Striscia, filo, piastra in lega 625 (UNS N07718/W.Nr. 2.4668)

Product Description: Inconel Alloy is a nickel-chromium-molybdenum-niobium alloy with a high resistance to corrosion and oxidation, as well as fatigue and radiation resistance. It is also known as UNS N06625 or Inconel 625 and is identified by the material number 2.4856. Commonly used in various industries, Inconel Alloy contains the following materials: Nickel (Ni) 50-55%, Chromium (Cr) 17-21%, Niobium (Nb) 4.75-5.5%, and Molybdenum (Mo) 2.8-3.3%.

Inconel Alloy is available in numerous shapes, such as wire, strip, rod, pipe, and plate, and is made according to the ASTM standard. The material is characterised by its exceptional fatigue resistance and excellent oxidation and corrosion resistance, making it suitable for high-temperature applications. Inconel 625 is delivered in a solid state and has a wide range of applications, including aerospace engineering, chemical processing, nuclear engineering, and marine engineering.

Caratteristiche:

• Product Name: Inconel Alloy

• Shape: Wire, Strip, Rod, Pipe, Plate
• Raw Materials: NI50-55%, CR17-21%, NB4.75-5.5%, MO2.8-3.3%
• Features: Fatigue Resistance, Radiation Resistance, Oxidation Resistance, Corrosion Resistance
• Alloy Type: Nickel-based Deformed Superalloy
• Application: Parts For Aero-engine, Nuclear Energy Industry And Petroleum Applications

• No 6625, UNS N06625, Inconel 625 seamless pipe

Applicazioni:

Customization:

Process performance and requirements

Elaborazione termica

The suitable thermal processing temperature is 1120-900℃. The cooling water can be extinguished or other forms. Rapid thermal annealing should be followed by cooling in time to ensure good performance. Thermal processing materials should be heated to a temperature limit to ensure that the final processing temperature of the processed plastic when the deformation reaches 20% should not be lower than 960°C.

Lavorazione a freddo

Solution treatment should be carried out after cold working. The work hardening rate is greater than that of austenitic stainless steel, so the processing equipment should be adjusted accordingly, and there should be an intermediate annealing process during the cold working process.

Welding process

The alloy has satisfactory welding performance and can be welded by argon arc welding, electron beam welding, seam welding, spot welding and other methods.

Parts heat treatment process

The heat treatment of aviation parts is usually carried out according to the standard heat treatment system and the direct aging heat treatment system.

Application scope

Due to its high temperature strength, excellent corrosion resistance and easy processability at 700°C, 718 can be widely used in various high-demand situations.

Support and Services:

Inconel Alloy is a nickel-chromium-based alloy, designed to provide superior corrosion and oxidation resistance for a wide variety of applications. Our technical support team is dedicated to providing customers with fast and knowledgeable service. Our team is available to answer any questions about ordering, installation, setup, maintenance, troubleshooting and repair.