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Product Details
PH-steel 17-4 PH
PH-steel 17-4 PH — UNS S17400; AISI 630; EN 1.4542 / X5CrNiCuNb16-4; JIS SUS630; commonly known as 17-4PH, 17-4 Precipitation-Hardening Stainless Steel.PH Stainless Steel, Precipitation-Hardening Stainless Steel, Grade 630, Type 630, 17Cr-4Ni PH Stainless Steel.
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Category
Stainless Steel
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Grade
17-4 PH / UNS S17400 / 1.4542
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Standard
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Product Form
ASTM A564 / ASTM A693 / ASTM A705 / AMS 5604 / AMS 5643
Round Bar / Forged Bar / Plate / Sheet / Forged Ring / Shaft / Fasteners / Valve Components / Precision Machined Parts
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Thickness
0.5–150 mm
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Width
1000–2500 mm
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Length
2000–6000 mm
Features
17-4 PH is a chromium-nickel-copper precipitation-hardening stainless steel designed to combine high mechanical strength with good toughness and corrosion resistance. Its martensitic structure can be strengthened through controlled precipitation-hardening heat treatments.
Copper plays an important role in the age-hardening response, while niobium contributes to strengthening and metallurgical stability. The alloy can achieve different combinations of strength, hardness and toughness through various aging conditions.
Common heat-treatment conditions include H900, H925, H1025, H1075, H1100 and H1150. H900 generally provides higher strength and hardness, while higher-temperature aging conditions provide increased ductility and toughness with reduced strength.
17-4 PH is widely used for shafts, fasteners, valve components, pump parts, aerospace components and other highly loaded parts where a combination of mechanical strength and corrosion resistance is required.
Surface Finish | Bright / Pickled / Ground / Polished / Machined |
Technique | Hot Rolled / Forged / Solution Treated / Age Hardened / Cold Finished / Machined |
Applications | Aerospace Components, Turbine Parts, Shafts, Fasteners, Valves, Pump Components, Marine Equipment, Chemical Processing, High-Strength Structural Parts |
High tensile and yield strength
Excellent precipitation-hardening response
Good corrosion resistance
Good toughness
High hardness after aging
Multiple heat-treatment conditions available
Good dimensional stability during aging
Good fatigue performance
Suitable for highly stressed components
Widely used in aerospace and industrial equipment
Chemical Composition (%)
Mechanical Properties (Typical)
Element | Composition (%) |
Fe | Balance |
Cr | 15.00–17.50 |
Ni | 3.00–5.00 |
Cu | 3.00–5.00 |
Nb + Ta | 0.15–0.45 |
Mn | ≤ 1.00 |
Si | ≤ 1.00 |
C | ≤ 0.07 |
P | ≤ 0.040 |
S | ≤ 0.030 |
Property | Typical Value |
Tensile Strength | Approx. 1,310 MPa |
Yield Strength (0.2%) | Approx. 1,170 MPa |
Elongation | Approx. 10% |
Hardness | Approx. 40 HRC |
Density | Approx. 7.75 g/cm³ |
Mechanical properties may vary depending on product form, dimensions, aging condition, heat treatment, and applicable material specification.
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