Inconel bars

Product Details:

Specifications

Specialist of Inconel material, High strength and hard material.

Alloy 718 is a precipitation hardenable nickel-based alloy designed to display exceptionally high yield, tensile and creep-rupture properties at temperatures up to 1300°F. The sluggish age-hardening response of alloy 718 permits annealing and welding without spontaneous hardening during heating and cooling. This alloy has excellent weldability when compared to the nickel-base superalloys hardened by aluminum and titanium. This alloy has been used for jet engine and high-speed airframe parts such as wheels, buckets, spacers, and high temperature bolts and fasteners.

 

 

 

standard ASTM B637 AMS 5662 AMS 5663 AMS 5664 PWA 1009 PWA 1010 GE B50TF15

 

Additional Information:

• Pay Mode Terms: T/T (Bank Transfer)
• Port of Dispatch: chennai,mumbai
• Delivery Time: 2-3 days

Product Details:

Minimum Order : Customer Requirement

Supplier ability : 500 Tons / Tons per week

Payment Terms : L/C , T/T

Material : INCONEL 718 Rod

Standard : ASTM / AISI / JIS / DIN / GB

Length : Cutting for customer Requirement

Hot Rolled Stainless Steel

Payment : Usually 30% of the amount by T/T as deposit and the balance money show be paid by T/T after got the taxed B/L or L/C.

Product Details:

Inconel 718 Rod Bar is just one of the nickel chromium alloys. Inconel 718 Rod Bar is but one of the 12 or so different Inconel alloys have good resistance to oxidation, reducing environments, corrosive environments, high temperature environments, cryogenic temperatures, relaxation resistance and good mechanical properties. Typical applications for Inconel 718 Rod Bar include furnace muffles, electronic components, heat treating equipment, steam generator tubing, heat exchangers, radiant tubes, aircraft engine parts, spray bars, nuclear reactors, hot extrusion tooling, bolts, etc.

Product Details:

INCONEL alloy 718: For most applications, INCONEL alloy 718 is specified as: solution annealed and precipitation hardened . Alloy 718 is hardened by the precipitation of secondary phases (e.g. gamma prime and gamma double-prime) into the metal matrix. The precipitation of these nickel - (aluminum, titanium, niobium) phases is induced by heat treating in the temperature range of 1100 to 1500°F. For a proper metallurgical reaction the aging constituents (aluminum, titanium, niobium) must be in solution. If they are precipitated as some other phase or are combined in some other form, they will not precipitate correctly and the full strength of the alloy with not be achieved. To perform this function the material must first be solution heat treated (solution annealed is a synonymous term). If the material is to be machined, formed, or welded, it typically is purchased in the mill annealed or stress relieved condition. The material is then fabricated in its most malleable condition. After fabrication, it can be heat treated as required per the applicable specification.

Product Details:

General Description:

A Nickel/Chromium alloy with good oxidation resistance at high temperatures. It is resistant to chloride ion stress corrosion cracking, corrosion by pure water and caustic corrosion. Used for furnace components, in chemical and food processing, nuclear engineering and for spark electrodes.

Product Details:

INCONEL® alloy 600 General Description: A Nickel/Chromium alloy with good oxidation resistance at high temperatures. It is resistant to chloride ion stress corrosion cracking, corrosion by pure water and caustic corrosion. Used for furnace components, in chemical and food processing, nuclear engineering and for spark electrodes.

Product Details:

 

Minimum Order : Customer Requirement

Supplier ability : 500 Tons / Tons per week

Payment Terms : L/C , T/T

Material : Inconel 718 Rod

Standard : ASTM / AISI / JIS / DIN / GB

Length : Cutting for customer Requirement

Hot Rolled Stainless Steel plate

Payment : Usually 30% of the amount by T/T as deposit and the balance money show be paid by T/T after got the taxed B/L or L/C.

Product Details:

Inconel 625 Rod
Ragavendra Engineering is the most acclaimed manufacturer, exporter, distributor and supplier of industrial ASTM B637 Inconel 625 Rod with required test certificates. Our material is certified to the highest industry standards. You can also Order small quantities, we will be happy to quote best price for small and large quantities & can typically deliver the ASTM B637 Inconel 625 Rod in minimum time frame anywhere around the globe.Our broad product range makes your individual wishes possible and also meets the extraordinary demands.

