RA333 Data Sheet [Heat Resistant Alloys] - Rolled Alloys

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RA333 ® 23Hot CorrosionHot corrosion in gas turbine engines is the rapid attackby a film of molten salt in an oxidizing atmosphere.Corrosion resistance is strongly dependent upon chromiumlevel. The alloying elements aluminum, vanadium,molybdenum, tungsten and columbium are detrimentalto hot salt corrosion resistance. 18,19RA333 with its high chromium and moderate level oftungsten and molybdenum, has excellent hot salt corrosionresistance. 20-23
RA333 AlloyRA333 ®RA333 combustion cans, scrolls and transition pieces for large land based gas turbine.24
Page 5 and 6: MachiningRA333 ®RA333 requires low
Page 7: Physical PropertiesRA333 ®Physical
Page 10 and 11: Effect of Elevated Temperature Expo
Page 12 and 13: RA333 ® 11Effect of Cold Drawing o
Page 14 and 15: RA333 ® 13Low Cycle FatigueElevate
Page 16 and 17: RA333 ® 15Rupture StrengthAverage
Page 18 and 19: RA333 ® 17Minimum Creep Rate
Page 20 and 21: RA333 ® 19OxidationRA333 has excel
Page 22 and 23: RA333 ® 21OxidationMetal Dusting1
Page 26 and 27: RA333 ® 25Hot CorrosionMaximumTime
Page 28 and 29: RA333 ® 27Aqueous CorrosionRA333 h
Page 30 and 31: Stress Corrosion CrackingResistance
Page 32 and 33: RA333 ® 31MetallographyTypical Mic
Page 34: DATA SHEET RA333 ® Temperance, MI

RA333 Data Sheet [Heat Resistant Alloys] - Rolled Alloys

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