Inconel 718 Forged Fittings

Hind Metal offers a wide range of Inconel 718 Forged Threaded Fittings to the clients, which are tested for its quality before being introduced in the market. Inconel 718 Forged Threaded Elbow (UNS N07718) also exhibits excellent tensile and impact strength.
Inconel 718 Forged Threaded Tee has better mechanical properties at lower temperatures than Nimonic 90 Forged Fittings and Inconel X – 750 Forged Threaded Fittings. Inconel 718 Forged Threaded Cross has been used for jet engine and high – speed airframe parts such as wheels, buckets, spacers, and high temperature bolts and fasteners. Inconel 718 Forged Threaded Cap is also used in gas turbines, rocket motors, spacecraft, nuclear reactors, pumps, and tooling. Inconel 718 Forged Threaded Fittings has excellent weldability compared to the nickel – base super alloys hardened by Aluminum and Titanium.
Hind Metal offers a wide range of Inconel 718 Forged Threaded Fittings to the clients, which are tested for its quality before being introduced in the market. Inconel 718 Forged Threaded Elbow (UNS N07718) also exhibits excellent tensile and impact strength. Inconel 718 Forged Threaded Tee has better mechanical properties at lower temperatures than Nimonic 90 Forged Fittings and Inconel X – 750 Forged Threaded Fittings. Inconel 718 Forged Threaded Cross has been used for jet engine and high – speed airframe parts such as wheels, buckets, spacers, and high temperature bolts and fasteners. Inconel 718 Forged Threaded Cap is also used in gas turbines, rocket motors, spacecraft, nuclear reactors, pumps, and tooling. Inconel 718 Forged Threaded Fittings has excellent weldability compared to the nickel – base super alloys hardened by Aluminum and Titanium. Meanwhile, these Inconel 718 Forged Threaded Coupling are also being offered in different sizes and shapes to our customers. Inconel 718 Forged Threaded Union has excellent strength from -423 degrees F to 1300 degrees F (-253 degrees C to 705 degrees C). These Inconel 718 Forged Threaded Bushing combines corrosion resistance and high strength with outstanding weldability, including resistance to post – weld cracking. To reap the best costs and performance benefits from metal additive layer manufacturing, aerospace applications focus on complex components made of high-value materials such as Inconel 718 Forged Threaded Plug.
The age-hardenable alloy can be readily fabricated, even into complex parts. Its welding characteristics, especially its resistance to postweld cracking, are outstanding.The ease and economy with which INCONEL alloy 718 can be fabricated, combined with good tensile, fatigue, creep, and rupture strength, have resulted in its use in a wide range of applications. Examples of these are components for liquid fueled rockets, rings, casings and various formed sheet metal parts for aircraft and land-based gas turbine engines, and cryogenic tankage. It is also used for fasteners and instrumentation parts.
Hind Metal produces INCONEL alloy 718 for use in oil field applications. This material is 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 typically solution heat treated at 1850-1900 °F and aged at 1450°F for six to eight hours and air cooled. Table 6 shows the mechanical properties this material will meet. Numerous proprietary heat treatments are used for INCONEL alloy 718 depending on the properties required. Such heat treatment sequences are usually developed by companies or agencies independent of the material supplier; consequently, discussion of procedures, tolerances, and resulting properties should be with that company or agency.