Alloy ХН62БМКТЮ (ЭП742)
	
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	Alloy KhN53KVMTYUB (EP741P)
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	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 |