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ODM Nickel Alloy Forging Bar Inconel 600 Bar / Rod For Aircraft Engine

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    Buy cheap ODM Nickel Alloy Forging Bar Inconel 600 Bar / Rod For Aircraft Engine from wholesalers
     
    Buy cheap ODM Nickel Alloy Forging Bar Inconel 600 Bar / Rod For Aircraft Engine from wholesalers
    • Buy cheap ODM Nickel Alloy Forging Bar Inconel 600 Bar / Rod For Aircraft Engine from wholesalers
    • Buy cheap ODM Nickel Alloy Forging Bar Inconel 600 Bar / Rod For Aircraft Engine from wholesalers

    ODM Nickel Alloy Forging Bar Inconel 600 Bar / Rod For Aircraft Engine

    Ask Lasest Price
    Brand Name : DINGSCO
    Model Number : According to customers requirements
    Certification : ISO 9001:2015,PED 2014/68/EU,API 6A,API-20B,TSG,NORSOK
    Price : Negotiable
    Payment Terms : T/T
    Supply Ability : Negotiable
    Delivery Time : (Sample Order) 7 days
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    ODM Nickel Alloy Forging Bar Inconel 600 Bar / Rod For Aircraft Engine

    ODM Nickle Alloy Forging Bar Inconel 600 Aircraft Engine Rocket


    Nickle Alloy Forging Bar:Using forging machinery to apply pressure to metal blanks to cause plastic deformation, thereby obtaining forgings with certain mechanical properties, shape, and size.


    Rolling Bar: The process of reducing the cross-section and increasing the length of metal stock by passing it through the gap between a pair of rotating rolls (of various shapes) is known as rolling.


    The Differences between Forging Bar and Rolling Bar:

    • Forged parts typically have a denser structure than rolled round bar, as evidenced by the detection of porosity in the material through hot acid etching methods.
    • Generally speaking, the quality of round bar produced by forging (referring to free forging here) is better than that produced by rolling. This is because forging requires repeated forging to achieve the same deformation as rolling for elongation (forging is free deformation, while rolling is constrained deformation).
    • when the length of the round bar is relatively long, it is difficult to produce in one heat with forging (still referring to free forging here). Multiple heating and forging processes are required. In such cases, it is not easy to compare the overall quality differences between forged and rolled round bar.
    • If advanced special forging methods (such as foreign advanced constrained forging and three-dimensional forging) are used, the quality of the forged round bar will always be higher than that of the rolled round bar.

    INCONEL ALLOY 600 (nickel-chromium-iron)(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:

    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:

    • It 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.
    • 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.

    Chemical Composition:


    ElementNi+CoCrFeCMnSSiCu
    Minimum(%)72146-----
    Max(%)-17100.1510.0150.50.5

    Thermal Properties:


    TemperatureCoefficient of ExpansionaElectrical ResistivityThermal ConductivitySpecific Heat
    °F10-6 in/in•°Fohm•circ•mil/ftBtu•in/ft2•h•°FBtu/lb•°F
    -2506.0-860.073
    -2006.3-890.079
    -1006.7-930.090
    705.86201030.106
    2007.46251090.111
    4007.76341210.116
    6007.96441330.121
    8008.16441450.126
    10008.46801580.132
    12008.66801720.140
    14008.96801860.145
    16009.16862000.149
    18009.3698--
    2000-704--
    °Cμm/m•°CμΩ•mW/m•°CJ/kg•°C
    -15010.9-12.5310
    -10011.7-13.1352
    -5012.3-13.6394
    2010.41.0314.9444
    10013.31.0415.9444
    20013.81.0517.3486
    30014.21.0719.0502
    40014.51.0920.5519
    50014.91.1222.1536
    60015.31.1322.1578
    70015.81.1325.7595
    80016.11.1327.5611
    90016.41.15-628

    Physical Properties
    Mean Coefficient of Thermal Expansion
    Temperature Range
    °F°Cin/in°Fcm/cm°C
    68205.8 x 10-610.4 x 10-6
    Mechanical Properties
    Typical Values at 68°F(20°C)
    Yield Strength 0.2% offset psiUltimate Tensile Strength (min.) psiElongation in 2"%
    35,00080,00030

    Recommended Tool Types & Machining Conditions:


    OperationsCarbide Tools
    Roughing, with severeinterruptionTurning or Facing C-2 andC-3 grade: Negative rakesquare insert, 45° SCEA1,1/32 in. nose radius. Tooholder: 5° neg. back rake5° neg. side rake. Speed:30-50 sfm,0.004-0.008 in.feed, 0.150 in depth of cut.Dry2, oil3, or water-base coolant 4.
    Normal roughingTurning or Facing C-2 orC-3 grade: Negative ratesquare insert, 45° SCEA,1/32 in nose radius. Tooholder: 5° neg. back rake5° neg. side rake. Speed:90 sfm depending on rigidity of set up, 0.010 infeed, 0.150 in. depth ofcut. Dry, oil, or water-base coolant.
    FinishingTurning or Facing C-2 0rC-3 grade: Positive rakesquare insert, if possible45° SCEA, 1/32 in.noseradius. Tool holder: 5° pos.back rake, 5° pos. siderake.Speed: 95-110 sfm0.005-0.007 in. feed,0.040 in. depth of cut. Dryor water-base coolant.
    Rough BoringC-2 or C-3 grade: lf inserttype boring bar, use standard positive raketools with largest possibleSCEA and 1/16 in. nose radius. lf brazed tool bargrind 0° back rake, 10° posside rake, 1/32 in. nose radius and largest possible SCEA.Speed: 70 sfm depending on the rigidityof setup, 0.005-0.008 infeed, 1/8 in. depth of cut.Dry, oil or water-base coolant.
    Finish BoringC-2 or C-3 grade: Usestandard positive raketools on insert type bars.Grind brazed tools as fofinish turning and facingexcept back rake may bebest at 0°. Speed: 95-110sfm,0.002-0.004 in feed.Water-base coolant.



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    ODM Nickel Alloy Forging Bar Inconel 600 Bar / Rod For Aircraft Engine


    Quality ODM Nickel Alloy Forging Bar Inconel 600 Bar / Rod For Aircraft Engine for sale
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