T160
T160 · alloy
T160
Bar,Plate |
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T165
T165 · alloy
T165
Bar,Plate |
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T170
T170 · alloy
T170
Bar,Plate |
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T180
T180 · alloy
T180
Bar,Plate |
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T185
T185 · alloy
T185
Bar,Plate |
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T190
T190 · alloy
T190
Bar,Plate |
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T195
T195 · alloy
T195
Bar,Plate |
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T2
T2 · alloy
T2
Bar,Plate | ASTM A213 T2
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T21
T21 · alloy
T21
Bar,Plate | ASTM A213 T21
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T22
T22 · alloy
T22
Bar,Plate | ASTM A213 T22
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T23
T23 · alloy
T23
Bar,Plate | ASTM A213 T23
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T24
T24 · alloy
T24
Bar,Plate | ASTM A213 T24
C:0.30-0.45;Mn:0.60-1.00;Si:0.15-0.35;Cr:0.50-1.00;P:≤0.035;S:≤0.040
T250
T250 · highstrength
T250
Bar,Forging | Maraging T250
Ni:17.0-19.0;Co:8.0-13.0;Mo:3.0-5.0;Ti:0.1-2.0;C:≤0.03
T3
T3 · copper
T3 copper (GB/T 5231)
Sheet, Plate, Bar, Tube, Rod, Wire, Strip | T 5231
Cu:99.70 min
T300
T300 · highstrength
T300
Bar,Forging | Maraging T300
Ni:17.0-19.0;Co:8.0-13.0;Mo:3.0-5.0;Ti:0.1-2.0;C:≤0.03
T350
T350 · highstrength
T350
Bar,Forging | Maraging T350
Ni:17.0-19.0;Co:8.0-13.0;Mo:3.0-5.0;Ti:0.1-2.0;C:≤0.03
T4
T4 · other
T4
Nickel/cobalt-base superalloy retaining high strength, creep and corrosion resistance at extreme temperature. Cobalt (≈5%) raises hot corrosion and wear resistance. Used in gas-turbine blades, aero-engine hot sections, combustors and advanced energy syste | ASTM A600 T4
C:0.70-0.80;W:17.0-19.0;Cr:3.75-4.50;V:0.80-1.20;Co:4.25-5.75;P:≤0.030;S:≤0.030
T5
T5 · other
T5
Nickel/cobalt-base superalloy retaining high strength, creep and corrosion resistance at extreme temperature. Cobalt (≈8.25%) raises hot corrosion and wear resistance. Used in gas-turbine blades, aero-engine hot sections, combustors and advanced energy sy | ASTM A600 T5
C:0.75-0.85;W:17.0-19.0;Cr:3.75-4.50;V:1.80-2.30;Co:7.00-9.50;P:≤0.030;S:≤0.030