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Journal ArticleDOI

Status of the United States Air Force's More Electric Aircraft initiative

J.S. Cloyd
- 01 Apr 1998 - 
- Vol. 13, Iss: 4, pp 17-22
TLDR
More Electric Aircraft (MEA) as discussed by the authors is a more electric aircraft, MEA approach to reduce the use of hydraulics and replace them with electrical power as the motive force for all aircraft functions.
Abstract
Since the early 1990's, the USAF has been successfully pursuing advancement in aircraft electrical power system technologies as a means of collectively establishing the capability to reduce dramatically or eliminate centralized hydraulics aboard aircraft and replace them with electrical power as the motive force for all aircraft functions. This overall approach (called the More Electric Aircraft, MEA) has been analytically determined to provide dramatic improvements in reliability, maintainability, supportability and operations/support cost as well as enhancements in aircraft weight, volume, and battle-damage reconfigurability. A time- and technology availability-phased research and development program has been structured to demonstrate the required electrical component and subsystems performance to allow equivalent or improved aircraft performance over the use of hydraulic power. This paper provides: (1) a brief historical treatment of technology milestones achieved which enabled the MEA approach; (2) a status of USAF and DoD research and development programs in electrical power generation, distribution, energy storage, systems integration and flight testing; (3) a description of some of the USAF's planned demonstration activities in aircraft electrical power subsystems; and (4) the dual use nature of many of these technologies enabling a variety of electric and hybrid electrically-propelled military weapon systems and commercial vehicles.

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Citations
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Journal ArticleDOI

Moving towards a more electric aircraft

TL;DR: In this article, the concept of a more electric aircraft (MEA) is described, which involves removing the need for on-engine hydraulic power generation and bleed air off-takes, and increasing use of power electronics in the starter/generation system of the main engine.
Journal ArticleDOI

Modeling, Design Optimization, and Applications of Switched Reluctance Machines—A Review

TL;DR: An in-depth literature review on the status and potential trends of the technology pertinent to the design and optimization of SRMs in the following aspects: the mathematical modeling of the electromagnetic and thermal fields in SRMs, the enhancement of the performances in terms of the torque ripple, acoustic noise, efficiency, and torque density, and the multiobjective design optimization incorporating all the above factors.
Journal ArticleDOI

A Review of More-Electric Aircraft

TL;DR: In this article, the authors introduce a review for the more-electric aircraft (MEA), which includes different options of generation and power system architectures. But, the authors highlight that the MEA put some challenge on the aircraft electrical system either in the amount of the required power or the processing and management of this power.
Journal ArticleDOI

In Situ Studies of Ion Transport in Microporous Supercapacitor Electrodes at Ultralow Temperatures

TL;DR: In this paper, a mesoporous electrochemical capacitor electrode with porosity and microstructure is used for rapid ion transport and effi cient ion electroadsorption in porous carbons.
Proceedings ArticleDOI

A review of more electric aircraft technology

TL;DR: A review of some of the notable MEA initiatives undertaken by the aerospace industry can be found in this paper, where the development of aircraft designs with improved performance to make them more efficient and environmentally friendly is the motivation underlying the concept of More Electric Aircraft (MEA).
References
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Patent

Integrated power system

TL;DR: In this article, an integrated power system for use with a gas turbine engine is provided for driving and steering a tracked vehicle under the control of the vehicle's operator, which includes a multispeed transmission for transmitting power from a free power turbine, included in the engine, to combining planetary gear systems driving the vehicle, elements of the combining planetary gears systems also being driven by a variable displacement hydraulic steering motor.