High Temp Metals 800-500-2141

Alloy AM350

Description

Alloy 350 is a chromium-nickel-molybdenum stainless steel which can be hardnened by martensitic transformation and/or precipitation hardening. It has been used for gas turbine compressor components such as blades, discs, rotors, shafts, and similar parts where high strength was required at room and intermediate temperatures. Depending upon the heat treatment, alloy 350 may have an austenitic structure for best formability, or a martensitic structure with strengths comparable to those of martensitic steels. The alloy normally contains about 5 to 10% delta ferrite. The corrosion resistance of alloy 350 approaches that of the chromium-nickel austenitic stainless steel

TYPICAL SPECIFICATION PACKAGES

UNS-S-35000

SHEET:AMS 5548, AMS-S-8840, B50T1140A, ASTM-A-693

ALLOYSIZEWEIGHT
CURRENT SHEET INVENTORY
Alloy AM3500.020 X 35.000 X 120.000
0.508MM X 889 X 3048
1384 LBS
628 KG
Alloy AM3500.025 X 35.500 X 120.000
0.635MM X 901.7 X 3048
2233 LBS
1013 KG
Alloy AM3500.032 X 36.000 X 120.000
0.8128MM X 914.4 X 3048
4613 LBS
2092 KG
Alloy AM3500.040 X 36.000 X 120.000
1.016MM X 914.4 X 3048
1168 LBS
530 KG
Alloy AM3500.050 X 36.000 X 120.000
1.27MM X 914.4 X 3048
2571 LBS
1166 KG
Alloy AM3500.063 X 36.000 X 120.000
1.6002MM X 914.4 X 3048
6345 LBS
2878 KG
Alloy AM3500.125 X 36.000 X 120.000
3.175MM X 914.4 X 3048
3739 LBS
1696 KG