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| Categories | Nickel Alloy Pipe |
|---|---|
| Brand Name: | Metal |
| Model Number: | Monel 400 |
| Certification: | SGS/BV/ABS/LR/TUV/DNV/BIS/API/PED |
| Place of Origin: | China |
| MOQ: | 500 KG |
| Price: | Negotiation |
| Payment Terms: | L/C, T/T, Western Union |
| Supply Ability: | 100 Ton Per Month |
| Delivery Time: | 15 Working days |
| Packaging Details: | Regular shipping packaging or depends on customer's requirement |
| Product Name: | Nickel Alloy Steel Pipe |
| Material Grade: | Incoloy 901 |
| Alloy or not: | Is Alloy |
| Section shape: | Round |
| Standard: | ASTM |
| Type: | Monel alloy |
| Usage: | Oil Pipe |
| Technic: | SMLS |
| Company Info. |
| TOBO STEEL GROUP CHINA |
| Verified Supplier |
| View Contact Details |
| Product List |
Incoloy 901 Alloy Seamless Pipe Nickel Alloy Pipe ASME B36.10 For Oil Pipe
GENERAL CHARACTERISTICS OF INCOLOY™ 901 ALLOY
This is an iron-base nickel-chromium superalloy that combines high strength and corrosion resistance at elevated temperatures.
Specification
Grades: Incoloy 901
Standards: ASTM. ASME AND API
Size: 15'' NB TO 150'' NB IN
Length: Single Random. Double Random & Required Length
Type: Seamless / ERW / Welded / Fabricated / CDW
End: Plain End. Beveled End. Treaded
| Production Name | Nickel Alloy Pipes |
| Standard | ASME/ANSI B16.9, ISO, JIS, DIN, BS,GB, SH, HG,QOST,ETC. |
| Size | 1/2’’~48’’(Seamless);16’’~72’’(Welded) |
| Wall thickness | Sch5~Sch160XXS |
| Manufacturing process | Push, Press, Forge, Cast, etc. |
| Nickel alloy steel | Alloy 200/Nickel 200/NO2200/2.4066/ASTM B366 WPN; |
| Package | Wooden cases, pallets, nylon bags or according to the customers' requirements |
| 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. |
| The third party inspection: | BV,SGS,LOIYD,TUV,and other party alloyed by clients. |
Chemical Properties
| CHEMICAL ANALYSIS | |
| C | Carbon 0.10 max |
| Mn | Manganese 1.00 max |
| Si | Silicon 0.60 max |
| Ni | Nickel 40.00/45.00 |
| Cr | Chromium 11.00/14.00 |
| Mo | Molybdenum 5.00/7.00 |
| Cu | Copper 0.50 max |
| Al | Aluminium 0.35 max |
| Ti | Titanium 2.35/3.10 |
| B | Boron 0.010/0.020 |
APPLICATIONS
The alloy is used for components in aircraft and gas turbines, such as turbine rotors, compressor discs, hubs and shafts, with a maximum service temperature around 1100ºF (595ºC).
MACHINABILITY
The alloy may be machined in all heat-treated conditions. Over
aging gives best machinability, but solution treatment is suitable
for most applications. Carbide tools are recommended for parts in
the fully aged condition.
Positive feeds should be used to overcome work hardening effects
WELDABILITY
The alloy is difficult to weld, but may be welded using the inert-gas-arc method. Welding should be done in the solution-treated condition and a post-weld solution treatment is recommended prior to stabilizing and/or aging.

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