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Aluminum Alloy, Hand Forgings 8.0Zn - 1.0Cu - 1.6Mg - 0.12Zr (7037-T7452) Solution Heat Treated, Compression Stress Relieved, and Overaged (Composition similar to UNS A97037)

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4456A
  • Current
Published 2019-11-25 by SAE International in United States

This specification covers an aluminum alloy in the form of hand forgings 11.000 inches (280 mm) and under in nominal thickness and of forging stock of any size (see 8.6).

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Aluminum Alloy, Plate (2397-T87), 2.8Cu - 1.4Li - 0.30Mn - 0.12Zr - 0.10Zn, Solution Heat Treated, Cold Worked, and Artificially Aged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4328B
  • Current
Published 2019-11-25 by SAE International in United States

This specification covers an aluminum alloy in the form of plate 3.000 to 6.000 inch (76.20 to 152.40 mm), inclusive, in nominal thickness (see 8.5).

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Aluminum Sheet, Laminated, Surface Bonded

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4013H
  • Current
Published 2019-11-25 by SAE International in United States

This specification covers aluminum and aluminum alloy foil in the form of laminated sheet.

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Design & analysis of 2 point aluminum upper control arm in modular multi link rear suspension system

ZF India Pvt Ltd.-Mayur Shamkant Kulkarni
  • Technical Paper
  • 2019-28-2564
Published 2019-11-21 by SAE International in United States
In current automobile market, due to the need of meeting future CO2 limits and emission standards, demand for hybrid systems is on the rise. In general, the requirements of modern automobile architecture demands modular chassis structure to develop vehicle variants using minimum platforms. The multi-link modular suspension system provides ideal solution to achieve these targets. To match ideal stiffness characteristics of system with minimum weight, aluminum links are proving a good alternative to conventional steel forged or stamped linkages. Design of current 2-point link (Upper Control Arm) is based on elasto-kinematic model developed using standard load cases from multi body dynamics. CAD system used is CATIA V5 to design upper control arm for rear suspension. This arm connects steering knuckle & rear sub frame. For Finite Element Analysis we used Hyperworks CAE tool to analyze design under all load cased & further optimization is done to resolve highly stressed zones. An optimized solution presented with a balance of ideal stiffness & strength. A CAD model developed with aluminum forged alloy (6082 - T6) is compared…
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Aluminum Alloy 2024, Bar, Rod, Shapes, Tube, and Wire, Extruded

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMSQQA200/3A
  • Current
Published 2019-11-19 by SAE International in United States

This specification covers the specific requirements for aluminum alloy 2024 bar, rod, shapes, tube, and wire produced by extrusion.

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Aluminum Alloy, Bar, Rod, Shapes, Structural Shapes, Tube, and Wire, Extruded: General Specification for

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMSQQA200C
  • Current
Published 2019-11-19 by SAE International in United States

This specification covers the general requirements for aluminum alloy bar, rod, shapes, structural shapes, tube, and wire extruded. Specific requirements for these products in a particular alloy are covered by the applicable detailed specification (See 6.3).

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INDIVIDUAL SHIELD TERMINATION, CONNECTOR, ELECTRICAL (CATEGORY 9)

AE-8C1 Connectors Committee
  • Aerospace Standard
  • AS85049/148
  • Current
Published 2019-11-15 by SAE International in United States
No Abstract Available.
This content contains downloadable datasets
Annotation ability available
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CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, NONENVIRONMENTAL, STRAIGHT, NON-SELF-LOCKING AND SELF-LOCKING, CATEGORY 3B (FOR MIL-DTL-5015 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS)

AE-8C1 Connectors Committee
  • Aerospace Standard
  • AS85049/31B
  • Current
Published 2019-11-14 by SAE International in United States
No Abstract Available.
Annotation ability available
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CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, NONENVIRONMENTAL, STRAIGHT, SELF-LOCKING AND NON-SELF-LOCKING, CATEGORY 3B (FOR MIL-DTL-38999 SERIES I AND II CONNECTORS)

AE-8C1 Connectors Committee
  • Aerospace Standard
  • AS85049/27B
  • Current
Published 2019-11-14 by SAE International in United States
No Abstract Available.
This content contains downloadable datasets
Annotation ability available
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CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, NONENVIRONMENTAL, SELF-LOCKING AND NON-SELF-LOCKING, 45°, CATEGORY 4B (FOR MIL-DTL-5015 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS)

AE-8C1 Connectors Committee
  • Aerospace Standard
  • AS85049/43B
  • Current
Published 2019-11-14 by SAE International in United States
No Abstract Available.
Annotation ability available