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GH3536
GH3536 alloy has good oxidation resistance and corrosion resistance, moderate endurance and creep strength below 900 ℃, and good cold and hot working formability and weldability. It is suitable for manufacturing combustion chamber components and other high-temperature components of aero-engines. It can be used for a long time below 900 ℃, and its short-term working temperature can reach 1080 ℃. Alloys that can bear certain stress and have oxidation or corrosion resistance at 600~1200 ℃. According to the matrix elements, it can be divided into iron-based superalloy, nickel-based superalloy and cobalt-based superalloy; According to the preparation process, it can be divided into deformed superalloy, cast superalloy and powder metallurgy superalloy. According to the strengthening methods, there are solid solution strengthening, precipitation strengthening, oxide dispersion strengthening and fiber strengthening (see metal strengthening). High temperature alloys are mainly used to manufacture high temperature components such as turbine blades, guide vanes, turbine discs, high pressure compressor discs and combustion chambers of aviation, naval and industrial gas turbines; It can also be used to manufacture energy conversion devices such as aerospace vehicles, rocket engines, nuclear reactors, petrochemical equipment and coal conversion.
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product details
|
Brand |
GH3536 |
|
Similar brands |
HastelloyX NiCr22FeMo UNS NO6002 |
|
Technicalstandard |
GJB 1952-1994 《Specification for cold rolled superalloy sheets for aircraft》 GJB 3020-1997 《Specification for superalloy ring blanks for aviation》 HB 5496-1992 《GH536 alloy round cake、Ring blank and ring part》 Q/CB 61-1996 《GH536 alloy cold-worked welded steel pipe for aviation》 |
| Classification |
Special alloy steel |
|
Performance |
Corrosion resistance |
|
Label |
Nickel-base superalloy Iron-based superalloy Cobalt-based superalloy |
|
Explain |
GH3536 alloy has good oxidation resistance and corrosion resistance, moderate endurance and creep strength below 900 ℃, and good cold and hot working formability and weldability. It is suitable for manufacturing combustion chamber components and other high-temperature components of aero-engines. It can be used for a long time below 900 ℃, and its short-term working temperature can reach 1080 ℃. Alloys that can bear certain stress and have oxidation or corrosion resistance at 600~1200 ℃. According to the matrix elements, it can be divided into iron-based superalloy, nickel-based superalloy and cobalt-based superalloy; According to the preparation process, it can be divided into deformed superalloy, cast superalloy and powder metallurgy superalloy. According to the strengthening methods, there are solid solution strengthening, precipitation strengthening, oxide dispersion strengthening and fiber strengthening (see metal strengthening). High temperature alloys are mainly used to manufacture high temperature components such as turbine blades, guide vanes, turbine discs, high pressure compressor discs and combustion chambers of aviation, naval and industrial gas turbines; It can also be used to manufacture energy conversion devices such as aerospace vehicles, rocket engines, nuclear reactors, petrochemical equipment and coal conversion. |
|
Density |
8.28g/cm3 |
Chemical composition:%
| Element |
NI |
Fe |
C |
Si |
Mn |
P |
S |
Cr |
Cu |
Mo |
Ti |
W |
B |
Co |
Al |
|
Min. |
Allowance |
17 |
0.05 |
- |
- |
- |
- |
20.5 |
- |
8 |
0.15 |
0.2 |
- |
0.5 |
- |
|
Max. |
20 |
0.15 |
1 |
1 |
0.025 |
0.015 |
23 |
0.5 |
10 |
- |
1 |
0.01 |
2.5 |
0.5 |
Note: The above information is for reference only. Some elements in different standards and specifications may be different.
*B. Ce is added according to the calculated amount.
The information of the above materials is rough description, and any deviation may be used for reference only
*Note: Please fill in the information accurately and keep the communication unblocked. We will contact you as soon as possible
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