Alloy KHN55VMTKJU (ЭИ929)
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Alloy KhN65VMTU (EI893)
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Alloy KhN62VMKU (EI867)
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Alloy KhN70MVU (EI828)
Alloy KhN70MVTYUB (EI598)
Alloy KhN70VMYUT (EI765)
Alloy CrN70VMFTU (EI826)
Alloy CrN70VMTUF (EI826; CrN70VMTUF)
Alloy KhN70VMTU (EI617)
Alloy KhN70 (EI442)
Alloy KhN68VMTYUK (EP693)
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Alloy BC4L
Alloy VZHL2
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Alloy VZHL12U
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Alloy KhN52KVMTYUB (EP975P)
Alloy KhN56MBYUD (EK62)
Alloy KhN56VMTU (EP199; VZh101)
Alloy KhN56VMKU (EP109)
Alloy KhN55MVU (EP454)
Alloy KhN55MVTs (ChS57)
Alloy KhN55MBYu (KhN63M9B2u; EP666)
Alloy KhN55VMTFKU (EI929)
Alloy KhN55VMTKU (EI929)
Alloy KhN54KVMTYUB (EP962P)
Alloy KhN53KVMTYUB (EP741P)
Alloy KhN57VKYUTMBL (ZhS6)
Alloy KhN51MTYUKFR (EP220)
Alloy KhN51KVMTYUB (EP741NP)
Alloy KhN50KVMTYUB (BB750)
Alloy KhN50VMTYUB (EP648)
Alloy KhN50VMTKFY (EP57)
Alloy KhN45MVTYUBR (EP718)
Alloy Kh15N60Yu3A (EP548)
Alloy H95S3Yu (EP711)
Alloy H95G (EP18)
Alloy H70M (EP495)
Designation
Name | The value |
---|---|
Designation GOST Cyrillic | ХН55ВМТКЮ |
Designation GOST Latin | XH55BMTKJu |
Transliteration | HN55VMTKYu |
The chemical elements | CrNi55ВCuTeCoAl |
Name | The value |
---|---|
Designation GOST Cyrillic | ЭИ929 |
Designation GOST Latin | EI929 |
Transliteration | EhI929 |
The chemical elements | - |
Description
Alloy KHN55VMTKJU used: for the manufacture of turbine blades.
Note
High-temperature Nickel-based alloy.
The recommended maximum operating temperature for limited time +950 °C.
The temperature of beginning of intensive scaling in air +1050 °C.
Standards
Name | Code | Standards |
---|---|---|
Sectional and shaped rolling | В32 | GOST 23705-79, TU 14-1-2970-80, TU 14-11-245-88 |
Classification, nomenclature and general norms | В30 | GOST 5632-72 |
Bulls. Blanks. Slabs | В31 | OST 3-1686-90 |
Chemical composition
Standard | C | S | P | Mn | Cr | Si | Ni | Fe | Cu | Al | V | B | Ti | Mo | W | Co |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
GOST 5632-72 | 0.04-0.1 | ≤0.01 | ≤0.015 | ≤0.5 | 9-12 | ≤0.5 | The rest | ≤5 | ≤0.3 | 3.6-4.5 | 0.2-0.8 | ≤0.02 | 1.4-2 | 4-6 | 4.5-6.5 | 12-16 |
Ni is the basis.
Mechanical characteristics
Section, mm | sT|s0,2, MPa | σB, MPa | d5, % | y, % | Brinell hardness number, MPa |
---|---|---|---|---|---|
Bars hot rolled and forged and according to GOST 23705-79. Annealing in air 1210-1230 °C (exposure 2 hours) + Heating to 1040-1060 (exposure 4 h), air cooling + Ageing at 840-860 °C (exposure 8 h), air cooling | |||||
730-780 | 980-1180 | 8-12 | 9-15 | 285-341 | |
390-490 | 570-770 | 8-28 | 12-38 | - | |
- | 340-440 | 17-25 | 20-30 | - |
Description mechanical marks
Name | Description |
---|---|
Section | Section |
sT|s0,2 | Yield strength or limit of proportionality with a tolerance for residual deformation of 0.2% |
σB | Limit short-term strength |
d5 | Elongation after rupture |
y | The relative narrowing |