PROPRIETARY Carpenter Waspaloy Nickel Alloys
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PROPRIETARY Carpenter Waspaloy Chemical Composition
Carpenter Technology Corporation, Product Data Sheets,
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PROPRIETARY Carpenter Waspaloy Physical Properties
Temperature
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PROPRIETARY Carpenter Waspaloy Heat Treatments
- Annealing: Hardening and strength properties are developed by precipitation of gamma prime (Ni3TiAl). The solution temperature for gamma prime is normally 1032/1043°C (1890/1910°F). This is also the temperature range at which grain growth begins. Annealed, or low hardness can be obtained only by cooling very rapidly from temperatures above the gamma prime solvus. Water quenching will result in hardnesses as low as Rockwell B 90, while air cooling will result in Rockwell C 28/30. Uniform low hardness cannot be obtained on sections having considerable mass. Air cooling is desirable for large sections.
Solution treatment: Best stress rupture and creep properties are generally obtained by high temperature solution treatments, 1038/1079°C (1900/1975°F). The 1975°F (1079°C) temperature will result in coarse grain size and lower tensile yield strength. If the alloy is treated below solvus temperature at, for example, a temperature of 1010°C (1850°F), the as-hot-worked grain size will be retained and high tensile yield strength will result, with some loss in stress-rupture properties. A practical compromise for adequate rupture properties, acceptable tensile properties and moderate grain growth is: solution treat just above the gamma prime solvus temperature, 1024/1038°C (1875/1900°F). Rotating parts are generally treated toward the low side, 1018/1024°C (1865/1875°F). For rupture-oriented applications, treating toward the high side, 1038/1051°C (1900/1925°F), is suggested.
Age: The normal aging treatment is: stabilize 843°C (1550°F) 4 hours, air cool, followed by precipitation aging 760°C (1400°F) 16 hours, air cool
PROPRIETARY Carpenter Waspaloy Mechanical Properties
Temperature
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PROPRIETARY Carpenter Waspaloy International Equivalent Materials
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- 15Cross References
- 14Composition
- 54Mechanical Properties
- 31Physical Properties
- 1Heat Treatment
- 1Metallography
- -Machinability
- 12Stress-Strain
- -Formability
- -Fatigue
- -Fracture
- 6Creep
- -Joints
- -Coatings
- -Dimensions
- -Tribology
- -Corrosion
- -Ageing
- -Weatherability
- -Irradiation
- 13Total Suppliers