Inconel 718 flanges have good resistance to oxidation and corrosion at temperatures within the effective strength range of the alloy in atmospheres encountered in jet engine and gas turbine operation.
ASTM B564 Inconel 718 Threaded Flange Grade 718 Inconel Flange is the most common grade of the hardenable Inconel. This precipitation-hardened nickel-chromium alloy combines outstanding corrosion resistance and high strength at elevated temperatures. The alloy is an about 2x as strong as Inconel grade 625 having excellent creep-rupture strength at temperatures to 1300¡ãF (700¡ãC) and usable up to 1800¡ãF (982¡ãC). Inconel grade 718 is often used in gas turbines, rocket motors, spacecraft, nuclear reactors, pumps, and tooling.
Inconel 718 flanges are constructed of nichrome. The material has the characteristics of high density, high temperature resistance, high acid resistance, high strength and high price. There are different types of flanges with different sizes, dimensions and specifications.
Inconel 718 flanges have excellent mechanical properties, are non-magnetic, and exhibit the required combination of good weldability and high strength over a wide temperature range.
Inconel 718 Blind Flanges provide high strength without heat treatment. Lap flanges have high tensile strength, mechanical strength, fatigue strength and yield strength. Inconel 718 flanges have excellent corrosion resistance properties such as oxidation, corrosion, pitting and crevice corrosion resistance for use in environments.
Inconel 718 is one of the popular grades containing nickel, chromium and molybdenum alloys as well as aluminum, niobium and titanium elements for excellent chemical and mechanical properties. This alloy provides excellent yield and tensile strength at elevated temperatures.
Inconel 718 is a Gamma Prime reinforced alloy with excellent mechanical properties at high temperatures as well as low temperatures up to around 1300 F. It is easy to machine and can be welded in the annealed or aged condition.
Nickel-based Inconel 718 is a precipitation hardening alloy containing iron, molybdenum, niobium, and certain amounts of titanium and aluminum. This superior alloy chemistry provides increased strength and flexibility.
Our Inconel 718 flanges should be machined as rigid and overloaded as possible. These Inconel 718 flanges are used in aerospace applications such as aircraft and rocket engines for many critical components such as blades and sheets.
Inconel 718 flanges are high yield flanges known to maintain their tensile strength even at high temperatures. They are resistant to a variety of severely corrosive environments. The nickel content in these flanges helps them last long in temperatures ranging from cryogenics to 1200°F.
One of the best features of Inconel 718 flange is that it has good mechanical properties such as high tensile strength and strength. Inconel 718 flanges have very high tensile strength at yield, creep and rupture strength properties.
Our 718 Inconel Alloy Flanges are designed in a variety of pressure rating configurations, and these flanges offer excellent features such as robust construction, durability, and high performance.
Inconel Alloy 718 Flanges, which is oxidation resistant throughout its useful temperature range. Machining of our Inconel 718 Slip On Flanges should be rigid and overpowered as much as possible.
Inconel 718 is a nickel-based superalloy ideal for applications requiring high strength in the temperature range from cryogenic to 1400¡ãF. Inconel 718 also has excellent tensile and impact strength.
Inconel 718 has good resistance to oxidation and corrosion at temperatures within the effective strength range of the alloy in the atmospheres encountered in jet engine and gas turbine operation.
Inconel 718 is a nickel-chromium-molybdenum alloy designed to resist a variety of severe corrosive environments, pitting and crevice corrosion. This nickel steel alloy also exhibits extremely high yield, tensile and creep rupture properties at elevated temperatures.
Uses of this nickel alloy range from cryogenics to long-term use at 1200¡ãF. One of the distinguishing features of the Inconel 718 composition is the addition of niobium to allow age hardening, allowing annealing and welding without spontaneous hardening during heating and cooling.
The addition of niobium, along with molybdenum, hardens the matrix of the alloy and provides high strength without the need for a strengthening heat treatment. Other popular nickel-chromium alloys are age hardened by adding aluminum and titanium. This nickel steel alloy is easy to manufacture and can be welded in the annealed or precipitation (age) hardened condition. This superalloy is used in a variety of industries such as aerospace, chemical processing, marine engineering, pollution control equipment and nuclear reactors.
Inconel 625 flanges are made from a corrosion-resistant, high-strength nickel-chromium alloy with a composition of 58% nickel and 20% chromium, as well as carbon, manganese, silicon, sulfur, copper and iron.
