By visiting this site, you accept the use of cookies. More about our cookie policy.

Alloy ХН55МБЮ (ХН63М9Б2Ю; ЭП666)

Alloy KhN66VMTYUB (EI698MP; VZH136) Alloy KhN67VMTU (EP202; KhN67MVTU) Alloy KhN65KMVYUB (EP800) Alloy CrN65VMYUTL (EI893L) Alloy KhN65VMTU (EI893) Alloy CrN65VMMBU (EP914; VZH131) Alloy CrN65VBMYu (EP902) Alloy KhN62MVKYu (EI867) Alloy KhN62VMYUT (EP708) Alloy KhN62VMKU (EI867) Alloy KhN62BMKTU (EP742) Alloy CrN62BMVY (EP709) Alloy KhN60MYUVT (EP539) Alloy KhN60MVTU (EP487) Alloy KhN60M (EP367; 06Kh15N60M1) Alloy KhN60KMYUVTB (EC9) Alloy CrN60KMYUBVTF (EP962) Alloy KhN60KVYUMB (EP957) Alloy KhN59VG (EK82) Alloy KhN58MBYUD (EK61) Alloy KhN58MBYu (EK171; VZH159) Alloy KhN58VMKYR (EP238) Alloy KhN57MTVU (EP590) Alloy KhN73MBTU (EI698) Alloy EP539LMU Alloy ChS70 Alloy ChS104 Alloy CNK7 Alloy KhN80TBY (EI607; KhN80T1BY (EI607A)) Alloy KhN80 (EI334) Alloy KhN77TURU (EI437BU) Alloy KhN77TUR (EI437B) Alloy KhN75TBU (EI869) Alloy KhN75VMU (EI827) Alloy CrN75VMFU (EI827) Alloy KhN57MKYUVTBR (EP958) Alloy KhN71MTYUB (EI698P) Alloy KhN70MVU (EI828) Alloy KhN70MVTYUB (EI598) Alloy KhN70VMYUT (EI765) Alloy CrN70VMFTU (EI826) Alloy CrN70VMTUF (EI826; CrN70VMTUF) Alloy KhN70VMTU (EI617) Alloy KhN70 (EI442) Alloy KhN68VMTYUK (EP693) Alloy KhN67MBYu (EP782) Alloy VZHL12E Alloy ZhS6KP Alloy ZhS30 Alloy ZhS3 Alloy ZhS16 Alloy BC9L Alloy BC4LM Alloy BC4L Alloy VZHL2 Alloy VZhL18 Alloy VZHL16 Alloy VZHL14H (VZHL14) Alloy ZhS6U Alloy VZHL12U Alloy VZhL1 Alloy 67H26M (EI639; NIMO-25) Alloy 58NHVKTBU (EP877; ХН58VCBTU) Alloy 50H6MFA Alloy 50H3CU (EP967) Alloy 3MI3U Alloy 10X20H77TU Alloy 03Х20Н45М4БЧ (ChS42) Alloy 03X20H45M4BRZ (ChS43) 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 ХН55МБЮ
Designation GOST Latin XH55MBJu
Transliteration HN55MBYu
The chemical elements CrNi55CuBeAl
Name The value
Designation GOST Cyrillic ХН63М9Б2Ю
Designation GOST Latin XH63M9B2Ju
Transliteration HN63M9B2Yu
The chemical elements CrNi63Cu9Be2Al
Name The value
Designation GOST Cyrillic ЭП666
Designation GOST Latin EP666
Transliteration EhP666
The chemical elements -

Description

Alloy ХН55МБЮ used: for the production of semi-finished products (forgings, rods, hot rolled sheets, pipes), intended for the manufacture of parts of gas turbine engines and plants; equipment engineering; pipeline fittings AC.

Note

High-temperature Nickel-based alloy.
The recommended maximum operating temperature for limited time +900 °C.
The temperature of beginning of intensive scaling in air +1100 °C.

Standards

Name Code Standards
Thermal and thermochemical treatment of metals В04 ST ЦКБА 016-2005
Bulls. Blanks. Slabs В31 TU 14-1-1214-75, TU 14-1-3626-83
Sectional and shaped rolling В32 TU 14-1-2606-79
Sheets and stripes В53 TU 14-1-3191-81
Metal forming. Forgings В03 TU 14-1-3628-83

Chemical composition

Standard C S P Mn Cr Si Ni Fe N Al Mo Nb Ce
TU 14-1-3626-83 ≤0.6 ≤0.015 ≤0.015 ≤0.8 16.5-18.5 ≤0.5 The rest 10.5-15 ≤0.03 1.2-1.8 8.5-10 1.5-2.5 0.01-0.02
TU 14-1-2606-79 ≤0.6 ≤0.02 ≤0.02 ≤0.8 16.5-18.5 ≤0.5 The rest 10.5-15 ≤0.03 1.2-1.8 8.5-10 1.5-2.5 -
Ni is the basis.
According to TU 14-1-2606-79, the chemical composition is given for the alloy of the grade KhN55MBY-VD (EP666-VD).
According to TU 14-1-3626-83, the chemical composition is given for the alloy grade KhN55MBY-VD (EP666-VD). Cerium is introduced into the metal by calculation and chemical analysis is not determined. The nitrogen content is determined in the finished metal. In the finished metal, the deviation from the chemical composition according to the carbon content is +0.010%, iron -1.0%. In the finished metal, a residual titanium content of not more than 0.20% is allowed. The deviation in titanium is +0.10%. In the finished rolled products, the presence of tungsten content not exceeding 0.20% and copper not exceeding 0.070%

Mechanical characteristics

Section, mm sT|s0,2, MPa σB, MPa d5, % y, % kJ/m2, кДж/м2
The bars as supplied on the other 14-1-2606-79 (longitudinal samples)
3.4-3.7 ≥600 ≥1050 ≥20 ≥30 245-490
3.4-3.7 ≥450 ≥500 ≥25 ≥30 -
Tubular billet on the other 14-1-3626-83. Annealing in air of 980±20 °C (exposure for 1 h) and Aging at 730±20 °With (extract 15 h) cooling with the furnace to 650±20 °C (exposure for 10 h), air cooling (longitudinal samples)
20-25 ≥590 ≥1030 ≥20 - -
20-25 ≥441 ≥590 ≥25 - -

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

Technological properties

Name The value
Macrostructure and contamination The macrostructure of billets on the other 14-1-3626-83 should not have shrinkage and looseness, bubbles, cracks, inclusions and delaminations are visible to the naked eye. Under the control of the workpiece on the transverse templet allowed: Central porosity - less than 1 point, point heterogeneity - no more than 2 points; - phase separation in the square - not more than 1 score. Contamination of metal non-metallic inclusions shall not exceed the maximum score: - oxides of point - 1.5 points; - oxides of stroke - 1.0 points; - silicates fragile - 1.0 points; - silicates plastic - 1.0 points; - silicates nodetoreplace - 1.0 points; - sulphides - 1.0 points. Nitrides and carbonitride monitored and actual results are recorded in the certificate of quality.

Our consultant will save your time

+49 (170) 650 7006
E-mail:
Telegram:
WhatsApp:

Subscription

Special offers and discounts. :)