Browse Topic: Magnesium alloys

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Liquid Runway Deicing/Anti-icing ProductAMS1435E (Current)03/12/2024
This specification covers runway deicing and anti-icing products in the form of a liquid. Unless otherwise stated, all specifications referenced herein are latest (current) revision.
G-12RDP Runway Deicing Product Committee
Liquid Runway Deicing/Anti-icing ProductAMS1435E-TEST-REC (Current)03/12/2024
This specification covers runway deicing and anti-icing products in the form of a liquid. Unless otherwise stated, all specifications referenced herein are latest (current) revision.
G-12RDP Runway Deicing Product Committee
Enhancing Microstructural Characteristics and Mechanical Properties in Friction Stir Welding of Thick Magnesium Alloy Plates through Optimization2024-01-501402/06/2024
This research explores friction stir welding (FSW) to examine the mechanical characteristics and microstructure of thick plates manufactured from the Mg-8Al-0.5Zn alloy. Applying the FSW procedure to warm-form an Mg-8Al-0.5Zn alloy for the differential case covering the gears in the car’s automotive technology. Weld quality was significantly improved after using response surface methodology (RSM) to examine various welding parameters and find the best configurations. Improved grain refinement and phase distribution in the weld zone were found in the microstructural study of 11.5 mm thick magnesium alloy plates using RSM-optimized parameters. By dynamic recrystallization, the grain size was reduced to 16 μm, which is fifteen times smaller than the original material, thanks to the good results of single-pass FSW welding. Welding results showing high-quality characteristics such as tensile strength (161.8 MPa), elongation (27.83%), and joint efficiency (98.96%) were achieved using the
Sabari, K., Muniappan, A., Singh, Mandeep
test 03/01auto testauto testauto testauto testauto testauto testauto testauto testauto testauto testauto testSAE-PP-0780701/03/2023
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Mutagaana, Festo
abc test 30/12auto testauto testauto testauto testauto testauto testauto testauto testauto testauto testauto testauto testauto testSAE-PP-0780612/30/2022
Mutagaana, F., "QE Testing 11/2-10 jms edit," SAE MobilityRxiv™ Preprint, submitted November 2, 2022, https://doi.org/10.47953/SAE-PP-07790.
Mutagaana, Festo
Magnesium Sheet Component Development and Demonstration Project2022-01-028603/29/2022
Most of the applications of magnesium in lightweighting of commercial cars and trucks are die castings rather than sheet metal, and automotive applications of magnesium sheet have typically been experimental or low-volume serial production. The overarching objective of project was to develop new low-cost magnesium alloys, and demonstrate warm-stamping of magnesium sheet inner and outer door panels from a 2013 MY Ford Fusion at a fully accounted integrated component cost increase over conventional steel stamped components of no more than $2.50/lb. saved. The project demonstrated the computational design of new Mg alloys from atomistic levels, cast new experimental alloy ingots and explored thermo-mechanical rolling processes to produce thin Mg sheet of desired texture. A new commercial Mg alloy sheet material was sourced and pretreated with protective coil coatings, and its properties fully characterized. The Mg sheet was warm-formed using novel lubricants into intermediate size
Gerken, Randy T., Ghaffari, Bita, Sachdev, Anil K., Mehta, Manish, Carter, Jon T.
Aluminum Alloy, Extruded Profiles (2065-T84) 4.2Cu - 1.2Li - 0.52Mg - 0.32Mn - 0.32Ag - 0.1Zr Solution Heat Treated, Stress Relieved by Stretching and Artificially AgedAMS4366A (Current)10/28/2021
This specification covers an aluminum-lithium alloy in the form of extruded profiles with a maximum cross-sectional area of 19 in2 (123 cm2) and a maximum circle size of 11 inches (279 mm) from 0.040 to 0.499 inch (1.00 to 12.50 mm) in thickness (see 8.7).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Extruded Profiles (2065-T84) 4.2Cu - 1.2Li - 0.52Mg - 0.32Mn - 0.32Ag - 0.1Zr Solution Heat Treated, Stress Relieved by Stretching and Artificially AgedAMS4366A-TEST-REC (Historical)10/28/2021
This specification covers an aluminum-lithium alloy in the form of extruded profiles with a maximum cross-sectional area of 19 in2 (123 cm2) and a maximum circle size of 11 inches (279 mm) from 0.040 to 0.499 inch (1.00 to 12.50 mm) in thickness (see 8.7).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Plate 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T7451) Solution Heat Treated, Stress Relieved, and Precipitation Heat TreatedAMS4205F (Current)10/22/2021
This specification covers an aluminum alloy in the form of plate up to 5.500 inches (139.70 mm), inclusive in thickness (see 8.5).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Plate 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T7451) Solution Heat Treated, Stress Relieved, and Precipitation Heat TreatedAMS4205F-TEST-REC (Historical)10/22/2021
This specification covers an aluminum alloy in the form of plate up to 5.500 inches (139.70 mm), inclusive in thickness (see 8.5).
