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GH3625
GH3625 (GH625) alloy is a solid solution strengthened nickel-based deformation superalloy with molybdenum and niobium as the main strengthening element. It has excellent corrosion resistance and oxidation resistance. It has good tensile and fatigue properties from low temperature to 980 ℃, and is resistant to stress corrosion in salt spray atmosphere. Therefore, it can be widely used in manufacturing aviation engine parts, aerospace structural parts, petrochemical equipment and other fields. GH3625 production execution standard: This standard is applicable to deformed superalloys, cast superalloys (equiaxed cast superalloys, directionally solidified columnar superalloys and single crystal superalloys), high-temperature alloy wires for welding, powder metallurgy superalloys, dispersion strengthened superalloys and intermetallic compound high-temperature materials.
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product details
|
Brand |
GH3625 |
|
Similar brands |
UNS/NO6625/ Inconel625(U.S.A)、NC22DNb(France)、W.Nr. 2.4856(Germany) |
|
Technicalstandard |
GJB 1953-1994 《Specification for hot-rolled superalloy bars for aircraft engine rotating parts》 GJB 2611-1996 《Specification for cold drawn superalloy bars for aircraft》 GJB 2612-1996 《Specification for cold drawn superalloy wire for welding》 GJB 3020-1997 《Specification for superalloy ring blanks for aviation》 GJB 3165-1998 《Specification for hot-rolled and forged superalloy bars for aircraft load-bearing parts》 GJB 3782-1999 《Specification for superalloy bars for aircraft》 HB 5198-1982 《Deformed superalloy bars for aircraft blades》 |
|
Classification |
Deformed superalloy bars for aircraft blades |
|
Performance |
Corrosion resistance Fatigue resistance |
|
Label |
Solution strengthened nickel-base wrought superalloy |
|
Explain |
GH3625 (GH625) alloy is a solid solution strengthened nickel-based deformation superalloy with molybdenum and niobium as the main strengthening element. It has excellent corrosion resistance and oxidation resistance. It has good tensile and fatigue properties from low temperature to 980 ℃, and is resistant to stress corrosion in salt spray atmosphere. Therefore, it can be widely used in manufacturing aviation engine parts, aerospace structural parts, petrochemical equipment and other fields. GH3625 production execution standard: This standard is applicable to deformed superalloys, cast superalloys (equiaxed cast superalloys, directionally solidified columnar superalloys and single crystal superalloys), high-temperature alloy wires for welding, powder metallurgy superalloys, dispersion strengthened superalloys and intermetallic compound high-temperature materials. |
|
Density |
8.4g/cm3 |
Chemical composition:%
| Element |
Ni |
Fe |
C |
Si |
Mn |
P |
S |
Cr |
Cu |
Mo |
Ti |
Nb |
Co |
Al |
|
Min. |
Allowance |
- |
- |
- |
- |
- |
- |
20 |
- |
8 |
- |
3.15 |
- |
- |
|
Max. |
5 |
0.1 |
0.5 |
0.5 |
0.015 |
0.015 |
23 |
0.07 |
10 |
0.4 |
4.15 |
1 |
0.4 |
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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