Inconel Wire

Product Details:

Super alloys are also called high performance alloys. They contain a number of elements in a variety of combinations to reach the desired result. These alloys can function in environments with high temperatures and severe mechanical stress, and also in cases where high surface stability is needed. Super alloys have good creep and oxidation resistance.

Strengthening of super alloys is performed by work hardening, solid-solution hardening, and precipitation hardening methods.

Nimonic Alloy 263™ is a British nickel-chromium-cobalt-molybdenum alloy specially meant for use in high temperature and high strength applications. This alloy can be precipitation-hardened.

The following datasheet will provide more details about Nimonic Alloy 263™.

Chemical Composition:

The following table shows the chemical composition of Nimonic Alloy 263™.

Physical Properties:

The physical properties of Nimonic Alloy 263™ are outlined in the following table.

Mechanical Properties:

The mechanical properties of Nimonic Alloy 263™ are provided below.

Product Details:

As a quality oriented enterprise, we are providing a range of Inconel 725 Wire.

Specifications:

• Usage: used for making fence of agricultural field
• Size: Customized

Features:

• Perfect strength
• Rust resistance
• Sturdy structure

Product Details:

Applications:
Springs operating from cryogenic temperatures up to 1300°F (704°C), fasteners and components requiring resistance to high temperature and corrosive environments.

Inconel® X750 is a precipitation hardenable Nickel-Chromium alloy with high strength at temperatures up to 1300°F (704°C) and oxidation resistance up to 1800°F (982°C). Inconel® X750 offers excellent resistance to relaxation and as a result it is widely used for springs operating at elevated temperatures.

Industries Supplied:
Oil & Gas Extraction and Processing, Nuclear, Aerospace, Power Generation and Automotive

Nominal Composition:

• Ni: 70.0 min
• Cr: 14.0 - 17.0
• Fe: 5.0 - 9.0
• Ti: 2.25 - 2.75
• Al: 0.40 - 1.0
• Cb (Nb): 0.70 - 1.20
• Mn: 1.0
• Si: 0.50 max
• C: 0.08 max
• S: 0.01 max
• Cu: 0.5 max

Physical Properties:

• Density: 0.299 lb/in3, (8.28 g/cm3)
• Modulus of Elasticity (E):
• At 70°F (20°C): 31.0 x 106 psi (214 GPa)
• At 1000°F (538°C): 26.7 x 106 psi (184 GPa)
• Modulus of Rigidity (G):
• At 70°F (20°C): 12.0 x 106 psi (82.7 GPa)
• Coefficient of Expansion:
• 7.8 µin/in.-°F (70°F to 1000°F)
• 14.5 µm/m-°C (20°C to 538°C)
• Electrical Resistivity: 20.1 µΩ.in, (122 µΩ.cm)
• Thermal Conductivity: 83 Btu-in/ft2hr-°F, (12.0 W/m-K)
• Applicable Specifications Wire:
• AMS 5698, AMS 5699, AMS 5778, NACE MR0175 (ISO 15156-3), ASTM B637, AMS 5667, AMS 5668, AMS 5670
• Typical Mechanical Properties – Spring Applications

Annealed

• Heat Treatment: 2000 - 2200°F (1093 - 1204°C)
• Tensile Strength: 130 ksi max; (896 MPa) max

No.1 Temper

• Heat Treatment: As supplied condition.
• Tensile Strength: 130 – 165 ksi; (896 – 1138 MPa)

• Heat Treatment: After spring coiling. Age: 1350°F (732°C) for 16 hours.

Tensile Strength: 165 - 220 ksi (1138 - 1517 MPa)

• Suggested Operating Conditions: Optimum resistance to relaxation at temperatures up to 1000°F (538°C) with moderate or low stresses.

Spring Temper

• Heat Treatment: As supplied condition.
• Tensile Strength: 160 - 220 ksi; (1103 - 1517 MPa)

Spring Temper + Aged

• Heat Treatment: After spring coiling. Age: 1200°F (649°C) for 4 hours.
• Tensile Strength: 180 - 250 ksi; (1241-1793 MPa)

• Suggested Operating Conditions: Optimum stress and low relaxation at temperatures up to 700°F (371°C)

Spring Temper + Solution + Aged (3 Step Heat treatment)

• Heat Treatment: After spring coiling. Solution Heat Treat: 2100°F (1149°C) for 2 hours and air cool. Age Harden at 1550°F (843°C) for 24 hours and air cool. Reheat to 1300°F(704°C) for 20 hours and air cool.
• Tensile Strength: 145 - 190 ksi; (1000-1310 MPa)

• Suggested Operating Conditions: Optimum resistance to relaxation at temperatures in the range 1000 – 1300°F (538 – 704°C).

