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GH2036
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product details
|
Brand |
GH2036 |
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Similar brands |
GH36 H20360 |
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Technicalstandard |
GB/T 14992-2005《Classification and designation of superalloy and intermetallic compound high-temperature materials》 GB/T 14994-2008《Cold drawn superalloy bars》 GJB 2611-1996 《Specification for cold drawn superalloy bars for aircraft》 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 aviation superalloy forged round cakes》 |
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Classification |
Special alloy steel |
| Label | Age-hardening iron-base superalloy |
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Explain |
GH2036 alloy is a precipitation hardening iron base superalloy strengthened by VC, with stable structure, good physical and mechanical properties at 600-650 ℃, and good machinability. In the superalloy series, the alloy is used at a low temperature, but it is widely produced and used, and has a wide range of applications. It is mainly used for turbine discs, bearing rings, fasteners and other high temperature components of aviation turbojet engines with a working temperature of 600-650 ℃. |
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Density |
7.85g/cm3 |
Chemical composition:%
| Element | Fe | C | Si | Mn | P | S | Cr | Ni | Mo | Ti | V | Nb |
| Z | Allowance | 0.34 | 0.3 | 7.5 | - | - | 11.5 | 7 | 1.1 | - | 1.25 | 0.25 |
| Max. | 0.4 | 0.8 | 9.5 | 0.035 | 0.03 | 13.5 | 9 | 1.4 | 0.12 | 1.55 | 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
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