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Development of PCX Electric

Honda Motor Co., Ltd.-Atsuo Ota
  • Technical Paper
  • 2019-28-2470
To be published on 2019-11-21 by SAE International in United States
We developed the electric motorcycle model “PCX ELECTRIC” that satisfies usability under the traffic environment in apan and ASEAN’s motorcycle sales major countries. The PCX ELECTRIC features easily removable battery packs, which practically helps eliminate the waiting time associated with charging the battery. The compactly designed EV system, which is efficiently packaged in the vehicle, uses two removable 48 V battery packs connected in series to realize a 96 V system suitable for driving the electric motorcycle. The EV system mounted on the body of the 2018 PCX achieves a motor power of 4.2 kW, top speed of 60 km/h, and cruising range of 41 km (at a steady 60 km/h). In addition, we developed a highly-convenient battery attaching system that enables fixing of the battery to the vehicle body and engaging of the connectors with a single action operation.
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A review on influence of different flushing methods on Material Removal Rate using EDM.

Manav Rachna International University-Gurpreet Singh Matharou
  • Technical Paper
  • 2019-28-2543
To be published on 2019-11-21 by SAE International in United States
Electrical release machining (EDM), is a material removal procedure whereby a coveted shape is acquired by utilizing electrical releases (sparks). Material is expelled from the work piece by a progression of quickly repeating current releases between cathode and anode, isolated by a dielectric fluid and subject to an electric voltage. At the point when the voltage between the two terminals is expanded, the power of the electric field in the volume between the anodes winds up more prominent than the quality of the dielectric (in any event in a few spots), which separates, enabling current to stream between the two cathodes. This wonder is the equivalent as the breakdown of a capacitor (condenser). Accordingly, material is expelled from the cathodes. Once the present stops (or is quit, contingent upon the sort of generator), new fluid dielectric is generally passed on into the between cathode volume, empowering the strong particles (flotsam and jetsam) to be diverted and the protecting properties of the dielectric to be reestablished. Including new fluid dielectric in the between anode volume is…
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Wiring Harness Optimization towards Wireless Vehicle

Eicher Motors Limited-Nikhil Baluja
  • Technical Paper
  • 2019-28-2530
To be published on 2019-11-21 by SAE International in United States
Paper Title - Wiring Harness Optimization towards Wireless vehicle Research and/or Engineering Questions/Objective (maximum 100 words)  In current scenario, wiring harness plays a vital role in inter-connecting electrical & electronic components fitted all across the vehicle.  As per cable standard, DIN 72551 or ISO 6722, copper conductors being used in stranded wires against cable cross-section & corresponding weight.  While going complete wire-less requires each component to have its own battery, ground, transmitter & receiver which indeed is a very costly affair to be employed in vehicle as huge development cost is required.  Here I'm suggesting an innovative method to make a vehicle apparently Wire-Less by creating local clusters connected to each other via conventional wiring harness & wire-less module.  Such method will apparently give a look of Wire-less vehicle itself & better advantages in terms of installation, service, troubleshooting, uptime & customer delight.  Moreover, direct benefits of Cost, Weight, FE will also be achieved. Methodology (maximum 150 words) # To start with this technology, I've divided it in different…
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CONNECTOR, PLUG, ELECTRICAL, SELF-LOCKING, COUPLING NUT, REAR RELEASE, CRIMP CONTACT, AN TYPE

AE-8C1 Connectors Committee
  • Aerospace Standard
  • AS34591D
  • Current
Published 2019-10-08 by SAE International in United States

Scope is unavailable.

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Terminal Junction System, Terminal Junction Blocks, Sectional, Bussing Modules, Feedback Type, Size 22-16, Series II

AE-8C2 Terminating Devices and Tooling Committee
  • Aerospace Standard
  • AS81714/61A
  • Current
Published 2019-10-01 by SAE International in United States

Scope is unavailable.

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Products of Tomorrow: October 2019

  • Magazine Article
  • TBMG-35286
Published 2019-10-01 by Tech Briefs Media Group in United States

This column presents technologies that have applications in commercial areas, possibly creating the products of tomorrow. To learn more about each technology, see the contact information provided for that innovation.

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TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, GROUNDING MODULES, STUD AND FLANGE TYPE MOUNTING, SERIES II

AE-8C2 Terminating Devices and Tooling Committee
  • Aerospace Standard
  • AS81714/63D
  • Current
Published 2019-09-30 by SAE International in United States

SCOPE IS UNAVAILABLE.

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TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, WIRE IN-LINE JUNCTIONS, SERIES II

AE-8C2 Terminating Devices and Tooling Committee
  • Aerospace Standard
  • AS81714/65A
  • Current
Published 2019-09-24 by SAE International in United States

Scope is unavailable.

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Aircraft Electrical Installations

AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
  • Aerospace Standard
  • ARP4404C
  • Current
Published 2019-09-19 by SAE International in United States
It is the purpose of this document to present design recommendations that will provide a basis for satisfactory and safe electrical installations in transport aircraft. This document is not intended to be a complete electrical installation design handbook. However, the requirements for safety extend so thoroughly throughout the electric systems that few areas of the installation are untouched by the document. It is recognized that individual circumstances may alter the details of any design. It is, therefore, important that this document not be considered mandatory but be used as a guide to good electrical application and installation design. Transport aircraft electric systems have rapidly increased in importance over a number of years until they are now used for many functions necessary to the successful operation of the aircraft. An ever increasing number of these functions are critical to the safety of the aircraft and its occupants. The greatly increased power available in electric systems is another factor in aircraft safety. These considerations make it essential that aircraft electrical design practices be carefully considered from the…
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TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, BUSSING MODULES, FEEDBACK TYPE, SIZES 22-12, SERIES II

AE-8C2 Terminating Devices and Tooling Committee
  • Aerospace Standard
  • AS81714/60C
  • Current
Published 2019-09-10 by SAE International in United States

Scope is unavailable.