Additional Information:

• Item Code: InconelX750SpringWire_UNS_N07750

Product Details:

INCONEL alloy X-750 (UNS N07750/W. Nr. 2.4669) is a precipitation-hardenable nickel-chromium alloy used for its corrosion and oxidation resistance and high strength at temperatures to 1300°F. Although much of the effect of precipitation hardening is lost with increasing temperature over 1300°F, heat-treated material has useful strength up to 1800°F. Alloy X-750 also has excellent properties down to cryogenic temperatures.

The economics of INCONEL alloy X-750 coupled with its availability in all standard mill forms has resulted in applications in a wide variety of industrial fields. In gas turbines, it is used for rotor blades and wheels, bolts, and other structural members. INCONEL alloy X-750 is used extensively in rocket-engine thrust chambers. Airframe applications include thrust reversers and hot-air ducting systems. Large pressure vessels are formed from INCONEL alloy X-750. Other applications are heat-treating fixtures, forming tools, extrusion dies, and test machine grips. For springs and fasteners, INCONEL alloy X-750 is used from sub-zero to 1200°F.

Depending on the application and the properties desired, various heat treatments are employed. For service above 1100°F, particularly where loads are to be sustained for long times, optimum properties are achieved by solution treating (2100°F) plus stabilisation treating (1550°F) plus precipitation treating (1300°F). For service below 1100°F, the alloy may be strengthened by precipitation treating after hot or cold working or by precipitation treating after equalising or solution treating. A furnace-cooling treatment is also used to develop optimum properties for some applications.

The various heat treatments and the properties developed are described under the section on Mechanical Properties.

Property values in this bulletin – the results of extensive testing – are typical of the alloy but, unless shown as limiting, should not be used as specification values.

Limiting Chemical Composition (%)

• Nickel (plus Cobalt) …………………………. 70.00 min.
• Chromium ……………………………………….14.0-17.0
• Iron……………………………………………………………………….5.0-9.0
• Titanium……………………………………………………………..2.25-2.75
• Aluminum…………………………………………………………..0.40-1.00
• Niobium (plus Tantalum)……………………………………….0.70-1.20
• Manganese………………………………………………………..1.00 max.
• Silicon……………………………………………………………….0.50 max.
• Sulfur……………0.01 max.
• Copper……………0.50 max.
• Carbon… ………0.08 max.
• Cobalt1 ………….1.00 max

Product Details:

Inconel 800, 800h, and 800ht are nickel-iron-chromium alloys having high resistance to carburization and oxidation in high-temperature exposure and with good strength. These nickel steel alloys are identical except for the higher level of carbon in alloy 800h, and the addition of up to 1. 20 % aluminum and titanium in alloy 800ht.

Incoloy 800 was the first of these alloys and it was slightly modified into incoloy 800h. The modification made was to control carbon (. 05-. 10%) and grain size to optimize stress rupture properties. Incoloy 800ht has more modifications to the combined aluminum and titanium levels (. 85-1. 20%) to ensure optimum high temperature properties.

The nickel alloy is dual certified (800h/ht) and combines the properties of both forms. Incoloy 800h/ht alloy was actually meant for high-temperature structural applications. These alloys are resistant to embrittlement from precipitation of sigma phase and chloride stress-corrosion cracking due to the nickel content. The corrosion resistance is quite high.

In the solution annealed condition, alloys 800h and 800ht have excellent creep and stress rupture properties. The dual certified 800h/ht alloy is commonly available also with mega mex.

Incoloy 800 is mainly used in applications with temperatures up to 1100° f, where alloys 800h and 800ht are normally used in temperatures above 1100° f where resistance to creep and rupture is required. The chemical balance allows the nickel steel alloy to exhibit excellent resistance to carburization, oxidation and nitriding atmospheres.

Incoloy 800ht will not become embrittled even after long periods of usage in the 1200-1600° f range where many stainless steels become brittle.

Product Details:

The limiting chemical composition of INCONEL alloy 617 is listed in Table 1. The high nickel and chromium contents make the alloy resistant to a variety of both reducing and oxidizing media. The aluminum, in conjunction with the chromium, provides oxidation resistance at high temperatures. Solid-solution strengthening is imparted by the cobalt and molybdenum.

The combination of high strength and oxidation resistance at temperatures over 1800°F (980°C) makes INCONEL alloy 617 an attractive material for such components as ducting, combustion cans, and transition liners in both aircraft and land-based gas turbines. Because of its resistance to high-temperature corrosion, the alloy is used for catalyst-grid supports in the production of nitric acid, for heat-treating baskets, and for reduction boats in the refining of molybdenum. INCONEL alloy 617 also offers attractive properties for components of power-generating plants, both fossilfueled and nuclear.