AMS D Nonferrous Alloys Committee
Rings, Flash Welded Aluminum and Aluminum AlloysAMS7488G (Current)10/18/2021
This specification covers flash welded rings made of aluminum and aluminum alloys.
AMS D Nonferrous Alloys Committee
Aluminum Alloy Sheet and Plate, Alclad One Side 4.4Cu - 1.5Mg - 0.60Mn (Clad One Side 2024-O) AnnealedAMS4077J (Current)10/15/2021
This specification covers an aluminum alloy in the form of sheet and plate from 0.010 to 0.499 inch (0.25 to 12.67 mm), inclusive, in thickness (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy Sheet and Plate, Alclad One Side 4.4Cu - 1.5Mg - 0.60Mn (Clad One Side 2024-O) AnnealedAMS4077J-TEST-REC (Historical)10/15/2021
This specification covers an aluminum alloy in the form of sheet and plate from 0.010 to 0.499 inch (0.25 to 12.67 mm), inclusive, in thickness (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Plate, 7.9Zn - 1.8Cu - 2.0Mg - 0.10Zr (7099-T7651) Solution Heat Treated, Stress Relieved, and OveragedAMS4364A (Current)09/15/2021
This specification covers an aluminum alloy in the form of plate from 1.000 to 6.000 inches (25.40 to 152.40 mm) in thickness (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy Extrusions 8.9Zn - 2.2Cu - 2.2Mg - 0.15Zr (7136-T76511, -T76510) Solution Heat Treated, Stress-Relieved, Straightened, and OveragedAMS4415B (Current)09/15/2021
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles (shapes), and tubing 0.040 to 4.000 inches (1.00 to 100.00 mm) in nominal diameter, least dimension, or wall thickness (see 8.7).
AMS D Nonferrous Alloys Committee
Aluminum Alloy Extrusions 8.9Zn - 2.2Cu - 2.2Mg - 0.15Zr (7136-T76511, -T76510) Solution Heat Treated, Stress-Relieved, Straightened, and OveragedAMS4415B-TEST-REC (Historical)09/15/2021
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles (shapes), and tubing 0.040 to 4.000 inches (1.00 to 100.00 mm) in nominal diameter, least dimension, or wall thickness (see 8.7).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Plate, 7.9Zn - 1.8Cu - 2.0Mg - 0.10Zr (7099-T7651) Solution Heat Treated, Stress Relieved, and OveragedAMS4364A-TEST-REC (Historical)09/15/2021
This specification covers an aluminum alloy in the form of plate from 1.000 to 6.000 inches (25.40 to 152.40 mm) in thickness (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Sheet and Plate 4.0Cu - 1.0Li - 0.40Mg - 0.35Ag - 0.13Zr (2195-T8) Solution Heat Treated, Cold Worked, and Artificially AgedAMS4474B (Current)09/13/2021
This specification covers an aluminum alloy in the form of sheet and plate with a thickness of 0.125 to 0.499 inch (3.20 to 12.67 mm), inclusive (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Sheet and Plate 4.0Cu - 1.0Li - 0.40Mg - 0.35Ag - 0.13Zr (2195-T8) Solution Heat Treated, Cold Worked, and Artificially AgedAMS4474B-TEST-REC (Historical)09/13/2021
This specification covers an aluminum alloy in the form of sheet and plate with a thickness of 0.125 to 0.499 inch (3.20 to 12.67 mm), inclusive (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Sheet 3.2Cu - 0.52Mg - 0.30Ag - 0.95 Li - 0.12Zr (2198-T8) Solution Heat Treated, Cold Worked, and Artificially AgedAMS4412B (Current)08/12/2021
This specification covers an aluminum alloy in the form of sheet from 0.063 to 0.249 inches (1.60 to 6.30 mm) in nominal thickness (see 8.7).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Sheet 3.2Cu - 0.52Mg - 0.30Ag - 0.95 Li - 0.12Zr (2198-T8) Solution Heat Treated, Cold Worked, and Artificially AgedAMS4412B-TEST-REC (Historical)08/12/2021
This specification covers an aluminum alloy in the form of sheet from 0.063 to 0.249 inches (1.60 to 6.30 mm) in nominal thickness (see 8.7).
AMS D Nonferrous Alloys Committee
Salts, Heat-Treating (For Metals)AMS2821 (Current)08/06/2021
This specification covers the procurement of granular heat-treating salts suitable for use in the molten state.
