Forged Blocks

Product Details:

Super alloys have good creep and oxidation resistance, and can be formed in different shapes. They contain a number of elements in a variety of combinations to achieve the desired result, and can function at very high temperatures and mechanical stress. They are classified into three groups such as nickel-based, iron-based and cobalt-based alloys.

Nimonic 90™ is a nickel-chromium-cobalt alloy which can be strengthened by adding aluminum and titanium.

Chemical Composition:

The following table shows the chemical composition of Nimonic 90™.

Physical Properties:

The physical properties of Nimonic 90™ are outlined in the following table.

Additional Information:

• Item Code: Nimonic_90_UNSN07090_AMS5829_DIN24632_ForgedBlock

Product Details:

We are remarkable entity, engaged in offering superior quality Inconel 625 Forged Block.

Specifications:

• Material: stainless steel
• Size: As per client’s need

Features:

• Rust proof
• Robustness
• High strength

Product Details:

90/10 cupronickel is a 90% copper, 10% nickel alloy that also contains small but important additions of iron and manganese to enhance overall strength corrosion resistance. This, combined with high ductility and toughness, makes it a popular grade for marine, architectural and industrial applications.

90/10 alloy offers designers and specifiers excellent resistance to stress corrosion, erosion, and biofouling in seawater and brackish water, excellent fabrication and welding properties, a high resistance to hydrogen embrittlement and the retention of mechanical properties down to cryogenic temperatures.

The material is released to the Defence Standard DEF STAN 02-879 Annex C, which supersedes both DEF STAN 02-779 and NES 779.

The most popular specifications in Europe and America are C70600, CN102 and CW352. These grades are most commonly specified within the marine, offshore, chemical, petrochemical and shipbuilding industries and are also widely used for handling seawater in all types of heat exchanger and cooling plant.

90/10 has undergone tests that indicate it has excellent antimicrobial properties. It is capable of killing 99.9% of a wide range of organisms within two hours, including MRSA, E.coli, influenza A (H1N1) and clostridium difficile. This has created a higher demand for the alloy in application areas such as hygienic and sanitary environments in hospitals, kitchens, nursing homes and other healthcare environments.

Related Specifications of 90/10

• CN102
• C70600
• C70610
• CW352H
• DEF STAN 02-879 Annex C
• DEF STAN 02-779
• NES 779
• BS2870
• BS2874
• ASTM B151
• EN 12163
• 2.0872
• NF A51-115
• CuNi10Fe1Mn

Nominal Composition of 90/10

Cu rem, Ni 10.0%, Fe 1.5%, Mn 0.7%

Mechanical Properties of 90/10
Key Features of 90/10:

• High ductility and toughness
• Excellent resistance to erosion and corrosion in seawater
• Inherent resistance to biofouling
• Excellent fabrication and welding properties
• Retention of mechanical properties down to cryogenic temperatures

Product Details:

Nimonic 80A alloy is a nickel-chromium alloy that is strengthened by the additions of titanium and aluminum. It has high tensile and creep-rupture properties at temperatures up to 815°C (1500°F).

The following datasheet will provide an overview of nimonic 80A alloy.

Chemical Composition:

The chemical composition of nimonic 80A alloy is outlined in the following table.

Physical Properties:

The following table shows the physical properties of nimonic 80A alloy.

Mechanical Properties:

The mechanical properties of nimonic 80A alloy are displayed in the following table.

Thermal Properties:

The thermal properties of nimonic 80A alloy are given in the following table.

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:

Being a notable enterprise of this industry, we are offering a wide range of 15-5 PH SS Forged Block.

Specifications:

• Size: As per client’s need
• Usage: used in construction industry

Features:

• Optimum durability
• High strength
• Rust resistance

Composition:

• Carbon 0.07 max.
• Manganese 1.00max.
• Phosphorus 0.040 max.
• Sulfur 0.030 max.
• Silicon 1.00 max.
• Chromium 14.00 - 15.50
• Nickel 3.50 - 5.50
• Copper 2.50 - 4.50
• Columbium plus Tantalum 0.15 - 0.45

Additional Information:

• Item Code: SS15-5_PH_ForgedBlock
• Pay Mode Terms: L/C (Letter of Credit),T/T (Bank Transfer),D/P,D/A,Other
• Port of Dispatch: Mumbai
• Production Capacity: 500 MT per month
• Delivery Time: 2 Day
• Packaging Details: As Per Request....

Product Details:

T630 is a 17-4 PH martensitic precipitation hardening stainless steel with a unique combination of high strength and good corrosive resistance. Supplied in either the H1075 (H580) aged condition with a tensile strength of 1000 Mpa minimum (HB 311 min.), or the H1150 (H620) double aged condition with a tensile strength of 930 Mpa minimum (HB 277 min.). It is characterised by high tensile strength and high yield strength obtained by solution annealing, followed by a single or double low temperature (precipitation) age hardening treatment. Coupled with a corosion resistance comparable to 304 austenitic stainless steel in many corrosive environments.630 in the H1075 (H580) aged condition can be re-aged if necessary at a higher temperature simply by heating at the required temperature for the required duration. 630 in the H1075 (H580) And H1150 (H620) aged condition, can also be re-aged at a lower temperature by re-solution annealing, followed by age hardening at the required temperature for the required duration. It is used extensively by the Marine, Aerospace, Chemical, Petrochemical, Food Processing, Paper and general metalwork industries. Here it is employed for applications such as: Pump Shafts, Aircraft Fittings, Valve Stems, Hydraulic Fittings, Studs, Bushings, Screws, Fasteners, Couplings, Wear rings, Rollers and Food Handling Equipment etc.

