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Magnesium Alloys in Aircraft Seats - Engineering Design and Fabrication Recommended Practices
- Aerospace Standard
- ARP6256
- Current
Aluminum Alloy, Alclad Sheet and Plate 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti Alclad 2219-T31; Sheet, Solution Heat Treated and Cold Worked Alclad 2219-T351; Plate, Solution Heat Treated and Stress Relieved
- Aerospace Material Specification
- AMS4095E
- Current
Ceramic Bound Materials: A Suitable Solution for Light Brakes
- Technical Paper
- 2019-01-2109
- DOI: https://doi.org/10.4271/2019-01-2109
Aluminum Alloy, Alclad Sheet and Plate 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075; -T76 Sheet, -T7651 Plate) Solution and Precipitation Heat Treated
- Aerospace Material Specification
- AMS4316B
- Current
Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (2024, -T3 Sheet/-T351 Plate with 1-1/2% Alclad) Solution Heat Treated, Cold Worked and Naturally Aged
- Aerospace Material Specification
- AMS4041T
- Current
Aluminum Alloy Bars, Rods, and Wire, Rolled or Cold Finished 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-F) As Fabricated, or When Specified, Annealed (7075-O)
- Aerospace Material Specification
- AMS4186E
- Current
Aluminum Alloy Bars, Rods, and Wire Rolled or Cold Finished, and Rings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T6, 7075-T651) Solution and Precipitation Heat Treated
- Aerospace Material Specification
- AMS4122M
- Current
Aluminum Alloy, Clad One Side, Sheet 1.25Mn - 0.12Cu (No. 11-0 Brazing Sheet) Annealed
- Aerospace Material Specification
- AMS4063F
- Current
Aluminum Alloy, Rolled or Cold Finished, Bars and Rods 12.2Si - 1.0Mg - 0.90Cu - 0.90Ni (4032-T651) Solution Heat Treated, Stress Relieved, Artificially Aged
- Aerospace Material Specification
- AMS4319C
- Current
Shear Assisted Processing and Extrusion
- Magazine Article
- TBMG-34754
Shear Assisted Processing and Extrusion (ShAPE™) allows creation of wire, bar, and tubular extrusions that show significant improvement in material properties; for example, magnesium extrusions have been manufactured with unprecedented ductility (how far the material can stretch before it breaks) and energy absorption (how much energy can be absorbed during compression of a tubular extrusion) over conventional methods.