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The local DC Power Distribution System of More Electric Aircraft has to be able to sustain bidirectional power flow to and from electromechanical devices. Because the mechanical source (Turbine Engine) is unidirectional, some storage and dissipation systems are necessary to store or/and dissipate the returned energy to maintain the DC bus voltage to the reference value. Different power management...
The local DC power distribution system of More Electric Aircraft is one of the cores of the electric power transmission. Because the mechanical source (turbine engine) is unidirectional, the system is not totally reversible. Some storage and dissipation systems are necessary to store or/and dissipate the returned energy to maintain the dc bus voltage. Different power-management strategies are proposed...
The local DC Power Distribution System of More Electric Aircraft is one of the cores of the electric power transmission. Because of some unidirectional devices (diode bridge and anti-run-back diodes), the system is not totally reversible. Some storage and dissipation systems are necessary to store or/and dissipate the returned energy to maintain the DC bus voltage. Power management strategies are...
With the more and more stringent energy crises and greenhouse effect, ldquomore electricrdquo transports are considered to be one of the solutions. The more electric aircraft and hybrid electric vehicle are the representation of ldquomore electricldquo transports. Some aspect of these two means of transport as installed capacity, role of electricity, electric sources, energy storage techniques and...
The local DC power distribution system (PDS) of a more electric aircraft is one of the cores of the electric power transmission. Generally, the PDS is made up of small power subsystems designed on their own stand-alone operation. But the interaction between the subsystems (sources and loads) induces some problems of stability. This paper compares the different stability behaviours of two load models:...
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