Hastelloy, Monel, Inconel Alloy
The minimum of mechanical properties:
|
Alloy state |
Tensile strength Rm N/mm2 |
Yield strength R P 0.2 N/mm2 |
Extensibility A 5% |
Brinell hardness HB |
|
annealing treatment |
550 |
240 |
30 |
≤195 |
|
solid solution treatment |
500 |
180 |
35 |
≤185 |
Inconel 601
Inconel 601 Chemical composition:
|
Alloy |
% |
Ni |
Cr |
Fe |
C |
Mn |
Si |
Cu |
Al |
P |
S |
|
601 |
Min. |
58 |
21 |
|
|
|
|
|
1.0 |
|
|
|
Max. |
63 |
25 |
Balance |
0.1 |
1.5 |
0.5 |
1 |
1.7 |
0.02 |
0.015 |
The minimum of mechanical properties:
|
Alloy state |
Tensile strength Rm N/mm2 |
Yield strength R P 0.2 N/mm2 |
Extensibility A 5% |
Brinell hardness Hb |
|
annealing treatment |
650 |
300 |
30 |
- |
|
solid solution treatment |
600 |
240 |
30 |
≤220 |
Inconel 625
Chemical composition
|
Alloy |
% |
Ni |
Cr |
Mo |
Nb+N |
Fe |
Al |
Ti |
C |
Mn |
Si |
Cu |
P |
S |
|
625 |
Min. |
58 |
20 |
8 |
3.15 |
|
|
|
|
|
|
|
|
|
|
Max. |
|
23 |
10 |
4.15 |
5 |
0.4 |
0.4 |
0.1 |
0.5 |
0.5 |
0.5 |
0.015 |
0.015 |
Alloy minimum mechanical properties in the room temperature:
|
Alloy state |
Tensile strength Rm N/mm2 |
Yield strength R P 0.2 N/mm2 |
Elongation A 5% |
Brinell hardness HB |
|
625 |
760 |
345 |
30 |
≤22 |
Inconel 718
Chemical composition:
|
Alloy |
% |
Ni |
Cr |
Fe |
Mo |
Nb |
Co |
C |
Mn |
Si |
S |
Cu |
Al |
Ti |
|
718 |
Min. |
50 |
17 |
Balan ce |
2.8 |
4.75 |
|
|
|
|
|
|
0.2 |
0.7 |
|
Max. |
55 |
21 |
3.3 |
5.5 |
1 |
0.08 |
0.35 |
0.35 |
0.01 |
0.3 |
0.8 |
1.15 |
The minimum of mechanical properties:
|
Alloy state |
Tensile strength Rm N/mm2 |
Yield strength R P 0.2 N/mm2 |
Extensibility A 5% |
Brinell hardness HB |
|
solid solution treatment |
965 |
550 |
30 |
≤363 |
Ti, Ni, Zr Material
Pure Titanium and Titanium Alloy for Aerospace Application
|
|
Material |
N |
C |
H |
Fe |
O |
Residuals |
Al |
V |
|
|
Max |
Max |
Max |
Max |
Max |
Each Max |
Total Max |
||||
|
Pure Titanium |
TA1 |
0.03 |
0.10 |
0.015 |
0.25 |
0.20 |
0.1 |
0.4 |
|
|
|
TA2 |
0.05 |
0.10 |
0.015 |
0.30 |
0.25 |
0.1 |
0.4 |
|
|
|
|
Titanium Alloy |
TC4 |
0.03 |
0.10 |
0.015 |
0.25 |
0.20 |
0.1 |
0.4 |
5.5-6.75 |
3.5-4.5 |
|
Pure Titanium |
Gr1 |
0.03 |
0.08 |
0.015 |
0.20 |
0.18 |
|
|
|
|
|
Gr2 |
0.03 |
0.08 |
0.015 |
0.30 |
0.25 |
|
|
|
|
|
|
Titanium Alloy |
Gr5 |
0.05 |
0.08 |
0.015 |
0.40 |
0.20 |
|
|
5.5-6.75 |
3.5-4.5 |
Nickel Materials
|
|
Material |
N |
C |
Fe |
Si |
S |
Mn |
Cu |
Ni |
|
Pure Nickel |
UNS N02200 |
|
0.15 |
0.40 |
0.35 |
0.01 |
0.35 |
0.25 |
99.0 |
|
UNS N02201 |
|
0.02 |
0.40 |
0.35 |
0.01 |
0.35 |
0.25 |
99.0 |
Zirconium Materials
|
Material |
N |
C |
H |
Fe+Cr |
O |
Ha |
Zr |
Nb |
|
R60702 |
0.025 |
0.05 |
0.005 |
≤0.2 |
0.16 |
4.5 |
99.2 |
|
|
R60704 |
0.025 |
0.05 |
0.005 |
:0.2-0.4 |
0.18 |
4.5 |
97.5 |
|
|
R60705 |
0.025 |
0.05 |
0.005 |
≤0.2 |
0.18 |
4.5 |
95.5 |
2.0-3.0 |