Alloy ХН62БМКТЮ (ЭП742)
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Alloy KhN70MVTYUB (EI598)
Alloy KhN70VMYUT (EI765)
Alloy CrN70VMFTU (EI826)
Alloy CrN70VMTUF (EI826; CrN70VMTUF)
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Alloy ZhS16
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Alloy BC4L
Alloy VZHL2
Alloy VZhL18
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Alloy VZHL14H (VZHL14)
Alloy ZhS6U
Alloy VZHL12U
Alloy VZhL1
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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 | ХН62БМКТЮ |
Designation GOST Latin | XH62BMKTJu |
Transliteration | HN62BMKTYu |
The chemical elements | CrNi62BeCuCoTeAl |
Name | The value |
---|---|
Designation GOST Cyrillic | ЭП742 |
Designation GOST Latin | EP742 |
Transliteration | EhP742 |
The chemical elements | - |
Description
Alloy ХН62БМКТЮ used: for the production of disks of gas turbine engines ground-based (gas compressor units, gas turbine driven power plants).
Standards
Name | Code | Standards |
---|---|---|
Bulls. Blanks. Slabs | В31 | OST 1 90367-85, TU 14-1-3998-85 |
Metal forming. Forgings | В03 | TU 14-1-2617-79 |
Chemical composition
Standard | C | S | P | Mn | Cr | Si | Ni | Fe | Al | B | Ti | Mo | Nb | Ce | Co | La |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
TU 14-1-3998-85 | 0.04-0.08 | ≤0.01 | ≤0.015 | ≤0.4 | 13-15 | ≤0.3 | The rest | ≤1 | 2.4-2.8 | ≤0.01 | 2.4-2.8 | 4.5-5.5 | 2.4-2.8 | ≤0.01 | 9-11 | ≤0.1 |
Ni is the basis.
According to TU 14-1-3998-85, the chemical composition is presented for the alloy ХН62БМКТЮ-ИД (ЭП742-ИД) of vacuum-arc remelting with smelting of the parent metal in a vacuum induction furnace. In the finished metal, deviations of the chemical composition are permissible: in titanium ± 0.10%, in aluminum ± 0.10%, in niobium ± 0.10%, in carbon -0.020%, in sulfur +0.0010%, in boron +0 , 0050%. Lanthanum, boron and cerium are introduced into the metal by calculation and chemical analysis are not determined. The content of residual elements of vanadium and tungsten is not more than 0.20% of each, the residual content of copper is not more than 0.070%.
According to TU 14-1-3998-85, the chemical composition is presented for the alloy ХН62БМКТЮ-ИД (ЭП742-ИД) of vacuum-arc remelting with smelting of the parent metal in a vacuum induction furnace. In the finished metal, deviations of the chemical composition are permissible: in titanium ± 0.10%, in aluminum ± 0.10%, in niobium ± 0.10%, in carbon -0.020%, in sulfur +0.0010%, in boron +0 , 0050%. Lanthanum, boron and cerium are introduced into the metal by calculation and chemical analysis are not determined. The content of residual elements of vanadium and tungsten is not more than 0.20% of each, the residual content of copper is not more than 0.070%.
Mechanical characteristics
Section, mm | sT|s0,2, MPa | σB, MPa | d5, % | y, % | kJ/m2, кДж/м2 | Brinell hardness number, MPa |
---|---|---|---|---|---|---|
Forgings (washers) on the other 14-1-3998-85. Hardening in air, 1060-1100 °C (exposure 8 h) + Aging at 770-790 °C (aging 16 h), air cooling (samples tangential) | ||||||
≥755 | ≥1210 | ≥13 | ≥14 | ≥294 | 302-376 | |
Forgings (washers) on the other 14-1-3998-85. Annealing in air 1090-1120 °C (exposure 8 h) + Aging at 840-860 °C (exposure 6 h), air cooling + Ageing at 770-790 °C (aging 10-16 h), air cooling (samples tangential) | ||||||
≥755 | ≥1210 | ≥13 | ≥14 | ≥294 | 302-376 |
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 |
kJ/m2 | Toughness |