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Nimonic® Alloy 105 Special Alloys For Clean Energy And Oceaneering High Performance

    Buy cheap Nimonic® Alloy 105 Special Alloys For Clean Energy And Oceaneering High Performance from wholesalers
     
    Buy cheap Nimonic® Alloy 105 Special Alloys For Clean Energy And Oceaneering High Performance from wholesalers
    • Buy cheap Nimonic® Alloy 105 Special Alloys For Clean Energy And Oceaneering High Performance from wholesalers
    • Buy cheap Nimonic® Alloy 105 Special Alloys For Clean Energy And Oceaneering High Performance from wholesalers
    • Buy cheap Nimonic® Alloy 105 Special Alloys For Clean Energy And Oceaneering High Performance from wholesalers
    • Buy cheap Nimonic® Alloy 105 Special Alloys For Clean Energy And Oceaneering High Performance from wholesalers
    • Buy cheap Nimonic® Alloy 105 Special Alloys For Clean Energy And Oceaneering High Performance from wholesalers
    • Buy cheap Nimonic® Alloy 105 Special Alloys For Clean Energy And Oceaneering High Performance from wholesalers

    Nimonic® Alloy 105 Special Alloys For Clean Energy And Oceaneering High Performance

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    Brand Name : CMMC
    Model Number : As per specification and drawing
    Certification : ISO 9001, AS9100 etc
    Price : Negotiable
    Payment Terms : D/P, L/C, T/T
    Supply Ability : 200 metric tons per month
    Delivery Time : 60-90 days
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    Nimonic® Alloy 105 Special Alloys For Clean Energy And Oceaneering High Performance

    Alloy 105, Nimonic® alloy 105 for ultra-supercritical thermal turbine blade, forgings, ring, fastener etc


    1 PRODUCT

    Alloy 105, Nimonic® alloy 105 for ultra-supercritical thermal turbine blade, aero-engine turbine blades, forgings, ring, discs, sections, bolts and fasteners, etc.


    2 EQUIVALENT DESIGNATION

    GH4105, W.Nr.2.4634, NiCo20Cr15MoAlTi(DIN), HR3(BS)


    3 APPLICATION

    Alloy 105 is used for thermal turbine blades, materials for key high temperature components of ultra-supercritical thermal turbine, discs, aero-engine turbine blades, forgings, ring, sections, bolts and fasteners, etc.


    4 CHEMICAL COMPOSITION (wt%):

    FeNiCoCrTiCuMoZr
    ≤1.0Balance18.0-22.014.0-15.71.18-1.50≤0.204.5-5.50.070-0.15
    CAlMnSiPSB
    0.05-0.174.5-4.90≤0.40≤0.25≤0.015≤0.0100.003-0.010

    5 PHYSICAL CONSTANTS

    Density: 8.01 g/cm³ (0.289 lb/in³)

    Melting Range: Liquidus temperature 1345°C, solidus temperature 1290°C.


    6 MECHANICAL PROPERTY

    Tensile properties: extruded bar subsequently forged

    The data given in Table below and presented graphically in Figures 1 and 2 represent the tensile properties for extruded bar subsequently forged after the 3-stage heat treatment.

    Strain rate 0.005/min to proof stress (at room temperature), 0.002/min to proof stress (at elevated temperatures) and 0.1/min thereafter.

    Heat treatment 4 h/1150°C/AC + 16 h/1050-1065°C/AC + 16 h/850°C/AC

    Temperature °C0.1% proof stress0.2% proof stressTensile strength

    Elongation on 5.65

    √So, %

    Reduction of area

    %

    MPaMPaMPa
    2079682711801616
    10076079311852124
    20074577411882434
    30073976611622024
    40073276311262333
    50074878211482331
    60073576911112232
    70073976810752633
    8006807148362434
    9003904114912838
    10001521561894360
    110028315613299

