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Aircraft Multi-Bus Electrical System Using a Hall-Effect Sensing Device

Authors: I. W. Moody;

Aircraft Multi-Bus Electrical System Using a Hall-Effect Sensing Device

Abstract

<div class="htmlview paragraph">The multi-bus electrical system, using a Hall-effect sensing device, is designed to meet FAR requirements. The system allows the automatic separation of a faulted bus through the use of the Hall-effect device. Should the loss of both generators occur, the battery will automatically become isolated from the loads associated with the generators as well as automatic isolation of the electric heat and the air conditioning motor. The battery is capable of supplying essential power for at least 30 minutes on the battery (if a 34-AH NiCad is used) in night, IFR, icing conditions. The system can be pre-flight tested from the cockpit and this capability can be used by field service for problem solving in the field.</div>

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selected citations
These citations are derived from selected sources.
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
0
Average
Average
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