Machinability of stainless steel grade 17-7 PH is rated at 75 % of B1112. On machining, this alloy shows long gummy chips and requires chip breakers. While machining will provide excellent results the slow speeds and constant feeds are recommended.
FormingForming attributes of this alloy are like to the 301 stainless steel. Intermediate annealing might be necessary for radical forming operations.
WeldingMost common arc and resistance strategies have been effectively utilized with 17-7 PH. It is recommended that inert gas shielding is utilized during fusion welding to decrease the oxidation of aluminum during the process. Preheating and post-weld annealing are not compulsory with this alloy.
Heat TreatmentCONDITION C - Results from heavy cold working (generally 45-50% reduction) of solution treated material. CONDITION CH900- Heat Condition C material to 900 F (482 C), holds for 1 hour, air cool. CONDITION A1750- After fabrication, heat solution treated material to 1750 F (955 C), hold for 10 minutes, cool rapidly to room temperature. CONDITION R100- Within 1 hour of treating to Condition A1750, cool to -100 F (-73 C) and hold for 8 hours. The Air warm to room temperature. CONDITION RH 950- From Condition R100 material, heat to 950 F (510 C), holds for 90 minutes, air cool. CONDITION T- After fabrication, heat to 1400 F (760 C) and hold for 90 minutes. Within 60 minutes, cool to 55 F (13 C), and hold for 1/2 hour. CONDITION TH1050- from Condition T, heat to 1050 F (565 C) and hold for 90 minutes, air cool.
Cold WorkingIn Condition A, this material can be effectively formed by utilizing most common process.
Annealing1950 F (1066 C) for 3 minutes for each .1 inch (2.5 mm) of thickness, air cool.
HardeningSolution anneal at 2150 F for 4 hours with air cooling. Follow with 1975 F for 4 hours and air cool, then 1550 F for 24 hours, air cool and 1400 F for 16 hours, air cool to finish the precipitation hardening process, resistant to liquid oxygen, hydrogen and ammonia. For optimum performance, material must be clean and free of scale and impurities.
Chemical Composition %C | Al | Si | P | S | Cr | Mn | Ni | Fe |
0.09 max | 0.75 - 1.50 | 1.0 max | 0.04 max | 0.03 max | 16.0 - 18.0 | 1.0 max | 6.50 - 7.75 | Remainder |
Tensile Strength (ksi) | 0.2% Yield Strength (ksi) | Elongation% in 2 inches |
120 | 45 | 35 |
Units | Temperature in °C | |
Density | 7.80 g/cm³ | Room |
Specific Heat | 0.11 Kcal/kg.C | 22° |
Melting Point | 1406 - 1440 °C | - |
Modulus of Elasticity | 200 KN/mm² | 20° |
Electrical Resistivity | 80 µΩ.cm | Room |
Coefficient of Expansion | 11.1 µm/m °C | 20 - 100° |
Thermal Conductivity | 16.4 W/m -°K | 20° |
Sheet / Plate | Bar | Forging | Wire |
A 693 | A 564 | A 579 | A 313 |
Manufacturing |
Fasteners |
Custom Machining |
Custom Fabrication |
Stamped Parts |
Flanges |
Raw Materials |
Bars |
Wires |
Sheets |
Plates |