Product Code : AL-NIC263-NN-SP
Nimonic C-263 is an age-hardenable Nickel-Cobalt-Chromium-Molybdenum alloy designed for a combination of aged strength properties with exceptional fabrication characteristics. Nimonic C-263 shows excellent intermediate temperature tensile ductility.and is typically used for applications such as aircraft turbine engine and land-based turbine applications.
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Product Information
Nimonic C-263 is an age-hardenable Nickel-Cobalt-Chromium-Molybdenum alloy designed for a combination of aged strength properties with exceptional fabrication characteristics. Nimonic C-263 shows excellent intermediate temperature tensile ductility.and is typically used for applications such as aircraft turbine engine and land-based turbine applications.
Synonyms
Nicrofer 5120, Hastelloy C263 and Nimonic 263.
Nimonic C-263 Sheet Specification
Size：customized
Purity: customized
Per your request or drawing
We can customized as required
UNS N07263
Werkstoff Nr. 2.4650
BS HR10 Rod and Bar
BS HR 206 Plate, Sheet, Strip
BS HR 404 Seamless Tube
AECMA PrEn 2199 Bar
AECMA PrEn 2200 Forgings
AECMA PrEn 2201 Bar
AECMA PrEn 2202 Tube
AECMA PrEn 2203 Sheet, Strip
AECMA PrEn 2418 Plate
DIN 17750 Plate, Sheet, Strip
DIN 17751 Pipe and Tube
DIN 17752 Bar and Rod
DIN 17753 Wire
DIN 17754 Forgings
AMS 5872 Sheet, Plate and Strip
AMS 5886 Bar, Forgings, Rings
AFNOR NCK 20 D
AIR 9165 Sheet, Plate, Rod, Bar and Forgings
MSRR 7035
MSRR 7036
GE B50A774A
Tradename's: Nicrofer 5120, Hastelloy C263 and Nimonic 263.
Properties（Theoretical）
| Density | 8.36 g/cm3 | 0.302 lb/in³ |
| Melting Point | 1325 °C | 2415 °F |
| Coefficient of Expansion | 10.6 μm/m• °C (20 – 100 °C) | 5.7 x 10-6 in/in• °F (70 – 212 °F) |
| Modulus of Elasticity | 222.5 kN/mm² | 32270 ksi |
| Approx. tensile strength（Annealed） | <1000 N/mm² | <145 ksi |
| Approx. operating temperature depending on load** and environment（Annealed） | up to 800 °C | up to 1500 °C |
| Approx. tensile strength（Annealed + Aged） | 1000 – 1200 N/mm² | 145 – 174 ksi |
| Approx. operating temperature depending on load** and environmentAnnealed + Aged） | up to 800 °C | up to 1500 °C |
| Approx. tensile strength（Spring Temper） | 1200 – 1500 N/mm² | 174 – 217 ksi |
| Approx. operating temperature depending on load** and environment（Spring Temper） | up to 800 °C | up to 1500 °C |
Chemical Composition
| Element | Min % | Max % |
| C | 0.04 | 0.08 |
| AI | 0.3 | 0.6 |
| Co | 19 | 21 |
| Cr | 19 | 21 |
| Mo | 5.6 | 6.1 |
| B | – | 0.005 |
| Bi | – | 0.0001 |
| Cu | – | 0.2 |
| Fe | – | 0.7 |
| Pb | – | 0.002 |
| Si | – | 0.4 |
| Mn | – | 0.6 |
| S | – | 0.007 |
| Ag | – | 0.0005 |
| Ti | 1.9 | 2.4 |
| Ti+AI | 2.4 | 2.8 |
| Ni | Bal |
We can customized as required
Applications of Nimonic C-263 Sheet
Nimonic C-263 Sheet combines properties which make it suitable for a variety of fabricated component applications in both aircraft turbine engine and industrial turbine applications. These include low-temperature combustors, transition liners, and some ring components.
Packing of Nimonic C-263 Sheet
Standard Packing:
Typical bulk packaging includes palletized plastic 5 gallon/25 kg. pails, fiber and steel drums to 1 ton super sacks in full container (FCL) or truck load (T/L) quantities. Research and sample quantities and hygroscopic, oxidizing or other air sensitive materials may be packaged under argon or vacuum. Solutions are packaged in polypropylene, plastic or glass jars up to palletized 440 gallon liquid totes Special package is available on request.
ATTs’ Nimonic C-263 Sheet is carefully handled to minimize damage during storage and transportation and to preserve the quality of our products in their original condition.