Limiting Chemical Composition, %, of INCONEL alloy 617

• Nickel…………………………………………………………………44.5 min.
• Chromium…………………………………………………………..20.0-24.0
• Cobalt………………………………………………………………..10.0-15.0
• Molybdenum ………………………………………………………..8.0-10.0
• Aluminum………………………………………………………………0.8-1.5
• Carbon ………………………………………………………………0.05-0.15
• Iron……………………………………………………………………..3.0 max.
• Manganese ………………………………………………………….1.0max.
• Silicon …………………………………………………………………1.0 max.
• Sulfur ………………………………………………………………0.015 max.
• Titanium………………………………………………………………0.6max.
• Copper………………………………………………………………..0.5 max.
• Boron ………………………………………………………………0.006 max.

Product Details:

High tensile, creep, and rupture strength; outstanding fatigue and thermal-fatigue strength; oxidation resistance; and excellent weldability and brazeability are the properties of INCONEL alloy 625 that make it interesting to the aerospace field. It is being used in such applications as aircraft ducting systems, engine exhaust systems, thrust-reverser systems, resistancewelded honeycomb structures for housing engine controls, fuel and hydraulic line tubing, spray bars, bellows, turbine shroud rings, and heat-exchanger tubing in environmental control systems. It is also suitable for combustion system transition liners, turbine seals, compressor vanes, and thrust-chamber tubing for rocket.

The outstanding and versatile corrosion resistance of INCONEL alloy 625 under a wide range of temperatures and pressures is a primary reason for its wide acceptance in the chemical processing field. Because of its ease of fabrication, it is made into a variety of components for plant equipment. Its high strength enables it to be used, for example, in thinner-walled vessels or tubing than possible with other materials, thus improving heat transfer and saving weight. Some applications requiring the combination of strength and corrosion resistance offered by INCONEL alloy 625 are bubble caps, tubing, reaction vessels, distillation columns, heat exchangers, transfer piping, and valves.

Limiting Chemical Composition, %

• Nickel…………………………………………….…………58.0 min.
• Chromium………………………………………..…………20.0-23.0
• Iron………………………………………………..………….5.0 max.
• Molybdenum……………………………….…………………8.0-10.0
• Niobium (plus Tantalum)………………………..………….3.15-4.15
• Carbon……………………………………………..……….0.10 max.
• Manganese………………………………………….……….0.50 max.
• Silicon……………………………….………………………0.50 max.
• Phosphorus……………………………………….………..0.015 max.
• Sulfur…………………………………..……….…..……..0.015 max
• Aluminum…………………………………………………..0.40 max.
• Titanium……………………………….……………………0.40 max.
• Cobalta ……………………………………………………….1.0 max.

Additional Information:

• Item Code: Inconel625Wire

Product Details:

INCONEL® (nickel-chromium-iron) alloy 600 (UNS N06600/W.Nr. 2.4816) is a standard engineering material for applications which require resistance to corrosion and heat. The alloy also has excellent mechanical properties and presents the desirable combination of high strength and good workability.

The limiting chemical composition of INCONEL alloy 600 is shown in Table 1. The high nickel content gives the alloy resistance to corrosion by many organic and inorganic compounds and also makes it virtually immune to chloride-ion stress-corrosion cracking. Chromium confers resistance to sulfur compounds and also provides resistance to oxidizing conditions at high temperatures or in corrosive solutions. The alloy is not precipitation hardenable; it is hardened and strengthened only by cold work.

The versatility of INCONEL alloy 600 has led to its use in a variety of applications involving temperatures from cryogenic to above 2000°F (1095°C).

The alloy is used extensively in the chemical industry for its strength and corrosion resistance. Applications include heaters, stills, bubble towers and condensers for processing of fatty acids; evaporator tubes, tube sheets and flaking trays for the manufacture of sodium sulfide; and equipment for handling abietic acid in the manufacture of paper pulp.

The alloy’s strength and oxidation resistance at high temperatures make it useful for many applications in the heat-treating industry. It is used for retorts, muffles, roller hearths and other furnace components and for heat-treating baskets and trays.

 

INCONEL alloy 600 is used in the electronic field for such parts as cathode-ray tube spiders, thyratron grids, tube support members and springs. The alloy is a standard material of construction for nuclear reactors. It has excellent resistance to corrosion by high-purity water, and no indication of chloride-ion stress-corrosion cracking in reactor water systems has been detected. For nuclear applications, the alloy is produced to exacting specifications and is designated INCONEL alloy 600T.

Chemical Composition:

• Nickel (plus Cobalt)…………………………………………….72.0 min.
• Chromium…………………………………………………………14.0-17.0
• Iron ………………………………………………………………..6.00-10.00
• Carbon …………………………………………………………….0.15 max.
• Manganese……………………………………………………….1.00max
• Sulfur……………………………………………………………..0.015 max.
• Silicon……………………………………………………………..0.50max.
• Copper…………………………………………………………….0.50 max