Tel : 0086-0371-86172891
Tel : 0086-0371-86172891
Equal material : UNS N08330
According to the matrix elements can be divided into iron based high temperature alloy, nickel based alloy and cobalt base superalloy. The preparation process can be divided into the deformation of high temperature alloy, high temperature alloy, high temperature alloy and powder metallurgy superalloy. According to strengthen the way of solid solution strengthening, precipitation strengthening, oxide dispersion strengthened with fiber reinforced etc.. X12CrNiS135-16 stainless steel, has excellent corrosion resistance, excellent polishing performance, excellent wear resistance, hardening has excellent stability.
|
Grade |
Ni |
Cr |
Fe |
C max |
Si |
Mn max |
P max |
S max |
|
SS330 |
34.0-37.0 |
17.0-20.0 |
Balance |
0.08 |
0.75-1.50 |
2.0 |
0.030 |
0.030 |
X12CrNiS135-16 steel mechanical property
|
Tensile strength |
Yield strength |
Elongation in% |
Hardness, Rockwell B |
|
552-586 MPa |
207-296MPa |
40-45 |
70-85 |
X12CrNiS135-16 steel physical property:
X12CrNiS135-16 steel Density:8.0g/cm3
X12CrNiS135-16 steel melting point: 1399 degree
X12CrNiS135-16 steel product supplied: X12CrNiS135-16 forgings, X12CrNiS135-16 steel bar, X12CrNiS135-16 steel sheet, X12CrNiS135-16 steel plate, X12CrNiS135-16 steel wire, X12CrNiS135-16 steel tube, X12CrNiS135-16 steel pipe, X12CrNiS135-16 steel fittings, X12CrNiS135-16 flanges.
X12CrNiS135-16 steel application:
Aircraft, ships and industrial gas turbine turbine blades, guide vane, turbine, high pressure compressor disk and combustion chamber of high temperature components, also used in the manufacture of aircraft, rocket engine, nuclear reactor, petrochemical equipment and coal conversion of energy conversion device.
