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AMS Index - January 2020

  • Index
  • AMSJAN-2020
To be published on 2020-02-20 by SAE International in United States
No Abstract Available.
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Characterization of Friction Stir Processed Aluminum-Graphene Nanoplatelets Composites

SAE International Journal of Materials and Manufacturing

Sree Vidyanikethan Engineering College, India-P. Bhanu Prakash, P.C. Krishnamachary, K.C. VaraPrasad
  • Journal Article
  • 05-13-02-0007
Published 2020-01-23 by SAE International in United States
The present study deals with the investigation on microstructural and mechanical properties of friction stir processed (FSPed) pure Aluminum (Al)-Graphene Nanoplatelets (GNPs) composites. Composite specimens such as castings were made by blending 0.5 wt.%, 1.0 wt.%, 1.5 wt.%, and 2.0 wt.% of GNPs in pure Al matrix using the ultrasonic-assisted stir casting technique (UASCT). Also for enhancement of mechanical properties via grain refinement the friction stir processing (FSP) has been employed, as well as mechanical properties like tensile strength and microhardness were evaluated. Moreover, the microstructural analysis were done using Scanning Electron Microscope (SEM), Field Emission Scanning Electron Microscope (FESEM), transmission electron microscopy (TEM), and X-Ray Diffraction (XRD) examination were also performed for inspecting the changes occurred during synthesis of the fabricated composites after FSP. After FSP, the experimental studies exposed that a uniform plastic deformation of GNPs in the pure Al matrix was achieved with less porosity that is leading to increment in mechanical properties with 11.26% enhancement in tensile strength and 12.17% enhancement in microhardness and thereby proves its potential for diverse engineering…
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Oil, Reference, for "L" Stock Rubber Testing

AMS CE Elastomers Committee
  • Aerospace Material Specification
  • AMS3020B
  • Current
Published 2020-01-17 by SAE International in United States

This specification covers a petroleum-based reference oil.

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Plating, Silver, Copper Strike, Low Bake

AMS B Finishes Processes and Fluids Committee
  • Aerospace Material Specification
  • AMS2412L
  • Current
Published 2020-01-16 by SAE International in United States

This specification covers the requirements for silver deposited on metal parts with a copper strike between the basis metal and the silver deposit.

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Alloy, Sheet and Strip, 42Fe - 37.5Ni - 14Co - 4.8Cb (Nb) - 1.6Ti, Solution Heat Treated, Precipitation Hardenable, Multiple Melted, High Temperature, Low Expansion

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5892C
  • Current
Published 2020-01-14 by SAE International in United States

This specification covers a low expansion iron alloy in the form of sheet or strip 0.250 inch (6.35 mm) and under in nominal thickness (see 8.7).

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Titanium Alloy, Round Bar and Wire, 3AI - 8V - 6Cr - 4Mo - 4Zr, Consumable Electrode Melted, Solution Heat Treated and Cold Drawn

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4957G
  • Current
Published 2020-01-14 by SAE International in United States

This specification covers a titanium alloy in the form of round bar and wire, 0.625 inch (15.88 mm) and under in nominal diameter or thickness.

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Chemical Film Treatment for Aluminum Alloys, General Purpose Coating

AMS B Finishes Processes and Fluids Committee
  • Aerospace Material Specification
  • AMS2473J
  • Current
Published 2020-01-14 by SAE International in United States

This specification establishes the requirements for chemical-film (conversion) coatings on aluminum alloys.

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Titanium Alloy Sheet, Strip, and Plate, 6Al - 4V, Solution Heat Treated

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4903D
  • Current
Published 2020-01-14 by SAE International in United States

This specification covers a titanium alloy in the form of sheet strip and plate up through 2.000 inches (50.80 mm), inclusive.

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Titanium Alloy Bars, Forgings and Forging Stock, 7.0Al - 4.0Mo, Annealed

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS6915C
  • Current
Published 2020-01-14 by SAE International in United States

This specification covers a titanium alloy in the form of bars up through 6.000 inches (152.40 mm) inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 6.000 inches (152.40 mm), inclusive and stock for forging of any size.

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Anodic Treatment of Aluminum Alloys Sulfuric Acid Process, Undyed Coating

AMS B Finishes Processes and Fluids Committee
  • Aerospace Material Specification
  • AMS2471J
  • Current
Published 2020-01-13 by SAE International in United States

This specification establishes the requirements for undyed anodic coatings on aluminum alloys.