Assembly for control and/or monitoring of funtional members of an aircraft
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
N/A
Issued Date -
Oct 31, 2002
app pub date -
May 25, 2001
filing date -
Jan 24, 2000
priority date (Note) -
Abandoned
status (Latency Note)
Importance
Abstract
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).
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