aircraft power distribution system
A power distribution system, aircraft technology, applied in instrumentation, power distribution, electrical components, etc., can solve problems such as doubling design and logistics costs
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[0040] From now on, the current development of the protection board structure can envisage the replacement of the microprocessor used so far for each protected path by a set of at least two microprocessors for controlling all the protected paths (that is to say, For example, 16 microprocessors for a 16-way protection board). figure 2The main elements of such a fender are shown. It can be seen that the two redundant microprocessors (5a, 5b) control the control means (6a, 6b) of the power units of the protected path via intermediary means (7a, 7b, 7n) for determining the instructions to be transmitted , 6n), wherein the intermediary device is able to determine which microprocessor instruction has to be transferred. The aforementioned microprocessors are each connected to means for measuring the status of the protected path, and to the aircraft bus (4a, 4b).
[0041] Such a protective board allows a substantial reduction in the number of microprocessors used (while reducing we...
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