Batang Bulat Paduan Suhu Tinggi

dapatkan harga terbaru

Jenis pembayaran:	L/C,T/T
Inkoterm:	FOB,EXW
Min. Memesan:	1 Piece/Pieces
Transportasi:	Ocean,Land,Express
Pelabuhan:	shanghai

Hubungi sekarang

Deskripsi Produk

Atribut Produk

& pengiriman paket

Deskripsi Produk

Atribut Produk

Merek: Hosea

Origin: Cina

& pengiriman paket

Menjual unit	:	Piece/Pieces
Tipe paket	:	paket standar

The file is encrypted. Please fill in the following information to continue accessing it

Deskripsi Produk

Batangan bundar superalloy kami dirancang untuk aplikasi industri yang melibatkan suhu ekstrem, lingkungan korosif, dan kondisi tekanan tinggi, sehingga menghasilkan kinerja luar biasa di sektor kedirgantaraan, energi, dan industri umum. Diproduksi dari superalloy berbasis nikel-kromium (seperti Inconel 718, mengandung 52,5% Ni, 19% Cr, dan 3% Mo), batangan ini tahan terhadap suhu pengoperasian terus-menerus hingga 1.200°C (2.192°F) sekaligus menawarkan ketahanan unggul terhadap oksidasi, sulfidasi, dan deformasi mulur. Produk ini mematuhi standar AMS 5662, ASTM B637, dan ASME SB637, sehingga menawarkan masa pakai sepuluh kali lebih lama dibandingkan paduan konvensional dalam kondisi yang berat.

Diameter: 5 mm–300 mm (ditarik dingin/digulung panas)

Panjang: 1 m–6 m (standar) / dipotong khusus hingga 12 m

Permukaan Akhir: Canai panas, ditarik dingin, dipoles (Ra ≤0,8 μm)

Sifat Mekanik (Inconel 718): Kekuatan Hasil ≥1,100 MPa | Kekuatan Tarik ≥1.400 MPa | Perpanjangan ≥12% | Kekerasan ≤35 HRC

Parameter Category	Inconel 718	Haynes 282	Waspaloy	Nimonic 80A
Material Standard	ASTM B637, UNS N07718	ASTM B637, UNS N07208	AMS 5708, UNS N07001	BS HR 901, UNS N07080
Chemical Composition (%)	Ni: 50–55, Cr: 17–21, Fe: Balance, Mo: 2.8–3.3, Nb+Ta: 4.75–5.5, Ti: 0.65–1.15, Al: 0.2–0.8	Ni: 56–59, Co: 9–11, Cr: 19–21, Mo: 8.5–9.5, Ti: 2.0–2.4, Al: 1.4–1.6	Ni: 54–57, Cr: 18–21, Co: 12–15, Mo: 3.5–5.0, Ti: 2.75–3.25, Al: 1.2–1.6	Ni: 70–75, Cr: 18–21, Ti: 1.8–2.7, Al: 1.0–1.8, Fe: ≤3.0
Tensile Strength (MPa)	1275–1550 (Aged)	1000–1170 (Aged)	1170–1380 (Aged)	900–1100 (Aged)
Yield Strength (MPa)	1035–1350 (Aged)	760–895 (Aged)	830–1030 (Aged)	600–850 (Aged)
Elongation (%)	≥12 (in 50mm gauge length)	≥15 (in 50mm gauge length)	≥12 (in 50mm gauge length)	≥15 (in 50mm gauge length)
Hardness	Rockwell C35–45	Rockwell C30–38	Rockwell C35–42	Rockwell C25–35
Density (g/cm³)	8.19	8.28	8.22	8.19
Melting Range (°C)	1260–1336	1315–1370	1330–1390	1360–1425
Thermal Conductivity (W/m·K)	11.4 (20°C)	11.0 (20°C)	11.8 (20°C)	12.5 (20°C)
Thermal Expansion (10⁻⁶/°C)	13.0 (20–100°C)	12.9 (20–100°C)	13.2 (20–100°C)	13.8 (20–100°C)
Max Service Temperature (°C)	700 (continuous)	800 (continuous)	815 (continuous)	750 (continuous)
Creep Rupture Strength	200 MPa (100h at 650°C)	150 MPa (100h at 750°C)	170 MPa (100h at 730°C)	120 MPa (100h at 700°C)
Oxidation Resistance	Excellent up to 700°C in air.	Good up to 800°C (Cr-rich oxide).	Excellent up to 815°C (Cr/Ti oxide).	Good up to 750°C (Cr/Al oxide).
Heat Treatment	Aging: 720°C/8h + 620°C/8h.	Solution: 1120°C + Aging: 800°C/8h.	Solution: 1080°C + Aging: 760°C/16h.	Aging: 700–800°C for 16h.
Surface Finishes	Hot Rolled, Cold Drawn, Polished.	Hot Rolled, Annealed & Descaled.	Hot Rolled, Peeled, Polished.	Hot Rolled, Pickled & Passivated.
Diameter Range (mm)	5–300	5–250	5–300	5–200
Length (m)	3–6 (standard), Custom up to 12.	3–6 (standard)	3–6 (standard)	3–6 (standard)
Key Applications	Aerospace turbine discs, fasteners, nuclear reactors.	Gas turbine blades, exhaust systems, power generation.	Jet engine shafts, bolts, afterburner components.	Gas turbine blades, exhaust valves, industrial furnace parts.