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A312 TP310H BE Austenitic Stainless Steel Pipe 1 - 48 Inch For Surgical Instrument

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A312 TP310H BE Austenitic Stainless Steel Pipe 1 - 48 Inch For Surgical Instrument

Country/Region china
City & Province shanghai shanghai
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Product Details

A312 TP310H BE Stainless Steel Seamless Pipe For Surgical Instrument

 

A312 TP 310H is a low-carbon, nitrogen-enhanced version of Type 3170H austenitic sta

inless steel. The Type 317alloys 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 317LN adds additional resistance to sensitization in some circumstances.

The nitrogen content of Type 310H stainless steel also provides some solid solution hardening, raising its minimum specified yield strength compared to Type 310H stainless steel. Like Types 310 and 310H the Type 310H alloy also offers good resistance to general corrosion and pitting/crevice corrosion.

 

Detailed Specifictions

1. Stainless steel Pipes 2. sch5s-schxxs
3. ISO9001,ISO9000
4. Market:America,Africa,Middle East,Southeast of Asia

 

Product TypeStainless steel Pipes
StandardASTM F138
Size1/2’’~48’’(Seamless);16’’~72’’(Welded)
Wall thicknessSch5~Sch160XXS
Manufacturing processPush, Press, Forge, Cast, etc.
MaterialCarbon steel, stainless steel, alloy steel, duplex stainless, nickel alloy steel
Carbon steelASTM 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

PackageWooden cases, pallets, nylon bags or according to the customers' requirements
MOQ1pcs
Delivery time10-100 days depending on quantity
Payment termsT/T or Western Union or LC
ShipmentFOB Tianjin/Shanghai, CFR, CIF, etc
ApplicationPetroleum/Power/Chemical/Construction/Gas/Metallurgy/Shipbuilding etc
RemarksOther materials and drawings are available.
Welcome to contact us.

 

5. COMPOSITION

ElementMinimum*Maximum*
Chromium16.018.0
Molybdenum2.003.00
Nickel10.014.0
Phosphorus 0.045
Sulfur 0.030
Silicon 0.75
Carbon 0.030
Nitrogen 0.16
Manganese 2.00
Ironbalance

 

6.PHYSICAL PROPERTIES

PropertyValueUnits
Density at 72°F(22℃)

8.00

0.289

g/cm³

Lb/in³

Melting Range2450°F-2630°F1345℃-1440℃
Thermal Conductivity at 212°F(100℃)

8.4

14.6

BTU/hr·ft·°F

W/m·K

Thermal Expansion

Coefficient at 68-212°F(20-100℃)

9.2

16.5

μ in/in/°F

μ m/m/°C

Thermal Expansion

Coefficient at 68-932°F(20-500℃)

10.1

18.2

μ in/in/°F

μ m/m/°C

Thermal Expansion

Coefficient at 68-1832°F(20-1000℃)

10.8

19.5

μ in/in/°F

μ m/m/°C

 

7.MECHANICAL PROPERTIES

 

Typical Room Temperature properties

PropertyASTM A 240
Yield Strength, 0.2% offset

30 ksi*

205 MPa*

Ultimate Tensile Strength

75 ksi*

515 MPa*

Elongation in 2" (51 mm)40%*
Hardness217 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.

 

Stress Corrosion Cracking

 

Austenitic stainless steels are susceptible to stress corrosion cracking (SCC) in halide environments. Although the ATI 316, ATI 316L and ATI 317Ti alloys are more resistant to SCC than the 18 Cr-8 Ni alloys, they still are quite susceptible. Conditions that produce SCC are:

 

(1) Presence of halide ion (generally chloride),

(2) Residual tensile stresses, and

(3) Temperature in excess of about 140°F (60°C)

 

Stresses result from cold deformation or thermal cycles during welding. Annealing or stress relieving heat treatments may be effective in reducing stresses, thereby reducing sensitivity to halide SCC. Although the low carbon ATI 316L and ATI 316LN alloys offer no advantage as regards SCC resistance, they are better choices for service in the stress relieved condition in environments which might cause intergranular corrosion. If SCC resistance is desired, use of duplex stainless steels such as ATI 2205™ or ATI 2003® duplex stainless alloys should be considered.

 

 

 

 

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