Sign In | Join Free | My himfr.com
Home > Special Alloys For Clean Energy And Oceaneering >

UNS N07090 / W.Nr. 2.4632 Nickel Based Alloys Good Formability And Weldability

    Buy cheap UNS N07090 / W.Nr. 2.4632 Nickel Based Alloys Good Formability And Weldability from wholesalers
     
    Buy cheap UNS N07090 / W.Nr. 2.4632 Nickel Based Alloys Good Formability And Weldability from wholesalers
    • Buy cheap UNS N07090 / W.Nr. 2.4632 Nickel Based Alloys Good Formability And Weldability from wholesalers
    • Buy cheap UNS N07090 / W.Nr. 2.4632 Nickel Based Alloys Good Formability And Weldability from wholesalers
    • Buy cheap UNS N07090 / W.Nr. 2.4632 Nickel Based Alloys Good Formability And Weldability from wholesalers
    • Buy cheap UNS N07090 / W.Nr. 2.4632 Nickel Based Alloys Good Formability And Weldability from wholesalers
    • Buy cheap UNS N07090 / W.Nr. 2.4632 Nickel Based Alloys Good Formability And Weldability from wholesalers

    UNS N07090 / W.Nr. 2.4632 Nickel Based Alloys Good Formability And Weldability

    Ask Lasest Price
    Brand Name : CMMC
    Model Number : As per specification and drawing
    Certification : ISO 9001, PED, API etc
    Price : Negotiable
    Payment Terms : D/P, L/C, T/T
    Supply Ability : 300 metric tons per month
    Delivery Time : 60-90 days
    • Product Details
    • Company Profile

    UNS N07090 / W.Nr. 2.4632 Nickel Based Alloys Good Formability And Weldability

    Nickel based Alloy 90 (UNS N07090, W.Nr. 2.4632) semi-products for clean energy and power generating


    1 PRODUCT

    Nickel based Alloy 90 (UNS N07090, W.Nr. 2.4632) semi-products for clean energy and power generating.

    Standard semi-product forms include sheet, strip, plate, round bar, flat bar, forging, hexagon, ring, disc, wire and fastener etc.


    2 EQUIVALENT DESIGNATION

    GH4090, UNS N07090, NIMONIC® alloy 90, W.Nr. 2.4632, 2.4969, AWS 030


    3 APPLICATION

    The alloy is used for turbine blades, discs, forgings, ring sections, fasteners, clamp, seal ring, elastic element and hot-working tools.


    4 OVERVIEW

    Alloy 90 is a wrought nickel-chromium-cobalt base alloy strengthened by additions of titanium and aluminum. It has been developed as an age-hardenable creep- resisting alloy for service at temperatures up to 920°C (1688°F).

    The alloy has high tensile strength and creep resistance, good oxidation resistance and corrosion resistance in 815~870°C, high fatigue strength and good formability and weldability under the action of repeated cooling and heating.


    5 CHEMICAL COMPOSITION (wt%):

    Table 1 (wt%)

    FeNiCoCrZrTiPbBBi
    ≤1.50Balance15.0-21.018.0-21.0≤0.152.00-3.00≤0.0020≤0.02≤0.0001
    CuCAlMnSiPSAg
    ≤0.20≤0.131.00-2.00≤1.00≤1.00≤0.020≤0.015≤0.0005

    6 PHYSICAL PROPERTIES

    Density:ρ=8.18 g/cm3(0.296lb/in3)

    Melting range:1310-1370℃(2390-2500°F)


    7 MECHANICAL PROPERTIES

    Tensile Properties of Extruded Bar Subsequently Forged

    Heat treatment 8 h / 1080°C (1975°F) / AC + 16 h / 700°C (1290°F) / AC

    Temperature0.1% Proof Stress0.2% Proof StressTensile strengthElongation onReduction of area
    °C°FMPa103 ksiMPa103 ksiMPa103 ksi5.65ÖSo, %%
    206879111581311712511812841
    10021275711077711312021742642
    20039273210675110911751702642
    30057271510473410711691702843
    40075271510473210611481672844
    50093270610272610511201622843
    600111269810172310510921582339
    70012926901007111039651401317
    80014725518057383683991016
    90016522844130044346502137
    1000183245748776117797

