Inconel Series – NEWCORE GLOBAL PVT. LTD http://www.newcoreglobal.com NEWCORE GLOBAL PVT. LTD Fri, 14 Sep 2018 06:53:52 +0000 en-US hourly 1 https://wordpress.org/?v=4.8.7 Inconel 600 http://www.newcoreglobal.com/product/inconel-600/ http://www.newcoreglobal.com/product/inconel-600/#respond Sat, 19 Aug 2017 04:46:32 +0000 http://www.newcore.net.in/?post_type=product&p=1827 Model Number: Inconel 600 Application: Chemical process industry, heat treating fixtures, airframe components and nuclear reactors.]]> Product Detail

Equivalent designations: Inconel 600, UNS N06600, Alloy 600, NS312, NS3102, Nickelvac 600, Ferrochronin 600, DIN W. Nr. 2.4816
Place of Origin: India
Application: Chemical process industry, heat treating fixtures, airframe components and nuclear reactors.

Product list:
Wire: 0.01-10mm
Strip: 0.05*5.0-5.0*250mm
Bar: φ4-50mm; Length 2000-5000mm
Pipe: φ6-273mm; δ1-30mm; Length 1000-8000mm
Sheet: δ 0.8-36mm; Width 650-2000mm; Length 800-4500mm
Specification:
Model Number: Inconel 600
Brand Name: Newcore
Technique: Cold Rolled
Grade: Inconel600/Alloy 600/UNS NO6600
Surface: Black/Bright (According to your request)
Delivery condition: Solution Annealed
Guarantee: We bear all the problems of product quality
Shape: Forging
Standard: ASTM ASME
Certification: ISO 9001:2008
Color: Nickel Nature
Packing: Common sea freight wooden case package/ Also can be customized
Payment: L/C,T/T
Delivery: Usually sample lead time is 7 days after payment has been confirmed.

Technical Information

Inconel 600 has good resistance to corrosion and high temperature, and has high strength and good fabricability. It resists chloride-ion-incurred stress corrosion cracking, sulfur compounds and oxidizing conditions at high temperatures.
1. Chemical composition
2. Physical properties

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Character:

Resistant to a wide range of corrosive media.

Virtually immune to chlorine ion stress corrosion cracking

Non-magnetic

Excellent mechanical properties

High strength and good weldability under a wide range of temperatures

Application: 

Chemical industry

Aerospace

Heat treating industry

Pulp and paper industry

Food processing

Nuclear Engineering

Gas turbine component

 

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Inconel 601 http://www.newcoreglobal.com/product/inconel-601/ http://www.newcoreglobal.com/product/inconel-601/#respond Sat, 19 Aug 2017 04:37:49 +0000 http://www.newcore.net.in/?post_type=product&p=1822 Model Number: INCONEL 601 Grade: INCONEL 601, ALLOY 601, UNS N06601, DIN W. NR. 2.4851]]> Product Detail

Specification:
Model Number: INCONEL 601
Brand Name: Newcore
Grade: INCONEL 601, ALLOY 601, UNS N06601, DIN W. NR. 2.4851
Surface: According to your request
Guarantee: We bear all the problems of product quality
Shape: Forging
Standard: ASTM ASME
Certification: ISO 9001:2008
Color: Nickel Nature
Packing: Common sea freight wooden case package/ Also can be customized
Payment: L/C,T/T
Delivery: Usually sample lead time is 7 days after payment has been confirmed.

Technical Information

1. Chemical composition
2. Physical properties
3. Hot and Cold FormingThe temperature range for hot-forming INCONEL alloy 601 is 1600-2250°F (870-1230°C). Hot-working operations involving large deformations should be performed at 1900-2250°F (1040-1230°C). The alloy has low ductility at temperatures from 1200 to 1600°F (650-870°C) and should not be worked in that range. Light working at temperatures below 1200°F (650°C) can be done to develop high tensile properties. The material was hot-worked from 6-in. (152- mm) diameter rounds to 4-in. (102-mm) squares and air-cooled. Transverse specimens from the centers of the bars were used for the tests. The rate of cooling following hot-working is not critical with respect to thermal cracking. To avoid sensitization, however, the alloy should be cooled rapidly through the 1000-1400°F (540-760°C) temperature range.

