|Inconel 718 Price||Origin|| Price in INR
| Price in USD
|Price in Euro
|Inconel 718 Price in India||Indian||Rs 3200/-||$46||€39|
|Inconel 718 Price in Japan||Japanese||Rs 3500/-||$51||€43|
|Inconel 718 Price in UK / Europe||European||Rs 3700/-||$54||€46|
|Inconel 718 Price in USA||USA||Rs 4500/-||$65||€56|
ASTM B637, B 670, B 906
UNS Number N07718
In what forms is Inconel 718 Available at Steel Tubes India?
Inconel 718 Chemical Composition, %
|50.00-55.00||Remainder||17.00-21.00||.30 max||2.80-3.30||4.75-5.50||.08 max||.35 max|
|.015 max||.015 max||.35 max||.65-1.15||.20-.80||1.00 max||.006 max|
In what applications is Inconel 718 used?
- Chemical processing
- Liquid fuel rocket motor components
- Pollution-control equipment
- Nuclear reactors
- Cryogenic storage tanks
- Valves, fasteners, springs, mandrels, tubing hangers
- Well head completion equipment and blow out preventers (BOP’s)
- Gas turbine engine parts
Inconel 718 ASTM Specifications
Inconel 718 Mechanical Properties
Typical room temperature properties, 1800°F annealed condition
|Ultimate Tensile Strength, psi||.2% Yield Strength psi||Elongation %||Hardness Rockwell B|
|Inconel 718||2.4668||N07718||NCF 718||–||–||–||–|
Inconel 718 is a nickel chromium material with high-strength, corrosion-resistant used at -423° to 1300°F. This age-hardenable alloy can be readily fabricated, even into complex parts and Its welding characteristics, especially its resistance to postweld cracking, are amazing. The ease and economy with which INCONEL alloy 718 W.Nr. 2.4668 can be fabricated, combined with good tensile, fatigue, creep, and rupture strength, have resulted in its use in a wide range of applications.
Components for liquid fueled rockets, rings, casings and various formed sheet metal parts for aircraft and land-based gas turbine engines, and cryogenic tankage. UNS N07718 inconel alloy 718 is also used for fasteners and instrumentation parts.
Haycon produces INCONEL alloy 718 for use in oil field applications. This material is subjected to be produced under the NACE specification MR0175 which requires the solution annealed and aged material to meet a maximum hardness value of 40 Rockwell C. Such material is solution heat treated at 1850-1900 °F and aged at 1450°F for six to eight hours and air cooled finally.