Product Details:

Inconel 718 Round BarsRagavendra Engineering is a known stockist of Inconel 718 Round Bars, where the age – hardened condition gives better chip action on chip breaker tools and produces a better finish. Inconel 718 Square Bars accounts for up to 50 % of the weight of aircraft turbojet engines, being the main component for discs, blades and casing of the high pressure section of the compressor and discs as well as some blades of the turbine section. The precipitation of this nickel – (aluminum, titanium, and niobium) phases in Inconel 718 Flat Bars is induced by heat treating in the temperature range of 1100 Degree F to 1500 Degree F. This is the preferred treatment in tensile – limited applications for Inconel 718 Threaded Bars as it produces the best transverse ductility in heavy sections, impact strength and low temperature notch tensile strength. Common Applications of Inconel 718 Hollow Bars: Jet engine components, Oil & gas, and Gas turbine operations. Inconel 718 Hexagonal Bars has good mechanical properties – tensile, fatigue and creep – rupture. Inconel 718 Triangular Bars is often used in aerospace, rocket motors, space shuttles, spacecraft, nuclear reactors, turbo pump seals, tooling and pumps. Inconel 718 Bars has excellent weldability when compared to the nickel – base super alloys hardened by aluminum and titanium. The results indicated that the fine – grained ring forgings can be obtained by forging the fine – grained Inconel 718 Rods.

Product Details:

INCONEL 718 ROUND BARNickel Alloy 718 Round Rods have both high strength properties and good corrosion resistance and weldability. It is commonly used for valves, fasteners, tubing materials and mandrels. Alloy 718 has excellent cryogenic and heat ranges.It is heat treatable, has moderately good corrosion resistance, weldability and formability.

Product Details:

Inconel 625 RAGAVENDRA ENGINEERING Alloys is a leading supplier of Inconel 625. Alloy 625 is a nickel-chromium alloy known and used for corrosion and oxidation resistant, high strength and fabricability. Because of its resistance to corrosion, pressure and heat, Inconel 625 is ideal for applications int the power industry, aerospace, and chemical processing components and hardware and marine industries.RAGAVENDRA ENGINEERING offers Inconel 625 (nickel UNS N06625)in the following sheet, plate and bar:This nickel-based product is supplemented by various alloys and metals that support its performance characteristics. Type analysis specifications are as follows:Carbon: Min. 0/Max. 0.10Chromium: Min. 20.0/Max. 23.0Iron: Min. 0/Max. 5.0Silicon: Min. 0/Max. 0.50Manganese: Min. 0/Max. 0.50Sulfur: Min. 0/Max. 0.015Phosphorus: Min. 0/Max. 0.015Molybendum: Min.8.0/Max. 10.0Titanium: Min. 0/Max. 0.40Cobalt: Min. 0/Max. 1.0Columbium-tantalum alloy: Min. 3.15/Max. 4.15Aluminum: Min. 0/Max. 0.40 Applications Inconel 625 Alloy is frequently used for:Heat shieldsTubingCombustion and chimney linersValvesPipingDistillation columnsBubble capsReaction vesselsHeat exchangersFurnace hardwareGas turbine engine duct workEquipment used to produce acidSour gas production tubesRAGAVENDRA ENGINEERING is also your source for a number of other Inconel alloys, including Inconel 188, Inconel 600, Inconel 718, Inconel X-750 and Haynes 617.

Additional Information:

• Pay Mode Terms: T/T (Bank Transfer)
• Port of Dispatch: CHENNAI
• Production Capacity: I TON PER MONTH
• Delivery Time: 2-3 DAYS

Product Details:

Inconel 718 RodRagavendra Engineering is a known stockist of Inconel 718 Round Bars, where the age – hardened condition gives better chip action on chip breaker tools and produces a better finish. Inconel 718 Square Bars accounts for up to 50 % of the weight of aircraft turbojet engines, being the main component for discs, blades and casing of the high pressure section of the compressor and discs as well as some blades of the turbine section. The precipitation of this nickel – (aluminum, titanium, and niobium) phases in Inconel 718 Flat Bars is induced by heat treating in the temperature range of 1100 Degree F to 1500 Degree F. This is the preferred treatment in tensile – limited applications for Inconel 718 Threaded Bars as it produces the best transverse ductility in heavy sections, impact strength and low temperature notch tensile strength. Common Applications of Inconel 718 Hollow Bars: Jet engine components, Oil & gas, and Gas turbine operations. Inconel 718 Hexagonal Bars has good mechanical properties – tensile, fatigue and creep – rupture. Inconel 718 Triangular Bars is often used in aerospace, rocket motors, space shuttles, spacecraft, nuclear reactors, turbo pump seals, tooling and pumps. Inconel 718 Bars has excellent weldability when compared to the nickel – base super alloys hardened by aluminum and titanium. The results indicated that the fine – grained ring forgings can be obtained by forging the fine – grained Inconel 718 Rods.