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Cast Stainless Steel Technology Developments Cast Stainless Steel Technology Developments Raymond Monroe SFSA CN3MN CF8 CD4Cu CB 7 Cu CA 15 Calculation of Chromium Equivalent and Nickel Equivalent CrE = %Cr + 2 × %Si + 1.5 × %Mo + 5 × %V NiE = %Ni + 0.5 × %Mn + 30 × %C + 0.3 × %Cu Ferrite from Chemistry Schoefer Diagram 2.2 2.1 • Chemistry: C=0.07, 2 Mn=0.56, Si=1.30, 1.9 P=0.028, S=0.009, 1.8 o i t 1.7 Cr=19.5, Ni=10.7, a 1.6 on R i t i Mo=2.18 (Cb ~ 0.05 1.5 pos m o and N ~ 0.04) 1.4 C i N / r 1.3 C • ASTM A800 predicts 1.2 10.5 volume percent 1.1 1 ferrite with a range of Cr Cr (%) + 1.5Si (%) + 1.4 Mo (%) + Nb (%) − 4.99 0.9 e = 6.5 to 14.5 (chromium Ni e Ni (%) + 30 C (%) + 0.5Mn (%) + 26 ( N − 0.02 %) + 2.77 0.8 0 10203040506070 equivalent to nickel Volume Percent Ferrite equivalent = 1.19) Means of Calculating Ferrite • Severn Gage: 11 • Feritscope: 7 • Magne-Gage: 2 • Two different instruments: 5 • Manual point count • ASTM A800 • 1949 Schaeffler Diagram • WRC Diagram Unit of measure: • FN: 8 (all 4 of the non- foundry) • Volume percent: 7 • Use both methods: 2 Identification of Phases by Composition FERRITE AUSTENITE Stainless Steels - Strength Grade Yield (ksi) UTS (ksi) CF8 70 30 CF3MN 75 37 4A(2205) 90 60 6A(Zeron 100) 100 65 Stainless Steel - Corrosion Grade Critical pitting temperature oC CF8 5 (calculated) CF3MN 29 (calculated) 4A(2205) 35 - 40 6A(Zeron100) 45 – 55 Pseudo Phase Diagram for 68 % Fe – Cr Ni CCT Diagram - CD3MN 5oC/min 2oC/min 1oC/min 0.5oC/min 0.1oC/min 0.01oC/min 1100 1050 TTT curves 1000 (initial & final) 950 900 850 800 750 700 Temp. (Celsius) 650 CCT curves 600 none (non-equil. 550 initial & final) 500 1 10 100 1000 10000 100000 Time (minutes) Cooling Rate=1oC/min, Cooling Rate=0.5oC/min Cooling Rate=0.1oC/min Cooling Rate=0.01oC/min σ phase <<1% σ phase <1% σ phase =8.72% ±3.38 σ phase =17.62% ±3.46 CCT Diagram - CD3MWCuN V0.175mm/sec V0.150mm/sec V0.100mm/sec 5oC/min 2oC/min 1oC/min 0.5oC/min 0.1oC/min 1100 1050 1000 950 TTT curves (initial & final) ) 900 us 850 si o 800 Cooling Rate=0.1 C/min σ phase =10.60% ±2.82 (Cel 750 mp. 700 Te 650 none 600 CCT curves (non-equil. 550 initial & final) 500 1 10 100 1000 Time (minutes) Cooling Rate=0.5oC/min σ phase =10.37% ±2.22 Bridgman furnace Cooling Rate=5oC/min Cooling Rate=2oC/min Cooling Rate=1oC/min V=0.1mm/sec,σ phase<1% σ phase =3.61% ±2.64 σ phase =7.10% ±2.12 σ phase =10.09% ±1.13 PROBLEM - Corrosion of High Alloy (6 wt% Mo) Stainless Steel Castings Wrought AL6XN ACN3MNs-Solidified AL6XN 1150oC/4 hrs Current minimum required heat treatment – 1150 °C/ 1hr (ASTM Standards A743 10 Dendrite cores Mo and A351) 8 Cast alloys and welds not as corrosion resistant due to: 6 – microsegregation element – presence of σ phase 4 Wt % of 2 OBJECTIVE: Develop heat treating schedules and welding procedures that restore the corrosion resistance of castings 0 and welds to a level comparable to that of wrought 010203040 counterpart alloys Distance (µm) Typical Homogenization Results 1205 4 Hour CK3MCuN 10 1150As Ca 4 stH oCKur 3CMKCu3MNCuN 10 10 % Mo t 9 Dendrite Cores Mo w Mo 9 ) w 9 n ( % o t i n ( t 8 w o i a t 8 n ( r 8 a o t i r t n a e r 7 t n 7 nc e 7 ncent o o nc o %) C 6 C C 6 6 num num 55 bde 5 y bdenum l bde y o y l l M o o 44 M 4 M 33 3 000 2020 50 4040 6061000 8080 150 100100 120120200 141400 250 161600 181803000 Distance (microns) DDiissttaanncece ( (mMicicroronns)s) • 1205 °C/4 hours needed for complete homogenization CN3MN Corrosion Results – ASTM G48A 25.0% 22.3% ) 20.0% 18.0% 18.3% % ( s 15.0% 13.8% 13.2% Los 10.0% ght i e 5.4% ASTM Minimum 5.0% W 5.0% 1.7% 0.0% AL6XN As Cast 1150 1 Hour 1150 2 Hour 1150 4 Hour 1205 1 Hour 1205 2 Hour 1205 4 Hour CN3MN λ = 80ε −0.33 Model can be used as a predictive tool to determine effective heat treatment times for CN3MN prepared with various cooling rates Need to establish acceptable cooling rate from the heat treating temperature to avoid formation of brittle secondary phase Collaboration with Scott Chumbley (Iowa State) Results from C. Muller and Scott Chumbley, Iowa State University Impact toughness Impact Toughness (ft-lbs) Grain boundary precipitates Impact toughness decreases significantly with time at 870 oC, which could occur for large castings cooled slowly from the heat treating temperature Need to establish critical cooling rates in order to avoid embrittlement. Toughness and Corrosion CK3MCuN CN3MN Performance Charpy Impact Toughness decreases significantly with an extremely slow cooling rate (0.01°C/sec) Charpy Impact Toughness is unaffected by