Alloy ХН55ВМТФКЮ (ЭИ929)

Designation

Name The value
Designation GOST Cyrillic ХН55ВМТФКЮ
Designation GOST Latin XH55BMTFKJu
Transliteration HN55VMTFKYu
By chemical elements CrNi55ВCuTePCoAl
Name The value
Designation GOST Cyrillic ЭИ929
Designation GOST Latin EI929
Transliteration EhI929
By chemical elements -

Description

Alloy ХН55ВМТФКЮ used: for the production of hot-rolled bars; various components of aircraft and power engineering.

Standards

Name Code Standards
Bars and shapes В32 TU 14-1-223-72, TU 14-1-402-72

Chemical composition

Standard C S P Mn Cr Si Ni Fe Cu Al V B Ti Mo W Co
TU 14-1-402-72 ≤0.12 ≤0.01 ≤0.015 ≤0.5 9-12 ≤0.5 Rest ≤5 ≤0.07 3.6-4.5 0.2-0.8 ≤0.02 1.4-2 4-6 4.5-6.5 12-16
TU 14-1-223-72 0.04-0.1 ≤0.01 ≤0.015 ≤0.5 9-12 ≤0.5 Rest ≤5 ≤0.07 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.
According to TU 14-1-223-72 in the alloy, the introduction of cerium is possible up to 0.020%; the presence of antimony, tin, bismuth and arsenic is not allowed for 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. At the consumer's request, the bars are supplied with a carbon content in the range of 0.08-0.12% and in this case the alloy is marked EI929A.

Mechanical properties

Section, mm σU, MPa d5, % y, % HB, MPa
Bars and rods, hot-rolled (20-55 mm) and machined (20-40 mm) TU 14-1-223-72. Annealing in air 1210-1230 °C (exposure 2 hours) + Heating to 1040-1060 °C (exposure 4 h), air cooling + Ageing at 840-860 °C (exposure 8 h), air cooling
≥570 ≥8 ≥12 285-341

Description mechanical marks

Name Description
σU Limit short-term strength
d5 Elongation after rupture
y The relative narrowing
HB Brinell hardness number