4. Machining

All standard machining operations are readily performed on INCONEL alloy 601. For the best machinability, the alloy should be in the solution-treated condition.

5. Joining

INCONEL alloy 601 exhibits good weldability and is readily joined by conventional welding products and processes. Welding products are available which provide high joint efficiencies and heat resistance. The choice of welding product is dependent upon the service conditions to which the fabricated alloy 601 component will be exposed.

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1. Character

Alloy 601 has good resistance to heat and corrosion, especially outstanding to oxidation at elevated temperatures up to 1200℃. It also has high strength, good fabricability and good resistance to aqueous corrosion.

2. Application 

Chemical process industry

Waste incinerators

Power generation equipment

Feat treating equipment

Gas turbine engine components

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Inconel 617 http://www.newcoreglobal.com/product/inconel-617/ http://www.newcoreglobal.com/product/inconel-617/#respond Sat, 19 Aug 2017 04:30:31 +0000 http://www.newcore.net.in/?post_type=product&p=1817 Model Number: INCONEL 617 Grade: INCONEL 617, ALLOY 617, UNS N06617, DIN W. NR. 2.4663A]]> Product Detail

Specification:

Model Number: INCONEL 617
Brand Name: Newcore
Grade: INCONEL 617, ALLOY 617, UNS N06617, DIN W. NR. 2.4663A
Surface: According to your request
Guarantee: We bear all the problems of product quality
Shape: Forging
Standard: ASTM ASME
Certification: ISO 9001:2008
Color: Nickel Nature
Packing: Common sea freight wooden case package/ Also can be customized
Payment: L/C,T/T
Delivery: Usually sample lead time is 7 days after payment has been confirmed.

Technical Information

1. Chemical composition
2. Physical properties
3. Hot and Cold FormingAlloy 617 has good hot formability, but it requires relatively high forces because of its inherent strength at elevated temperatures. In general, the hot-forming characteristics of alloy 617 are similar to those of INCONEL alloy 625. The temperature range for heavy forming or forging is 1850 to 2200°F (1010 to 1205°C). Light working can be done at temperatures down to 1700°F (925°C). INCONEL alloy 617 is readily cold formed by conventional procedures although its work-hardening rate. For best results, the alloy should be cold formed in the fine-grain condition, and frequent intermediate anneals should be used. Annealing for cold forming should be done at 1900°F (1040°C).4. Heat TreatmentINCONEL alloy 617 is normally used in the solutionannealed condition. That condition provides a coarse grain structure for the best creep-rupture strength. It also provides the best bend ductility at room temperature. Solution annealing is performed at a temperature of 2150°F (1175°C) for a time commensurate with section size. Cooling should be by water quenching or rapid air cooling.

5. Machining

Cutting tools should be sharp and have positive rake angles to minimize work hardening of the material. Cutting feed and depth of cut must be sufficient to prevent burnishing of the workpiece surface.

6. Joining

INCONEL alloy 617 has excellent weldability. INCONEL Filler Metal 617 is used for gas-tungsten-arc and gas-metalarc welding while INCONEL Welding Electrode 117 is used for shielded metal-arc welding. The composition of the filler metal matches that of the base metal, and deposited weld metal is comparable to the wrought alloy in strength and corrosion resistance.

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1. Character

Alloy 617 has excellent resistance to oxidation and carburization at high temperatures. It also resists a wide range of corrosive aqueous environments. Alloy 617 has high strength and maintains much of its strength at elevated temperatures.

