
| Item | Size |
| Plate/Sheet | 0.5~60.0mm (THK)*2000mm(WIDTH)*6000mm(LENGTH) |
| Bar (Round) | Φ5.5~250mm |
| Bar (Square) | 40~240mm*40~240mm |
| Strip | 0.05~3.0mm (THK)*≤420mm(WIDTH) |
| Seamless Pipe | 0.2mm~508mm (OD)*0.5mm~18mm(WT) |
| Welded Tube | 0.5mm~120mm (OD)*0.05mm~10mm(WT) |
| Wire | Φ0.1mm~18mm |
|
ement
|
Content
|
|
Ni+Co
|
50 - 55 %
|
|
Cr
|
17 - 21 %
|
|
Fe
|
BAL
|
|
Nb+Ta
|
4.75 - 5.5 %
|
|
Mo
|
2.8 - 3.3 %
|
|
Ti
|
0.65 - 1.15 %
|
|
Al
|
0.2 - 0.8 %
|
|
operty
|
Metric
|
Imperial
|
|
Density
|
8.19 g/cm3
|
0.296 lb/in3
|
|
Melting point
|
1336 °C
|
2437 °F
|
|
Co-Efficient of Expansion
|
13.0 µm/m.°C
(20-100 °C) |
7.2x10-6 in/in.°F
(70-212 °F) |
|
Modulus of rigidity
|
77.2 kN/mm2
|
11197 ksi
|
|
Modulus of elasticity
|
204.9 kN/mm2
|
29719 ksi
|
2. Professional loading team avoid package damage.
3. Goods label with traceable batch number and shipping information.
4. Different production lines for different products makes various size and type available.
5. Varous sizes and materials stock make fast lead time.
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