Stainless steels are known as high-alloy steels. They contain about 4-30% of chromium. They are further divided into martensitic, austenitic, and ferritic steels. Another group of stainless steels are known as precipitation-hardened steels. 

Grade 17-4 stainless steel is the most widely used steel of the precipitation hardening grade steels. It has high toughness, strength, and corrosion resistance..

Features:

• Excellent durability
• Fine finish
• Sturdiness

Carbon 0.07 max. Manganese 1.00 max. Phosphorus 0.040 max. Sulfur 0.030 max. Silicon 1.00 max. Chromium 15.00 - 17.50 Nickel 3.00 - 5.00 Copper 3.00 - 5.00 Columbium plus Tantalum 0.15 - 0.45
Grinding and Polishing

440C in the hardened and tempered condition requires care with finish grinding and polishing to avoid overheating as this can lower the hardness and corrosion resistance.

Elevated Temperature Use

Excellent oxidation resistance up to 1100oF (540oC).Exposure to temperature range 600 – 900oF (290 – 480oC) long term may result in reduced toughness but this can sometimes be minimilized by using higher ageing temperatures. As a general guide for short term exposure at elevated temperatures the ageing temperature should be at least 50oF (28oC) above the working temperature.

Welding

May be welded satisfactorily by shielded fusion and resistance welded processes, however oxyacetylene welding is not recommended due to the posibility of carbon pick up Filler metal when required should be similar to the parent metal if strength is important otherwise standard austenitic stainless filler wire 308L may be satisfactory. Pre-heating is not generally required.Welding in the solution annealed condition may be carried out satisfactorily, however welding in the H1150 (H620) condition reduces the effects of high welding stresses. Following welding in the solution annealed condition, parts can be directly age hardened as required, however those in the H1150 (H620) condition should be re-solution annealed and then age hardened as required.

Applications:

• Nuclear reactor
• Aircraft and gas turbines
• Oil field
• Chemical process components
• Paper mill

Specifications:

• UNS S17400
• ASTM A564
• DIN 50602
• AMS 5642
• MIL-S-25043
• Grade 630
• WS 1.4542
• ASME SA564
• X5CrNiCuNb16-4
• AFNOR Z6CNU1704

Additional Information:

• Item Code: SS17_4_PH_UNSS17400_AMS5643_DIN14542_ForgedBlock
• Pay Mode Terms: L/C (Letter of Credit),T/T (Bank Transfer),D/P,D/A,Other
• Port of Dispatch: Mumbai JNPT
• Production Capacity: 500 MT per month
• Delivery Time: 30 Day
• Packaging Details: As Per Request

Product Details:

High levels of nickel and chromium provide corrosion resistance in reducing and oxidizing environments. The substantial molybdenum content enhances resistance to reducing media and provides a high degree of resistance to pitting and crevice corrosion. Additionally, the combination of elements makes the alloy resistant to hydrogen embrittlement and stresscorrosion cracking. The properties of INCONEL alloy 725 are useful for a range of applications that require outstanding corrosion resistance along with high strength. The alloy is used for hangers, landing nipples, side pocket mandrels and polished bore  eceptacles in sour gas service, where it resists the effects of hydrogen sulfide, chlorides and carbon dioxide. The alloy is also attractive for high strength fasteners in marine applications, where it resists corrosion, pitting and crevice attack in sea water.

Chemical Composition, %:

• Nickel……………………………………………………………….55.0-59.0
• Chromium…………………………………………………………19.0-22.5
• Molybdenum…………………………………………………………7.0-9.5
• Niobium……………………………………………………………..2.75-4.0
• Titanium……………………………………………………………….1.0-1.7
• Aluminum…………………………………………………………0.35 max.
• Carbon…………………………………………………………….0.03 max.
• Manganese………………………………………………………0.35 max.
• Silicon……………………………………………………………..0.20 max.
• Phosphorus…………………………………………………….0.015 max.
• Sulfur……………………………………………………………..0.010 max.
• Iron……………………………………………………………………Balance*

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 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.

In the aeronautical field, INCONEL alloy 600 is used for a variety of engine and airframe components which must withstand high temperatures. Examples are lockwire, exhaust liners and turbine seals.

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.

