Electrical distribution system for an aircraft
A power distribution system and aircraft technology, applied in the direction of instruments, power distribution, electrical components, etc., can solve the problems of doubling design and logistics costs
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[0040] From now on, the current development of the protection board architecture can envisage the replacement of the hitherto single use of each protected path microprocessor by a set of at least two microprocessors for controlling all 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 reduc...
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