2. Application 

Gas turbine engine combustion cans and ducts

Heat treating equipment

Petrochemical processing

Power plant equipment

Catalyst-grid supports in nitric acid production

 

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Inconel 625 http://www.newcoreglobal.com/product/inconel-625/ http://www.newcoreglobal.com/product/inconel-625/#respond Sat, 19 Aug 2017 04:22:30 +0000 http://www.newcore.net.in/?post_type=product&p=1812 Model Number: Inconel 625 Application: Chemical processing, specialized seawater equipment, pulp and paper production.]]> Product Detail

Equivalent designations: Inconel 625, UNS N06625, DIN W. Nr. 2.4856, Alloy 625, NS336, NS3306, NiCr22Mo9Nb
Place of Origin: India
Application: Chemical processing, specialized seawater equipment, pulp and paper production.
Product list:

Specification:

Wire: 0.01-10mm
Strip: 0.05*5.0-5.0*250mm
Bar: φ4-50mm;Length 2000-5000mm
Pipe: φ6-273mm;δ1-30mm;Length 1000-8000mm
Sheet: δ0.8-36mm;Width 650-2000mm;Length 800-4500mm
Model Number: Inconel 625
Brand Name: Newcore
Shape: Forging
Standard: ASTM ASME
Certification: ISO 9001:2008
Color: Nickel Nature
MOQ: 500kg
Packing: Common sea freight wooden case package/ Also can be customized
Payment: L/C,T/T
Delivery: Usually sample lead time is 7 days after payment has been confirmed.

Technical Information

Inconel 625 has excellent strength at temperatures up to 816℃. At higher temperatures, its strength is generally lower than that of other solid solution strengthened alloys. Inconel 625 has good oxidation resistance at temperatures up to 980℃ and shows good resistance to aqueous corrosion, but is relatively moderate compared to other more capable corrosion resistant alloys.

1. Produces process
Raw material→ Smelting→ Drawing→ Rolling→ Annealing→ Finished product→ Detection→ Packing→ Shipping
2. Chemical composition
3. Physical properties

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1. Characters

High creep-rupture strength

Oxidation resistant to 1800°F

Seawater pitting and crevice corrosion resistant

Immune to chloride ion stress corrosion cracking

Non-magnetic

2. Application 

Chemical process industry and sea water application. Inconel 625 is used in short term applications at temperatures up to 816℃. For long term service, it is best restricted to a maximum of 593℃, because long term exposure above 593℃ will result in significant embrittlement.

1. Aircraft ducting systems

2. Aerospace

3. Jet engine exhaust systems

4. Engine thrust-reverser systems

5. Specialized seawater equipment

6. Chemical process equipment

 

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Inconel 718 http://www.newcoreglobal.com/product/inconel-718/ http://www.newcoreglobal.com/product/inconel-718/#respond Sat, 19 Aug 2017 04:04:37 +0000 http://www.newcore.net.in/?post_type=product&p=1806 Grade: ALLOY 718, UNS N07718, DIN W. NR. 2.4668 Surface: According to your request]]> Product Detail
Specification:
Inconel 718 alloy is a body-centered tetragonal γ “and a face-centered cubic γ ‘phase precipitation strengthened nickel-based superalloy, has a good overall performance in the temperature range of -253 ~ 700 ℃, 650 ℃ below the yield strength of the Habitat modification the first high-temperature alloys, and has a good anti-fatigue, anti-radiation, anti-oxidation, corrosion resistance, and good processing properties, welding performance and long-term organizational stability, capable of producing complex parts of various shapes in space, nuclear energy , the oil industry, obtained in the above temperature range a very wide range of applications.
Another characteristic of this alloy is Alloy particularly sensitive to thermal processing, master alloy phase precipitation and dissolution of the relationship between law and technology organization, performance, and between, you can make reasonable and feasible technical rules for different requirements, it is can be obtained to meet the different intensity levels and use requirements of the various parts. There are varieties of supply forgings, forged bars, roll bars, cold-rolled bars, round cake, rings, plates, strips, wire, tube and so on. It can be made into plates, rings, blades, shafts, fasteners and elastic components, sheet metal structural parts, casing and other components of long-term use in aviation.
Brand Name: Newcore
Grade: ALLOY 718, UNS N07718, DIN W. NR. 2.4668
Surface: According to your request
Guarantee: We bear all the problems of product quality
Shape: Round
Standard: ASTM ASME
Certification: ISO 9001:2008
Color: Nickel Nature
Packing: Common sea freight wooden case package/ Also can be customized
Payment: L/C,T/T
Delivery: Usually sample lead time is 7 days after payment has been confirmed.