AMS B Finishes Processes and Fluids Committee
Inspection, Ultrasonic, Wrought Metals, Process forAMSSTD2154E (Current)07/15/2021
The purpose of this standard is to provide uniform methods for the ultrasonic inspection of wrought metals and wrought metal products.
AMS K Non Destructive Methods and Processes Committee
Inspection, Ultrasonic, Wrought Metals, Process forAMSSTD2154E-TEST-REC (Historical)07/15/2021
The purpose of this standard is to provide uniform methods for the ultrasonic inspection of wrought metals and wrought metal products.
AMS K Non Destructive Methods and Processes Committee
The Chemical Milling ProcessARP1331C (Current)07/15/2021
This practice provides recommendations concerning the chemical milling of aluminum, magnesium, high temperature nickel alloys, titanium alloys, copper alloys, and specialty alloys.
AMS B Finishes Processes and Fluids Committee
Aluminum Alloy Forgings and Rolled or Forged Rings and Forging Stock 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061 - T4) Solution Heat Treated and Naturally AgedAMS4146H (Current)07/07/2021
This specification covers an aluminum alloy in the form of die forgings up to 4 inches (102 mm), hand forgings up to 8 inches (203 mm), rolled or forged rings up to 2.5 inches (63.5 mm) in thickness, and forging stock (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Clad One Side Sheet 0.6Mg - 0.35Si - 0.28Cu (No. 23 Brazing Sheet) As FabricatedAMS4465B (Current)07/07/2021
This specification covers an aluminum alloy in the form of sheet, clad on one side.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Welding Wire 7.0Si - 0.52Mg (357)AMS4246F (Current)07/07/2021
This specification covers an aluminum alloy in the form of welding wire.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Clad Two Sides Sheet 0.6Mg - 0.35Si - 0.28Cu (No. 24 Brazing Sheet) As FabricatedAMS4460B (Current)07/07/2021
This specification covers an aluminum alloy in the form of sheet, clad on two sides.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Clad Two Sides Sheet 0.6Mg - 0.35Si - 0.28Cu (No. 24 Brazing Sheet) As FabricatedAMS4460B-TEST-REC (Historical)07/07/2021
This specification covers an aluminum alloy in the form of sheet, clad on two sides.
AMS D Nonferrous Alloys Committee
Aluminum Alloy Forgings and Rolled or Forged Rings and Forging Stock 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061 - T4) Solution Heat Treated and Naturally AgedAMS4146H-TEST-REC (Historical)07/07/2021
This specification covers an aluminum alloy in the form of die forgings up to 4 inches (102 mm), hand forgings up to 8 inches (203 mm), rolled or forged rings up to 2.5 inches (63.5 mm) in thickness, and forging stock (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Clad One Side Sheet 0.6Mg - 0.35Si - 0.28Cu (No. 23 Brazing Sheet) As FabricatedAMS4465B-TEST-REC (Historical)07/07/2021
This specification covers an aluminum alloy in the form of sheet, clad on one side.
AMS D Nonferrous Alloys Committee
Aluminum Alloy Bars, Rolled or Cold Finished 1.0Mg - 0.60Si - 0.30Cu - 0.20Cr (6061-T451) Solution Heat Treated and Stress Relieved by StretchingAMS4128E (Current)06/28/2021
This specification covers an aluminum alloy in the form of bars and rods 0.500 inch (12.7 mm) to 8.000 inches (203.2 mm) in nominal diameter or least difference between parallel sides and up to 50 square inches (322.6 square centimeters) in cross-sectional area (see 8.7).
AMS D Nonferrous Alloys Committee
Aluminum Alloy Bars, Rolled or Cold Finished 1.0Mg - 0.60Si - 0.30Cu - 0.20Cr (6061-T451) Solution Heat Treated and Stress Relieved by StretchingAMS4128E-TEST-REC (Historical)06/28/2021
This specification covers an aluminum alloy in the form of bars and rods 0.500 inch (12.7 mm) to 8.000 inches (203.2 mm) in nominal diameter or least difference between parallel sides and up to 50 square inches (322.6 square centimeters) in cross-sectional area (see 8.7).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Extrusions 0.68Mg - 0.40Si (6063-T6) Solution and Precipitation Heat TreatedAMS4156L (Current)06/10/2021
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing up to and including 1.000 inch (25.4 mm) in diameter, least thickness, or tube wall thickness (see 8.7).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Extrusions 0.68Mg - 0.40Si (6063-T6) Solution and Precipitation Heat TreatedAMS4156L-TEST-REC (Historical)06/10/2021
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing up to and including 1.000 inch (25.4 mm) in diameter, least thickness, or tube wall thickness (see 8.7).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Plate 4.0Zn - 2.0Mg - 0.32Mn (7019-T651) Solution Heat Treated, Stress Relieved, and Artificially AgedAMS4409A (Current)05/18/2021
This specification covers an aluminum alloy in the form of plate 0.500 to 4.500 inch (12.7 to 114.3 mm), inclusive, in nominal thickness (see 8.5).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Plate 4.0Zn - 2.0Mg - 0.32Mn (7019-T651) Solution Heat Treated, Stress Relieved, and Artificially AgedAMS4409A-TEST-REC (Historical)05/18/2021
This specification covers an aluminum alloy in the form of plate 0.500 to 4.500 inch (12.7 to 114.3 mm), inclusive, in nominal thickness (see 8.5).
