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Journal ArticleDOI

The More Electric Aircraft: Technology and challenges.

Patrick Wheeler, +1 more
- 01 Dec 2014 - 
- Vol. 2, Iss: 4, pp 6-12
TLDR
The importance of power electronics as an enabling technology for this step change in aircraft design is considered, and examples of typical system designs are discussed in this article, as well as the exciting future challenges for the aerospace industry.
Abstract
The More Electric Aircraft concept offers many potential benefits in the design and efficiency of future large, manned aircraft. In this article, typical ?aircraft electrical power systems and associated loads are described as well as the exciting future challenges for the aerospace industry. The importance of power electronics as an enabling technology for this step change in aircraft design is considered, and examples of typical system designs are discussed.

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Citations
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Proceedings ArticleDOI

High-Frequency LLC Converter with Narrow Frequency Variations for Aircraft Applications

TL;DR: In this paper , the authors describe the design and implementation of a compact and high-frequency LLC converter with wide input voltage range (from 220 V to 320 V), output power ranges (from 250 W to 1.5 kW), high efficiency (over 96 % at full power), high power density (32 kW/dm), and narrow frequency variations (15 %).

Speed/Torque Ripple Reduction of High-Speed Permanent Magnet Starters/Generators With Low Inductance for More Electric Aircraft Applications

TL;DR: In this paper , an active damping technique is applied to the speed loop to increase the anti-disturbance capability and generate a smoother reference for the current loop, whereas an adaptive output voltage saturation limit is utilized to limit the peak value of current to prevent overcurrent and torque spikes.
Journal ArticleDOI

Voltage distribution in the windings of high temperature inverter-fed motors

TL;DR: In this paper, the voltage distribution between stator coils is computed with high-frequency equivalent circuits that consider the magnetic couplings and the stray capacitances, and the influence of grounding system of the DC link is considered for computing the voltage spikes in the motor windings.
Journal ArticleDOI

Wide Bandgap-Based Power Electronics for Aerospace Applications

TL;DR: In this article , the authors present a power electronics architecture for the future generation of power converters, motor drives, and solid-state circuit breakers with unprecedented power density, efficiency, and reliability.

Wide Bandgap-Based Power Electronics for Aerospace Applications

TL;DR: Aerospace applications are not new but potentially the final frontiers for power electronics research and developments as mentioned in this paper , because of the need for fuel saving and greenhouse gas reduction, more electric aircraft (MEA), unmanned aerial vehicles (UAVs), electric vertical takeoff and landing (eVTOL) aircraft, and future hybrid and turbo electric propulsion call for a new generation of power converters, motor drives, and solid-state circuit breakers with unprecedented power density, efficiency, and reliability.
References
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Proceedings ArticleDOI

More-electric aircraft-system considerations

I. Moir
TL;DR: In this paper, the authors address some of the issues and trends becoming apparent in aircraft electrical power systems and present a number of developments at the component level that are well advanced and will increase electrical power levels.
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