cooling rate above 1°C/sec Corrosion Performance decreases at an extremely slow cooling rate (0.01°C/sec) CK3MCuN CN3MN Corrosion Performance is unaffected by cooling rate above 1°C/sec Slow cooling rate sample shows evidence of grain boundary attack Corrosion of Welds in Super Austenitic Stainless Steel Castings CN3MN CN3MN CN3MN 1205oC/4 hrs with As-Cast 1205oC/4 hrs Autogenous Weld Base 1 cm Metal Weld Welding reintroduces the microsegregation profile 1 cm 1 cm Percent Mass Loss Percent Mass Loss CN3MN CN3MN CN3MN 1205°C/4hr As-Cast 1205°C/4hr with Autogenous Weld 22% 2% 14% Corrosion Resistance as a Function of Dilution (IN686 Filler Metal Welds on CN3MN) ASTM G48a Temperature: 75° C Solution: FeCl3 (Ferric Chloride) 1 cm 1cm 1cm 1cm 6.2 wt% Mo Weld Metal Base Metal 7.9 wt% Mo 1cm 11.0 wt% Mo 14.0 12.4 wt% Mo wt% Mo Corrosion performance increases with decreasing dilution level Corrosion performance of weld can restored to level of cast material at dilution levels below ~ 50% Corrosion Resistance as a Function of Dilution (IN72 Filler Metal Welds on CN3MN) ASTM G48a Temperature: 75° C Solution: FeCl3 (Ferric Chloride) 1 cm 1 cm 3.2 wt% Mo 6.2 wt% Mo 31.5 wt% Cr 5.1 wt% Mo 20.6 wt% Cr 24.4 wt% Cr Base Weld Metal Metal 1 cm 1 cm 1cm 1.3 wt% Mo 2.3 wt% Mo 38.5 wt% Cr 34.9 wt% Cr Corrosion performance increases with decreasing dilution level IN72 Filler metal unable to avoid localized corrosion in weld Corrosion Results: IN686 Filler Metal Heat Treatments have a significant effect on corrosion performance Post weld heat treatments (PWHT) will mitigate negative effects of dilution Heat treatments should be done after welding, if possible (no need to control dilution) Post Weld Heat Treatment at 1205°C/4hr produces the best corrosion resistance Air-Set Pouring Nondestructive Examination •Surface –Visual – Magnetic particle examination (MT) – Liquid penetrant examination (PT) • Volume – Radiographic examination (RT) – Ultrasonic examination (UT) Examination •Visual – ASTM A802 – MSS SP55 • Magnetic Particle – ASTM E709 – ASTM E125 – MSS SP53 • Liquid Penetrant – ASTM E165 Method – ASTM E433 Acceptance – MSS SP93 Visual Examination • Equipment required: surface comparator, pocket rule, straight edge, workmanship standards • Enables detection of: surface flaws – cracks, porosity, slag inclusions, adhering sand, scale, etc. • Advantages: low cost, can be applied while work is in process to permit correction of faults • Limitations: applicable to surface defects only, provides no permanent record • Remarks: should always be the primary method of inspection, no matter what other techniques are required Inspection 1 Inspection 2 erator 1 p O Casting 3 erator 2 p O Operator 2 Operator 1 Inspection 1 Foundry 3 I nspection 2 Liquid Penetrant Examination • Equipment required: commercial kits containing fluorescent or dye penetrants and developers, application equipment for the developer, a source of ultraviolet light – if fluorescent method is used • Enables detection of: surface discontinuities not readily visible to the unaided eye • Advantages: applicable to magnetic and nonmagnetic materials, easy to use, low cost • Limitations: only surface discontinuities are detectable Methodology • To determine the resolution of the process – Only data from a minimum of three inspections per casting for each inspector was used. – An indication must be detected at least 50% of the time or the data was not considered so results are a best case situation. • The results were grouped by casting type, if multiple geometries were used, and also by inspector (to eliminate variation from inspector to inspector). • Sample standard deviation was used as a measure of resolution. Foundry 3 • High alloy steel, visible liquid penetrant. • One casting shape, 10-15 lb cast weight. • Three Inspectors. • Twenty-four pieces per part type. • Three runs per inspector • Measured length and sketched location of indications on part drawing. • A total of 216 inspections were made. Casting Geometry 1 Inspector 1 Inspector 2 Inspector 3 All Box-and-Whisker Plot Box-and-Whisker Plot Box-and-Whisker Plot Box-and-Whisker Plot 0.009 0.013 0.017 0.021 0.025 0 0.1 0.2 0.3 0.4 0 0.005 0.01 0.015 0.02 0.025 00.10.20.30.4 Standard Deviation Standard Deviation Standard Deviation Standard Deviation 95% confidence interval 95% confidence interval 95% confidence interval 95% confidence interval for mean for mean for mean for mean 0.0” to 0.04” 0.0” to 0.2” 0.0” to 0.02” 0.01” to 0.5” Punch Line – The resolution for all inspectors is about 0.4”.
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