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Inconel 625 u bend tube ASTM B444 UNS N06625 for Aerospace Industry

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Inconel 625 u bend tube ASTM B444 UNS N06625 for Aerospace Industry

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Brand Name :YUHONG
Model Number :ASTM B444/ASME SB444
Certification :ABS, GL, DNV, NK, PED, AD2000, GOST9941-81, CCS, ISO 9001-2008
Place of Origin :China
MOQ :100KGS
Price :Negotiable
Payment Terms :T/T, L/C at sight
Supply Ability :1000 tons per month
Delivery Time :Depends on quantity
Packaging Details :Ply-wooden Case /Iron Case/ Bundle with plastic Cap
Standard :ASTM B444/ASME SB444
Grade :Inconel 625 / UNS N06625
O.D. :4 - 219mm
W.T. :0.5 - 20mm
Type :Seamless and Welded
Packaging :Ply-wooden Case Or Iron Case
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Seamless U Bend Tube ASTM B444 Inconel 625 UNS N06625 Heat Exchangers

What is Inconel 625?

ASTM B444 is the standard specification for nickel-chromium alloy tubing, which consists of a nickel-chromium-molybdenum-niobium alloy. The main reason why these alloys are considered very useful in the manufacture of high quality tubing products is that it has high resistance to oxidation and corrosion and has a high melting point in both water and high temperature applications. The nickel based alloys are very ductile and therefore can be easily plated and welded, thus making them suitable for a variety of industries where extreme and harsh temperatures are important factors.ASTM B444 Seamless and ASTM B444 Seamless Tubing are suitable for use in aerospace industry piping systems, aviation jet engine exhaust systems, engine thrust reserve systems, specialized seawater equipment, chemical process equipment, etc.

Chemical Composition:

Element C Mn Si Fe S Cr2 Al-Ti Ni
min. - - - - - 20.0 - 58.0
max. 0.10 0.50 0.50 5.0 0.015 23.0 0.40 -

Inconel 625 Mechanical Properties & Heat Treatment

Mechanical properties of alloy N06625 grade 1 (annealed) pipe: tensile strength ≥ 120 ksi [827 MPa]; yield strength ≥ 60 ksi [414 MPa]; elongation within 2″ ≥ 30%. Mechanical properties of alloy N06625 Grade 2 (solution annealed) pipe: tensile strength ≥ 100 ksi [690 MPa]; yield strength ≥ 40 ksi [276 MPa]; elongation within 2″ ≥ 30%. Annealing heat treatment shall be carried out at a temperature of not less than 1600°F [871°C]. Solution annealing heat treatment shall be performed at a temperature of not less than 2000°F [1093°C] with a subsequent stabilized annealing temperature of at least 1800°F [982°C] to increase sensitivity.

Equivalent of Inconel 625

Alloy UNS No Old British Euronorm GOST Japanese JIS
BS En No AFNOR
Inconel 625 N06625 NA 21 NiCr22Mo9Nb 2.4856 NC22DNB4M ХН75МБТЮ NCF 625

Heat Treated Materials


Condition of Supply
Heat Treatment (After Forming)
Annealed / Spring Temper Stress relieve at 260-370°C (500-700°F) for 30-60 minutes and air cool.
Condition Approx Tensile Strength Approx Service Temp.
Annealed 800-1000 N/mm2 116-145 ksi -200 to +340°C -330 to +645°F

Typical properties of Inconel 625


Property
Metric Imperial
Density 8.44 g/cm3 0.305 lb/in3
Melting point 1350 °C 2460 °F
Co-Efficient of Expansion 12.8 μm/m.°C
(20-100°C)
7.1x10-6 in/in.°F
(70-212°F)
Modulus of rigidity 79 kN/mm2 11458 ksi
Modulus of elasticity 205.8 kN/mm2 29849 ksi

Applications:

  • Aircraft ducting systems
  • Aerospace
  • Jet engine exhaust systems
  • Engine thrust-reverser systems
  • Specialized seawater equipment
  • Chemical process equipment

Inconel 625 u bend tube ASTM B444 UNS N06625 for Aerospace Industry

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