Alloy ХН60КВЮМБ (ЭП957)

Designation

Name The value
Designation GOST Cyrillic ХН60КВЮМБ
Designation GOST Latin XH60KBJuMB
Transliteration HN60KVYuMB
By chemical elements CrNi60CoВAlCuBe
Name The value
Designation GOST Cyrillic ЭП957
Designation GOST Latin EP957
Transliteration EhP957
By chemical elements -

Description

Alloy ХН60КВЮМБ used: for the manufacture of stamped and forged parts, blades and fasteners ground high-temperature stationary gas turbines and aircraft turbines.

Standards

Name Code Standards
Processing of metals by pressure. Forgings В03 TU 108.01.60-86
Bars and shapes В32 TU 14-1-4827-90

Chemical composition

Standard C S P Mn Cr Si Ni Fe Al B Mo Nb W Ce Zr Co Y
TU 108.01.60-86 ≤0.05 ≤0.01 ≤0.02 ≤0.5 10.6-12 ≤0.4 Rest ≤1.5 5.2-6 ≤0.01 2.5-4.5 1-2 8.5-10.2 ≤0.02 ≤0.05 8.5-10.5 ≤0.05
TU 14-1-4827-90 ≤0.05 ≤0.01 ≤0.015 ≤0.5 10.6-12 ≤0.4 Rest ≤1.5 5.2-6 ≤0.01 2.5-4.5 1-2 8.5-10.2 ≤0.02 ≤0.05 8.5-10.5 ≤0.05
Ni is the basis.
According to TU 108.01.60-86 the chemical composition is given for the alloy KhN60KVYUMB-VD (EP957-VD).
According to TU 14-1-4827-90 the chemical composition is given for the alloy KhN60KVYUMB-VD (EP957-VD). It is possible to replace cerium with other elements from the REM group. Boron, cerium, zirconium, yttrium are introduced into the metal by calculation and chemical analysis are not determined. The residual copper content is not more than 0.070%.

Mechanical properties

sT|s0,2, MPa σU, MPa d5, % y, % KCU, kJ/m2 HB, MPa
Turbine blades in the state of delivery on the other 108.01.60-86 (samples)
≥882 ≥1177 ≥10 - ≥245 340-385
≥784 ≥833 ≥5 - - -
Bars-pressestelle with a diameter of 105 mm in the delivery state on the other 14-1-4827-90. Heating to 1170-1190 °C (extract 3 hours), cooling oven for 30-45 min. to 1030 °C, then air cooling to 840-860 °C (extract 15 h), air cooling (longitudinal samples)
≥885 ≥1180 ≥10 ≥10 ≥245 -
≥785 ≥830 ≥4 - - -

Description mechanical marks

Name Description
sT|s0,2 Yield strength or limit of proportionality with a tolerance for residual deformation of 0.2%
σU Limit short-term strength
d5 Elongation after rupture
y The relative narrowing
KCU Toughness
HB Brinell hardness number

Technological properties

Name The value
Weldability Hard welded alloy.