Alloy KHN70VMTJU (ЭИ617)
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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)
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Alloy KhN67MBYu (EP782)
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Alloy BC4L
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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 | ХН70ВМТЮ |
Designation GOST Latin | XH70BMTJu |
Transliteration | HN70VMTYu |
The chemical elements | CrNi70ВCuTeAl |
Name | The value |
---|---|
Designation GOST Cyrillic | ЭИ617 |
Designation GOST Latin | EI617 |
Transliteration | EhI617 |
The chemical elements | - |
Description
Alloy KHN70VMTJU used: for the manufacture of hot-rolled bars; working and nozzle blades of gas turbines.
Note
High-temperature Nickel-based alloy.
The recommended maximum operating temperature for a long time +850 °C.
The temperature of beginning of intensive scaling in air to +1000 °C.
Standards
Name | Code | Standards |
---|---|---|
Sectional and shaped rolling | В32 | GOST 23705-79, TU 14-1-1477-75, TU 14-1-223-72, TU 14-1-402-72, TU 14-1-5-2-73, 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 | Ce |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
TU 14-1-223-72 | 0.04-0.1 | ≤0.01 | ≤0.015 | ≤0.5 | 13-16 | ≤0.6 | The rest | ≤5 | ≤0.07 | 1.7-2.3 | 0.1-0.5 | ≤0.02 | 1.8-2.3 | 2-4 | 5-7 | ≤0.02 |
TU 14-1-402-72 | ≤0.12 | ≤0.01 | ≤0.015 | ≤0.5 | 13-16 | ≤0.6 | The rest | ≤5 | ≤0.07 | 1.7-2.3 | 0.1-0.5 | ≤0.02 | 1.8-2.3 | 2-4 | 5-7 | ≤0.02 |
GOST 5632-72 | ≤0.12 | ≤0.01 | ≤0.015 | ≤0.5 | 13-16 | ≤0.6 | The rest | ≤5 | ≤0.3 | 1.7-2.3 | 0.1-0.5 | ≤0.02 | 1.8-2.3 | 2-4 | 5-7 | ≤0.02 |
Ni is the basis.
According to TU 14-1-223-72 in the alloy, the presence of antimony, tin, bismuth and arsenic is allowed for no more than 1 point of the spectral analysis scale. Boron and cerium are introduced into the metal by calculation and chemical analysis is not determined.
According to TU 14-1-223-72 in the alloy, the presence of antimony, tin, bismuth and arsenic is allowed for no more than 1 point of the spectral analysis scale. Boron and cerium are introduced into the metal by calculation and chemical analysis is not determined.
Mechanical characteristics
Section, mm | σB, MPa | d5, % | y, % | Brinell hardness number, MPa |
---|---|---|---|---|
Bars hot rolled and forged and according to GOST 23705-79, THE 14-1-223-72. Hardening in air, 1180-1200 °C (exposure 2 hours) + Heating to 1040-1060 (exposure 4 h), air cooling + Ageing at 790-810 °C (aging 16 h), air cooling | ||||
- | - | - | 299-341 | |
≥670 | ≥3 | ≥8 | - | |
≥690 | ≥7 | ≥10 | - | |
- | - | - | 299-341 |
Description mechanical marks
Name | Description |
---|---|
Section | Section |
σB | Limit short-term strength |
d5 | Elongation after rupture |
y | The relative narrowing |
Technological properties
Name | The value |
---|---|
Weldability | Trudnosmyvaemye. |