UNS N07001 AMS 5544 Sheet Nickel Alloys
UNS N07001 AMS 5544 Sheet Nickel Alloys Manufacturer
AMS 5544 is a specification of Nickel Waspaloy, which is a nickel-base age-hardenable superalloy with excellent high-temperature strength and good corrosion resistance by combustion products. This superalloy that can be used at temperatures up to 1200°F (650°C) for critical rotating applications, such as rotating parts, and up to 1600°F (870°C) for less demanding applications. It is available as plate, sheet, and strip. We are the best manufacturer of UNS N07001 AMS 5544 Sheet Nickel Alloys
Table of Contents
ToggleThe AMS 5544 specification is intended for parts that require high-temperature creep and stress rupture properties. The heat treatment is as follows:
- Annealing – heat to 1975°F (1080°C), and then air cool for 30 minutes;
- Solution heat treatment – heat to 1825°F (995°C) and then air cool for 2 hours;
- Stabilization treatment – reheat to 1550°F (845°C), and air cool for 4 hours;
- Age hardening – reheat to 1400°F (760°C), and air cool for 16 hours to produce hardness of 33-44 Rockwell C.
Please note that scale may be formed on the alloy during heat treatment in oxidizing atmospheres. However, this doesn’t affect the properties of the alloy and can be removed by acid pickling or mechanically.
AMS 5544 can be readily welded only in carefully controlled circumstances, using argon-arc methods and the Waspaloy AMS 5828 filler metal. Welds should be avoided in high-stress environments.
Hot working of AMS 5544 is done at 2140-1800°F (1170-980°C), while hydroforming, drawing, spinning, bending, and rolling can be used for cold working.
Attribute | Value |
AMS Number | AMS 5544 |
Alloy | Waspaloy |
Type | Nickel |
UNS | N07001 |
Cross Reference Spec | – |
Misc./Shape | Waspaloy-sheet |
Nickel Superalloy Waspaloy
Technical Data Sheet
WASPALOY is a nickel based age hardenable alloy that possesses high temperature strength while still having a good corrosion resistance, especially to oxidation. WASPALOY can be used at temperatures up to 650°C (1200°F) which is critical rotating applications. WASPALOY is used in gas turbine engine components, missile systems, shafts, spacers, seals, rings, casings, fasteners and many other uses in engine hardware, airframe assemblies. Pankh Steel is the leading UNS N07001 AMS 5544 Sheet Nickel Alloys Manufacturer in India.
Chemical Composition Limits | |||||||||||||||
Weight % | Cr | B | Zr | Al | Ti | Mo | Co | Cu | Fe | S | Si | Mn | C | P | Ni |
Waspaloy | 18-21 | 0.003-00.1 | 0.02-0.12 | 1.2-1.6 | 2.75-3.25 | 3.5-5.0 | 12-15 | 0.50 max | 2 max | 0.030 max | 0.75 max | 1 max | 0.02-0.10 max | 0.030 max | Bal |
Typical Mechanical Properties
Material | Condition | Thickness | Temp | Tensile Strength ksi | Yield Strength ksi | Elongation in 4D | Hardness HRC |
Sheet | Sol Treated, Stabilization + Precipitation HT | 0-0.020″ | Room | 170 | 110 | 15 | 34-44 |
Sheet | Sol Treated, Stabilization + Precipitation HT | 0-0.020″ | 1000°F | 145 | 100 | 13 | |
Sheet | Sol Treated, Stabilization + Precipitation HT | over 0.020″ | Room | 175 | 115 | 20 | 34-44 |
Sheet | Sol Treated, Stabilization + Precipitation HT | over 0.020″ | 1000°F | 150 | 105 | 15 |
Properties as per AMS 5544. Heat Treatment is as follows:
- Annealing 1975°F / 30 mins and Air Cool
- Solution Heat Treatment 1825°F / 2hrs and Air Cool
- Stabilization Heat Treatment 1550°F /4hrs and Air Cool
- Precipitation Heat Treatment 1400°F / 16 hrs and Air Cool
Bar Properties
- Properties as per AMS 5708 type 2 (capable of AMS 5709) Heat Treatment is as follows
- Solution Treat 1900 – 1975°F / 1-4 hours and Air Cool
- Resulting hardness not higher than 302HB
- Stabilization Heat Treatment Heat to 1550°F / 4 hrs and Air Cool
- Precipitaion Heat Treatment Heat to 1400°F / 16 hrs and Air Cool
- Resulting hardness 32-42 HRC
Availability
WASPALOY is available in Round Bar, Flat Bar, Forging Stock, Extruded Section, Wire, Plate, Sheet, Strip and Welding Wire. For all stock availability contact Sales.
Specifications
- Rod, Bar, Wire and Forging Stock
- ASTM B 637, ISO 9723, ISO 9724, ISO 9725, AMS 5704, AMS 5706, AMS 5707, AMS 5708, AMS 5709, AMS 5828, MAM 5706, AECMA PrEN 2193, AECMA PrEN 2194, AECMA PrEN 2406, AECMA PrEN 2958, AECMA PrEN 2959, AECMA PrEN 2960, AECMA PrEN 3220.
Plate, Sheet and Strip
AMS 5544, AECMA PrEN 2195
Other
UNS N07001, W. Nr 2.4654, MSRR 7192
Technical Data Sheet
WASPALOY is a nickel based age hard enable alloy that possesses high temperature strength while still having a good corrosion resistance, especially to oxidation. WASPALOY can be used at temperatures up to 650°C (1200°F) which is critical rotating applications. WASPALOY is used in gas turbine engine components, missile systems, shafts, spacers, seals, rings, casings, fasteners and many other uses in engine hardware, airframe assemblies.
Chemical Composition Limits | |||||||||||||||
Weight % | Cr | B | Zr | Al | Ti | Mo | Co | Cu | Fe | S | Si | Mn | C | P | Ni |
Waspaloy | 18-21 | 0.003-00.1 | 0.02-0.12 | 1.2-1.6 | 2.75-3.25 | 3.5-5.0 | 12-15 | 0.50 max | 2 max | 0.030 max | 0.75 max | 1 max | 0.02-0.10 max | 0.030 max | Bal |
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