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1. Character

Alloy 718 is an age-hardenable Alloy-chromium alloy that combines corrosion resistance with high strength and good fabricability. It has high creep-rupture strength at temperatures up to 700 OC. Its excellent relaxation resistance contributes to its application in springs.

2. Application 

Gas turbine engines

Rocket motors

Nuclear reactors

Spacecraft

 

3. Hot Forming

Because of its strength, INCONEL alloy 718 is more resistant than most materials to deformation during hot forming. It is readily hot-worked if sufficiently powerful equipment is used. Hot forming is performed in the 1650°-2050°F temperature range. In the last operation, the metal should be worked uniformly with a gradually decreasing temperature, finishing with some light reduction in the 1650°-1750°F range. This procedure is necessary to ensure notch ductility in stress-rupture applications when material has been annealed and aged. In heating for hot working, the material should be brought up to temperature, allowed to soak a short time to ensure uniformity, and withdrawn. To avoid duplex grain structure INCONEL alloy 718 should be given uniform reductions. Final reductions of 20% minimum should be used for open-die work and 10% minimum for closed-die work. Parts should generally be aircooled from the hot-working temperature rather than waterquenched. Care should be taken to avoid overheating the metal by heat buildup due to working. Also, the piece should be reheated when any portion has cooled below 1650°F. Preheating tools and dies to 500°F is recommended. Any ruptures appearing on the surface of the workpiece must be removed at once. Following annealing and aging, specimens were rupturetested at 1200°F and 100 ksi. Success in achieving notchrupture ductility with forgings of alloy 718 through this type of procedure has also been reported by others.

4. Cold Forming 

INCONEL alloy 718 can be cold-formed by standard procedures used for steel and stainless steel.

5. Machining

INCONEL alloy 718 can be readily machined, but its high strength and work-hardening characteristics must be considered in the selection and use of proper tool materials and design, operating speeds, and coolants. When machined in the age-hardened condition the alloy will have a slightly better finish; chip action on chipbreaker tools will be better. The use of annealed material, however, provides easier machining and longer tool life.

6. Super-Plastic Forming

This alloy, designated INCONEL alloy 718SPF, is available as annealed sheet in thicknesses from 0.02 to 0.08 inches (0.5 to 2.0 mm) in widths up to 36 inches (914 mm). The specification SAE AMS 5950 was developed to define the requirements for the alloy.

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Inconel X750 http://www.newcoreglobal.com/product/inconel-x750/ http://www.newcoreglobal.com/product/inconel-x750/#respond Sat, 19 Aug 2017 03:58:38 +0000 http://www.newcore.net.in/?post_type=product&p=1800 Grade: INCONELX-750, GH4145, N07750, NCF750B, 2.4669 Surface: According to your request]]> Product Detail
Specification:
Inconel X-750 alloy are mainly γ ‘[Ni3 (Al, Ti, Nb)] aging phase strengthened nickel-base superalloy, below 980 ℃ with good resistance to corrosion and oxidation resistance below 800 ℃ has higher strength below 540 ℃ has good resistance to relaxation properties, but also has good formability and weldability. The plane of the alloy is mainly used in the manufacture of aircraft engines, work in the following 800 ℃ and require higher strength corrosion-resistant annular member, structural parts and bolts and other parts, in the following 540 ℃ working with medium or low resistance to stress and relaxation of requirements springs and coil springs. It can also be used in the manufacture of gas turbine blades and other turbine parts. We can supply varieties of sheet, strip, bar, forgings, ring member, wire and tubing.
Brand Name: Newcore
Grade: INCONELX-750, GH4145, N07750, NCF750B, 2.4669
Surface: According to your request
Guarantee: We bear all the problems of product quality
Shape: Forging
Standard: ASTM ASME
Certification: ISO 9001:2008
Color: Nickel Nature
Packing: Common sea freight wooden case package/ Also can be customized
Payment: L/C,T/T
Delivery: Usually sample lead time is 7 days after payment has been confirmed.

