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17-4PH H1150
Penn Stainless inventory now includes Alloy 17-4 (H1150, UNS S17400) in sheet, sheet coil, plate, round bar, processed flat bar and tubular products.
General Properties
Alloy 17-4 is a chromium-copper precipitation hardening stainless steel that is used for applications requiring high strength and a moderate level of corrosion resistance. It is one of the most widely used precipitation hardening grades, as it has high strength hardness up to about 572°F while demonstrating good corrosion resistance in all heat treated conditions. Alloy 17-4 has adequate resistance to atmospheric corrosion or in diluted acid salts where its corrosion resistance is equivalent to Alloy 304 or 430. Alloy 17-4 can be heat treated to a variety of temperatures to develop a wide range of properties. Its mechanical properties can be optimized with heat treatment where very high yield strength up to 180 ksi can be achieved. Alloy 17-4 should not be used at temperatures above 572°F or at very low temperatures.
Specifications: UNS S17400
Applications:
Alloy 17-4 is commonly used for applications requiring high strength and a moderate level of corrosion resistance. Some applications that frequently use Alloy 17-4 include:
- Aircraft
- Nuclear waste casks
- Paper mills
- Oil fields
- Mechanical components
- Chemical process components
- Food industry
- Aerospace
Standards:
- ASTM/ASME: UNS S17400
- EURONORM: X5CrNiCuNb16.4
- AFNOR: Z6CNU17-04
- DIN: 1.4542
Corrosion Resistance:
- Withstands corrosive attacks better than any of the standard hardenable stainless steels.
- Comparable to Alloy 304 in most media.
- Corrosion resistant in some chemical, petroleum, dairy, and food process industries.
- Subject to crevice or pitting attack if exposed to stagnant sea water for any length of time.
Weldability:
- Successfully welded by most common fusion and resistance methods.
- Should not be joined by oxyacetylene welding.
- Generally no pre-heating required.
- Inter-pass temperature must be limited to 248°F.
- Better toughness is obtained in the weld after a complete heat treatment.
Elevated Temperature Use:
- Excellent resistance to oxidation to approximately 1100°F.
- Long-term exposure to elevated temperature can result in reduced toughness in the precipitation hardened conditions.
Processing – Hot Forming:
- To forge, heat uniformly to 2150 / 2200°F and hold for half hour per inch.
- Preferred temperature range for hot forming is at 650-900°F, while the steel is still austenitic.
- To ensure the best condition for the hardening operations, the forgings must be re-heat treated at 1875-1925°F.
- Cool forgings to below 90°F to ensure grain refinement.
Processing – Cold Forming:
- Alloy 17-4 is limited to mild operations since in the annealed (solution treated) condition the material is hard.
- For severe cold working the material should be heat treated to condition H1150. This will help prevent possible cracking.
- Bend radius in excess of 7T is often required.
- To improve stress corrosion resistance after cold forming, re-aging at the precipitation-hardening temperature is recommended.
Machinability:
- Can be machined in both solution-treated and precipitation-hardening conditions.
- Machining conditions may vary with hardness of material.
- High-speed tools or preferably carbide tools with standard lubrication are normally used.
Chemical Properties:
TYPE | Cr | Ni | Cu | Cb + Ta | C | Mn | P | S | Si |
---|---|---|---|---|---|---|---|---|---|
17-4 (Alloy 630) | min: 15.0 max: 17.5 |
min: 3.0 max: 5.0 |
min: 3.0 max: 5.0 |
min: 0.15 max: 0.45 |
0.07 max |
1.00 max |
0.04 max |
0.03 max |
1.00 max |
Mechanical Properties:
Sheet-Plate
Hardening or Precipitation Treatment at 1150°F | ||||||
---|---|---|---|---|---|---|
Thickness, inches |
Ultimate Tensile Strength, ksi min. |
0.2% Yield Strength, ksi min. |
Elongation % in 2″ min. | Reduction in Area min. % | Hardness, Rockwell, min. / max |
Hardness, Brinell, min. / max. |
Under 0.1875″ | 135 | 105 | 8 | — | C28 – C38 | — |
0.1875″ to 0.625″ |
135 | 105 | 10 | 35 | C26 – C36 | 269 / 352 |
0.625″ to 4.0″ | 135 | 105 | 16 | 40 | C26 – C36 | 269 / 352 |
Bar
Hardening or Aging Treatment at 1150°F | ||||||
---|---|---|---|---|---|---|
Thickness, inches |
Ultimate Tensile Strength, ksi min. |
0.2% Yield Strength, ksi min. |
Elongation % in 2″ min. | Reduction in Area min. % | Hardness, Rockwell, min. / max |
Hardness, Brinell, min. / max. |
Up to 8.0 in. incl. | 135 | 105 | 16 | 50 | 28 | 277 |
Physical Properties:
Heat Treated Condition | H1150 |
---|---|
Density, lbs/in3 | 0.2843 |
Electrical Resistivity, microhm-cm | - |
Specific Heat, BTU/lb/°F (32-212°F) | - |
Thermal Conductivity, BTU/hr/ft^2/in/°F | |
300°F | - |
500°F | - |
860°F | - |
900°F | - |
Mean Coefficient of Thermal Expansion, in/in/°F | |
-100 to 70°F | 6.1 x 10^-6 |
70 – 200°F | 6.6 x 10^-6 |
70 – 400°F | 6.9 x 10^-6 |
70 – 600°F | 7.1 x 10^-6 |
70 – 800°F | 7.2 x 10^-6 |
70 – 900°F | 7.3 x 10^-6 |
Modulus of Elasticity, ksi | |
Modulus of Rigidity, ksi | 10.0 x 10^3 |
Poisson’s Ratio (all conditions) | 0.272 |
Product Information
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