AMS D Nonferrous Alloys Committee
Aluminum Alloy Die Forgings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73) Solution and Precipitation Heat TreatedAMS4141H (Current)04/28/2021
This specification covers an aluminum alloy in the form of die forgings up to 6 inches in thickness and forging stock of any size ordered to inch/pound units (see 8.8).
AMS D Nonferrous Alloys Committee
Aluminum Alloy Die Forgings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73) Solution and Precipitation Heat TreatedAMS4141H-TEST-REC (Historical)04/28/2021
This specification covers an aluminum alloy in the form of die forgings up to 6 inches in thickness and forging stock of any size ordered to inch/pound units (see 8.8).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated, Stress Relieved, and OveragedAMS4050K (Current)04/22/2021
This specification covers an aluminum alloy in the form of plate.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated, Stress Relieved, and OveragedAMS4050K-TEST-REC (Historical)04/22/2021
This specification covers an aluminum alloy in the form of plate.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Rolled or Cold-Finished, Bars, Rods, Wire, and Flash Welded Rings and Stock for Flash Welded Rings Annealed 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-O)AMS4115K (Current)04/14/2021
This specification covers an aluminum alloy in the form of rolled or cold-finished bars, rods, and wire, of flash welded rings, and of stock for flash welded rings.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Bars, Rods, and Wire 1.0Mg - 0.60Si - 0.30Cu - 0.20Cr (6061-T4) Cold Finished, Solution Heat Treated and Naturally AgedAMS4116K (Current)04/14/2021
This specification covers an aluminum alloy in the form of bars, rods, and wire.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Bars, Rods, and Wire 1.0Mg - 0.60Si - 0.30Cu - 0.20Cr (6061-T4) Cold Finished, Solution Heat Treated and Naturally AgedAMS4116K-TEST-REC (Historical)04/14/2021
This specification covers an aluminum alloy in the form of bars, rods, and wire.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Rolled or Cold-Finished, Bars, Rods, Wire, and Flash Welded Rings and Stock for Flash Welded Rings Annealed 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-O)AMS4115K-TEST-REC (Historical)04/14/2021
This specification covers an aluminum alloy in the form of rolled or cold-finished bars, rods, and wire, of flash welded rings, and of stock for flash welded rings.
AMS D Nonferrous Alloys Committee
Cleaner, Aircraft Glass WindowAMS1534C (Current)04/07/2021
This specification covers two types of aircraft glass window cleaners in the form of a ready-to-use liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-O) AnnealedAMS4476A (Current)02/11/2021
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing up to 5.000 inches (127.00 mm), inclusive in nominal diameter or least thickness (bars, rods, wire, profiles) or nominal wall thickness (tubing) (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-O) AnnealedAMS4476A-TEST-REC (Historical)02/11/2021
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing up to 5.000 inches (127.00 mm), inclusive in nominal diameter or least thickness (bars, rods, wire, profiles) or nominal wall thickness (tubing) (see 8.6).
AMS D Nonferrous Alloys Committee
A Comparative Life Cycle Assessment of Magnesium Front End Autoparts: A Revision to 2010-01-0275SAE-PP-0018501/29/2021
The Magnesium Front End Research and Development (MFERD) project under the sponsorship of Canada, China, and USA aims to develop key technologies and a knowledge base for increased use of magnesium in automobiles. The primary goal of this life cycle assessment (LCA) study is to compare the energy and potential environmental impacts of advanced magnesium based front end parts of a North American-built 2007 GM-Cadillac CTS using the current steel structure as a baseline. An aluminium front end is also considered as an alternate light structure scenario. A “cradle-to-grave” LCA is conducted by including primary material production, semi-fabrication production, autoparts manufacturing and assembly, transportation, use phase, and end-of-life processing of autoparts. This LCA study was done in compliance with international standards ISO 14040:2006 [1] and ISO 14044:2006 [2]. While weight savings result in reductions of energy use and climate change emissions during the use phase of the car
Mutagaana, Festo
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