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OwnerLoic Yann Guillemin, Jean-Clair Pradier +2inventors
InventorsLoic Yann Guillemin, Jean-Clair Pradier, Pierre Ballarini, Jacques Etienne Emmanuel Barrois
Estimating the term…
Assembly (10) for control and/or monitoring of functional members (32, 36, 40, 42, 46, 48, 54, 56) of an aircraft, of the type comprising at least two modules (30, 34, 38, 44, 50, 52) for control and/or monitoring of functional members and gateways for transferring data between said modules and at least one main data transport bus (14) of the aircraft. It comprises at least one secondary serial bus (16) allowing the transport of data according to the CAN protocol. Each control and/or monitoring module (30, 34, 38, 44, 50, 52) comprises at least one interface (70) for communication with at least one serial bus according to the CAN protocol, the control and/or monitoring modules (30, 34, 38, 44, 50, 52) being connected to the or to each secondary bus (16) across the or each communication interface (70). Said assembly furthermore comprises at least one communication gateway (18, 20) ensuring the transfer of data between the or each main bus (14) and the or each secondary bus (16).
Assembly (10) for control and/or monitoring of functional members (32, 36, 40, 42, 46, 48, 54, 56) of an aircraft, of the type comprising at least two modules (30, 34, 38, 44, 50, 52) for control and/or monitoring of functional members and means for transferring data between said modules and at least one main data transport bus (14) of the aircraft, characterized in that it comprises at least one secondary serial bus (16) allowing the transport of data according to the CAN protocol, in that each control and/or monitoring module (30, 34, 38, 44, 50, 52) comprises at least one interface (70) for communication with the secondary bus (16) according to the CAN protocol, the control and/or monitoring modules (30, 34, 38, 44, 50, 52) being connected to the or to each secondary bus (16) across the or each communication interface (70), and in that said assembly furthermore comprises at least one communication gateway (18, 20) ensuring the transfer of data between the or each main bus (14) and the or each secondary bus (16).
Assembly according to any one of the preceding claims, characterized in that the or each communication gateway (18, 20) is adapted to ensure a conversion of the data from the CAN protocol to the ARINC 629 protocol of the main bus.
Dependencies are inferred from the claim text.