Results 211 to 220 of about 192,046 (260)
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Potential for electric aircraft
Nature Sustainability, 2019Commercial aircraft rely on liquid hydrocarbon fuels. Short-range all-electric aircraft have promise to reduce environmental impacts while remaining cost-competitive; however, they will require significant battery improvements.
Venkatasubramanian Viswanathan +1 more
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The Journal of the Royal Aeronautical Society, 1945
A meeting of the Royal Aeronautical Society was held in the lecture hall of the Institution of Mechanical Engineers at Storey's Gate, St. James's Park, Westminster, London, S.W.1, on Thursday, March 8th, 1945, at which a paper on “Electrics for Aircraft,” by Mr. C. G. A. Woodford, A.M.I.E.E., A.F.R.Ae.S., was read and discussed.
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A meeting of the Royal Aeronautical Society was held in the lecture hall of the Institution of Mechanical Engineers at Storey's Gate, St. James's Park, Westminster, London, S.W.1, on Thursday, March 8th, 1945, at which a paper on “Electrics for Aircraft,” by Mr. C. G. A. Woodford, A.M.I.E.E., A.F.R.Ae.S., was read and discussed.
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Proceedings of the IEE Part A: Power Engineering, 1956
An account of early cables is followed by a statement of present-day requirements. Descriptions of the standard cables are given, together with current rating data. Further needs are indicated and possible designs are discussed.
D.W. Bird, D.C. Hancock, D.B. McKenzie
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An account of early cables is followed by a statement of present-day requirements. Descriptions of the standard cables are given, together with current rating data. Further needs are indicated and possible designs are discussed.
D.W. Bird, D.C. Hancock, D.B. McKenzie
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Electrical machines for aircraft
Proceedings of the IEE Part A: Power Engineering, 1956The electrical machines used in aircraft differ greatly from normal industrial machines because they must have the lowest possible weight and bulk, but must be capable of operating over a wide range of ambient temperature and air pressure at varying altitudes.
B. Adkins, W. Philipp, A. Hossle
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An electric deicing system for aircraft
Electrical Engineering, 1949This paper covers an electric ice removal system as applied to a recent experimental airplane. The system is described in detail from the power generators to the ice removal blankets and includes such items as extent of ice protection coverage, construction and installation of ice removal blankets, system electric power requirements, and system control.
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AIRCRAFT ELECTRICAL INSTALLATIONS
2017<div class="section abstract"> <div class="htmlview paragraph">It is the purpose of this document to present design recommendations that will provide a basis for satisfactory and safe electrical wiring installations in transport aircraft. This document is not intended to be a complete electrical installation design handbook.
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Requirements for aircraft electric motors
Electrical Engineering, 1944DESIGN requirements for electric motors intended for use on aircraft maybe classified roughly into performance and construction. These two classifications are not completely independent of one another, as some of the construction requirements will have pronounced effect on the performance characteristics, Performance characteristics may be subdivided ...
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Influence of Electricity on Aircraft Instrumentation
Transactions of the American Institute of Electrical Engineers, 1944CURRENT bibliographies on aircraft instruments list a reference to an early article dated 1904–40 years ago. This paper, describing an altimeter, has been followed by thousands more indicating the interest and technical advancements in aircraft instruments. The needs of the aircraft industry have been met by the instrument manufacturers.
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Electric gun turrets for aircraft
Electrical Engineering, 1944THIS war has seen an unprecedented development of armament, both offensive and defensive, for military aircraft. One of the most widely used and, therefore, perhaps one of the most important of these has been the power-driven gun turret, three or four of which are used on all our heavy bombers, and one or more on most smaller bombers and equivalent ...
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Proceedings Eighth Annual Applied Power Electronics Conference and Exposition,, 2002
The More Electric Aircraft (MEA) concept is based on utilizing electric power to drive aircraft subsystems. With advancing electric power technology it will be feasible to use high power density electrical power components to drive the majority of aircraft subsystems.
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The More Electric Aircraft (MEA) concept is based on utilizing electric power to drive aircraft subsystems. With advancing electric power technology it will be feasible to use high power density electrical power components to drive the majority of aircraft subsystems.
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