Standard: ASME, ASTM, EN, UNS, GB, DIN, JIS
Product Certification: ISO, CE, RoHS
Payment Terms: T/T, L/C, PayPal, Western Union
Incoloy 901 is used for components in aircraft and gas turbines, such as turbine rotors, compressor discs, hubs and shafts, with a maximum service temperature around 1100ºF (595ºC).
1. Standard Exporting package.
2. Original package or neutral package.
3. According to clients ' needs.
4. Shipped in10-35 days after payment.
Q: How can I get the price?
A: You can contact us through sending inquiry, calling, or get details price list by E-mail.
Q: How long is the delivery time?
A: It depends on quantity. Usually, 10-35 working days.
Q: Can I get sample to check the quality?
A: Of course. We can supply sample, and free for some small value products.
Q: Do you provide OEM service?
A: Yes, we do. Customized design is available.
Q: What is your payment term?
A: L/C, T/T, PayPal, Western Union, etc.
Q: What certificate do your products have?
A: CE, ISO9001, RoHS, SGS, etc.
A nickel-iron-chromium alloy containing titanium and aluminum for precipitation hardening and molybdenum for solid-solution strengthening. The alloy has high yield strength and creep resistance at temperatures to about 1110°F (600°C). A substantial iron content enables the alloy to combine high strength with good forging characteristics. Used in gas turbines for discs and shafts. Standard products form is round.
Alloy 901 has good corrosion resistance to the atmospheres normally found in jet engine operations. It has slightly lower scaling resistance than such alloy as Types 309 and 310 stainless steel.