DP2790 Waspaloy Powder (UNS N07001)

Catalog No. DP2790
Appearance Gray metallic powder
Grade Alloy Grade: Waspaloy Related Grades: Waspaloy (A

Waspaloy (UNS N07001) Powder can be bought at Stanford Advanced Materials (SAM). With rich experience and knowledge in the metals industry, SAM is a global manufacturer of high-quality Waspaloy Powder.

Related Products: Alloy 188 PowderHastelloy X PowderInconel 625 PowderInconel 718 Powder

 

Waspaloy Powder Description

Waspaloy (UNS N07001) is an age-hardenable, nickel-based superalloy with very good strength at temperatures up to about 1800°F (980°C). It is widely used as a wrought material for forged and fabricated gas turbine and aerospace components. Its strength is generally comparable to R41 alloy, and is superior to that of alloy 718 at temperatures above 1200-1300°F (650-705°C). Waspaloy is typically used in high-temperature applications, particularly in gas turbines.

Stanford Advanced Materials (SAM) is a worldwide supplier of high-quality Waspaloy (UNS N07001) Powder who has over two decades of experience in the manufacture and sale of Waspaloy (UNS N07001) products.

 

Waspaloy Powder Specifications

Product Name

Waspaloy (UNS N07001) Powder

Alloy Grade

Waspaloy

Related Grades

Waspaloy (Am)
Nc20K14(Fr)

Composition

C 0.03-0.10
Cr 18.0-21.0
Ni Bal
Co 12.0-15.0
Mo 3.50-5.00
Al 1.20-1.60
Ti 2.75-3.25
B 0.003-0.010

Zr 0.02-0.08
Fe 2.0 max
B 0.010 max
Cu 0.15 max
Mn 0.15 max
Si 0.015 max
P 0.015 max
S 0.10 max

Size Grades

-105+45micron

-53+15micron

ASTM

/

AMS Specification

5706, 5707, 5708, 5709

 

Waspaloy Powder Applications

Waspaloy Powder is often used in extreme environments. It is common in gas turbine blades, seals, rings, shafts, and turbine disks. The NIST certified reference material 1243, a standard for X-ray fluorescence spectroscopy is made from Waspaloy. Waspaloy alloy can be cold-formed in the annealed condition, and may also be hot-formed at temperatures of 1900°F (1040°C) or above. Weldability is somewhat limited by susceptibility to strain age cracking under conditions of heavy restraint. The alloy exhibits good resistance to gas turbine combustion environments at temperatures up to about 1600°F (870°C).

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