Turkish
WASPALOY (2.4654, UNS N07001)
Waspaloy is an aging hardener, nickel-based superalloy. Waspaloy has very high strength at temperatures up to 980oC (1800oF).
Waspaloy is widely used in the manufacture of gas turbine parts and parts used in the aviation industry, for processing and forging. It is comparable to Rene 41 as a strength, but it is superior to Inconel 718.
MAIN FEATURES OF WASPALOY
The waspaloy alloy (UNS N07001) is a hardened, nickel based super alloy with very good strength up to about 1800 ° F (980 ° C). Waspaloy is widely used as hammered material for aviation components.
Waspaloy strength is generally comparable to the Rene 41 alloy and its strength is superior to that of the Inconel 718 alloy at temperatures above 1200-1300 ° F (650-705 ° C). The waspaloy alloy is cold-formable in annealed condition and can also be hot-formed at temperatures of 1900 ° F (1040 ° C) or higher.
| Composition | Standards | Specifications | Key features | Applications | ||||||||||||||||||||||||||||||||||||||||||||||||||
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AMS 5544 AMS 5706 AMS 5708 AMS 5828 ASTM B637 |
W.Nr 2.4654 UNS N07001 AWS 170 |
Very high strength at high temperatures
Its strength is similar to that of the Rene 41 and is much higher than the Inconel 718. It can be subject to aging. |
Gas turbine parts
Parts for aviation industry Spring and fasteners |
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| Density | 8.16 g/cm³ | 0.295 lb/in³ | ||||||||||||||||||||||||||||||||||||||||||||||||||||
| Melting point | 1330°C | 2425°F | ||||||||||||||||||||||||||||||||||||||||||||||||||||
WASPALOY STANDARDS
| HAYNES Waspaloy alloy (N07001) | |
| Waspaloy sheet,plate, strip | AMS 5544 |
| Waspaloy bar, rod, wire | AMS 5704, AMS 5706, AMS 5707, SB 637/B 637 |
| Waspaloy welding wire | AMS 5828 |
| Waspaloy forging | AMS 5704, AMS 5706, AMS 5707, SB 637/ B637 |
