UNS S31653 / 316LN Austenitic Stainless Steel Pipe: (UNS S31653)
316LN (UNS S31653) is a low-carbon, nitrogen-enhanced version of Type 316 molybdenum-bearing austenitic stainless steel. The Type 316 alloys are more resistant to general corrosion and pitting/crevice corrosion than the conventional chromium-nickel austenitic stainless steels such as Type 304. They also offer higher creep, stress-rupture and tensile strength at elevated temperature. The nitrogen in Type 316LN adds additional resistance to sensitization in some circumstances.
The nitrogen content of Type 316LN stainless steel also provides some solid solution hardening, raising its minimum specified yield strength compared to Type 316L stainless steel. Like Types 316 and 316L, the Type 316LN alloy also offers good resistance to general corrosion and pitting/crevice corrosion.
Typical Manufacturing Specifications
ASTM F138
ASTM F2181
Also individual customer specifications.
Detailed Specifictions
1. Stainless steel Pipes
2. sch5s-schxxs
3. ISO9001,ISO9000
4. Market:America,Africa,Middle East,Southeast of Asia
Product Type | Stainless steel Pipes |
Standard | ASTM F138 |
Size | 1/2''~48''(Seamless);16''~72''(Welded) |
Wall thickness | Sch5~Sch160XXS |
Manufacturing process | Push, Press, Forge, Cast, etc. |
Material | Carbon steel, stainless steel, alloy steel, duplex stainless, nickel alloy steel |
Carbon steel | ASTM A234 WPB, WPC; |
Stainless steel |
304/SUS304/UNS S30400/1.4301 304L/UNS S30403/1.4306; 304H/UNS S30409/1.4948; 309S/UNS S30908/1.4833 309H/UNS S30909; 310S/UNS S31008/1.4845; 310H/UNS S31009; 316/UNS S31600/1.4401; 316Ti/UNS S31635/1.4571; 316H/UNS S31609/1.4436; 316L/UNS S31603/1.4404; 316LN/UNS S31653; 317/UNS S31700; 317L/UNS S31703/1.4438; 321/UNS S32100/1.4541; 321H/UNS S32109; 347/UNS S34700/1.4550; 347H/UNS S34709/1.4912; 348/UNS S34800; |
Alloy steel |
ASTM A234 WP5/WP9/WP11/WP12/WP22/WP91; ASTM A860 WPHY42/WPHY52/WPHY60/WPHY65; ASTM A420 WPL3/WPL6/WPL9; |
Duplex steel |
ASTM A182 F51/S31803/1.4462; ASTM A182 F53/S2507/S32750/1.4401; ASTM A182 F55/S32760/1.4501/Zeron 100; 2205/F60/S32205; ASTM A182 F44/S31254/254SMO/1.4547; 17-4PH/S17400/1.4542/SUS630/AISI630; F904L/NO8904/1.4539; 725LN/310MoLN/S31050/1.4466 253MA/S30815/1.4835; |
Nickel alloy steel |
Alloy 200/Nickel 200/NO2200/2.4066/ASTM B366 WPN; Alloy 201/Nickel 201/NO2201/2.4068/ASTM B366 WPNL; Alloy 400/Monel 400/NO4400/NS111/2.4360/ASTM B366 WPNC; Alloy K-500/Monel K-500/NO5500/2.475; Alloy 600/Inconel 600/NO6600/NS333/2.4816; Alloy 601/Inconel 601/NO6001/2.4851; Alloy 625/Inconel 625/NO6625/NS336/2.4856; Alloy 718/Inconel 718/NO7718/GH169/GH4169/2.4668; Alloy 800/Incoloy 800/NO8800/1.4876; Alloy 800H/Incoloy 800H/NO8810/1.4958; Alloy 800HT/Incoloy 800HT/NO8811/1.4959; Alloy 825/Incoloy 825/NO8825/2.4858/NS142; Alloy 925/Incoloy 925/NO9925; Hastelloy C/Alloy C/NO6003/2.4869/NS333; Alloy C-276/Hastelloy C-276/N10276/2.4819; Alloy C-4/Hastelloy C-4/NO6455/NS335/2.4610; Alloy C-22/Hastelloy C-22/NO6022/2.4602; Alloy C-2000/Hastelloy C-2000/NO6200/2.4675; Alloy B/Hastelloy B/NS321/N10001; Alloy B-2/Hastelloy B-2/N10665/NS322/2.4617; Alloy B-3/Hastelloy B-3/N10675/2.4600; Alloy X/Hastelloy X/NO6002/2.4665; Alloy G-30/Hastelloy G-30/NO6030/2.4603; Alloy X-750/Inconel X-750/NO7750/GH145/2.4669; Alloy 20/Carpenter 20Cb3/NO8020/NS312/2.4660; Alloy 31/NO8031/1.4562; Alloy 901/NO9901/1.4898; Incoloy 25-6Mo/NO8926/1.4529/Incoloy 926/Alloy 926; Inconel 783/UNS R30783; NAS 254NM/NO8367; Monel 30C Nimonic 80A/Nickel Alloy 80a/UNS N07080/NA20/2.4631/2.4952 Nimonic 263/NO7263 Nimonic 90/UNS NO7090; Incoloy 907/GH907; Nitronic 60/Alloy 218/UNS S21800 |
