Nimonic PK33/ SAE AMS 5829; AECMA Pr EN 2295 Strip Sheet bar
overview
Alloy PK33 is a superalloy which is highly resistant to thermal shock and thermal fatigue. It is a vacuum processed nickelbase alloy that was developed to provide a sheet
material offering improved ductility in welded
assemblies and high creep strength to replace
NIMONIC alloys 80A and 90
Alloy PK33 also offers superb weldability, is often used in high strength applications at elevated temperatures, such as in gas turbine hot sections or enclosures for industrial furnace hot sections.
Limiting Chemical Composition, %
Carbon ..................................................................................................................................................................................0.07 max.
Silicon....................................................................................................................................................................................0.50 max.
Copper...................................................................................................................................................................................0.20 max.
Iron........................................................................................................................................................................................1.00 max.
Manganese...........................................................................................................................................................................0.50 max.
Chromium........................................................................................................................................................................16.00--20.00
Titanium...............................................................................................................................................................................1.50--3.00
Aluminum.............................................................................................................................................................................1.70--2.50
Sulfur...................................................................................................................................................................................0.015 max.
Silver.................................................................................................................................................................................0.0005 max.
Cobalt...............................................................................................................................................................................12.00--16.00
Molybdenum........................................................................................................................................................................5.00--9.00
Boron...................................................................................................................................................................................0.005 max.
Zirconlum...............................................................................................................................................................................0.06 max.
Sulfur...................................................................................................................................................................................0.015 max.
Nicke........................................................................................................................................................................................Balance.
Physical Constants
Below are some physical constants and thermal properties of
Density |
Mg/m3...................................................................................8.00 |
lb/in3...................................................................................0.289 | |
Melting Range |
Liquidus Temperature °C....................................................1355 |
Solidus Temperature °C......................................................1310 |
Mechanical properties
Properties |
Metric |
Imperial |
Tensile strength (precipitation hardened, value at room temperature) |
900MPa |
131000 psi |
Yield strength (@strain 0.200%, precipitation hardened, value at room temperature) |
450MPa |
653000psi |
Elongation at break (precipitation hardened) |
28% |
28% |
Corrosion Resistance
Nimonic PE11 offers exceptional strength, corrosion resistance, and creep and fatigue resistance at elevated temperatures. This advanced material is used in a range of applications, including aerospace, power generation, and industrial processes.
Forming
Nimonic PE16™ has good ductility and can be easily formed using all the conventional methods. This alloy is stronger than regular steel; hence it requires a more powerful equipment to complete the forming process. It is recommended that heavy-duty lubricants be used while cold forming. At the end of this process all traces of lubricant has to be cleaned off to prevent embrittlement.
Welding
Nimonic PE16™ can be welded using traditional welding methods. Some of the commonly used methods are shielded metal-arc welding, gas metal-arc welding, submerged-arc welding, and gas-tungsten arc welding. It is recommended that matching alloy filler metal should be used and that the weld beads should be slightly convex. Before the welding process begins, the surface to be welded should be cleaned and should be free from oil, paint or crayon stains.
Heat Treatment
Nimonic PE16™ has to be solution annealed at 1038°C (1900°F) for 4 h and then air cooled. This process is repeated twice at 799°C (1470°F) for 2 h and air cooled, and at 699°C (1290°F) for 16 h and air cooled, so as to complete the precipitation hardening process.
Available Forms
We provide you with a variety of product forms, including but not limited to.
● Strips & Tape
● Wire & Welding
● Pipe & Tube
● Sheet & Foils
● Flanges & Forgins
description2



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