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GH3600
GH3600 is a Ni-Cr-Fe based solid solution strengthened deformed superalloy, which has good thermal strength and high plasticity below 800 ℃, and good high-temperature corrosion resistance and oxidation resistance below 1000 ℃. The alloy has stable structure after long-term use, and has excellent cold and hot processing, welding properties and low temperature mechanical properties. The alloy can be strengthened by cold working and can be connected by resistance welding, fusion welding or brazing. It is suitable for making engine combustion chamber working under 700 ℃~800 ℃ and anti-oxidation parts bearing low load under 1100 ℃. GH3600 alloy is a kind of anti-oxidation nickel-based superalloy suitable for bearing low load below 1100 ℃, while GH3600 alloy tubes for aerospace are mainly used for the hydrogen and oxygen rocket engine of the upper stage power unit of the launch vehicle; Scope of application: evaporation tank in petrochemical industry, machinery for acid and alkali industry, catalytic regenerator; Nuclear reactor power generation equipment and heat exchanger; Jet engine parts, afterburning parts of turbojet engines; And other parts used under high temperature;
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product details
|
Brand |
GH3600 |
|
Similar brands |
H30300 GH30 |
|
Technicalstandard |
GB/T 14994-2008 《Cold drawn superalloy bars》 GJB 2297-1995 《Specification for cold drawn (rolled) seamless superalloy tubes for aircraft》 GJB 2611-1996 《Specification for cold drawn superalloy bars for aircraft》 GJB 3020-1997《Specification for superalloy ring blanks for aviation》 GJB 3317-1998 《Specification for hot-rolled superalloy plates for aircraft》 GJB 3165-1998 《Specification for hot-rolled and forged superalloy bars for aircraft load-bearing parts》 |
|
Classification |
Alloy steel |
|
Performance |
Corrosion resistance High temperature strength |
|
Label |
Solution strengthened nickel base superalloy |
|
Explain |
GH3600 is a Ni-Cr-Fe based solid solution strengthened deformed superalloy, which has good thermal strength and high plasticity below 800 ℃, and good high-temperature corrosion resistance and oxidation resistance below 1000 ℃. The alloy has stable structure after long-term use, and has excellent cold and hot processing, welding properties and low temperature mechanical properties. The alloy can be strengthened by cold working and can be connected by resistance welding, fusion welding or brazing. It is suitable for making engine combustion chamber working under 700 ℃~800 ℃ and anti-oxidation parts bearing low load under 1100 ℃. GH3600 alloy is a kind of anti-oxidation nickel-based superalloy suitable for bearing low load below 1100 ℃, while GH3600 alloy tubes for aerospace are mainly used for the hydrogen and oxygen rocket engine of the upper stage power unit of the launch vehicle; Scope of application: evaporation tank in petrochemical industry, machinery for acid and alkali industry, catalytic regenerator; Nuclear reactor power generation equipment and heat exchanger; Jet engine parts, afterburning parts of turbojet engines; And other components used under high temperature;. |
|
Density |
8.4g/cm3 |
Chemical composition:%
| Element |
Fe |
C |
Si |
Mn |
P |
S |
Cr |
Ni |
Ti |
Nb |
Al |
|
Min. |
6 |
- |
- |
- |
- |
- |
14 |
72 |
- |
- |
- |
|
Max. |
10 |
0.15 |
0.5 |
1 |
0.04 |
0.015 |
17 |
- |
0.5 |
1 |
0.35 |
Note: The above information is for reference only. Some elements in different standards and specifications may be different.
The information of the above materials is rough description, and any deviation may be used for reference only
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