    8 CORROSION RESISTANCE

    Oxidation in Air (continuous heating)

    Descaled weight loss (mg/cm2) after 100 hours at

    800°C900°C950°C1000°C1100°C
    0.462.525.510.411.23

    Intermittent Heating (cooling to room temperature every 24 hours)

    Descaled weight loss (mg/cm2) after 100 hours at

    800°C900°C950°C1000°C1100°C
    3.028.128.1817.7

    Resistance to atmospheres containing SO2

    AtmosphereDescaled Weight loss (mg/cm2) after 1000 hours at
    600°C700°C800°C900°C
    3% SO2 – Argon3.71840
    3% SO2 – Air4.58.11.42
    3% SO2 – 5% O2 – Argon1.94.21.33.7

    9 MICROSTRUCTURE

    The main enhancement of the alloy is the γ′-Ni3(Al,Ti), which precipitates into different square particles in the grain, which is also visible in the grain boundary. The carbide is precipitated in a discontinuous strand in the grain boundary.


    10 WORKING INSTRUCTION

    Formability

    The alloy is easily to get internal crack when forging, not allowed heavy hammer strikes, no low temperature chamfering.

    Before charging into the heating furnace, the furnace temperature cannot be higher than 700°C. The final heating temperature is 1150±10°C. Forging start at temperature not less than 1060°C, and the final forging temperature is not less than 950°C.

    The rolling heating temperature is 1160°C, and the finishing temperature not lower than 950°C.

    Cold drawn product shall undergo cold deformation of 8%~12% after final intermediate annealing.

    Hot working

    Alloy 90 should be hot worked in the range 1050-1200°C (1922-2192°F).

    Interstage annealing

    Interstage annealing should be at 1040°C (1904°F) followed by a water quench or air cooling.

    Cold drawn bar

    1080±10°C; holding time see table below, air cooling or water cooling, +750±10°C,4h, air cooling.

    Diameter or minor section size mm≤3>3~6>6~12.5>12.5~25
    Time hours1248

    Sheet and strip (soft state)

    Softened at 1100~1150°C,1~10min, cooled in appropriate medium, +750±10°C, 4h, air cooled

    Sheet and strip (hard state)

    700~725°C,4h, air cooled

    Spring wire (cold drawn)

    600±10°C,16h, air cooled or 650±10°C,4h, air cooled

    Spring wire (cold drawing and solid solution)

    1080±10°C, 8h, air cooling +700~750, 4h, air cooling

    Machining

    Alloy 90 should be in the fully heat-treated condition for all machining operations. The high material hardness in this condition, 250-350 HV, requires the use of stringent machining techniques.


    11 STANDARD SPECIFICATION

    Rod, Bar, Wire and Forging Stock

    BS HR2, HR501, HR502 and HR503

    BS 3075 NA 19

    SAE AMS 5829 Nickel Alloy, Corrosion and Heat Resistant, Welding Wire 56ni 19.5cr 16.5co 2.5ti 1.5al Vacuum Induction Melted

    AECMA PrEN 2295, 2296, 2297, 2400, 2401, 2669 and 2670.

    ISO 15156-3 (NACE MR 0175)

    NCK 20TA


    Plate, Sheet and Strip

    BS HR202

    AECMA PrEN 2298.


    Pipe and Tube

    BS HR402

    AECMA PrEn 2299


    12 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) Patented technologies.

    (4) Ultra-purity smelting process: VIM + IG-ESR + VAR

    (5) Excellent high performance.


    13 BUSINESS TERM

    Minimum Order QuantityNegotiable
    PriceNegotiable
    Packaging Detailswater prevent, seaworthy transport, mill’s export standard packing
    MarkAs per order
    Delivery Time60-90 days
    Payment TermsT/T, L/C at sight, D/P
    Supply Ability300 metric tons per month

    Quality UNS N07090 / W.Nr. 2.4632 Nickel Based Alloys Good Formability And Weldability for sale
    Inquiry Cart 0
    Send your message to this supplier
     
    *From:
    *To: China Machinery Metal Jiangsu Co., Ltd.
    *Subject:
    *Message:
    Characters Remaining: (0/3000)