Nickel Alloy, Brazing Filler Metal 71Ni 10Si 19Cr, 1975 to 2075°F (1080 to 1135°C) Solidus-Liquidus Range
- Aerospace Material Specification
This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of powder in a suitable binder.
This filler metal has been used typically for joining corrosion and heat resistant steels and alloys requiring corrosion and oxidation resistant joints with good strength at elevated temperatures, but usage is not limited to such applications.
|Aerospace Material Specification||Nickel Alloy, Brazing Filler Metal 73Ni - 0.75C - 4.5Si - 14Cr - 3.1B - 4.5Fe 1790 °F (977 °C) Solidus to 1970 °F (1077 °C) Liquidus|
|Aerospace Material Specification||Nickel Alloy, Brazing Filler Metal 82Ni - 4.5Si - 7.0Cr - 3.1B - 3.0Fe 1780 °F (971 °C) Solidus to 1830 °F (999 °C) Liquidus Range|
|Aerospace Material Specification||Nickel Alloy, Brazing Filler Metal 92Ni - 4.5Si - 3.1B 1800 to 1900 °F Solidus-Liquidus Range|
Data Sets - Support Documents
The committee of Corrosion and Heat Resistant Steels and Alloys and Specialty Steels and Alloys, AMS Committee F, will prepare, coordinate, and revise documents related to corrosion and heat resistant steels and alloys and specialty steels and alloys technology, such as stainless steels and nickel and base alloys, through the participation of metals suppliers, users, and interested government agencies. Committee activities shall provide a forum for the cooperative interchange of ideas and experience of the participants, resulting in the publication of specifications that embody sound, established aerospace industry practices and requirements to serve the suppliers and customers of aerospace materials.