    Figure 1 Heat treatment 4h/1150°C/AC + 16h/1050-1065°C/AC + 16h/850°C/AC


    Figure 2 Heat treatment 4h/1150°C/AC + 16h/1050-1065°C/AC + 16h/850°C/AC


    7 CORROSION RESISTANCE
    Oxidation in Air

    Table 7-1 Continuous Heating, descaled weight loss (mg/cm²) after 100 hours at

    800°C900°C950°C1000°C1100°C
    0.110.490.991.436.41

    Table 7-2 Intermittent heating (Cooling to room temperature every 24 hrs), descaled weight loss (mg/cm²) after 100 hours at

    800°C900°C950°C1000°C1100°C
    1.191.591.6113.3

    Table 7-3 Cyclic Heating (15 min in furnace, 5 min outside furnace)

    TemperatureTime to onset of spalling (h) at max cycle temperature ofRate of spalling (mg/cm²/h) at max cycle temperature ofWeight change in 100 h (mg/cm²) at max cycle temperature of
    °C°C°C°C
    890>10000.66
    910>10001.05
    9906000.15-51.9
    10103000.408-229
    10901500.946-748
    1110751.17-955

    Table 7-4 Resistance to atmospheres containing SO2

    AtmosphereDescaled weight loss (mg/cm²) after 1000 hours at
    600°C700°C800°C1000°C
    3% SO2-Argon1.68.715
    3% SO2-Air2.31.10.60.6
    3% SO2-5% O2-Argon2.10.50.62.1

    8 WORKING INSTRUCTION

    Hot working
    Alloy 105 may be hot worked in the temperature range 1050-1200°C.

    Annealing

    Interstage annealing of Alloy 105 should be carried out at 1150°C followed by air cooling of fluidized bed quenching. Water quenching is not recommended as severe surface cracking may result from thermal shock.

    Machining

    Alloy 105 should be in the fully heat-treated condition for all machining operations. The high hardness range 320-385 HV, necessitates the use of tungsten carbide tipped tools. High speed steel shock-proof tools can be used if the cut is of an intermittent nature.

    Heat treatment

    The heat treatment recommended is dependent on the intended service condition.

    Two heat treatments are recommended as follows:

    (a) 4 h/1150°C/AC+16 h/1050-1065°C/AC+16h/850°C/AC

    (b) 4 h/1125°C/AC+16 h/850°/AC

    In general, heat treatment (a) is intended for optimum long-term creep strength and ductility at operating temperatures in the range 850-950°C. Heat-treatment (b) may be used where long-term properties are not of paramount importance and tensile strength, elongation and impact strength may be enhanced for operating temperatures up to 700°C. When applying heat-treatment (b), it is essential to ensure that cooling from 1125°C takes place freely and is not delayed due to close packing of components.

    Examples of the use of these heat treatments are as follows:

    (a) Turbine blades, discs, forgings and ring sections, all of which may be produced from as extruded, as forged or subsequently cold worked starting stock

    (b) Bolts and fasteners for which extruded and cold worked bar or section is recommended as starting stock.


    9 STANDARD SPECIFICATION

    BS. HR3 billets, bars and forgings

    AICMA Ni-P61-HT billets, bars and forgings

    Swedish Defence Material Administration MH.14 forged bar

    DIN designation NiCo20Cr15MoAlTi forged bar

    AFNOR NCKD 20ATv AECMA PrEn 2179-2181


    10 COMPETITIVE ADVANTAGE

    (1) More than 50 years experience of research and develop in high temperature alloy, corrosion resistance alloy, precision alloy, refractory alloy, rare metal and precious metal material and products.
    (2) 6 state key laboratories and calibration center.
    (3) Patent technologies.

    (4) High performance.


    11 BUSINESS TERM

    Minimum Order QuantityNegotiable
    PriceNegotiable
    Packaging DetailsWater prevent, seaworthy transport, non-fumigation wooden box
    MarkAs per order
    Delivery Time60-90 days
    Payment TermsT/T, L/C at sight, D/P
    Supply Ability200 metric tons / Month

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