Method for analyzing an aircraft electrical structure by searching for equipotentials in embedded graphs
AssigneeAirbus Operations GmbH
InventorLudovic Farnaud
Life of this patent
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AssigneeAirbus Operations GmbH
InventorLudovic Farnaud
Estimating the term…
An aircraft electrical structure comprises equipment items that are interconnected by cables. A processing system constructs (400) a digital representation of the electrical structure in the form of nested graphs. A first graph represents the electrical structure by first arcs representing the cables and first nodes representing the equipment items. A second graph represents an internal interconnection structure between at least one input and at least one output of each equipment item which has such an internal interconnection structure, second arcs representing interconnections between inputs and outputs, second nodes representing the inputs and the outputs concerned. The first graph is obtained from contextual data (411) describing the electrical structure and each second graph is obtained from a generic model (412) for each type of equipment item concerned. An analysis is carried out by performing a search (404) for equipotentials by browsing through the nested graphs. Thus, the analysis is facilitated.
A method for assisting in locating and correcting a fault or defect in an electrical structure of an aircraft, wherein the electrical structure comprises equipment items interconnected by cables, the method comprising the following steps performed by a processing system including electronic circuitry:
A method for assisting in locating and correcting a fault or defect in an electrical structure of an aircraft, and the method includes:
Dependencies are inferred from the claim text.