Haynes 233 Alloy Sheet

Haynes 233 Alloy Sheet

Haynes 233 is a new nickel-based superalloy designed to provide excellent oxidation resistance and superior creep strength at extreme temperatures up to 1149°C (2100°F).Haynes 233 Alloy Sheet supplied by Lork Group is often the aviation grade material favored by customers.
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Haynes 233 alloy plate is a new nickel-cobalt-chromium-molybdenum-aluminum alloy that achieves excellent oxidation resistance through the formation of a protective alumina layer. At the same time, its high creep strength comes from solid solution strengthening and carbide strengthening.

 

Additionally, for use at low to intermediate temperature applications (below the gamma-prime solvus of 1767°F (964°C)), the Haynes 233 alloy sheet can be age-hardened by heat treatment to produce even greater strength. Finally, the alloy can be readily fabricated using conventional methods since it exhibits good hot workability, cold formability, and weldability. Potential applications include hot gas path components in aerospace and industrial gas turbines, industrial heating fixtures and sensors, and various structural components in the emerging energy and chemical process markets.

 

Chemical Composition

 

Element

Content (%)

Nickel

48 (Balance)

Chromium

19

Cobalt

19

Molybdenum

7.5

Titanium

0.5

Aluminum

3.3

Iron

1.5 max.

Manganese

0.4 max.

Silicon

0.20 max.

Carbon

0.1

Boron

0.004

Tantalum

0.5

Tungsten

0.3 max.

Yttrium

0.025 max.

Zirconium

0.03

 

Heat Treatment Sheet

 

Haynes 233 alloy sheet is supplied in the mill (solution) annealed condition and may be used in either the solution annealed or age-hardened condition, depending on application. Solution annealing is typically performed by heating to a temperature in the range of 2100 to 2150°F (1149 to 1177°C) for a time commensurate with thickness, followed by a water quench. The solution annealed condition is most appropriate for applications above 1767°F (964°C). Alloy 233 can be age-hardened to significantly increase strength at low to intermediate temperatures (below the gamma-prime solvus of 1767°F (964°C)). A typical age-hardening heat treatment for this alloy is 1650°F/4h/AC + 1450°F/8h/AC (899°C/4h/AC + 788°C/8h/AC).

 

Application

 

  • Hot gas components in aerospace and industrial gas turbines
  • Industrial heating fixtures and sensors
  • Various structural components in the emerging technology market

 

 

FAQS

 

If you have any other questions, please contact me!

 

Q: Can you produce nickel alloy bars?

A: Yes, we can produce nickel alloy bars according to your requirements.

Q: What is your minimum order quantity?

A: Our minimum order quantity is 50 kg. Larger quantity, lower price.

Q: How long is your delivery time?

A: Generally delivery time for stock is 3 days, and customization takes 15 working days or more, but it is also affected by your specific requirements or order quantity.

Q: Can you provide samples?

A: For small parts, we can provide a free e-sample of regular sizes, but the shipping costs will be borne by you. For a large parts sample, we will include it in the order amount. Please confirm with our sales department for your specific requirements.

Q: How can l quickly get the price list?

A: Directly send us an email with detailed specifications, and you will get the official price list in 1 hour.

Q: How do you control product quality?

A: From the selection of raw materials to transportation and packaging, every production process will be tested and evaluated. Only products that have passed all tests can be delivered for export.

Q: Can you provide processing services?

A: Yes, we also provide processing services to our customers. It is one of our goals to provide specialized services such as bending, water cutting, laser cutting, digging holes, welding, slitting of coils, and other fabrications according to the drawings.

 

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