1. Character

Alloy X750 is an age-hardenable Alloy-chromium alloy. It has good corrosion and oxidation resistance and high strength at temperatures up to 700 OC. It also has good properties down to cryogenic temperatures. Its corrosion resistance performance is similar to Alloy 600.

2. Application 

Gas turbine engines

Rocket motors

Heat treating fixtures

Nuclear reactors

Pressure vessels and airframes

3. Heating and Pickling

Heating: To avoid thermal cracking, localized heating is not recommended. The entire part should be heated to the hot-working temperature. Alloy X-750 should be air-cooled after heating. Liquid quenching is not recommended, particularly for large sections or complex parts because it can set up stresses that may cause thermal cracking during subsequent heating. Very large sections may require furnace cooling. The heat treatments most often used for alloy X-750 have been identified in the section on Mechanical Properties. When heated at intermediate temperatures (in the range of about 900° to 1600°F), INCONEL alloy X-750, like other precipitation-hardenable alloys, is hardened rather than softened. If annealed or solution-treated alloy X-750 is placed in service in this temperature range (although this is not usually done), the alloy will harden and contract slightly. In addition, ductility is lowered if alloy X-750 is exposed in this range under stress. Optimum schedules for precipitation hardening are given in the section on Mechanical Properties. Depending on end use, material can be precipitation-treated in the solution-treated, annealed, hot-worked, or cold-worked condition. For service below about 1100°F, in some cases higher strength is obtained by combining some cold work with precipitation treating. Heat treatments used in conjunction with welding alloy X-750 are discussed later under “Joining”.

4. Pickling

Heat-treated INCONEL alloy X-750, like nickelchromium alloys in general, forms oxide films even when heated and cooled in atmospheres that keep other types of alloys bright. (It can be bright-annealed only in very dry hydrogen or argon, or in a vacuum.) Oxide or scale is therefore the usual surface condition for pickling. Pretreatment in a fused salt bath is strongly recommended for most effective removal of scale. A nitric-hydrofluoric acid pickling bath, however, can be employed directly for removal of some types of scale. INCONEL alloy X-750 is subject to intergranular attack in this solution, particularly if the alloy is in the precipitation-hardened condition. Time in bath should be kept to a minimum. Bath temperature is critical; maximum temperature should not exceed 125°F. The pickling tank must be properly ventilated because the fumes are toxic. For appropriate pickling procedures refer to the “Fabricating” publication mentioned above. Scale can be successfully mechanically removed by barrel tumbling, fine-grit and vapor blasting.

5. Fabricating

INCONEL alloy X-750 is readily fabricated by processes common to industry. Procedures and tools must be selected that will be appropriate for its high strength and characteristic strain-hardening rates.

