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17-4PH Stainless Steel Round Bar High Strength Precipitation Hardening Grade for Aerospace & Industrial Use
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x| Products Name | 17-4PH Stainless Steel Bar | Diameter | 10 - 350mm |
|---|---|---|---|
| Length | 6m Or Cutting Any Length As Request | Surface | Black Or Polishing |
| Service | Cutting | Standard | ASTM DIN GB EN |
| Other Products | Round Bar, Square Bar, Flat Bar.etc | Technique | Hot Rolled |
17-4PH Stainless Steel Round Bar High Strength Precipitation Hardening Grade for Aerospace & Industrial Use
Products Specification
| Products Name | 17-4PH Stainless Steel Round Bar |
| Grade |
303,303Cu,304,304L,309S,310S,310H,316L,316Ti,316H,317L,321,329,347,410,415,420, 430F,431,440A/B/C,2205,2507,904l,254SMO,253MA,CD4MCU,XM-19,17-4PH,15-5PH,17-7PH,660,C276,600,601,625,718,800,800H,825,926.etc |
| Products Diameter Range | φ3mm - φ350mm |
| Length | 6m/pcs or cutting any length as request |
| Surface | Pickling finishing, bright finishing |
| Standard | ASTM JIS,GB,DIN EN |
| Service | Cutting |
| Other Shape | Square , Flat, Hexagonal, Round.etc |
| Loading Port | Shanghai Port |
| MOQ | 50 kgs |
- High Strength-to-Weight Ratio: Achieves tensile strengths up to 1310 MPa (190 ksi) after aging at 480°C.
- Excellent Corrosion Resistance: Comparable to Type 304 stainless steel in many environments, including atmospheric exposure, mild acids, and salt spray.
- Good Machinability & Weldability: Can be readily machined in the solution-annealed condition and welded using standard techniques (post-weld aging often required).
- Heat Treatable for Performance Tuning: Mechanical properties can be precisely adjusted via aging temperature (480–620°C).
- Biocompatible & Non-Magnetic: Suitable for medical implants and sensitive electronic applications.
| Element | Content (%) |
|---|---|
| Carbon (C) | ≤ 0.07 |
| Manganese (Mn) | ≤ 1.00 |
| Silicon (Si) | ≤ 1.00 |
| Chromium (Cr) | 15.5 – 17.5 |
| Nickel (Ni) | 3.0 – 5.0 |
| Copper (Cu) | 3.0 – 5.0 |
| Niobium + Tantalum (Nb+Ta) | 0.15 – 0.45 |
| Phosphorus (P) | ≤ 0.04 |
| Sulfur (S) | ≤ 0.03 |
| Iron (Fe) | Balance |
| Aging Condition | Tensile Strength (MPa) | Yield Strength (MPa) | Elongation (%) | Hardness (HRC) |
|---|---|---|---|---|
| H900 (480°C / 1h) | ≥ 1310 | ≥ 1180 | ≥ 10 | ≥ 40 |
| H925 (550°C / 4h) | ≥ 1060 | ≥ 1000 | ≥ 12 | ≥ 35 |
| H1025 (580°C / 4h) | ≥ 1000 | ≥ 860 | ≥ 13 | ≥ 31 |
| H1150 (620°C / 4h) | ≥ 930 | ≥ 725 | ≥ 16 | ≥ 28 |
Engineering Insight: For aerospace landing gear or turbine blades, H900 provides maximum strength. For nuclear valve stems or surgical tools where toughness and stress-corrosion resistance are prioritized, H1150 is preferred.
| Diameter Range | Standard Lengths | Surface Finish Options |
|---|---|---|
| 6 mm – 300 mm (0.25" – 12") | 2m, 3m, 6m (custom lengths available) | Black hot-rolled, Peeled & Polished, Centerless Ground, Bright Drawn |
| Tolerances | Per ASTM A484 / ISO 286 (h9 to h11 achievable on ground bars) | — |
-
Solution Annealing:
- Temperature: 1020–1060°C
- Cooling: Rapid quench (water or air) to retain martensitic structure.
- Resulting hardness: ≤ 38 HRC (machinable condition).
-
Aging (Precipitation Hardening):
- Typical cycles: 480°C to 620°C for 1–4 hours, followed by air cooling.
- No further quenching required—aging is performed directly from ambient or preheated state.
Caution: Avoid prolonged exposure between 350–450°C, where spinodal decomposition may cause embrittlement due to G-phase (Ni₁₆Si₇Mn₆) formation along grain boundaries.
| Industry | Typical Components | Why 17-4PH? |
|---|---|---|
| Aerospace | Jet engine parts, helicopter rotor hubs, landing gear pins | High strength at elevated temps, fatigue resistance |
| Oil & Gas | Downhole tools, wellhead valves, subsea connectors | Resists chloride stress corrosion cracking |
| Nuclear Energy | Reactor control rods, safety valve stems | Stability under radiation + moderate corrosion resistance |
| Medical | Surgical clamps, orthopedic implants, dental instruments | Biocompatibility, sterilizability, non-magnetic |
| Industrial | High-strength shafts, gears, pump axles, molds | Wear resistance + dimensional stability after aging |
- Machining: Best performed in the solution-treated (soft) condition. Use carbide tools, low cutting speeds, and ample coolant to avoid work hardening.
- Welding: Preheat to 100–150°C if needed; post-weld aging restores strength in the heat-affected zone (HAZ).
- Forming: Limited cold formability due to martensitic structure—warm forming (>200°C) recommended for complex shapes.
- Surface Enhancement: Laser peening, nitriding (≤400°C), or shot peening can further improve fatigue life and surface hardness.
- Chemical analysis (OES verified)
- Mechanical test data (tensile, hardness, impact if required)
- Ultrasonic inspection (optional for aerospace grades)
- Traceability via heat number
- Global Stock Network: Ready inventory in Asia, Europe, and North America for fast delivery.
- Precision Manufacturing: Advanced rolling and grinding lines ensure tight tolerances and consistent microstructure.
- Technical Support: In-house metallurgists assist with heat treatment parameters, failure analysis, and material selection.
- Sustainability Focus: Recycled content >60%; compliant with EU Green Deal initiatives.