Limiting 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

Product Details:

Inconel nickel-chromium-iron alloy 601 (UNS N06601/W.Nr. 2.4851) is a general-purpose engineering material for applications that require resistance to heat and corrosion. An outstanding characteristic of INCONEL alloy 601 is its resistance to hightemperature oxidation. The alloy also has good resistance to aqueous corrosion, has high mechanical strength, and is readily formed, machined and welded. The limiting chemical composition of INCONEL alloy 601 is listed in Table . The composition is a facecentered-cubic solid solution with a high degree of metallurgical stability. The alloy’s nickel base, in conjunction with substantial chromium content, provides resistance to many corrosive media and hightemperature environments. Oxidation resistance is further enhanced by the aluminum content.Alloy 601 is a standard material of construction for various types of thermal-processing equipment. Industrial-heating applications include baskets, trays, and fixtures for annealing, carburizing, carbonitriding, nitriding and other heat-treating operations. In industrial furnaces, the alloy is used for radiant tubes, muffles, retorts, flame shields, strand-annealing tubes, woven-wire conveyor belts, chain curtains, burner nozzles, and electrical resistance heating elements. Other thermal-processing applications are thermocouple protection tubes, furnace-atmosphere generators, and infrared radiant screens.Chemical-processing applications for alloy 601 include process heaters, condenser tubes in sour-water strippers, and insulating cans in ammonia reformers. The alloy is also used for combustor components and catalyst grid supports in equipment for nitric acid production.In petrochemical processing, the alloy is used for catalyst regenerators and air preheaters in the manufacture of high-density polyethylene. In pollution-control applications, INCONEL alloy 601 is used for thermal reactors in exhaust systems of gasoline engines and for combustion chambers in solidwaste incinerators.

Chemical Composition:

• Nickel ………………………………………………58.0-63.0
• Chromium…………………………………………………..21.0-25.0
• Iron ………………………………………………………….Remainder
• Aluminum ………………………………………………1.0-1.7
• Carbon………………………………………………………0.10 max.
• Manganese …………………………………………….1.0 max.
• Sulfur ……………………………………………………0.015 max.
• Silicon ……………………………………………….0.50 max.
• Copper…………………………………………………….1.0 max.

Product Details:

Aluminum alloys tend to lose their strength when they are exposed to temperatures of about 200-250°C. However, their strength increases at subzero temperatures. They have high corrosion resistance.

The following datasheet will discuss in detail about the aluminum 6351 alloy.

Chemical Composition:

The chemical composition of the aluminum 6351 alloy is tabulated below.

Physical Properties:

The following table shows the physical properties of the aluminum 6351 alloy.

Mechanical Properties:

The mechanical properties of the aluminum 6351 alloy are outlined in the following table.

Product Details:

Product Details:

The age-hardenable alloy can be readily fabricated, even into complex parts. Its welding characteristics, especially its resistance to postweld cracking, are outstanding.

The ease and economy with which INCONEL Alloy 718 can be fabricated, combined with good tensile, fatigue, creep, and rupture strength, have resulted in its use in a wide range of applications. Examples of these are components for liquid fuelled rockets, rings, casings and various formed sheet metal parts for aircraft and land-based gas turbine engines, and cryogenic tankage. It is also used for fasteners and instrumentation parts.

Physical Constants And Thermal Properties:

Some physical constants of INCONEL alloy 718 are shown in Table 2. Modulus data appear in Tables 3 and 4, and thermal properties in Table 5. The values in these tables will vary slightly, depending on the composition and condition of the specimen tested. They are typical but are not suitable for specification purposes.

Limiting Chemical Compositions (%):

• Nickel (plus Cobalt) ……………………………. 50.00-55.00
• Chromium ……………………………. 17.00-21.00
• Iron …………………………………. Balance*
• Niobium (plus Tantalum) ……………………. 4.75-5.50
• Molybdenum ………………………… 2.80-3.30
• Titanium ……………………………………….. 0.65-1.15
• Aluminium ………………………………………………………………..0.20-0.80
• Cobalt …………………………………………………………………….1.00 max.
• Carbon……………………………………………………………………0.08 max.
• Manganese ……………………………………………………………..0.35 max.
• Silicon …………………………………………………………………….0.35 max.
• Phosphorus……………………………………………………………0.015 max.
• Sulfur…………………………………………………………………….0.015 max.
• Boron ……………………………………………………………………0.006 max.
• Copper……………………………………………………………………0.30 max

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.

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:

On account of our advanced production setup, we are able to provide Inconel 713 Forged Block at the most reasonable cost.

Specifications:

• Designing type: Forged
• Size: Customized

Features:

• Easy to use
• Optimum strength
• Excellent finish

Product Details:

Super alloys or high performance alloys are of three types that include iron-based, cobalt-based and nickel-based alloys. These alloys can be strengthened by precipitation hardening, solid-solution hardening and work hardening methods. Super alloys contain good oxidation and creep resistance and are available in varied shapes. These alloys can function under high mechanical stress and high temperatures and also in places that require high surface stability. Super alloy A-286 is an iron-based high temperature and high strength alloy. The following datasheet provides an overview of super alloy A-286.

Chemical Composition:

The chemical composition of super alloy A-286 is outlined in the following table.

Product Details:

The limiting chemical composition of INCONEL alloy 617. 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.