Package | Wooden cases, pallets, nylon bags or according to the customers' requirements |
MOQ | 1pcs |
Delivery time | 10-100 days depending on quantity |
Payment terms | T/T or Western Union or LC |
Shipment | FOB Tianjin/Shanghai, CFR, CIF, etc |
Application | Petroleum/Power/Chemical/Construction/Gas/Metallurgy/Shipbuilding etc |
Remarks | Other materials and drawings are available. |
Welcome to contact us. |
5. COMPOSITION
Element | Minimum* | Maximum* |
Chromium | 16.0 | 18.0 |
Molybdenum | 2.00 | 3.00 |
Nickel | 10.0 | 14.0 |
Phosphorus | 0.045 | |
Sulfur | 0.030 | |
Silicon | 0.75 | |
Carbon | 0.030 | |
Nitrogen | 0.16 | |
Manganese | 2.00 | |
Iron | balance |
6. PHYSICAL PROPERTIES
Property | Value | Units |
Density at 72°F(22ºC) |
8.00 0.289 |
g/cm³ Lb/in³ |
Melting Range | 2450°F-2630°F | 1345ºC-1440ºC |
Thermal Conductivity at 212°F(100ºC) |
8.4 14.6 |
BTU/hr·ft·°F W/m·K |
Thermal Expansion Coefficient at 68-212°F(20-100ºC) |
9.2 16.5 |
μ in/in/°F μ m/m/°C |
Thermal Expansion Coefficient at 68-932°F(20-500ºC) |
10.1 18.2 |
μ in/in/°F μ m/m/°C |
Thermal Expansion Coefficient at 68-1832°F(20-1000ºC) |
10.8 19.5 |
μ in/in/°F μ m/m/°C |
Available Tube Product form
Straight
Coiled
Seamless
Typical Applications
Orthopaedic implants
Trauma nails
Neurological applications
Surgical instruments
Industries predominantly using this Grade
Chemical processing
High performance liquid chromatography (hplc)
Medical
316LN stainless is a single phase austenitic (face centered cubic) stainless steel at all temperatures up to the melting point. The alloy can not be hardened by heat treatment. The alloy is nonmagnetic in the annealed condition. Its magnetic permeability is typically less than 1.02 at 200 H (Oersteds). Permeability values for cold de-formed material vary with composition and the amount of cold deformation, but are usually higher than that for annealed material.
7. MECHANICAL PROPERTIES
Typical Room Temperature properties
Property | ASTM A 240 |
Yield Strength, 0.2% offset |
30 ksi* 205 MPa* |
Ultimate Tensile Strength |
75 ksi* 515 MPa* |
Elongation in 2" (51 mm) | 40%* |
Hardness | 217 Brinell** 95 HRB** |
* minimum, ** maximum
Fatigue Resistance
The fatigue strength or endurance limit is the maximum stress below which a material is unlikely to fail in 10 million cycles in an air environment. For austenitic stainless steels as a group, the fatigue strength is typically about 35 percent of the tensile strength. However, substantial variability in service results is experienced since additional variables such as corrosive conditions, type of loading and mean stress, surface condition, and other factors affect fatigue properties. For this reason, no definitive endurance limit value can be given which is representative of all operating conditions.
Product picture