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Magnesium Alloys in Aircraft Seats - Engineering Design and Fabrication Recommended Practices

Aircraft SEAT Committee
  • Aerospace Standard
  • ARP6256
  • Current
Published 2019-10-31 by SAE International in United States
This document is a guide to the application of magnesium alloys to aircraft interior components including but not limited to aircraft seats. It provides background information on magnesium, its alloys and readily available forms such as extrusions and plate. It also contains guidelines for “enabling technologies” for the application of magnesium to engineering solutions including: machining, joining, forming, cutting, surface treatment, flammability issues, and designing from aluminum to magnesium.
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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

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4095E
  • Current
Published 2019-10-01 by SAE International in United States
This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 0.499 inch (0.51 to 12.67 mm) inclusive, in nominal thickness (see 8.4) alclad two sides.
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Ceramic Bound Materials: A Suitable Solution for Light Brakes

2Dto3D S.r.l.s.-Marco Dastrù
Chilches Materials S.A.-José Carlos Serrano-Posada
Published 2019-09-15 by SAE International in United States
A ceramic bound matrix has been investigated to be used as a friction material. The materials were produced by means of ceramic technology using frits containing silicates, and ceramic friction modifiers such as tin oxide, zircon, iron oxide, magnesium oxide. Four formulations were tested by means of a tribometer (pin-on-disc tester) using a gray cast iron counterpart. Test section included speeds between 1 and 12 ms-1, and loads between 25 and 400 N. The coefficient of friction of the tested specimens were between 0.7 and 0.4, and exhibited sensitivity to speed at low loads (25 N), while they are quite stables at high loads (400N). The characterization of the tribolayers was carried out by means of scanning electron microscopy. The four developed materials were named A, B, C, and D. They exhibited different wear rates and coefficients of friction. All the materials exhibited sensitivity to speed, while showed a lower sensitivity to load. The coefficient of friction level seems to be suitable for brake applications, oscillating between 0.6 and 0.4, depending on the test section.…
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Aluminum Alloy, Alclad Sheet and Plate 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075; -T76 Sheet, -T7651 Plate) Solution and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4316B
  • Current
Published 2019-09-10 by SAE International in United States
This specification covers an aluminum alloy in the form of Alclad sheet and plate 0.040 to 1.000 inch, incl (1.02 to 25.40 mm, incl) in nominal thickness (see 8.4).
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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

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4041T
  • Current
Published 2019-09-03 by SAE International in United States
This specification covers an aluminum alloy in the form of sheet and plate alclad two sides, over 0.187 to 1.000 inch (over 4.750 to 25.40 mm) in nominal thickness, supplied in the -T3/-T351 temper.
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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)

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4186E
  • Current
Published 2019-08-01 by SAE International in United States
This specification covers an aluminum alloy in the form of bars, rods, and wire, in the sizes shown in 3.3.3, in the “as fabricated (F) temper” (see 8.5). When specified, product shall be supplied in the annealed (O) condition.
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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

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4122M
  • Current
Published 2019-08-01 by SAE International in United States
This specification covers an aluminum alloy in the form of rolled or cold finished bars, rods, and wire, and of flash welded rings conforming to the dimensions listed in Table 2 (see 8.4).
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Aluminum Alloy, Clad One Side, Sheet 1.25Mn - 0.12Cu (No. 11-0 Brazing Sheet) Annealed

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4063F
  • Current
Published 2019-07-18 by SAE International in United States
This specification covers an aluminum alloy in the form of clad sheet from 0.006 to 0.249 inches (0.15 to 6.32 mm), inclusive, in thickness (see 8.6).
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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

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4319C
  • Current
Published 2019-07-12 by SAE International in United States
This specification covers an aluminum alloy in the form of bars and rods 0.750 to 3.500 inches (19.05 to 88.90 mm), inclusive, in nominal diameter or least distance between parallel sides (see 8.5).
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Shear Assisted Processing and Extrusion

  • Magazine Article
  • TBMG-34754
Published 2019-07-01 by Tech Briefs Media Group in United States

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.

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