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CONNECTOR, RECEPTACLE, CABLE CONNECTING, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT, ENVIRONMENT RESISTING, INDIVIDUAL RELEASE, CRIMP TYPE CONTACTS (CLASS A, F, AND W - SERIES 3)

AE-8C1 Connectors Committee
  • Aerospace Standard
  • AS81511/45A
  • Current
Published 2020-03-20 by SAE International in United States

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Human Factor Considerations in the Implementation of IVHM

HM-1 Integrated Vehicle Health Management Committee
  • Aerospace Standard
  • AIR6915
  • Current
Published 2020-03-20

This SAE Aerospace Information Report (AIR) offers information on how human factors should be considered when developing and implementing IVHM capabilities for both military and civil fixed wing aircraft. These considerations will cover the perception, analysis, and action taken by the flight crew and the maintenance personnel in response to outputs from the IVHM system. These outputs would be onboard realtime for the flight crew and post flight for maintenance. This document is not intended to be a guideline; it is intended to provide information that should be considered when designing and implementing future IVHM systems.

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Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel Systems

AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee
  • Aerospace Standard
  • AIR1616B
  • Current
Published 2020-03-19 by SAE International in United States
MIL-STD-1290, 14 CFR 27.952, and 14 CFR 29.952 provide crash resistant fuel system design and test criteria that significantly minimize fuel leaks and occurrence of post-crash fire in survivable impacts. This document does not change and does not authorize changes in or deviations from MIL-Standard or regulatory requirements. This document provides guidance for the design, performance, and test criteria for self-sealing breakaway valves.
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CONNECTOR, RECEPTACLE, FLANGE MOUNT, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT, ENVIRONMENT RESISTING, INDIVIDUAL RELEASE, CRIMP TYPE CONTACTS (CLASS A, F, AND W - SERIES 4)

AE-8C1 Connectors Committee
  • Aerospace Standard
  • AS81511/51A
  • Current
Published 2020-03-19 by SAE International in United States
No Abstract Available.
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CONNECTOR ACCESSORIES, ELECTRICAL, TERMINATION, SHIELD SPLIT SUPPORT RING, COMPOSITE, NONENVIRONMENTAL, STRAIGHT, CATEGORY 7

AE-8C1 Connectors Committee
  • Aerospace Standard
  • AS85049/93C
  • Current
Published 2020-03-19 by SAE International in United States
No Abstract Available.
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Coupling Assembly, V-Retainer, High Pressure High Temperature, Pneumatic Tube

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
  • Aerospace Standard
  • AS1895E
  • Current
Published 2020-03-19 by SAE International in United States
This SAE Aerospace Standard establishes the requirements for a V-retainer coupling, flanges, and seal suitable for joining high pressure and high temperature ducting in aircraft bleed air systems. The rigid coupling joint assembly, hereafter referred to as “the joint,” shall operate within the temperature range of -65 to +1200 °F.
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CONNECTOR, RECEPTACLE, FLANGE MOUNT, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT, ENVIRONMENT RESISTING, INDIVIDUAL RELEASE, CRIMP TYPE CONTACTS (CLASS A, F, AND W - SERIES 3)

AE-8C1 Connectors Committee
  • Aerospace Standard
  • AS81511/41A
  • Current
Published 2020-03-19 by SAE International in United States
No Abstract Available.
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A Modular Internal Combustion Engine Blow Rig and Cold-Flow Analysis Concept for Industrial Particle Image Velocimetry Measurements under Steady, Near-Reality Charge Air Conditions

SAE International Journal of Engines

Duale Hochschule Baden Wurttemberg Ravensburg, Germany-Martin Lichtmes, Martin Freitag
MTU Reman Technologies GmbH Magdeburg (Rolls Royce Power Systems), Germany-Mathias Frenzel, Peter Harder
  • Journal Article
  • 03-13-03-0022
Published 2020-03-19 by SAE International in United States
A modular, stationary IC engine blow rig for differential and integral flow field measurements using particle image velocimetry (PIV) has been developed. Unlike conventional PIV blow rigs, the given design is capable of operating under near-reality charge air conditions, that is, highly pressurized, hot intake air supply at high flow rates. Its conceptual flexibility as well as peripheral infrastructure allow for comprehensive and wide-ranging flow field analysis. Because of a modular architecture, it is neither confined to a specific cylinder head design nor limited solely to the application of PIV for differential flow field analysis. It also already accounts for direct inlet flow determination through an additional PIV access point upstream of the cylinder head. The inlet and outlet ducts have been designed with regular shapes and smooth walls, such that a digital twin-type CFD model of the blow rig is conveniently feasible. A specifically developed pseudostereoscopic reconstruction method is applied to acquire fully 3D volumetric velocity fields from plain sequential 2D measurements using only a single PIV camera and laser sheet. The resulting volumetric…
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Analysis and Design of Hybrid Transmission Systems

  • Professional Development
  • C2006
Published 2020-03-18

There is a significant gap between the Chinese and international hybrid technologies in terms of vehicle fuel consumption, system integration and cost due to weak accumulation of hybrid transmission products and technology and serious shortage of technical force for the development and application of high-level hybrid transmissions.

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Hydrogen Fuel Quality for Fuel Cell Vehicles

Fuel Cell Standards Committee
  • Ground Vehicle Standard
  • J2719_202003
  • Current
Published 2020-03-18 by SAE International in United States
This standard provides background information and a hydrogen fuel quality standard for commercial proton exchange membrane (PEM) fuel cell vehicles. This report also provides background information on how this standard was developed by the Hydrogen Quality Task Force (HQTF) of the Interface Working Group (IWG) of the SAE Fuel Cell Standards Committee.
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