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
1360 LBS
617 KG
Alloy AM3500.025 X 35.500 X 120.000
0.635MM X 901.7 X 3048
2173 LBS
986 KG
Alloy AM3500.032 X 36.000 X 120.000
0.8128MM X 914.4 X 3048
3869 LBS
1755 KG
Alloy AM3500.040 X 36.000 X 120.000
1.016MM X 914.4 X 3048
580 LBS
263 KG
Alloy AM3500.050 X 36.000 X 120.000
1.27MM X 914.4 X 3048
2017 LBS
915 KG
Alloy AM3500.063 X 36.000 X 120.000
1.6002MM X 914.4 X 3048
2706 LBS
1227 KG
Alloy AM3500.125 X 36.000 X 120.000
3.175MM X 914.4 X 3048
3274 LBS
1485 KG