Hot Forming: Sufficiently powerful equipment is important when hot-forming alloy X-750 because of its resistance to deformation. The recommended temperature range for hot working alloy X-750 is 1800°-2200°F range. All heavy hot working should be done above 1900°F. Forgings can be finished with some light reduction in the 1800°-1900°F range. Below 1800°F the metal is stiff and hard to move, and attempts to work it may cause splitting. Steam hammers are well suited for working INCONEL alloy X-750 since the work can be handled rapidly with a minimum of chilling. When the alloy is forged on presses, the metal is in contact with the dies or blocks for a relatively long time, and the surface layers may be chilled to temperatures below the correct hot-working range. The work should be reheated as often as may be needed to maintain uniform temperature throughout the piece and to avoid rupture arising from localized chilling. Approximately 20% final reduction should be done below 2000°F to ensure meeting the requirements of AMS 5667, 5670, 5671, and 5747.

Cold Forming: INCONEL alloy X-750 is successfully cold-formed by a variety of processes. To guard against rupturing, care must be taken to incorporate sufficient anneals when a forming operation consists of successive reductions.

6. Machining

INCONEL alloy X-750 is machined at practical and economical rates. Because of precipitation-hardened alloy X-750’s high strength and hardness, rough machining is usually done before precipitation hardening. Finish machining then follows precipitation treating. Precipitation hardening relieves machining stresses; therefore, allowance must be made for possible warpage. A slight permanent contraction takes place during precipitation treating, but precipitation treated material has good dimensional stability. Accurate dimensions and a good finish will result from following these practices.

7. Joining 

Welding processes recommended for alloy X-750 are gastungsten-arc, plasma-arc, electron-beam, resistance, and pressure-oxyacetylene welding. In welding INCONEL alloy X-750 by the gas-tungstenarc process, INCONEL Filler Metal 718 is used. Joint efficiencies are nearly 100% at room temperature and 80% at 1300°-1500°F, based on the results of stress-rupture tests.

Alloy X-750 should be in the annealed or solutiontreated condition prior to welding. It is possible to weld it when it is in the precipitation-treated condition, but neither the weld or the heat-affected zone should be subsequently precipitation-treated or exposed to service temperatures within the precipitation-hardening temperature range because of the danger of parent-metal cracking. If alloy X- 750 has been precipitation-hardened and then welded and is expected to be exposed to precipitation-treating temperatures during service, the weldment should be annealed or solution-treated and re-precipitation-treated. In all cases, care must be taken during assembling and welding to minimize high stresses. Alloy X-750 weldments should be solution-treated prior to precipitation treating. Rate of heating of the weldment up to temperature must be fast and uniform to keep to a minimum time of exposure to temperatures in the precipitation-hardening range. The most practical means of obtaining the rapid heating rate is to charge the fabricated part to a preheated furnace. Sometimes preweld heat treatments will be beneficial – in cases where material to be welded is in restraint or if the weldment is complex, and especially if the assembly is too complicated for carrying out a postweld anneal. Two preweld treatments that have been proved effective are: 1. 1550°F/16 hr, A.C. 2. 1950°F/1hr, F.C. at a rate of 25°-100°F/hr to 1200°F, A.C. Repair welding of parts that have been in service should be followed by solution treating (heating rapidly through the precipitation-hardening range) and re-precipitation treating. Interbead or interlayer cleaning must be provided to remove the oxide films that form during welding. (Complete protection of the weld metal by gas-shielded processes is difficult to achieve.) If these films are not removed periodically, they can become sufficiently heavy to interfere with proper fusion and reduce joint strength. Power wire brushing serves only to polish the oxide surface; the weld bead must be abrasive-blasted or -ground. Frequency of cleaning depends on how much oxide has accumulated. All grit must be removed before welding is resumed. INCONEL alloy X-750 may be brazed by conventional procedures using many of the commercial brazing alloys. Precipitation treating, if desired, must take place after brazing; therefore, an alloy should be selected that melts above precipitation-treating temperatures. Nickel-base brazing alloys are particularly useful with alloy X-750. Alloy X-750 is readily joined by spot, projection, seam, and flash resistance welding processes. Equipment must be of adequate capacity. In general, alloy X-750 is resistance welded in the annealed or solution-treated condition.

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